AMS Issue 14 Amendment 01

a321

aircraft

maintenance schedule

VIETNAM AIRLINES

TECHNICAL DEPARTMENT

GIA LAM AIRPORT

200 NGUYEN SON - LONG BIEN - HA NOI

reference: vna AMS A321

Issue = 14 Date :12 Sep 2013 Amendment = 01 Date :

Approved by: civil aviation administration of vietnam

80 GIAO THONG VAN TAlcue HANG KRONG VI~T NAM

so 'J] Lf IQD-CHK

CONG BoA XA HOl CJ-llJ NGHIA VI~T NAMDoc Hip - Tu do - Hanh phllC

Ha N(Ji, ngay 12 thang 'I nom 2014

QUYET t)!NH

Y~ viec: Phe chuan tai li~u AMS A321 PH 14, Sf) 01cua T6ng cong ty H KYN

Cl)C TRUONG CVC HANG KHONG VI~T NAM

- Can cu Luat T-Tangkh6ng dun dung Viet Naill ngay 29/06/2006;- Can CLI' Quyet dinh 94/20091QD- TTg ngay 16/0712009 cua Thu tuong Chinhphu guy dinh chirc nang, nhiem vu, quyen han va co du t6 chuc cua Cue hangkh6ng Viet Nam;

- Can cir guy dinh cua BO guy che an roan hang kh6ng dan dung ITnh vue taubay va khai thac tau bay ban hanh theo thong nr s6 01/201 1ITT-BGTVT ngay27/01/20 I 1 cua B0 giao thong Van tai;

- Xet d~ ngh] cua T6ng cong ty HK VN tai cong van s6 476/TC1'1-1K-ATCL&A ngay 11104/2014;

- Theo c1~nghi cua Truong Phong Tieu chuan an toan bay,

QUyj.~T D!NH

Di~lI 1- Phe chuftn Ta i lieu "Cluro'ng triuh bao dtJ'i':i'rlg tau bay A321" (AMSA321 PH 14, SD 01) cua T6ng cong ty HK YN;

Di~u 2- T6ng cong ty HKYN chiu trach nhiern ap dung theo dung quy dinh cuaAMS A321, PH 14, SF) 01;

f)i~u 3- Phong Tieu chuan an loan bay chiu trach nhiern ki~m tra, giam sat d~tai lieu AMS 1\321, PH 14 SD 01 (1U'(),e tuan thu nghiem rue.

Di6u 4- QL1y~t dinh nay co hieu lire sau 15 ngay k~ nr ngay ky.c:i-:';;:'i 1-.--

NO'i IIfI~lI:

- C~IC tnrong (de bao cao);- T6ng Cry HKYN;- Luu YT, TCA T8, 7'1(~

Vietnam Airlines Aircraft type: A321 Issue: II/Date: 29-04-2011VNA-EN-F121 AMS Issue 14 Amendment No: 01- Date: 22-01-2014 Page III

. In accordance with MPD revision 39

Maintenance Schedule Amendment Approval Submission (Certification)

Date: Checked by: Department: Date:

~

r.s XU3h Duong St25 "J4/3/101f.

Submitted by: Department:

NGUYEN cue THINH DEPUTY TECHNICALDIRECTOR

Compliance Statement:

This Maintenance Schedule complies with the manufacturer's rrururnurn maintenance and inspection requirements and that requirements of theAirworthiness Authority for the airframe, engine (on wing), systems, and components except wherein previously or hereby approved by theAirworthiness Authority.

Signed ..~... Name J~~.Xpan.D.tidn Position [).J2IR.c.C:.W&-..... Date ,,19.!3/UJ/+. .

Organisation: Vietnam Airlines Corporation

The above Maintenance Schedule/Maintenance Schedule Amendment isapproved with the following exceptiones): Signature;\])J~/~~~~~ .

Name: .lV.: ../) ~ 7!!!t! .Date: J-.1. ../ ..d....;.?!?!4:.: .For:

(Airworthiness Authority)

TRANSMITTAL LETTER 09/2013

AMENDMENT NO 00 - ISSUE 14

REF: MAINTENANCE SCHEDULE A321 AMS VNA.

Please find attached amendment 01 issue14 to the above referenced schedule. Please embody this

amendment into the maintenance schedule in your possession and duly sign any copy this transmittal

letter on completion to Gialam Library.

INSTRUCTIONS:

1. Remove and discard entirely Aircraft Maintenance Schedule A321.

2. Insert new Aircraft Maintenance Schedule A321 amendment 01, issue 14.

...............................................................................................................................................................................

The undersigned certifies that AMS copy number................ has been amended in accordance with transmittal

letter Jan/2014.

Signed.......................................... Name............................................................. Date..........................................

Issue 14 Amendment 01 Date: JAN 2013

A321 AIRCRAFT MAINTENANCE SCHEDULE

RECORD OF AMENDMENTS

ALL AMENDMENTS TO THIS SCHEDULE WILL BE ACCOMPLISHED BY EITHER THE ORIGINATING DOCUMENT FOR THE "MASTER SCHEDULE" AND "MASTER COPY" OR BY LETTER OF TRANSMITTAL FOR SCHEDULE "COPY HOLDERS". ENTER THE NUMBER IN NUMERICAL ORDER TOGETHER WITH THE DATE INSERTED AND THE SIGNATURE OF THE PERSON AMENDING THIS SCHEDULE.

ISSUE NO. ISSUE DATE AMDT NO. AMDT DATE INSERTED DATE SIGNATURE

01

01

02

02

03

04

05

05

06

06

07

07

07

08

08

09

10

APR. 2001

APR. 2001

MAR.2002

MAR.2002

APR. 2004

OCT. 2004

AUG. 2005

AUG. 2005

NOV. 2006

NOV. 2006

OCT. 2007

OCT. 2007

OCT. 2007

MAR. 2009

MAR. 2009

AUG 2010

OCT 2010

00

01

00

01

00

00

00

01

00

01

00

01

02

00

01

00

00

APR. 2001

MAY 2001

MAR. 2002

MAR.2003

APR. 2004

OCT. 2004

AUG. 2005

JUN. 2006

NOV. 2006

MAR. 2007

OCT. 2007

JAN. 2008

OCT. 2008

MAR 2009

SEP. 2009

AUG 2010

OCT 2010

Issue 14 Amendment 01 Date: JAN 2013


RECORD OF AMENDMENTS

10

10

11

11

11

11

12

13

13

13

13

13

14

14

OCT 2010

OCT 2010

APR 2011

APR 2011

APR 2011

APR 2011

FEB 2012

AUG 2012

AUG 2012

AUG 2012

AUG 2012

AUG 2012

SEP 2013

SEP 2013

01

02

00

01

02

03

00

00

01

02

03

04

00

01

FEB 2011

MAR 2011

APR 2011

JUN 2011

JUL 2011

OCT 2011

FEB 2012

AUG 2012

OCT 2012

JAN 2013

APR 2013

JUL 2013

SEP 2013

JAN 2014


1. General This maintenance schedule is approved by The Civil Aviation Authority of Vietnam. No changes or alterations shall be made to this maintenance schedule without the prior consent of The Civil Aviation Authority of Vietnam. 2. Amendment procedures One copy of the maintenance schedule amendment form(s) showing the justification for such amendment(s) will be submitted by Vietnam Airlines to The Civil Aviation Authority of Vietnam for approval. When the amendment(s) are finally approved, a copy is returned to Vietnam Airlines for insertion into the 'master copy' and the appropriate amendment number is recorded on the record sheet. One copy is retained by The Civil Aviation Authority of Vietnam for insertion into the 'master schedule'. 3. Copy holders of the schedule Amendment(s) will be issued to copy holders of the maintenance schedule by means of a 'transmittal letter' and shall contain a list of highlights with information about significant changes and instructions of accomplishment. 4. Schedule holders and distribution Note: distribution of amendment(s) to copy holders of the maintenance schedule will be through the technical library of Vietnam Airlines.

Distribution list

Manual number Holder

Master schedule CAAV

01 Technical Department

02 Safety - Quality and Security Department

03, 04, 05 VAECO

Master copy Technical Department Library

ISSUE: JAN 2014

SECTION: 0-LEP

PAGE: 1


SECTION 0

SUMMARY OF CHANGES

LIST OF EFFECTIVE PAGES

SECTION MVT PAGE ISSUE

0-LEP R 1 SEP 2013

0-TOC R 1 SEP 2013

0- REASON FOR ISSUE N 1 JAN 2014

0- SUMMARY OF CHANGES R 1 JAN 2014





SECTION 0

SUMMARY OF CHANGES

TABLE OF CONTENTS

SUBJECT SECTION

SUMMARY OF CHANGES 0

ISSUE: SEP 2013

SECTION: 0-TOC

PAGE: 1

A321 aircraft maintenance schedule

Section 0

SUMMARY OF CHANGES

ISSUE: JAN 2014 SECTION 0 PAGE 1

REASON FOR ISSUE 14 AMENDMENT 01

Revise AMS to update maintenance document for new A321 aicraft: MSN 5916 VN-

A608, MSN 5958 VN-A609, MSN 5994 VN-A610. Update RII task. Update Terminal

check, weekly check.


Section 0

SUMMARY OF CHANGES


ISSUE 14 AMENDMENT 00

SECTION 0: SUMMARY OF CHANGES - Change: “Reason for Issue” item.

SECTION 1: GENERAL INTRODUCTION

- Update new A321 aircraft MSN 5916 VN-A608, MSN 5958 VN-A609, MSN 5994 VN-A610 to AMS.

- Update FC unit. - Update DY unit: 24 calendar hour elapsed. “DY” interval may be

counted from 00:00 o’clock of next day (has not to incdule remaining day time since task completion).

- Revise RII introduction SECTION 2: LINE MAINTENANCE CHECKS

- Terminal Check: Add Emergency Equipment check (Item 11c) - Weekly Check: add Emergency equipment check (Item 5a), add

galley check (Item 6,7), Add IFE check (Item 8)

SECTION 4: SCHEDULED AIRCRAFT MAINTENANCE

Job Card Amendment Code Amendment reasons

ZL-191-01-2 R EFF UPDATE

ZL-324-01-1 R ADD NOTE: RII TASK

ZL-332-01-1 R ADD NOTE: RII TASK



200413-03-1 R EFF UPDATE

215200-08-1 D DELETED TASK







271400-02-2 R ADD NOTE: RII TASK









Section 0

SUMMARY OF CHANGES





31-ECO-01-1 R ADD THRESHOLD NOTE






323105-02-1 R EFF, REF UPDATE

323105-03-1 R REACTIVE










491600-B5-1 D DELETED TASK



494000-B3-2 R EFF UPDATE



















Section 0

SUMMARY OF CHANGES












































Section 0

SUMMARY OF CHANGES




































SECTION 1

GENERAL INTRODUCTION

ISSUE: JAN 2014

SECTION: 1-LEP

PAGE: 1



1-LEP R 1 SEP 2013

1-TOC R 1 SEP 2013

1-General Introduction R 1 JAN 2014


SECTION 1


TABLE OF CONTENTS

SUBJECT SECTION

GENERAL INTRODUCTION 1

ISSUE: JAN 2014

SECTION: 1-TOC

PAGE: 1


ISSUE: JAN 2014 SECTION 1 PAGE: 1

SECTION1


1. GENERAL

This A321 Maintenance Schedule is based on the A319/A320/A321 Maintenance Planning Document - Revision 39 Issue 00, Jul/2013 customized in accordance with VIETNAM AIRLINES

National Requirements,

General Maintenance Policy,

Vendors Recommendations.

Aircraft Definition (Basic version, model and modification status),

It is also kept updated by additions/ amendments/ or intervals arising from:

− In service experience,

− Reliability Program Document Issue 02, Amendment 00

And the following issues of the A318/A319/A320/A321 Airworthiness limitations Section documents and engine document are covered in this A321 AMS issue:

ALS Part 1: Safe Life Airworthiness Limitation Items (SL-ALI), revision 02, May 13/11.

ALS Part 2: Damage Tolerant Airworthiness Limitation Items (DT-ALI), Rev 02, May 28/13.

ALS Part 3: Certification Maintenance Requirements (CMR) EASA version, Rev 01, Jun 15/12.

ALS Part 4: Ageing Systems Maintenance (ASM), Revision 01, Jun 15/12.

ALS Part 5: Fuel Airworthiness Limitations (FAL), Issue 4, 14 Sep 2012.

V2500 A1/A5 Interactive Electronic Technical Manual (IETM), Rev date: Aug 01/12 .

The AMS is kept updated by additions or amendments from sources mentioned here in above and detailed in the following section. Attention is drawn to the fact that although the Maintenance Planning Document will reflect all repetitive scheduled maintenance tasks promulgated by ALS Parts, AOT, ISB, SIL, AD/CN, …, it is the VNA’ responsibility to adjust his programs on receipt of the source document and not to wait until the amended A318/A319/A320/A321 MPD revision has been published.

This Maintenance Schedule is applicable to the following aircraft:



FLT S/N MODEL MSN REGISTRATION NUMBER

ENGINE

001 A321-231 2255 VN – A344 V2533-A5

002 A321-231 2261 VN – A345 V2533-A5

003 A321-231 2267 VN – A347 V2533-A5

004 A321-231 2303 VN – A348 V2533-A5

005 A321-231 2974 VN – A350 V2533-A5

006 A321-231 3005 VN – A351 V2533-A5

007 A321-231 3013 VN – A352 V2533-A5

008 A321-231 3022 VN – A353 V2533-A5

009 A321-231 3198 VN – A354 V2533-A5

010 A321-231 3315 VN – A356 V2533-A5

011 A321-231 3355 VN – A357 V2533-A5

012 A321-231 3600 VN – A358 V2533-A5

013 A321-231 3737 VN – A359 V2533-A5

014 A321-231 3862 VN – A360 V2533-A5

015 A321-231 3964 VN – A361 V2533-A5

016 A321-231 3966 VN – A362 V2533-A5

017 A321-231 4136 VN – A363 V2533-A5

018 A321-231 4213 VN – A365 V2533-A5

019 A321-231 4277 VN – A366 V2533-A5

020 A321-231 4315 VN – A367 V2533-A5

021 A321-231 4211 VN – A322 V2533-A5

022 A321-231 4669 VN - A323 V2533-A5

023 A321-231 4703 VN - A324 V2533-A5

024 A321-231 4737 VN - A325 V2533-A5

025 A321-231 4783 VN - A326 V2533-A5

026 A321-231 4826 VN - A327 V2533-A5

027 A321-231 4863 VN - A329 V2533-A5

028 A321-231 4945 VN - A331 V2533-A5

029 A321-231 4971 VN - A332 V2533-A5

030 A321-231 5164 VN - A334 V2533-A5



FLT S/N MODEL MSN REGISTRATION NUMBER

ENGINE

031 A321-231 5241 VN – A335 V2533-A5

032 A321-231 5247 VN – A336 V2533-A5

033 A321-231 5251 VN – A338 V2533-A5

034 A321-231 5275 VN – A339 V2533-A5

035 A321-231 5297 VN – A390 V2533-A5

036 A321-231 5306 VN – A392 V2533-A5

037 A321-231 5340 VN – A393 V2533-A5

038 A321-231 5385 VN – A395 V2533-A5

039 A321-231 5392 VN – A396 V2533-A5

040 A321-231 5418 VN – A397 V2533-A5

041 A321-231 5438 VN – A399 V2533-A5

042 A321-231 5456 VN – A601 V2533-A5

043 A321-231 5469 VN – A602 V2533-A5

044 A321-231 5495 VN – A603 V2533-A5

046 A321-231 5555 VN – A604 V2533-A5

047 A321-231 5699 VN – A605 V2533-A5

048 A321-231 5709 VN – A606 V2533-A5

049 A321-231 5916 VN – A608 V2533-A5

050 A321-231 5958 VN - A609 V2533-A5

051 A321-231 5994 VN - A610 V2533-A5

This document is sorted by ATA-Section and Task number.



2. TASK INTERVAL FRAME

Operational units (usage parameters)

"FH" (Flight Hours) : Elapsed time between wheels lift off and touchdown.

"CY", “FC” (Flight Cycle) : A complete take off and landing sequence.

"LD" (Landing) : An operation of an aircraft touching the runway and coming to a full stop or performing a ‘touch and go’.

“AH" (APU Hours) : APU operating hours.

Calendar units

“HR" (Hour) : One calendar hour elapsed

"DY" (Day) : 24 calendar hour elapsed. “DY” interval may be counted from 00:00 o’clock of next day (has not to incdule remaining day time since task completion

"MO" (Month) : One calendar month (can be calculated as 1/12

calendar year).

"YE" (Year) : One calendar year ((can be calculated as 365,25

days).

Other codes

– "NR" (National Requirement)

Task known as being subject to national regulatory requirement.

– “VR" (Vendor Recommendation)

Interval value dependent on task vendor recommendation.

– "NT" (Note)

Refer to the note at the end of the task description

Maintenance check requirements

Terminal check - N.E. 36 hours elapsed time.

Weekly check - N.E. 8 days

"A" check - N.E. 750 FH or 04 MO

"2A" check - N.E. 1500 FH or 08 MO

"4A" check - N.E. 3000 FH or 16 MO

"C" check - N.E. 24 MO or 7500 FH or 5000 FC

"2C" check - N.E. 48 MO or 15000 FH or 10000 FC





The A check shall be numbered in the following manner:

Interval

Check number 3000 FH or 16 MO

3000 FH or 16 MO

3000 FH or 16 MO

3000 FH or 16 MO

A01 A

A02 A + 2A

A03 A

A04 A + 2A + 4A

The C check shall be numbered in the following manner:

Interval

Check number 96 MO or 30000 FH or 20000 FC

96 MO or 30000 FH or 20000 FC

96 MO or 30000 FH or 20000 FC

96 MO or 30000 FH or 20000 FC

C1 C

C2 C + 2C

C3 C

C4 C + 2C + 4C

Structure program

For the Structures Program the basic thresholds and intervals for environmental deterioration related items are as follows:

Threshold 6 Years and 12 Years

Interval 6 Years and 12 Years.

Thresholds and intervals for fatigue damage related items are given in Flight Cycles (and Flight Hours for range sensitive items).

Zonal inspection program

For the Zonal Inspection Program the basic intervals are 4 months and multiples, 20 months and 40 months, 6 Years and 12 Years.

3. GENERAL RULES

The following rules, apply to the A321 MAINTENANCE SCHEDULE

3-1 Vietnam Airlines' manuals shall contain the details and responsibilities for accomplishing the maintenance identified by this document.



3-2 The overall reliability of the A321 will be monitored by Vietnam Airlines' system for continuous analysis and surveillance as required by the operator's Regulatory Authority.

3-3 Category II/III landing capabilities and RVSM capability are inherent functions of the basic design standard of the aircraft. Scheduled tasks necessary for these operations have been considered in the development of this program.

3-4 Task intervals may be changed in accordance: with the Regulator, Authority practices and rules. In this respect, attention is drawn to the source of the task.

3-5 Weight Variant applicability and weight limits: some SSIs have different limitations or fatigue inspection requirements depending on the Weight Variant of each aircraft. The list of the approved WV is provided in the Type Certificate Data Sheet (TCDS), N°A.064 issued by the EASA, together with associated modification configuration(s). The relevant weight variant of VNA’s A321 fleet, A321-231 is listed in following table:

VARIANT 000

(BASIC) 001

(MOD 28960)

Max. Ramp Weight (kg) 89 400 93 400

Max. Take-off Weight (kg) 89 000 93 000

Max. Landing Weight (kg) 75 500 77 800

Max. Zero Fuel Weight (kg) 71 500 73 800

Minimum Weight (kg) 47 500 47 500

3-6 The airworthiness limitations contained herein allow operation up to the Limit of Validity (LOV) in FC or FH whichever occurs first. The relevant LOV values are stated below.

The LOV reflects the limit of validity of the engineering data that supports the structural maintenance program.

The aircraft shall not be operated beyond these values unless the manufacturer has updated maintenance documents to include a clearly defined LOV extension.

Item

Model A/C Reg

MSN WEIGHT

VARIANTS MOD GROUP

LOV Airframe

FH FC

1 A321-231 A344 2255 000 21-2A 60,000 48,000

2 A321-231 A345 2261 000 21-2A 60,000 48,000

3 A321-231 A347 2267 000 21-2A 60,000 48,000

4 A321-231 A348 2303 000 21-2A 60,000 48,000

5 A321-231 A350 2974 001 28960 21-2B 60,000 48,000

6 A321-231 A351 3005 001 28960 21-2B 60,000 48,000

7 A321-231 A352 3013 001 28960 21-2B 60,000 48,000

8 A321-231 A353 3022 001 28960 21-2B 60,000 48,000



Item

Model A/C Reg

MSN WEIGHT

VARIANTS MOD GROUP

LOV Airframe

9 A321-231 A354 3198 001 28960 21-2B 60,000 48,000

10 A321-231 A356 3315 001 28960 21-2B 60,000 48,000

11 A321-231 A357 3355 001 28960 21-2B 60,000 48,000

12 A321-231 A358 3600 000 21-2A 60,000 48,000

13 A321-231 A359 3737 001 28960 21-2B 60,000 48,000

14 A321-231 A360 3862 001 28960 21-2B 60,000 48,000

15 A321-231 A361 3964 001 28960 21-2B 60,000 48,000

16 A321-231 A362 3966 001 28960 21-2B 60,000 48,000

17 A321-231 A363 4136 001 28960 21-2B 60,000 48,000

18 A321-231 A365 4213 001 28960 21-2B 60,000 48,000

19 A321-231 A366 4277 001 28960 21-2B 60,000 48,000

20 A321-231 A322 4311 001 28960 21-2B 60,000 48,000

21 A321-231 A367 4315 001 28960 21-2B 60,000 48,000

22 A321-231 A323 4669 000 21-2A 60,000 48,000

23 A321-231 A324 4703 000 21-2A 60,000 48,000

24 A321-231 A325 4737 000 21-2A 60,000 48,000

25 A321-231 A326 4783 000 21-2A 60,000 48,000

26 A321-231 A327 4826 000 21-2A 60,000 48,000

27 A321-231 A329 4863 000 21-2A 60,000 48,000

28 A321-231 A331 4945 000 21-2A 60,000 48,000

29 A321-231 A332 4971 000 21-2A 60,000 48,000

30 A321-231 A334 5164 000 21-2B 60,000 48,000

31 A321-231 A335 5241 001 21-2B 60,000 48,000

32 A321-231 A336 5247 001 21-2B 60,000 48,000

33 A321-231 A338 5251 000 21-2A 60,000 48,000

34 A321-231 A339 5275 000 21-2A 60,000 48,000

35 A321-231 A390 5297 001 21-2B 60,000 48,000

36 A321-231 A392 5306 000 21-2A 60,000 48,000

37 A321-231 A393 5340 000 21-2A 60,000 48,000

38 A321-231 A395 5385 000 21-2A 60,000 48,000

39 A321-231 A396 5392 000 21-2A 60,000 48,000

40 A321-231 A397 5418 000 21-2A 60,000 48,000

41 A321-231 A399 5438 000 21-2A 60,000 48,000

42 A321-231 A601 5456 000 21-2A 60,000 48,000

43 A321-231 A602 5469 001 21-2B 60,000 48,000

45 A321-231 A603 5495 000 21-2A 60,000 48,000

46 A321-231 A604 5555 000 21-2A 60,000 48,000

47 A321-231 A605 5699 000 21-2A 60,000 48,000

48 A321-231 A606 5709 001 21-2B 60,000 48,000

49 A321-231 A608 5916 000 21-2A 60,000 48,000

50 A321-231 A609 5958 000 21-2A 60,000 48,000

48 A321-231 A610 5994 001 21-2B 60,000 48,000



3-7 Vietnam Airlines should be aware of the various inspection techniques such as X-Ray, ultrasonic, eddy current, radio isotope... which are available and described in the Non-Destructive Testing Manual (NTM). The use of such techniques can be developed to provide a valuable adjunct to the prescribed visual inspections. For any substitution of such inspection technique, it must be ensured that the same damage size will be detectable by the proposed technique with, at least, the same level of confidence.

3-8 Items that are life limited will be removed from service according to the life limits referenced in the aircraft "Type Certificate Data Sheet" or in the appropriate section of the engine or aircraft manufacturer's manuals.

3-9 Tasks coming from any of the ALS parts must not be deleted and should be handled with specific associated rules, as described in the subject documents. ALS Part 3 tasks have specific rules regarding escalation as follows:

CMR* * : Task interval may be escalated by the operator, in accordance with an approved reliability program.

CMR* : Task interval shall not be escalated by the operator.

3-10 Tasks may be considered to conform to the requirements of the scheduled maintenance program if accomplished as part of a regulatory authorities approved/accepted equivalent check/test by flight crew.

3-11 It is the responsibility of Vietnam Airlines to adjust his own maintenance program in accordance with his National Requirements and to comply with existing rules with respect to reporting to his Regulatory Authority and to the manufacturer events having effects on the continued airworthiness of the aircraft.

In addition to the above

Vietnam Airlines must be aware of manufacturer and vendors recommendations and/or requirements published through Inspection Service bulletin (ISB), Service Information Letter (SIL), All Operators Letter (AOL), All Operators Telex (AOT) and other documents dealing with maintenance, since they can not be immediately reflected in the Maintenance Program.

For engines, APU, and main components, Vietnam Airlines should also consider manufacturer's manuals for additional task once the engines or the components are in the shop.

Vietnam Airlines shall refer to Airbus Industries technical publications (Aircraft Maintenance Manual, Non Destructive Testing Manual, and Structure Repair Manual) for maintenance practices and procedures.

When two thresholds or intervals, in different units, are assigned to a task, and when not otherwise stated, the interval expiring fast shall apply.



3-12 The maintenance clock does not stop while the aircraft is in maintenance condition. Although the aircraft does not collect any FH or FC when being on ground, attention has to be given to tasks, where the interval is expressed in calendar time (hours, days, month, and year). All tasks that become due at the time of the maintenance visit have to be performed prior to return to service. However, there is no need to repeat inspections during the check event. E.g. during a 4 weeks downtime, tasks with interval 8 DY only need to be performed at the end of the check (for return to service).

The tasks and frequencies in this AMS have been developed and are valid for aircraft in operation. If an aircraft is not in operation e.g. parked or stored, the instructions quoted in AMS section 5 should be followed.

3-13 Unless otherwise specified by AIRBUS in the delivery documentation of an aircraft, the starting point for calculation of the due dates or times of all aircraft maintenance tasks (whether the intervals are quoted in Flight Cycles, Flight Hours or Calendar time) is to be the first flight of that aircraft. The date of Transfer of Title to a customer may be used for calculation of the due date of tasks with a calendar interval if that transfer occurs within 90 days of the date of the first flight of the aircraft and the aircraft has been stored or parked in accordance with AIRBUS procedures according to AMM Chapter 10. The start date for the overhaul period of an overhauled landing gear is the date of the gear's first flight after overhaul.

The following exceptions apply:

• STR, ALI tasks quoted in terms of FH or FC: the first flight is the starting point for calculation.

• ASM tasks quoted in terms of FH or FC: the first flight is the starting point for ASM tasks quoted in terms of FH or FC.

• For TIME CONTROLLED ITEM equipment with intervals defined by the vendor or by National Requirements (VR or NR): The date of manufacture is the starting point unless otherwise stated by vendor or national authority.

• The start date for the overhaul period of an overhauled landing gear is the date of the gear's first flight after overhaul.

• For items covered by CN/AD: as stated in the CN/AD.

• Where a Damage Tolerant item is transferred from one aircraft to another, the required maintenance task threshold and intervals for the transferred item are to be respected:

- For the threshold, the “next due” inspection (in calendar, FC or FH) is to be calculated from the date of the first flight after installation of the item on the first aircraft.

- For the interval, the “next due” inspection (in calendar, FC or FH) is to be calculated from the date of the previous task performance on the transferred item.



If the required inspections on the transferred item are performed as part of the installation process, then the “next due” inspection for maintenance counts from the installation date. If the date of the ToT occurs more than 3 months after of the date of the first flight of the aircraft, Airbus is to be consulted for advice. On request Airbus can define specific maintenance tasks to be performed prior to the ToT that may allow the aircraft delivery date to be used as the starting point for calculation of the due dates.

3-14 ANNUAL UTILIZATION AND MAINTENANCE REVIEW.

The periods / frequencies of the maintenance tasks in this schedule are generally based on an anticipated annual utilization of 3000 FLIGHT HOURS and large variations in the annual utilization of individual aircraft could invalidate the effectiveness of certain tasks. If the annual utilization varies by more than 25% from that anticipated, the operator accepts that he or his contracted maintenance organization must review the maintenance tasks and periods with a view to making any necessary adjustments.

In addition to variations in utilization the data contained in this schedule will be reviewed at least annually by the operator or his contracted maintenance organization, to ensure that the detailed requirements continue to be valid in the light of operating experience.

3-15 METHOD OF NEXT DUE CHECK CALCUALTION

When determine the next due of a check, use the following method:

- If CRS date is after Due Date then the Next Due = Due Date +Interval.

- If CRS date is before Due Date then the Next Due = CRS date +Interval.

4. CONTINUOUS AIRWORTHINESS

Maintenance tasks and frequencies required by the MRB Document (individually identified in this document) together with limitations of life limited parts are Published in the documents of A318/A319/A320/A321 ALS - Airworthiness Limitations Section and IAE A319/A320/A321/V2500-A5 - Chapter 05 -Time Limits Manual.

Constitute the instructions that the manufacturers consider as essential for proper maintenance of the aircraft.

For the manufacturer and Vietnam Airlines common benefit, significant maintenance information will be reported to the manufacturer to be considered for further development of the A319/A320/A321 MPD.

5. DOCUMENTS BREAKDOWN



The A321 AMS will be presented in 6 different sections as follows:

SECTION 0: SUMMARY OF CHANGES

- Reason for Issue

- Summary of changes

SECTION 1: GENERAL INTRODUCTION

SECTION 2: LINE MAINTENANCE CHECKS

- PRE-FLIGHT/TRANSIT CHECK

- TERMINAL CHECK

- WEEKLY CHECK

SECTION 3: SCHEDULED COMPONENT MAINTENANCE

- Sub-section 3.1: Engine LLP

- Sub-section 3.2: Landing Gear LLP

- Sub-section 3.3: System Life Limited Components

- Sub-section 3.4: Time Controlled Items List

SECTION 4: SCHEDULED AIRCRAFT MAINTENANCE

- Sub-section 4.1: Airworthiness Limitation Items (ALI)

- Sub-section 4.2: Certification Maintenance Requirement (CMR)

- Sub-section 4.3: Ageing Systems Maintenance (ASM)

- Sub-section 4.4: Fuel Airworthiness Limitation (FAL)

- Sub-section 4.5: Systems, APU and Power Plant

- Sub-section 4.6: Structure Program

- Sub-section 4.7: Zonal Program

- Sub-section 4.8: Fuel Saving Program

SECTION 5: SPECIAL PROCEDURES

- Sub-section 5.1: Unscheduled Maintenance Checks and Inspections.

- Sub-section 5.2: Parking and Storage Procedures

- Sub-section 5.3: Cold Weather Maintenance Procedure.

- Sub-section 5.4: Critical Design Configuration Control Limitations.

6. OVERALL DOCUMENTS DESCRIPTION The initial issue/amendment of the AMS was based on the first issue of the A318/A319/A320/A321 Maintenance Planning Document (MPD). The tasks and their frequencies given in the MPD, together with the requirements of Airworthiness Limitations documents shall be introduced in the Section 3, 4 and section 5.



Maintenance requirements promulgated through ALS Part 1 and ALS Part 4 - Subpart 4-2 are not included in MPD since they are not repetitive maintenance tasks. Therefore VNA shall be updated these mandatory requirements approved by Primary Type Certification Authorities on AMS as hereafter. 6.1 Section 3 – Scheduled Components Maintenance: The maintenance requirements related to many aircraft components, as listed in the manufacturer’s documents or mandated by Authority for an aircraft or the model aircraft:

- Sub-section 3.1- Engine LLP: Life limitation parts of CFM engine mentioned in paragraph 1 of this section and they are quoted from V2500 A1/A5 Interactive Electronic Technical Manual (IETM), Chapter 5.

- Sub-section 3.2 - Landing Gear LLP: Life limitation parts of lading gear system can be equipped for A320 aircraft. This sub-section is filtered from ALS part 1 (Safe life Airworthiness Limitation Items).

- Sub-section 3.3 - System Life Limited Components: The content of this sub-section is quoted from ALS part 4-subpart 4-2 (system life limited components) and ALS part 5-section 1-table 2 (life limits).

- Sub-section 3.4 - Time Controlled Items List: for detail interval of the maintenance task in section 4. This section is based on the following documents: ALS part 4-subpart 4-3, ALS part 5-section 1-table 1, vendor recommendations, national requirements, MPD task related to CMM.

6.2 Section 4 – Scheduled Aircraft Maintenance: This section includes all scheduled maintenance tasks related to the aircraft systems, structure and zonal inspection. The sub-sections are built on the following documents - Sub-section 4.1: The Structure section of MPD as well as ALS part 2

(Damage Tolerant Airworthiness Limitation Items). - Sub-section 4.2: The Systems/APU/Power Plant of MPD section as well as

ALS part 3 (Certification Maintenance Requirements) - Sub-section 4.3: The Systems/APU/Power Plant section of MPD as well as

ALS part 4 – subpart 4-3 (Systems Installations Maintenance Requirements). - Sub-section 4.4: The Systems/APU/Power Plant section of MPD as well as

ALS part 5 – section 1 – table 1 (Repetitive tasks) - Sub-section 4.5: The Systems/APU/Power Plant section of MPD. - Sub-section 4.6: The Structures section of MPD. - Sub-section 4.7: The Zonal section of MPD. - Sub-section 4.8: Fuel saving policy of VNA 6.3 Section 5 – Special Procedures This section is built on to introduce the special maintenance requirements such as unscheduled maintenance, preventive maintenance ect. The quoted documents are: - Sub-section 5.1: A320 AMM chapter 05-51 – inspection/checks after the

aircraft has gone through special or abnormal conditions. - Sub-section 5.2: A320 AMM 10-11-00-555-006 and AMM 10-12-00-553-005. - Sub-section 5.3: A320 AMM 12-31-00-600-001. - Sub-section 5.4: ALS part 5 – section 2 (Critical Design Configuration Control

Limitations).



7. METHOD OF PRESENTATION

Presentation of maintenance tasks

- The tasks are listed in increasing task reference order within each sub-section.

7-1 Task Number

Each task is identified by a specific task number. When a task has to be repeated in several specific zones, the task is assigned a single task number. But the several zones are indicated in "ZONE" column.

The task number comprises 9 digits organized as follow:

XX XX XX - XX - X

I I I

I I I

I I l effectively index

I I _____ Sequence number

I____________ __ ATA reference or first main zone

* ATA reference or first main zone.

- The ATA reference identifies the system/sub-system or component on which the task is to be accomplished.

- The main zone number is preceded by the letter code "ZL". For tasks to be repeated in several main zones, the first main zone or LH zone number is used (Aircraft zoning is given in MPD Volume 2, Section 10).

* Sequence number

- The sequence number is used to discriminate between different tasks relating to the same system, component, zone or structural significant item.

- Engine type is identified by "I" (IAE) in first digit.

- Vietnam Airlines originated tasks have "VN" as two first digits of the ATA reference number

* Modification index

- The effectivity index identifies different effectivity of the same work and for successive developments of a task introduced by modifications or specific requirement. However, in a few cases, the sequence number may be used for that purpose, when referenced documentation requires doing so.

- The technical status or specific requirement associated with each effectivity index is specified in the effectivity column. As a general rule, tasks with same first 8 digits in task number have same work description in the AMM.

7-2 Main Zone column

The "ZONE" column shows the positions) where the task has to be accomplished (repeated) according to the description. Quoting several positions means that the task has to be repeated in each position.



One zone number or one sub-major zone number or one major zone number identifies either each position.

When sub-major or major zone number is quoted to identify a unique position of a task, the more precise zone numbers are quoted in the description in case such additional information is estimated useful.

7-3 Description column

This column provides the following information

* Task title

Identifies the system/sub-system/component/zone/structural significant item concerned by the task.

* Task description

Gives a concise description of the work to be performed.

* Sampling Note: Sampling Program Inspection. When this note is not printed, the task has to be accomplished on all aircraft of the fleet. (Refer to A319/A320/A321 MPD, Section 3-Structure-Intro, chapter Sampling Program)

* CPCP Note: Requirements to control corrosion to level 1 or better (refer to A319/A320/A321 MPD Section 3-Structure - Intro, chapter Corrosion Prevention and Control Program)

* Task preparation (where applicable)

Specifies the preliminary steps (from a pre-established list) to be performed prior the maintenance task itself.

* Access (where applicable)

Specifies the identifiers of the access panels, linings or doors to be opened or removed for accomplishment of the task.

Their identifiers do not designate floor panels of passenger cabin and carpe holds but by frames numbers between which the floor panels have to be removed are quoted.

* Task code

Mnemonic code defining the type of task to be carried out

ADJ Adjustment/alignment/calibration

BSI Bore scope inspection

VCK Visual check. Check fluid level, Check detector

CHK Check for leaks, Check circuit continuity, Check fluid reserve on item, Check tension or pointer, Check charge pressure, Remove and check, Check torque

LKC Leak Check

CLN Cleaning

DRN Draining



DI Detailed inspection

ERU Engine run-up

FNT Functional test

GVI General visual inspection

INS Install

LUB Lubrication

SDI Non-destructive Testing

OPC Operational Check

OPT Operational Test

PRZ Pressurize

DIS Remove and discard

RAI Remove and install

RAR Remove and replace

RDG Reading

RDT Remove, discard and test

RST Remove for restoration

SVC Replenishment (fluid change)

SDI Special detailed inspection

SPL Sampling

SVC Servicing

TST Test

TPS Temporary Protection.

TUP Fluid Top Up

7-4 Threshold/Interval

This column provides the following information

* Threshold

This information, preceded by the letter "T", gives a specific value of an operational parameter or of a letter code defining the first accomplishment deadline of the task. When threshold is equal to the interval. The lever "T" may not show.

When the threshold is expressed in several units, the conjunction "OR" separate the different indications.

* Task interval

This information, preceded by the letter "I", gives a specific value of an operational parameter or of a letter code defining the maximum tine that can separate two complete accomplishments of the task.

When interval is equal to the threshold, the letter "I" may not show.

When the interval is expressed in several units, the conjunction "OR" separate the different indications.



7-5 CT INSPECTION COLUMN

An X in the CT column means that the task requires an inspection.

7-6 REFERENCE COLUMN

This column provides

The AMTOSS (AMT) and the AMM references of the task in the A321 Aircraft Maintenance Manual (AMM).

* References to technical publications where accomplishment instructions can be found.

* The reference of a special directive (French CN, German LTA, American AD, Inspection Service Bulletin - ISB, SIL) where additional information of the origin or justification will be found.

7-7 Men and M-H

Specifies

- The number of men and the corresponding man-hours required to carry out the task in each position quoted in "ZONE. Man-hours are expressed in hours and hundredth of hours.

For tasks which require to be performed in shop (example: landing gear restoration), men and man-hours shown correspond to the removal/installation of the item concerned (shop man-hours are not considered)

- The man-hours required opening and closing: the listed access panels.

The figures quoted do not include

* Preparatory work such as aircraft cleaning, positioning work stands, procuring consumable materials, connecting ground power carts, etc.

* Correction of defects found during task accomplishment.

* Correction for dead time and manpower efficiency.

Therefore these figures represent as such the man-hours actually needed

- The skill code, specifying the type of skill required for task accomplishment.

AF : Airframe IN : Avionics

CA : Cabin LU : Lubrication

CL : Cleaning QC : Non-Destructive Testing

EL : Electrical RA : Radio

EN : Power Plant UT : Utility

AV : Instrument NDT: Non Destructive Test

7-8 Effectivity column



The information given in this column defines the technical status of the aircraft on which the task is applicable.

The technical status is expressed as one, or a combination, of the following keywords

* Serial number indicates that the task is applicable to this particular aircraft in the A321 fleet or part of the A321 fleet.

* "ALL" indicates that the task is applicable to all aircraft in the fleet.



Vietnam Airlines A321

A M A S I S A I R C R A F T M A I N T E N A N C E S C H E D U L E

TASK Zone D E S C R I P T I O N Task Threshold C References A/C

NUMBER --------------------- Code Interval T EFF.

CHAPTER : 57 WINGS

575142-01-1

1

147

148

2

INBOARD FLAP ACTUATOR DRIVE ARM DVI

DETAILED VISUAL INSPECTION OF INBOARD FLAP,

INBOARD ACTUATOR DRIVE ARM, DRIVE STRUT AND

OUTER PART OF TRUNNION --------- 3

NOTE : 100% LIMIT = 20 YE

NOTE 2: SAMPLING 20% -------- 4

NOTE 3: CPCP -------- 5

PREP. : FLAP EXTENSION

Skill : 1 AF For 1.80 Hrs per zone ---------- 6

Access 734 744 --------- 7 0.00 Hrs

T 24000 FC

Or 10 YE

I 15000 CY

Or 10 YE

8

X AMM 575100/6 ALL

AMT 575100-200-004 10

9

Issue number: 02 Amendment No : 00 A.M.S. Page : STR -57/ 71

Date : 24/01/2002 Date : 24/01/2002 Ref : VN-001 ATA : 57

1 Task number 2 Position(s) of the task, identified by the zone 3 Task title, task description 4 Sample size

5 CPCP 6 Number of men and man-hours (in hours and hundredth of hours) per position 7 Access

8 Threshold, Interval 9 AMM, AMTOSS ref., Tech. Pub., Special Directives 10 Task effectivity



7-9 Permitted variations to maintenance periods

7-9-1 Vietnam Airlines or their contracted Maintenance Organization may vary the periods described by this Maintenance Schedule provided such variations are within the limits defined below.

7-9-2 Variations shall be permitted only when the periods prescribed by this Maintenance Schedule (or documents m support of this Maintenance Schedule) cannot be complied with due to circumstances which could not have reasonably been foreseen by Vietnam Airlines or by the contracted Maintenance Organization.

7-9-3 The decision to vary any of the prescribed periods shall be taken only by the Chief Inspector/Quality Manager or person of equivalent status on behalf of Vietnam Airlines or his contracted Maintenance Organization. Particulars of every variation so made shall be entered in the appropriate Log Book(s).

7-9-4 Maximum Variations:

The maximum variation of a prescribed period is indicated below table as follows:

Items controlled by Flight Hours Maximum variation of the prescribed period

5000 Flying hours or less 10%

More than 5000 Flying hours 500 Flying hours

Items controlled by Calendar Time Maximum variation of the prescribed period

Up to 12 months 10% but not exceeding 1 month

Between 13 and 36 months 2 months

More than 3 years 3 months

Items controlled by Landing/cycles Maximum variation of the prescribed period

500 landings/cycles or less 5% but not exceeding 25 FC

More than 500 landings/cycles 5% but not exceeding 250 FC

NOTE 1 : For ECO tasks, maximum variation of the prescribed period is 20%.

NOTE 2 : For items controlled by more than one limit, e.g. items controlled by Flying Hours or Flying Hours and Landings/cycles, the more restricted limit shall be applied.

NOTE 3 : The variations permitted above do not apply to:

Those periods included in the Maintenance Schedule which have been classified as mandatory by the CAAV.

ALI, CMR, AD/CN, FAL, ASM related tasks and Life limitations related items/components in AMS section 3.



8. SAMPLING PROGRAM

8-1 INTRODUCTION

The purpose of the Sampling Program is to detect systematic deterioration caused by the environment and/or fatigue, on a group of aircraft selected from those which have the highest age within a considered fleet. The Sampling Program is applicable to both Environmental Deterioration (ED) and Fatigue Damage (FD) SSIs, where the deterioration, should it occur, is considered as being progressive with age or operating usage. Only those SSIs for which a systematic environmental deterioration/fatigue damage characteristic has been analyzed will be considered for inclusion in the Sampling Program.

SSIs which are susceptible to Accidental Damage (AD) [Non-systematic] are not considered for the Sampling Program.

The Sampling Program terminates for each applicable SSI at the 100% Threshold, e.g. the 100% Threshold for all calendar-time Sampling Program items is 20 Years.

Sampling tasks have NOTE: SAMPLING 20% and NOTE: 100% LIMIT in DESCRIPTION column.

Following aircraft are selected for Sampling program:

MSN REGISTRATION NUMBER ENGINE

2255

2261

VN - A344

VN - A345

V2533-A5

V2533-A5

2267 VN - A347 V2533-A5

2303 VN - A348 V2533-A5

2974 VN - A350 V2533-A5

8-2 ARRANGEMENT OF INSPECTIONS

For the selected Sampling Program aircraft, inspections commence at the Sample Threshold and continue at each subsequent repeat inspection interval.

The same aircraft are to be inspected at each subsequent repeat inspection interval.

NOTE: The 100% Threshold is the threshold for all aircraft not selected for sampling.



9. CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

9-1 INTRODUCTION

The Structures Program includes requirements to control corrosion to Level 1 or better on all structural details, elements or assemblies which contribute significantly to carrying flight, ground, pressure or control loads, and whose failure could affect the structural integrity necessary for the safety of the aircraft. All Corrosion Prevention and Control Program (CPCP) requirements are indicated by the code ‘CPCP’ in the “SOURCE” column.

Some calendar-time tasks are also covered by the Sampling Program, i.e. they have a Sample Threshold/Interval. For these tasks, the 100% Threshold is the time at which the task becomes a CPCP task.

9-2 CORROSION LEVEL DEFINITIONS

The definitions for the various Levels of corrosion are as follows:

Level 1 Corrosion

Corrosion damage that does not require structural reinforcement or replacement.

or,

Corrosion occurring between successive inspections exceeds allowable limit but is local and can be attributed to an event not typical of operator usage of other aircraft in the same fleet (e.g. Mercury spill).

Level 2 Corrosion

Corrosion occurring between successive inspections that requires a single rework/blend-out, which exceeds allowable limits as defined by the manufacturer (SRM, SB, etc.), requiring a repair/reinforcement or complete or partial replacement of applicable structure.

Level 3 Corrosion

Corrosion found during first or subsequent inspection(s), which is determined (normally by the operator) to be an urgent airworthiness concern requiring expeditious action.

9-3 CPCP RULES

The effectiveness of the Corrosion Prevention and Control Program is determined by following the General Rules applicable to the Structures Program (refer to Paragraph 8) and the rules listed below (Refer also to CPCP Flow Chart and Decision Steps on following pages).

Level 1 Corrosion Findings

Should inspections consistently reveal corrosion Level 1 findings for a given area during repeat inspections on particular aircraft operated in



similar conditions, then the existing program is considered effective for the concerned area, and no change to the program is necessary.


Should inspections reveal that corrosion is Level 2 for a given area during repeat inspections, and then the existing program is not effective for the concerned area of the particular fleet.

In order to control corrosion to Level 1 or better, consideration should be given to one or more of the following corrective actions:

- Decreasing the inspection threshold/interval

- Considering a higher inspection level

- Re-considering the Program Concept

- Application/More frequent application of Temporary Protection System

- Embodiment of preventive modifications, where applicable

- Installation of parts with improved protection standard, where applicable

In this way, the program is self-regulating and will adjust itself to the optimum program.


Should inspections reveal that corrosion is Level 3 in a given area, and then the existing program is not effective for the concerned area.

In addition to the considerations given for Level 2 corrosion, an action plan calling for a one-time inspection of the concerned area should be expeditiously agreed with the local Aviation Authority and carried out on all aircraft of a similar age or older.

Airbus may be consulted to determine whether or not the airworthiness is affected. In this case all details of findings are to be promptly reported for detailed evaluation and the assistance required clearly expressed.

A periodic review of the Structures Program, with particular attention to reported fleet data shall be scheduled to maintain the target of this program to control corrosion to Level 1 or better on all structural details, elements or assemblies which contribute significantly to carrying flight, ground, pressure or control loads, and whose failure could affect the structural integrity necessary for the safety of the aircraft.



FLOW CHART TO DETERMINE CORROSION LEVELS



EXPLANATION ON FLOW CHART DECISION STEPS

DECISION STEP A - CORROSION FINDING

There is a corrosion finding which is considered to be more than a negligible finding.

DECISION STEP B - BEYOND ALLOWABLE LIMITS

The corrosion defect noticed on the considered aircraft is beyond the allowable limits as defined by the manufacturer (e.g. SRM, SB, etc.).

DECISION STEP C - AIRWORTHINESS AFFECTED

The corrosion defect is beyond the allowable limits which prevent the aircraft from flying in a safe condition.

When significant corrosion findings occur which could affect the structural integrity of the airplane Airbus can be consulted to determine whether or not the airworthiness is affected.

In this case all details of findings are to be promptly reported for detailed evaluation and the assistance required clearly expressed.

DECISION STEP D - DUE TO A NON TYPICAL EVENT

For the purpose of the flow chart, a non-typical event is an event which is considered to be not representative of the events which normally occurs or could occur in the concerned area.

As examples:

- Mercury spillage

- Corrosive fluid spillages when they are demonstrated to be exceptional, however when they are noticed to be systematic they cannot be considered as non-typical.

DECISION STEP E - CUMULATIVE CORROSION

The corrosion in this area has been blended out previously and only at latest inspection the cumulative blend out now exceeds allowable limits as defined by the manufacturer (e.g. SRM, SB, etc.).



10. REQUIRED INSPECTION ITEMS (RIIs)

Tasks as RIIs. include those tasks that could result in a failure, malfunction, or

defect that endangers the safe operation of the aircraft if the task is not

completed properly or if operators use improper parts or material. If other

persons perform maintenance task, operators may authorize them to

accomplish their RII requirement, provided that manual satisfies the

regulatory requirements

10-1 List of Other Persons. Maintenance Organization’s manual must include a

list of persons with whom Maintenance Organizationss have arranged for the

performance of any required inspections both within their organization and

within other organizations that perform maintenance on their behalf. This

listing must include a designation by occupational title of the personnel

authorized to perform each required inspection.

10-2 Certification. Maintenance Organizations grant an RII authorization to must

hold an appropriate airman’s certificate. This is an air carrier qualification

requirement; the individual does not exercise that certificate when

accomplishing the RII. Maintenance Organizationss must formally notify each

of these individuals of their RII authorization as well as its scope.

10-3 RII Requirements. Maintenance Organizations should clearly identify RII

requirements on work forms, job cards, engineering orders, etc., or by any

other method consistent with their maintenance program. A primary concept

of the RII function is to prevent any person who performs any item of work

from performing any required inspection of that work. Therefore, it is

important that Maintenance Organizationss identify RIIs whenever possible so

that everyone knows that an RII is required.

10-4 Standards and Limitations. Maintenance Organizations must set

procedures, standards, and limits necessary for required inspections and

acceptance or rejection of the RII. Maintenance Organizationss should have

those procedures, standards, and limits necessary for the accomplishment of

required inspections. Maintenance Organizations must also have those

rocedures, standards, and limits necessary for the acceptance or rejection of

each of RIIs.

10-5 Procedures. Maintenance Organizations’ manual must include procedures

to ensure that you perform and complete all required inspections before

releasing the aircraft to service.

Tasks required RIIs will be noted as RII tasks.



11. MAINTENANCE CLOCK STARTING POINT Unless otherwise specified by AIRBUS in the documentation of an aircraft at time of first delivery, the starting point for calculation of the due dates or times of all aircraft maintenance tasks is identified in the following paragraphs. A. General Rule The date of first Transfer of Title (ToT) may be used as the starting point for the following: - Systems / Power Plant tasks with intervals expressed in airframe FH, FC or Calendar Time (except as identified in paragraph 2.0) - Structure tasks with an interval quoted in Calendar Time - Zonal tasks NOTE: This may not be valid if the first ToT occurs more than 90 days after first flight. In this situation specific guidance may be given to the operator at time of delivery. If details are not available to subsequent operators then any task that has not yet been accomplished shall be conservatively planned with reference to first flight date. First flight shall be used for all structure tasks with an interval quoted in FH, FC or LDGS. Tasks with intervals quoted in terms of component FH or component FC (e.g. APU Hours, Engine Cycles, ACT FH) shall be counted from First Flight of the component. The time to start the clock for tasks with applicability determined by post-delivery modification embodiment is the date of embodiment B. Specific guidance - For ALS Part 2 (DT-ALI) tasks: • The threshold is the time at which the maintenance task is first due. + Threshold limitations quoted in FC or FH count from first flight. + Threshold limitations quoted in Calendar Time may be counted from the Transfer of Title to the first operator. • For repeat maintenance tasks, the interval usage parameter (Calendar Time, FC or FH) is counted from the time the task was previously performed. • In cases where the first maintenance is accomplished very early, the next inspection can be performed at the threshold if the period (Calendar Time, FC or FH) between initial task accomplishment and the threshold is greater than the interval. • When alternative inspection methods are provided, the next interval applicable is the one associated with the inspection method used at the previous inspection. • "Touch and Go" cycles can be neglected if they are less than 5% of the total number of Flight Cycles up to threshold inspection or between two consecutive inspections. Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold inspection or between two consecutive inspections. - For ALS Part 3 (CMR) tasks: • Limitations quoted in FH or Calendar Time may be counted from the Transfer of Title to the first Operator. This policy is agreed with EASA in consideration of the very low number of FH performed between first flight and delivery, and the methodology used to define the value of CMR task limitations. • Limitations quoted in FC count from first flight. - For ALS Part 4 (ASM) tasks:



• Limitations controlled at aircraft level and quoted in Calendar Time count from the Transfer of Title to the first operator • Limitations controlled at aircraft level and quoted in FH, FC or LDGS count from first flight. • Limitations controlled at component/subassembly level and quoted in Calendar Time, FH, FC or LDGS count from the date at which the component/item accomplishes the first flight for which it will undertake its intended function. - For ALS Part 5 (FAL) tasks: • Limitations quoted in Calendar Time may be counted from the Transfer of Title to the first operator. • Limitations quoted in FH or FC count from first flight. - For an overhauled landing gear or a new landing gear installed after first Transfer of Title: the start date for Calendar Time tasks is the date of the gear’s first flight after installation. If this first flight takes place more than 90 days after installation contact Airbus Maintenance Programs Engineering front desk: [email protected]. - For equipment having intervals defined by the vendor (VR) or by National Requirements (NR): the starting point is the date of manufacture or date of overhaul (for Calendar Time tasks) or the first flight for which it will undertake its intended function (for FH and FC tasks) unless otherwise stated by vendor or National Authority. - For components addressed by Airworthiness Directive (AD): as stated in the AD. - For components that are transferred between aircraft: If the required task on the transferred component is performed as part of the installation process, then the next performance of the task counts from the installation date. Otherwise: • For system and structural components transferred between aircraft, the threshold for Calendar Time tasks is counted from either the date at which the aircraft to which it was originally fitted had its first Transfer of Title (if applicable) or, for a new component installed after delivery, the date at which the component accomplishes its first flight. • For structural components transferred between aircraft, the threshold for FH, FC or LDGS tasks is counted from the date at which the component accomplishes its first flight. • For system components transferred between aircraft, the threshold for FH and FC tasks is counted from either the date at which the aircraft to which it was originally fitted had its first Transfer of Title (if applicable) or, for a new component installed after delivery, the date at which the component accomplishes its first flight.

Source Calendar Time Flight Hours

Flight Cycles or

Landings

SYSTEM TOT TOT TOT

MRBR STRUCTURE TOT 1st Flight 1st Flight

ZONAL TOT TOT TOT



Source Calendar Time Flight Hours

Flight Cycles or

Part 1 1st Flight 1st Flight 1st Flight

Part 2 TOT 1st Flight 1st Flight

ALS Part 3 TOT TOT TOT

Part 4 (aircraft level) TOT 1st Flight 1st Flight

Part 4 (component level) 1st Flight 1st Flight 1st Flight

Part 5 TOT 1st Flight 1st Flight

LDG overhaul or installation of new 1st Flight after N/A 1st Flight

gear after first TOT installation

NR,VR Date of Date of Date of

Maunufature or

Maunufature or Maunufature or

Overhaul * Overhaul * Overhaul *

AD see AD see AD see AD

* unless otherwise stated in Vendor or National Authority documentation

12. IMPLEMENTATION PERIOD

A. GENERAL The IMPLEMENTATION PERIOD is a Grace period for the first time accomplishment of new tasks added to a Maintenance Program of an aircraft already in service in case there is no specific note of compliance date. The following paragraphs suggest Implementation Periods for the tasks originating from the various MPD source documents. The Implementation Period, often referred to as a “Grace” period, is to assist with first time accomplishment of new tasks added to a maintenance program of an aircraft already in service.

B. AD The compliance date is identified in the AD.

C. Airworthiness Limitations Items (ALI)– ALS Part 2 ALI grace periods must be handled on a case by case basis, using specific utilization data from concerned aircraft. It would be ensured that there do not exceed the limitation without prior agreement with the manufacturer, the local airworthiness authority and the certificating authority. In exceptional circumstances an ALI may be issued which is already overdue on a particular aircraft. In such cases Vietnam Airlines will contact manufacture (Airbus) to provide guidance for specific advice.

D. Certification Maintenance Requirements (CMR)– ALS Part 3



In theory, a CMR cannot be added, or an existing CMR made more restrictive, to an in-service aircraft. All CMRs should be published before the subject design feature enters service, whether this is on the basic aircraft or as a result of a modification. If delays occur in CMR document approval it is possible that a CMR becomes valid after EIS. In this case, the CMR document transmittal letter will advise an appropriate grace period before first time accomplishment.

E. Aging System Maintenance (ASM) – ALS Part 4 Aging Sytem Maintenance tasks are being established in order to allow operation of aircraft systems beyond their original qualification. Beyond this point, ageing effects may affect the characteristics leading to an increased potential for failure. The Part 4 of the Airworthiness Limitations Section (ALS) will be refered to take the maintenance actions together with their limitation to help to qualify the systems for continued operation.

F. Fuel Airworthiness Limitation Items (FAL) – ALS Part 5 On aircraft that have already exceeded the task threshold, It is recommended that the FAL tasks are performed at the operator's next scheduled structural inspection at 6 YE or 12 YE.

G. MRB Report and MRB Report Temporary Revision (TR) MRB Report (MRBR) tasks arise from a theoretical analysis of the aircraft prior to entry into service. Tasks are categorized according to whether they are associated with hidden or evident conditions and according to their contribution to the avoidance of safety and non-safety related failure effects. Depending on Vietnam Airlines qualifications and overall VAECO maintenance experience, adjustments to initial maintenance program tasks and intervals approved by CAAV. Vietnam Airlines suggest that a local guideline could be as follows:

– For Systems/APU/Power Plant and ZIP tasks Perform at the next due interval. This might not be the next interval (for which the planning may be completed) but it would be expected in the following one. NOTE: If task elapsed time is short and any possible corrective action is easily addressed, Vietnam Airlines consider first performance of at least the FEC 5 and 8 tasks in the next convenient 750 FH / 750 FC / 100 days package. NOTE: It is recognized that in some cases access for tasks with higher interval (e.g. 24000 FH, 80 MO) is not available at the next C1 or C2 check events (where typically tasks with intervals 7500 FH / 15000 FH, 5000 FC / 10000 FC, 24 MO / 48 MO are performed), for example, fuel tank entry, galley or lavatory removal. In these cases, unless stated otherwise in the MRB Report transmittal letter, recommend accomplishment at the next due interval that is typically a 6 YE check event.

– For Structure Tasks with CALENDAR threshold/interval A revised CALENDAR requirement is normally associated with findings from environmental impacts like corrosion, water ingress etc. It is recommended to perform the task as soon as possible on at least one aircraft in the fleet in order to help make this assessment. Delay inaccomplishment may lead to higher repair costs but not to a loss of continued airworthiness. Note that if a safety concern exists, a new CALENDAR task recommendation on an in service aircraft would be promulgated by ISB (and possibly AD) in addition to inclusion in the MRB Report.

– For Tasks related to EWIS



On aircraft that have already exceeded the task threshold, recommend that the ATA 20 tasks with (EWIS) after task description are performed at next convenient check opportunity unless access is assessed as insufficient to perform the task without exceeding the scheduled out-of-service period. In this case, the task should be performed at the next suitable access opportunity (e.g. a structural inspection at 6 YE or 12 YE) but not exceeding the task interval counting from the MRBR Rev. 12 approval date (April 2007).

H. Inspection Service Bulletins / All Operator Telexes As for AD, these documents normally include a recommended compliance time. Where this is not stated, it is recommended that Vietnam Airlines follows the same guidance as for the MRB Report.

I. Service Information Letters It is recommended that Vietnam Airlines follows the same guidance as for the MRB Report.

13. GLOSSARY

Check

Task performed to ensure that a system or component is still serviceable (check of bottle weight, check of firing circuit continuity, etc.) or that pressures or fluid levels are correct (See also Visual Check).

Visual Check

An observation to determine that an item is fulfilling its intended purpose. Does not require quantitative tolerances. This is a failure finding task.

Detailed Visual Inspection or Detailed Inspection

Intensive visual check of a specified detail, assembly or installation for evidence of damage or irregularity. The inspection may require surface cleaning, elaborate access procedures including removal of components where necessary and the use of such inspection aids as a flash light, mirrors, magnifying glass, etc.

Functional Test

A quantitative check to determine if one or more functions of a system/sub-system or component perform, within specified limits.

This task may call for the use of special test equipment.

General Visual Inspection

A visual inspection of an interior or exterior area, installation or assembly to detect various damage, failure or irregularity. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or drop-light and may require removal or opening of access panels or doors. Stands, ladders or platform may be required to gain proximity to the area being checked.

Repeat Interval

The maximum permitted period (for all tasks not performed on a sampling basis) that can separate two consecutive accomplishment of the task.



Lubrication

Term covering all types of lubricant application by grease gun, squirt can, spray, brush or hand, for the purpose of maintaining the inherent design operating abilities of an item.

Limit of Validity It is the period of time, expressed in appropriate units (e.g. flight cycles) for which it has been shown that the established inspections and replacement times will be sufficient to allow safe operation and in particular to preclude development of widespread fatigue damage.

Maintenance Task

An action or set of actions, including corresponding planning data, required to achieve a desired outcome which maintains an item (component, system/ sub-system, structure) in, or restores an item to, serviceable condition. This term includes inspection and determination of condition.

Maintenance Significant Item

Item identified by the manufacturer, whose failure

- Could affect safety (ground or flight), and/or

- Is undetectable during operation, and/or

- Could have significant operational economic impact, and/or

- Could have significant non-operational economic impact.

Operational Test

A task to determine qualitatively that an item is fulfilling its intended purpose. This task may include the reading of the aircraft instruments but does not require the measurement of tolerances.

Replacement

The action whereby an item is removed and another new or restored item is installed in its place.

Restoration

Term covering all actions (on/off the aircraft) necessary to return the item to a specific standard.

Sampling

The monitoring and/or withdrawal of selected devices from service to permit determination of their condition at predetermined progressive intervals.

Special Detailed Inspection

An intensive check of a specific location requiring some special technique such as non-destructive test techniques, dye penetrated, high-powered magnification... and that may require disassembly procedures.



Structure Significant Item

A structural detail, structural element or structural assembly which is judged significant by the manufacturers because of the reduction in aircraft residual strength or loss of structural function which are consequences of its failure.

Threshold

Limit deadline for all tasks not performed on a sampling basis at which the task must be accomplished for the first time (subsequent accomplishment deadlines are rained by adding the repeat interval and its multiples to the threshold).

Touch and go

A ‘Touch and go’ is a landing in which an aircraft touches the runway and does

not come to a full stop prior to commencing an additional flight.

14. ABBREVIATIONS

The following abbreviations are used through out the present document:

AA : Airworthiness Authorities

A/C : Aircraft

AC : Alternating Current

AC : APU Change

ACARS : Aircraft Communication Addressing and Reporting System

ACC : Active Clearance Control

ACT : Additional Center Tank

ACAS : Airborne Collision Avoidance System

ACMS : Aircraft Condition Monitoring System

ACP : Area Call Panel

ACR : Avionics Communication Router

AD : FAA Airworthiness Directive

ADCN : Aircraft Data Communication Network

ADF : Automatic Direction Finder

ADIRS : Air Data and Inertial Reference System

ADIRU : Air Data/Inertia Reference Unit

AESS : Aircraft Environment Surveillance System

AFDX : Avionics full Duplex

AFM : Airplane Flight Manual

AFMS : Auxiliary Fuel Management System

AFS : Automatic Flight System

AFT : Rear



AGCM : Airborne Ground Check Module

AGU : Air Generation Units

AH : APU Operating Hours

AIB : Airbus

AIDS : Aircraft Integrated Data System

ALI : Airworthiness Limitation Item (ALS Part 2)

ALS : Airworthiness Limitation Section

AMM : Aircraft Maintenance Manual

AMT : Aircraft Maintenance Task Reference

AMTOSS : Aircraft Maintenance Task Oriented Support System

AOL : All Operators Letter

AOT : All Operator Telex

AOW : All Operator Wire

AP : Autopilot

APU : Auxiliary Power Unit

ARO : Anti Roll Out

ASM : Ageing System Maintenance (ALS Part 4)

ASSY : Assembly

ATA : ATA Specification

ATC : Air Traffic Control

ATT : Attitude

BAT : Battery

BCL : Battery Charge Limiter

BCRC : Bulk Crew Rest Compt.

BITE : Built-In Test Equipment

BSCU : Braking & Steering Control Unit

CAS : Cabin Attendant Seat

CFDS : Centralized Fault Display System

CFMI : CFM International

CMP : Configuration, Maintenance, Procedure and Dispatch Standards for Extended Diversion Time Operations (ETOPS)

CMR : Certification Maintenance Requirements (ALS Part 3)

CN : Consignee de Navigabilité (French Airworthiness Directive)

COMPT : Compartment

CPCP : Corrosion Prevention and Control Program



CRR : Crew Rest Room

CSU : Command Sensor Unit

CVR : Cockpit Voice Recorder

CWB : Center Wing Box

CY : Cycle

D : Deleted

DC : Direct Current

DDRMI : Digital Data Radio Magnetic Indicator

DET : Detailed Inspection

DFDR : Digital Flight Data Recorder

DGAC : Direction Générale de l’Aviation Civile (French Airworthiness Authority)

DI : Detailed Inspection

DMC : Display Management Computer

DS : Discard

DT : Damage Tolerance

DU : Display Unit

DY : Day

EASA : European Aviation Safety Agency

EC : Eddy Current Inspection Method

ECAM : Electronic Centralized Aircraft Monitoring

ECU : Engine Control Unit

EDP : Engine Driven Pump

EFIS : Electrical Flight Instrument System

EIS : Electronic Instrument System

ELAC : Elevator and Aileron Computer

ELT : Emergency Locator Transmitter

EMER : Emergency

EN : Endoscope Inspection Method

ESS : Essential

ETOPS : Extended-range Twin-engine Operation Performance Standard

EVAC : Evacuation

EVMU : Engine Vibration Monitoring Unit

EWIS : Electrical Wiring Interconnection System

EZAP : Enhanced Zonal Analysis Procedure



EXTIR : Extinguisher

FAA : United States Federal Aviation Administration

FAC : Flight Augmentation Computer

FAL : Fuel Airworthiness Limitations (ALS Part 5)

FADEC : Full Authority Digital Engine Control

FC : Flight Cycle

FC : Functional Check

FCOM : Flight Crew Operating Manual

FCRC : Flight Crew Rest Compt.

FD : Flight Director

FDUI : Flight Data Interface Unit

FEC : Failure Effect Category (5 evident safety; 6 evident operational; 7 evident economic; 8

hidden safety; 9 hidden non safety)

FH : Flight Hours

FL : Flight Hours

FR : Frame

FWD : Forward

GAPCU : Ground and Auxiliary Power Control Unit

GCU : Generator Control Unit

GLC : Generator Line Contactor

GPCU : Ground Power Control Unit

GPWS : Ground Proximity Warning System

GSE : Ground Support Equipment

GSM : Global System for Mobile communications

GRP x : Weight variant group “x”

GSE : Ground Support Equipment

GVI : General Visual Inspection

HDG : Heading

HFEC : High Frequency Eddy Current Inspection Method

HIRF : High Intensity Radiated Fields

HP : High Pressure

HPT : High Pressure Turbine

HR : Hour

I : Repeat Interval



IAE : International Aero Engine

IDG : Integrated Drive Generator

IFES : In Flight Entertainment System

INTRO : Introduction

ISB : (Inspection) Service Bulletin

ISIS : Integrated Standby Instrument System

JAA : Joint Aviation Authorities

JAR : Joint Aviation Requirement

LD : Landing

LD : Lower Deck

LDF : Lower Deck Facility

LDL : Lower Deck Lavatory

LDMCR : Lower Deck Mobile Crew Rest

LE : Leading Edge

LEP : List of Effective Pages

LFEC : Low Frequency Eddy Current Inspection Method

LGCIU : Landing Gear Control and Interface Unit

LH : Left Hand

LP : Low Pressure

LPC : Low Pressure Compressor

LPT : Low Pressure Turbine

LTA : German Airworthiness Directive

LU : Lubrication

LUR : Low Utilization Recommendation

LWR : Lower

MCDU : Multipurpose Control and Display Unit

MH : Man hours

MLG : Main Landing Gear

MO : Month(s)

MOD : Modification

MPD : Maintenance Planning Document

MRB : Maintenance Review Board

MSG : Maintenance Steering Group

MSI : Maintenance Significant Item

MSN : Manufacturer Serial Number



N : New

ND : Navigation Display

NDT : Non Destructive Testing

NLG : Nose Landing Gear

NR : National Requirements

NRV : Non Return Valve

NT : Note

NTM : Non Destructive Testing Manual

OP : Operational Check

PCU : Power Control Unit

PFD : Primary Flight Display

POB : Pressure off Brakes

PREP : Preparation

PTT : Press to Test

PTU : Power Transfer Unit

PW : Pratt & Whitney

PWS : Predictive Windshear System

QAD : Quick Attach Detach

R : Revised

RAT : Ram Air Turbine

RF : Resonance Frequency Inspection Method (e.g. Tap Test)

RH : Right Hand

RMP : Radio Management Panel

ROTO : Roto-test Inspection Method with Eddy Current Roto-probe

RS : Restoration

RSVR : Reservoir

S : Sampling

SB : Service Bulletin

SDI : Special Detailed Inspection

SIL : Service Information Letter

SMR : Scheduled Maintenance Report (engine)

SOV : Shut off Valve

SSI : Structure Significant Item

ST (G) R : Stringer

SV : Servicing



SYS : System

TBD : To be determined

TCAS : Traffic Collision Avoidance System

TE : Trailing Edge

THS : Trimmable Horizontal Stabilizer

TOC : Table of Content

TPIS : Tyre Pressure Indication System

TPS : Temporary Protection System

TR : Temporary Revision

UD : Upper deck

ULB : Underwater Locating Beacon

US : Ultrasonic Test Inspection Method

VC : Visual Check

VCC : Video Control Center

VHF : Very High Frequency

VR : Vendor Recommendation

YE : Year

15. REVISION

The updating of the present A321 AIRRAFT MAINTENANCE SCHEDULE is under VIETNAM AIRLINES responsibility based on the periodic revisions of the AIRBUS INDUSTRIE A319/A320/A321 Maintenance Planning Document (MPD) and other related technical documentations.



16. ASSISTANCE AND INFORMATION

Any query or comments regarding

* The A319/A320/A321 MPD should contact:

AIRBUS

CUSTOMER SERVICES

Maintenance Planning & Services

B.P. No. 33

F-31707 Blagnac Cedex

FRANCE

or TLX : 530 526 F

FAX : 33 (0) 5 61 93 28 72

SITA : TLSBT7X

[email protected]

* The A321 MAINTENANCE SCHEDULE should contact:

VIETNAM AIRLINES

HEAD OFFICE

TECHNICAL DIRECTOR

200 NGUYEN SON St., LONG BIEN Dist,

HANOI

VIETNAM

TEL: 84.4.38731774

FAX: 84.4.38273004

SITA: HDQEPVN


SECTION 2

LINE MAINTENANCE CHECKS

LIST OF EFFECTIVE PAGES SECTION MVT PAGE ISSUE

2-LEP R 1 SEP 2013 2-TOC R 1 SEP 2013 2-GENERAL INTRODUCTION R 1 SEP 2013 2-PRE-FLIGHT / TRANSIT CHECK LISTS R 1 SEP 2013 2-PRE-FLIGHT / TRANSIT CHECK LISTS R 2 SEP 2013 2-PRE-FLIGHT / TRANSIT CHECK LISTS R 3 SEP 2013 2-TERMINAL CHECK LISTS R 1 SEP 2013 2-TERMINAL CHECK LISTS R 2 JAN 2014 2-TERMINAL CHECK LISTS R 3 SEP 2013 2-WEEKLY CHECK LISTS R 1 SEP 2013 2-WEEKLY CHECK LISTS R 2 JAN 2014 2- WEEKLY CHECK LISTS R 3 JAN 2014

ISSUE: JAN 2014 SECTION 2 - LEP PAGE 1


SECTION 2

LINE MAINTENANCE CHECKS

TABLE OF CONTENTS

SUBJECT GENERAL LINE MAINTENANCE CHECK LISTS ISSUE: SEP 2013 SECTION 2 - TOC PAGE 1

I.A.W AMS A321 - Issue 14 Amd 01 A321 PRE-FLIGHT / TRANSIT CHECK Page 1 of 3

FROM No: VNA-TE-F36

Issued: 00 / Mar. 2009

QUY TRÌNH

KIỂM TRA TRƯỚC KHI BAY/GIỮA HAI LẦN BAY

PRE-FLIGHT/TRANSIT CHECK

Aircraft Type A321 Effectivity A/C Reg. No:

Check Definitions and Notifications

a) A “PRE-FLIGHT/TRANSIT Check” shall be performed before each flight but not earlier than 2 hours before

the flight. (It includes also the correction of troubles reported in the log book if the airworthiness of the aircraft

is affected).

b) All fluids uplifted during the “PRE-FLIGHT/TRANSIT Check” must be recorded on the current page of the

aircraft technical log

Safety Pre-caution at aircraft arrival

In accordance with Line Maintenance / Group Handling Procedures

Ensure parking area is clear of foreign objects or any other obstructions, check operation of aircraft exterior lights during

taxiing in, chock nose wheels fore and aft.

Item

Title / Task Description / Requirement

1 Remove all nose landing gear and main landing gear safety pins (before first flight of the day).

2 Review and action Technical Log book and Cabin Defect Log book, transfer entries to Technical Log book where necessary (transit only).

3 a. Do a safety check of flight compartment for proper position of controls.

b. Energize the aircraft electrical network IAW AMM task 244100/2.

c. Check security box for general condition ref. AMS task VN257000-01.

4 Remove all protective covers and blanks (before first flight of the day).

5 Check battery 1 and 2 volts immediately before selection of GPU / APU or if power has been off more than six hours.

BATT 1 AND 2 CHECK OFF

BATT 1 AND 2 VOLTAGE CHECK ABOVE 25.5V

Batteries voltage above 25.5V (battery capacity is above 50%).

If batteries voltage below 25.5V, a charging cycle of about 20 minutes is required.

BATT 1 AND 2 AUTO

EXT POWER ON

Check ECAM ELEC page, batteries contactor closed and batteries charging.

6 Inspect landing gear doors, wheels, brakes and tyres for condition. Check Oleo extensions appear normal.

7 Do walk around inspection of the whole aircraft exterior and check for obvious signs of fluid leaks and damage, loose or missing parts, obstruction of inlets / outlets, fuselage tail skid for damage of ground contact during take off (transit only), navigation / communication system antenna, static ports, TAT, pitot probes, AOA sensors, discharge indicators of oxygen and APU fire extinguisher.


Item


8 a. Drain water from each fuel tank (if the aircraft has been on the ground for six hours or more) IAW AMM task 12-32-28-281-001 ref. AMS task 281100-01-2.

b. Obtain water free samples from bowser or “Refueling truck” prior to refueling.

c. Refuel the aircraft up to required dispatch quantity IAW AMM task 121128/3, Make sure that, fuel uplift quantity discrepancy (between Aircraft’s indicator and Bowser’s indicator) is within limit (reference: APPENDIX 1) - Note: This requirement apply to all flights dispatched from Vietname’s Airports only.

Record uplift / content in the Technical Log book.

d. Ensure refuel coupling cap is in place and secured.

e. Ensure dipsticks are retracted and secured.

9 a. Inspection/Check of the Wheels and Tires IAW AMM task 32-41-00-210-002

b. Check and record tire pressure to aircraft technical logbook IAW AMM task 32-41-00-210-003 ref. AMS task 324100-01-1 (before first flight of the day).

10 Examine the torque link assembly. Make sure that it is correctly installed and there is no damage or wear.

11 Do an external inspection of engines including fan, inlet cowl, turbine and exhaust nozzle and cowlings for security.

12 Check engine oil on ECAM within 30 minutes of engine shut down and hydraulic level, uplift and record in Technical Log book if necessary (transit only).

13 Service toilet and fresh water systems as required, check for fluid leaks at toilet and water servicing panels. Rectify defects before flight.

14 Ensure any corrective actions made in the Technical Log book have been cleared.

15 RVSM REQUIREMENTS (ref. 748/TCTHK-ĐBCL 25th., July, 2007):

a. Inspection/Check of the Pitot Probes, Static Probes and AOA Sensors IAW AMM task 34-13-00 page block 601 (before first flight of the day).

b. Do a visual inspection around the static probes (left and right sides). Note:

In order to help the operator to determine easily the area to be inspected, Airbus proposes to draw on the fuselage some red marks as defined in SIL 34-064 (corners of a squares).

These marks are for information only and aim at easing the pre-flight check. In addition, they are not mandatory to archieve the RVSM certification. In case of scratches or dents around the static ports, the only applicable documentation is the SRM ATA 53.

16 Do security inspection of the whole aircraft as per “ MECHANIC” section in the form VNA-SQ-F81-09 (Aircraft Normal Security Check Report) and take the signature.

CAUTION: The Emergency Exit Doors 2LH/RH & 3LH/RH were always in armed condition after MOD A321-11-014-2010. So check the slide control handle of this Emergency Exit Doors in armed position and placard “ CHỈ MỞ CỦA KHI THOÁT HIỂM / EMERGENCY USE ONLY” on them for presence.

17 FINAL WALK AROUND INSPECTION:


Item


a. Ensure all doors and panels are secured, landing gear pins removed and stowed, engine intakes and air inlets clear of foreign objects.

b. Ensure no damage has been caused by ground equipment or during baggage loading.

c. Ensure towing lever is in normal (spring loaded) position and towing pin is removed.

d. Remove wheel chocks (upon flight crew instruction).

APPENDIX 1:

Fuel uplift quantity discrepancy limit (between Aircraft’s indicator and Bowser’s indicator)

(by fuel uplift quantity)

Fuel uplift quantity (Kg)

(by aircraft’s indicator)

Discrepancy (%)

Discrepancy (Kg)

0 ÷ 1000 Kg ≤ 5.8 ≤ 58

1000 Kg ÷ 2000 Kg ≤ 4.5 ≤ 90

2000 Kg ÷ 5000 Kg ≤ 3.8 ≤ 190

5000 Kg ÷ 10000 Kg ≤ 2.6 ≤ 260

10.000 Kg ÷ 20000 Kg ≤ 2.3 ≤ 460

More than 20000 Kg ≤ 1.6 ≤ 1600

(with uplift quantity less than 100,000 Kg)

Safety Pre-caution at aircraft departure

Dispatch aircraft in accordance with Line Maintenance / Ground Handling Procedures

Prior to engine start, ensure area is free of any loose objects and obstruction, any remaining entry / service doors are

secured closed and wheel chocks removed.

“RVSM Capability”

Prior to every flight, review the following and action as required:

a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance

(OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “RVSM

CAPABLE”.

b) Write in techlog if the A/C is not RVSM capable.

I.A.W AMS A321 - Issue 14 Amd 01 A321 TERMINAL CHECK Page 1 of 3

FROM No: VNA-TE-F37


QUY TRÌNH KIỂM TRA CUỐI NGÀY

TERMINAL/DAILY CHECK OR EQUIVALENT

Aircraft Type A321 Affectivity A/C Reg. No:

Check Definitions and Notifications

a) The “TERMINAL Check” shall be performed in principle every day and in any case interval must not exceed 36

hours elapsed time.

b) All fluids uplifted during the “TERMINAL CHECK” must be recorded on the current aircraft Technical Log page.

c) Preflight/Transit check is included in this terminal check procedure. If time to next flight is more than two (02)

hours, then it is required to perform preflight check again.


In accordance with Line Maintenance / Ground Handling Procedures

Ensure parking area is clear of foreign objects or any other obstruction, check operation of aircraft exterior lights during

taxiing in, chock nose wheels fore and aft

Item Title / Task Description / Requirement

1 Carry out Transit Check IAW form A321 - PRE-FLIGHT / TRANSIT CHECK.

2 Install wheel chocks, nose landing gear and main landing gear safety pins.

3 Install all protective covers and blanks.

4 Check seat covers and slide-raft covers for condition.

5 Check the serviceable status of the First Aid Kits and Medical Kits (seal, expired date, condition, etc), replaced if expired or has been used.

6 Do the following operational tests of:

a. External lights IAW AMM task 334100/5, 334200/5, 334600/5, 334700/5, 334800/5 and 334900/5.

b. Cabin lighting and passenger signs IAW AMM task 33-21-00-710-001.

7 Check general cockpit lighting, emergency torches and replenish spare bulb box as required.

8 Check lavatories for:

a. General condition, cleanliness and evidence of water leakage.

b. Effectiveness of waste disposal self-closing flaps and access doors, verify containment capability.

c. Damage and distortion to the waste bins and cleanliness and freedom from debris of the bin compartment.

d. Serviceability of ashtrays both inside and outside of the lavatories.

e. "NO SMOKING" signs both inside and outside of the lavatories.

9 With parking brake applied, check brake wear indicators of heat pack, leakage and overheating IAW AMM task 32-42-27-210-003 ref. AMS task 324227-01-1.

10 Do a general visual inspection of landing gear, landing gear doors and wheel IAW AMM task 05-27-00-200-001, including:

a. Nose landing gear and main landing gear proximity switches for security and cleanliness.

b. Main landing gear shock absorber for signs of leakage and normal extension.

c. Main landing gear sliding tube for scoring / damage and normal extension.

d. Nose landing gear shock absorber for signs of leakage and normal extension.



e. Wheels and tires (rim damage, sheared / missing tie bolts).

f. Hydraulic leaks (gear doors closed) .

g. Nose landing gear taxi light for cleanliness.


11 Do the following passenger cabin check:

a. Passenger cabin for general condition and cleanliness.

b. Galleys for general condition, cleanliness and evidence of water leakage.

c. Check the following emergency equipment for:

Proper installation/Location.

Damaged.

Security Seal (if having)

(Emergency Equipment Lits is attached in Techlog)

d. Wing upper surfaces and control surfaces through cabin windows for general condition and evidence of fluid leakage.

12 Records APU hours / cycles using ECB (APU Data/Oil Page) and DMU IAW AMM task 31-36-00-740-006.

13 Do a general visual inspection of the APU area including:

a. Air intake: flap closed.

b. Door: closed and secured.

c. Drain mast, drains and vents.

d. Exhaust.

e. Fire extinguisher overpressure indicator.

14 Do a general visual inspection from the ground of the stabilizers and the cone / rear fuselage IAW AMM task 05-23-00-200-001, including:

a. Trimmable horizontal stabilizers and elevators.

b. Fin and rudder.

c. Static dischargers.

15 Do a general visual inspection of the upper half of fuselage from the ground as far as visible IAW AMM task 05-22-00-200-001. Make sure that there are no signs of corrosion, cracks or damage.

16 Do a general visual inspection of the lower half of fuselage from the ground as far as visible IAW AMM task 05-21-00-200-001, including:

a. Avionics equipment vent air inlet valve.

b. Fresh water and wastewater drain masts.

c. Pitot probes, static ports, and AOA sensors IAW AMM task 34-13-00-200-001.

d. Exterior lights for cleanliness.

e. Radome: latches positively locked.

f. Crew oxygen cylinder overpressure indicator: green disc in place.

g. Outflow valve: no obstruction.

h. Antennas and beacon.



17 Do a general visual inspection of all service panels and doors as far as visible from the Ground IAW AMM task 05-28-00-200-001.

18 Do a general visual inspection of the wings as far as visible from the ground IAW AMM task 05-25-00-200-001, including:

a. Leading edge slats.

b. Leading edge ventilation air intake: no obstruction.

c. Landing light for cleanliness.

d. Surge tank air intake: no obstruction.

e. Fuel tank overpressure protector disc: white cross in view.

f. Navigation and strobe lights.

g. Static dischargers.

h. Control surfaces, flaps and track fairings: no damage or fluid leakage.

i. Lower wing surface: evidence of fuel leakage.

19 Do a general visual inspection (as far as visible) of the power plants, the nacelles and the pylons (cowlings closed) IAW AMM task 05-24-00-200-001, including:

a. Cowlings: panels, air outlets, security of latches.

b. Fan thrust reverser doors: latches secured (red indicator not protruding).

c. Drain mast and pylon drains: no obstruction or fluid leakage.

d. Access doors and over pressure doors: in place, closed and secured.

e. Engine air inlets: lip skins, inner and outer intake cowls.

f. Fan exhausts: acoustic lining, exit vanes and struts, thrust reverser blocker doors.

g. Turbine exhausts: 5th.Stage low pressure turbine blades, nozzle and plug (for damage and metal deposit).

20 Do the following:

a. De-energize the aircraft electrical network IAW AMM task 244100/2.

b. Ensure all doors and service panels are properly closed and secured.

c. Ensure all required protective covers and blanks installed.

Safety Pre-caution at aircraft departure

Dispatch aircraft in accordance with Line Maintenance / Ground Handling Procedures


secured closed and wheel chocks removed



a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance

(OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “RVSM

CAPABLE”.


I.A.W AMS A321 – Issue 14 Amd 01 A321 WEEKLY CHECK Page 1 of 3

FORM No: VNA-TE-F38


QUY TRÌNH KIỂM TRA NGOẠI TRƯỜNG

WEEKLY/LINE1/LINE2 CHECK OR EQUIVALENT

Aircraft Type A321 Effectivity A/C Reg. No:

A/C Reg.

No. Station Date

Tech

Log page

Work

Package

Check Definitions and Notifications a) The “Weekly Check” shall be carried out within every 08 days.

b) All fluids uplifted during the “Weekly Check” must be recorded on the current aircraft Technical Log page.

c) Preflight/Transit and Terminal check is included in this Weekly Check procedure. If time to next flight is more than

two (02) hours, then it is required to perform Preflight/Transit check again.


In accordance with Line Maintenance / Ground Handling Procedures

Ensure parking area is clear of foreign objects or any other obstruction, check operation of aircraft exterior lights during

taxiing in, chock nose wheels fore and aft

Item Title / Task Description / Requirement MECH INSP

1 Carry out terminal check IAW form A321 - TERMINAL/DAILY CHECK OR EQUIVALENT.

2 Clean all CRT/LCD screens.

3 Check crew / passenger seats and belts for general condition and attachment.


4 In passenger cabin:

a. Do a visual inspection of passenger compartment, including seat track covers, ceiling panels, light covers, window panels, forward and aft partitions and stowage, literature pocket and magazine rack, attendant seats, shroud and cover on each lavatory ref. CMS task VN252000-01.

b. Do a detailed visual inspection of waste compartment for damages and

sealing. Make sure the flaps operate normally, repair if necessary ref. CMS task VN253000-06.

c. Check pressure of emergency cylinder / accumulator of forward and aft

passenger / crew doors. IAW AMM task 52-10-00-210-004 ref. AMS task 521000-01-1.

d. Check emergency cylinder/accumulator pressure on pressure gauge IAW

AMM 52-22-00-200-001 ref. AMS task 522200-08-1.

e. Check pressure on portable oxygen cylinder gauges IAW AMM task 35-30-

00-210-004 ref. AMS task 353000-01-1.

f. Do a detailed inspection of portable oxygen mask IAW AMM task 35-30-00-

220-001 ref. AMS task 353000-07-1.

g. Cleaning of vacuum waste lines with chemical cleaning agent and crushed ice

IAW AMM task 38-31-00-100-010 ref. AMS task 383100-06-1.

5

a. Check the following emergency equipment for:

- Proper installation/location. - Damaged.

- Security Seal (if having)

Note: Emergency Equipment Lits is attached in Techlog



6

a. Check all Lavatories as below for general condition and functional operation as below.

- Waste Disposal Lid Spring Retention & Waste Enclosure Door Close

- Operational condition of Wash Basin Drain

- Lavatory Door Latch Sliding & Locking with Light On/Off

- Operational condition of Toilet Flushing

- Operational condition of Soap Dispenser and cleanliness

- Condition of Waste Compartment Fire Ext, Temp Indicator

- Condition of No Smoking Placard, Ashtray

7

a. Check all Galley as below for general condition and functional operation as below.

- Galley Sink Drain, Clogging

- Operational condition and cleanliness of Galley Inserts (Oven, C/M, W/B,

refrigerator)

- Cleanliness of inside of Oven

- Drain Clogging of inside of Ice Drawer Compartment.

8

IFE System Checks

a. Apply for A321-MPES system: - Test audio system IAW AMM task 23-33-00-710-002-A

- Test O/H video system IAW AMM task 23-36-00-710-001-A

- Operation check of the Video PA system

- Operation check of the Airshow system TASK 23-34-00-710-001-A

- Operation check of the Boarding Music system TASK 23-32-00-710-002-A

b. Apply for A321-DMPES system:

- Test of boading music, broadcast audio, broadcast video on O/H LCD, sky map, video PA and audio announcement IAW AMM TASK 23-33-00-710-005-A.

- Check the operation of all O/H LCD monitor.

- Carry Out Close Flight and Turn OFF IFE system after finish working.

c. Apply for A321-EFX system:

- Test of boading music, broadcast audio, broadcast video on O/H LCD, sky map, video PA and audio announcement IAW AMM TASK 23-33-00-710-005-A.

- Check AVOD on each B/C seats.

- Check the operation of all O/H LCD monitor.

- Carry Out Close Flight and Turn OFF IFE system after finish working

CAUTION: BEFORE ENTERING OR APPROACHING THE NLG / MLG WELLS / HYD COMPARTMENT MAKE CERTAIN DOORS ARE LOCKED AND COLLARS FITTED (MLG DOOR ACTUATOR) IN OPENED POSITION BY MEANS OF SAFETY PINS EQUIPPED WITH STREAMERS.

9 In nose landing gear and hydraulics compartment, do the following general visual inspection of:

a. Nose landing gear wheel well including zone 124 IAW AMM task 05-21-20-

200-002.

b. Components: installation external leakage.

c. Doors: structure, hinges, up-lock assembly and operating mechanism.

10 In main landing gear and hydraulics compartment, do the following general visual inspection of:

a. Main Gear Well and the Hydraulics Compartment (Zones 147 and 148) from the ground IAW AMM task 05-21-40-200-003.

b. Do a general visual inspection of main landing gear bay IAW AMM task 05-25-70-200-001.

c. Cylinder door and secondary door with main landing gear doors open.

d. Components: installation external leakage.

e. Doors: structure, hinges, up-lock assembly and operating mechanism.



11 In forward and aft cargo compartment, do the following general visual inspection of:

a. Cargo compartment decompression, lining and floor panels IAW AMM task 25-50-00-200-002 ref. AMS task 255000-01-1.

b. Forward and aft cargo compartment door skin external surface.

12 Check IDG oil level and filter differential pressure indicator IAW AMM task 24-21-51-200-010 ref. AMS task 242100-07-1.

13 Do the following operational tests of:

a. Emergency lights by “TEST EMER LIGHT SYS” push button IAW AMM task 33-51-00-710-001 ref. AMS task 335100-01-1.

b. AC emergency generation system IAW AMM task 24-24-00-710-001 ref. AMS task 242400-01-2 (CMR task).

114 Check engine oil level and replenish IAW AMM task 12-13-79-610-011.

a. L/H

b. R/H

15 Check APU oil level and replenish IAW AMM task 12-13-49-612-001.

16 Check CFDS (PFR) for slow door opening/closing messages IAW AMS Task 323105-03-1, AOT A320-32A1390 Note:Threshold of this task is 800 FC.

17 Replacement of the QAR Disk IAW AMM task 31-33-52-600-004 for flight data storage (Except A/C fitted with QAR P/N 2243800-73).

18 CERTIFY WEEKLY CHECK IN TECHNICAL LOG BOOK.

Safety Pre-caution at aircraft departure Dispatch aircraft in accordance with Line Maintenance / Ground Handling Procedures


secured closed and wheel chocks removed



a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance (OPM)

sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “RVSM

CAPABLE”.


CERTIFICATE OF RELEASE TO SERVICE

“The work recorded has been carried out in accordance with the requirements of VAR-145 for the time being in force and

in respect to that work the aircraft / aircraft equipment is considered fit for service”.

Date: Signature:.......................... Stamp Holder:..............................Time (UTC):

The stamp / signature in the inspection column denote work has been carried out in accordance with the above quirements.


SECTION 3

SCHEDULED COMPONENTS MAINTENANCE



3- LEP R 1 SEP 2013

3- TOC R 1 SEP 2013

3.0- GENERAL INTRODUCTION N 1 SEP 2013




3.1- A321 ENGINE LIFE LIMITED PARTS R 1 SEP 2013

3.1- A321 ENGINE LIFE LIMITED PARTS R 2 SEP 2013

3.1- A321 APU LIFE LIMIT PARTS N 1 JAN 2014






3.2- A321 LANDING GEAR LIFE LIMITED PARTS N 1 SEP 2013






3.3- A321 SYSTEM LIFE LIMITED COMPOMENTS N 1 SEP 2013

3.4- A321 TIME CONTROLLED ITEMS LIST N 1 SEP 2013









ISSUE: JAN 2014

SECSION 3 - LEP

PAGE: 1


SECTION 3


TABLE OF CONTENTS

SUBJECT

SUB-SECTION 3.0: GENERAL INTRODUCTION SUB-SECTION 3.1: A321 ENGINE/APU LIFE LIMIT PARTS SUB-SECTION 3.2: A321 LANDING GEAR LIFE LIMITED PARTS SUB-SECTION 3.3: A321 SYSTEM LIFE LIMITED COMPONENTS SUB-SECTION 3.4: A321 TIME CONTROLLED ITEMS LIST

ISSUE: JAN 2013 SECTION 3 - TOC PAGE 1


ISSUE: SEP 2013 SECTION 3 - GENERAL PAGE 1

SECTION 3



1. General

This section of the A321 Maintenance Programme divides into the sub-sections as follows:

- Sub-Section 3.1: A321 Engine/APU Life Limited Pars.

- Sub-Section 3.2: A321 Landing Gear Life Limited Parts.

- Sub-Section 3.3: A321 System Limited Components.

- Sub-Section 3.4: A321 Time Controlled Items List.

2. Sub-Section 3.1 - A321 Engine Life Limited Parts:

Life limited parts of the engine are published in the Time Limits Manual of the IEA TLM’s Engine Manual. The maximum life of an engine part is engine cycle that is defined as any flight consisting of one take-off and landing regardless of the length of flight or whether or not thrust reverser is used on landing. Each touch and go is considered an additional cycle. Parts must not be used after the total cycles for a part has equaled the maximum permitted for that part. 3. Sub-Section 3.2 - A321 Landing Gear Life Limited Parts: 3.1 This sub-section of AMS related to ALS ALS Part 1 - Safe Life Airworthiness Limitation Items and be included two tables: A321 LDG LLP SUB-PART 1-2 TABLE, A321

LDG LLP SUB-PART 1-3 TABLE which they are corrective ALS Sub-part 1-2 (Life limits) and ALS Sub-part 1-3 (Demonstrated fatigue lives). 3.2 SUB-PART 1-2 TABLE: Life limits Parts listed under this sub-part are those having a life limit less than the Limit Of Validity (LOV) due to failure during fatigue tests and whose failure could result in a catastrophic failure of the airplane. 3.3 SUB-PART 1-3 TABLE: Demonstrated fatigue lives

Parts listed under this sub-part are those having a demonstrated fatigue life without failure but whose failure could result in a catastrophic failure of the airplane. Where the values are less than the LOV, fatigue tests are still on going. For these parts, the life limitation provided (in flight hours and/or flight cycles and/or landings and/or calendar time, as applicable) is temporary waiting for finalization of the tests. If the demonstrated fatigue life reaches the LOV, it will remain in sub-part 1-3, if the part fails before the LOV, its Part Number (PNR) together with the life limit(s) will be transferred to sub-part 1-2.



3.3 A321 LDG LLP sub-part 1-2 and 1-3 tables provide the applicable life limitations only when PNR installations have been authorized. These tables do not ensure that a PNR has been validated for a specific individual aircraft MSN. PNR are authorized for installation on individual aircraft MSN by SB (and the associated modifications), which are published by Airbus. Life limitations quoted in sub-parts 1-2 and 1-3 are applicable to the undamaged detail parts as listed, not to the assembly or the aircraft on which they are installed. The limitation/replacement time indication is quoted on the same line/block of lines as the PNR. 3.4 Aircraft model applicability headers indicate aircraft models. When ‘x’ is entered in the model number, it stands for any number within the limits of the list of models e.g.:

A321-200 stands for: A321-211, A321-212, A321-213, A321-231... Life limitation applicability is allocated according to the aircraft model affected, e.g.: “X” stands for: All aircraft models defined by the applicability of the column.

3.5 Traceability and replacement requirements

In order to maintain aircraft airworthiness, it is mandatory to replace parts listed under sub-parts 1-2 and 1-3 at or prior to whichever of the life limitations occurs first, after any necessary adjustment of the stated life limitations in accordance with the instructions of paragraph 6 of ALS part 1, sub-part 1-0.

In the context of the ALS Part 1, the traceability means records that clearly demonstrate the history of parts back to initial entry into service of the part, so that life limitations are accurately applied. Traceability records may comprise, but are not limited to, the following:

- Application history (aircraft type, model, weight variant, MSN i.e. Manufacturer Serial Number, etc…)

- Maintenance actions carried out (Airworthiness Directives, modifications, repairs, inspections, etc…),

- Life accumulation (accounting for any individual aircraft to which a part may have been fitted).

Note: Traceability and monitoring of parts listed in sub-parts 1-2 and 1-3 is not required when a systematic replacement applies.

3.6 The Life limit of Landing gear‘s parts is not expressed in FH or FC but also mentioned in LDG that be defined as an operation of an aircraft touching the runway and coming to a full Stop or performing a ‘touch and go’. When the items listed in the table reach the life limitations, disposal/quarantine action must be taken. Beside the LOV of aircraft as has been introduced in Section 1, the LOV related to Landing Gear Safe Life Airworthiness Limitation Items as follows:

Aircraft series LOV in Landings

A321-200 60000 LDG



4. Sub-Section 3.3 - A321 System Life Limited Components:

4.1 This sub-section of ASM related to ALS part 4 –Subpart 4.2 : SYSTEMS LIFE LIMITED COMPONENTS. Components listed under this sub-section are those having a life limitation, due to the difficulty to define a continued/enhanced inspection program, and whose failure could contribute to an unsafe condition of the airplane.

4.2. The initial entry into service is defined for the aircraft (systems installations) as:

- The date of Transfer of Title to the first Operator for limitations in Calendar times, unless otherwise stated in any delivery documentation to the first Operator.

- The date of aircraft first flight for limitations in flight hours and/or flight cycles and/or landings.

The initial entry into service for the transferable systems items is defined as the date at which the item accomplishes the first flight for which it will undertake its intended function.

Note: Unless otherwise stated, this means for transferable items delivered on new aircraft (i.e. from Airbus Final Assembly Line) that the life accumulated before the aircraft delivery date/transfer of title date (e.g. as a result of test flights) must be taken into account.

4.3 This tables provide the applicable limitations only for systems installations that have been authorized. These tables do not ensure that a part number has been validated for a specific individual aircraft MSN. Part numbers are authorized for installation on individual aircraft MSN by Service Bulletins (and the associated modifications) that is published by Airbus.

4.4 Limitation/Replacement time indication

- In computing items’ life, calculations must include flight hours and/or flight cycles and/or landings and/or Calendar time (as applicable) since the initial entry into service of the item (unless otherwise stated).

- Life limitations quoted in sub-section are applicable to the undamaged items as listed, not to the aircraft on which they are installed. The limitation/replacement time indication is quoted on the same line/block of lines as the Part Number.

4.5 Traceability and replacement/maintenance requirements.

In order to maintain aircraft airworthiness, it is mandatory to replace items listed under sub-section 3.3 at or prior to whichever of the life limitations occurs first, after any necessary adjustment of the stated life limitation in accordance with the instructions of the formula in ALS part 4-0, item 3, paragraph C.

In the context of the ALS Part 4, traceability means records that clearly demonstrate the history of items back to initial entry into service, so that limitations are accurately applied. Traceability records may comprise, but are not limited to, the following:

- Application history (aircraft type, model, MSN i.e. Manufacturer Serial Number, etc…),



- Maintenance actions carried out (Airworthiness Directives, modifications, repairs, inspections, etc…),

- Life accumulation (accounting for any individual aircraft to which an item may have been fitted).

4.6 Limitation applicability. Limitation applicability may be allocated according to the aircraft MSN affected Aircraft type, series and model, e.g.

X: stands for all aircraft of the column. -231 stands for all -231 models of the column.

5. Sub-Section 3.4 - A321 Time Controlled Items List: 5.1This list is superseded “A321 Hardtime/life limit Components List” of previous A321 AMS revision and requires the implementation of vendor recommendation. Those tasks, which deal with time controlled items are to be seen as a planning help. They are neither demanded by any source document nor by any certification authority.

5.2 As well as previously, The purpose of this sub-section is to offer a direct access by listing the off-aircraft tasks (from Sections 4 in AMS) affecting following components/parts, got permission to use in the fleet (as show in IPC document) which are to be controlled independently from the airframe:

- Items with time limitations (given by the manufacturer), which must be removed and replaced (except consumables, expendables).

- Items which are tracked individually (independent from airframe or installation areas).

- Items to be sent into shop for maintenance (off aircraft).

5.3 Task interval of the time controlled items related to “SOURCE REF.” column of this list:

- “VR” : for time controlled item with intervals defined by the vendor: The date of manufacture is the starting point unless otherwise stated by vendor or national authority.

- “MPD”: for time controlled item with intervals defined by the aircraft manufacture, the starting point for calculation of the intervals are the same definitions of the all aircraft maintenance task in “General Rules” paragraph of Section 1.

5.4 Tasks are shown as they are in their original sub-section which they are regulated by task code (ALI, CMR, ASM, FAL, SYS…), except task code related to ALI, CMR, FAL - that is the tasks which corresponds to the ALS from part 1 to part 4.The remaining tasks shall not be considered as including all the safety related tasks, neither only safety related tasks.


A321 ENGINE LIFE LIMITED PARTS

IN CASE OF INCONSISTENCY BETWEEN THIS TABLE AND THE V2533-A5 SERIES ENGINE MANUAL CHAPTER 5

THE ENGINE MANUAL CHAPTER 5 IS THE REFERENCE

ISSUE: SEP 2013

SECSION 3 - A321 ENG LLP PAGE: 1

TIME LIMITS V2533-A5 (AQ03)

Revdate: 01 Nov 2012

Itm Description P/N Limit (Cycle)

1 DICS,A/O STG.1 FAN 5A0337 20000

2 DICS,A/O STG.1 FAN 5A1757 20000

3 DICS,A/O STG.1 FAN 5A1948 20000

4 SHAFT,ASS'Y STUB 5A0895 20000

5 DISC,ASS'Y STG1.5-2.5 LPC 5R0159 20000

6 DISC,ASSY OF-STAGE 3-8 6A6473/6A7385/6B1380 16000

7 DISC,ASSY OF-STAGE 3-8 6A7401/6B1384 16000

8 DISC,ASSY OF-STAGE 3-8 6A8316/6B1386/6B1404 20000

9 DISC,ASSY OF-STAGE 3-8 6A7705/6B1385 20000

10 DISC ASSY STAGE 9 TO 12 HP 6A4156 8000




14 SHAFT,ASSY REAR HP COMPRESS 6A5867 20000

15 SHAFT,ASSY REAR HP COMPRESS 6A7711/6B1419 20000

16 SEAL, ROTATING-REAR 6A5869 20000

17 SEAL,AIR,HPT,2STG 2A3179 15000




21 HUB,TURB,1STG 2A2801 15000

22 HUB,TURB,1STG 2A5001 20000

23 SEAL,AIR,HPT,1STG, OUTER 2A1350 15000


25 SEAL,AIR,HPT,1STG, INNER 2A3086 15000



28 HUB,TURB,2STG 2A3002 15000

29 HUB,TURB,2STG 2A4802 20000

30 PLATE,RTNG,BLADE,HPT,2STG 2A2097 15000



33 SEAL AIR,TURBINE,INNER,STG6 3A3063 20000







ISSUE: SEP 2013


TIME LIMITS V2533-A5 (AQ03)



36 DISK,TURBINE STG7 3A2512 20000






42 DISK,TURBINE,STG4 3A1984 20000




46 SEAL,AIR,TURBINE,STG7 3A1741 20000



49 SEAL,AIR TURBINE STG5 3A2423 20000



52 SHAFT,LP TURBINE 5A1732 20000






ISSUE: SEP 2013


TIME LIMITS V2533-A5 (SQ03)

Revdate: Aug /12

Itm Description P/N Limit

1 DICS,A/O STG.1 FAN 5A0337 20000

2 DICS,A/O STG.1 FAN 5A1757 20000











13 HUB,TURB,1STG 2A2801 15000

14 HUB,TURB,1STG 2A5001 20000






20 HUB,TURB,2STG 2A3002 15000

21 HUB,TURB,2STG 2A4802 20000




















ISSUE: SEP 2013



Revdate: Aug /12













ISSUE: SEP 2013





1 DICS,A/O STG.1 FAN 5A0337 20000

2 DICS,A/O STG.1 FAN 5A1757 20000

3 DICS,A/O STG.1 FAN 5A1948 20000



6 DISC,ASSY OF-STAGE 3-8

6A7401 / 6B1384 / 6B1391 16000

7 DISC,ASSY OF-STAGE 3-8 6A8316 / 6B1386 / 6B1404 / 6B1393 /

6B1405

20000







14 HUB,TURB,1STG 2A2801 15000

15 HUB,TURB,1STG 2A5001 20000




19 HUB,TURB,2STG 2A3002 15000

20 HUB,TURB,2STG 2A4802 20000



















ISSUE: SEP 2013


















ISSUE: SEP 2013



Revdate: May 01/11


1 DICS,A/O STG.1 FAN 5A0337 20000

2 DICS,A/O STG.1 FAN 5A1757 20000











13 HUB,TURB,1STG 2A2801 15000

14 HUB,TURB,1STG 2A5001 20000






20 HUB,TURB,2STG 2A3002 15000

21 HUB,TURB,2STG 2A4802 20000




















ISSUE: SEP 2013



Revdate: May 01/11










ISSUE: JAN 2014 SECTION 3 – APU LIFE LIMIT PARTS

A321 AUXILIARY POWER UNIT - LIFE LIMIT PARTS (APU PN: 3800708-1, PN: 4500001B)

IN CASE OF INCONSISTENCY BETWEEN THIS TABLE AND THE APU MANUAL, APU MANUAL IS THE REFERENCE

Description Part Number Serial Number Limit (Cycle)

1st Stage Rotor Assy. 3840161-1 08-03357-05775 30000

3840160-8 08-03357-05775 30000

Second Stage Turbine Rotor 3610894-11 10-156101-06712 10000

3840165-4 10-156101-06712 10000

Engine Compressor Impeller 3822391-6 10-162053-31041 30000

Turbine Shaft 3822504-3 10P29061 30000


3840160-8 08-03357-05784 30000


3840165-4 10-156101-07089 10000


Turbine Shaft 3822504-3 10P30197 30000


3840160-8 10-168522-01923 30000


3840165-4 10-156101-07069 10000


Turbine Shaft 3822504-3 10P29960 30000


3840160-8 10-168522-03278 30000


3840165-4 10-156101-10982 10000


Turbine Shaft 3822504-3 11P31548 30000


3840160-8 10-168522-00584 30000


3840165-4 11-156101-01496 30000


Turbine Shaft 3822504-3 11P31816 30000


3840160-8 10-168522-02877 30000


3840165-4 10-156101-11979 10000


Turbine Shaft 3822504-3 11P30676 30000


3840160-8 10-168522-02877 30000


3840165-4 10-156101-11979 10000


Turbine Shaft 3822504-3 11P30676 30000


3840160-8 10-168522-03808 30000


3840165-4 10-156101-12059 10000


Turbine Shaft 3822504-3 11P33468 30000


3840160-8 10-168522-02921 30000


3840165-4 11-156101-01115 30000


Turbine Shaft 3822504-3 11P34011 30000







3840160-8 10-168522-04327 30000


3840165-4 11-156101-01751 30000


Turbine Shaft 3822504-3 11P36169 30000


3840160-8 10-168522-03543 30000


3840165-4 11-156101-02940 30000


Turbine Shaft 3822504-3 11P36676 30000


3840160-8 10-168522-04360 30000


3840165-4 11-156101-02035 30000


Turbine Shaft 3822504-3 11P37714 30000


3840160-8 10-168522-04691 30000


3840165-4 11-156101-06342 30000


Turbine Shaft 3822504-3 11P39036 30000


3840160-8 10-168522-04274 30000


3840165-4 11-156101-06089 30000


Turbine Shaft 3822504-3 11P39034 30000


3840160-8 10-168522-04813 30000


3840165-4 11-156101-06294 30000


Turbine Shaft 3822504-3 11P39035 30000


3840160-8 10-168522-04279 30000


3840165-4 11-156101-06190 30000


Turbine Shaft 3822504-3 11P39039 30000


3840160-8 11-168522-01942 30000


3840165-4 11-156101-06038 30000


Turbine Shaft 3822504-3 11P39412 30000


3840160-8 10-168522-04679 30000


3840165-4 11-156101-04877 30000


Turbine Shaft 3822504-3 11P39409 30000


3840160-8 11-168522-01946 30000







3840165-4 11-156101-11816 30000


Turbine Shaft 3822504-3 11P39534 30000


3840310-3 10-156101-13821 30000


3840165-4 11-156101-04928 30000


Turbine Shaft 3822504-3 11P40940 30000


3840310-3 11-156101-06429 30000


3840165-4 11-156101-08811 30000


Turbine Shaft 3822504-3 11P42304 30000


3840310-3 11-156101-01572 30000


3840165-4 11-156101-10080 30000


Turbine Shaft 3822504-3 11P43338 30000


3840310-3 10-156101-12539 30000


3840165-4 11-156101-06095 30000


Turbine Shaft 3822504-3 12P46906 30000


3840310-3 11-156101-07316 30000


3840165-4 11-156101-11338 30000


Turbine Shaft 3822504-3 12P47816 30000


3840310-3 11-156101-05344 30000


3840165-4 11-156101-10105 30000


Turbine Shaft 3822504-3 12P48167 30000


3840310-3 11-156101-08099 30000


3840165-4 11-156101-10796 30000


Turbine Shaft 3822504-3 12P48200 30000


3840310-3 11-156101-08037 30000


3840165-4 11-156101-11564 30000


Turbine Shaft 3822504-3 12P48163 30000


3840310-3 11-156101-02420 30000







3840165-4 11-156101-11358 30000


Turbine Shaft 3822504-3 12P48165 30000


3840310-3 10-156101-12360 30000


3840165-4 11-156101-13832 30000


Turbine Shaft 3822504-3 12P48544 30000


3840310-3 11-156101-06963 30000


3840165-4 11-156101-09677 30000


Turbine Shaft 3822504-3 12P48844 30000


3840310-3 12-156101-00310 30000


3840165-4 11-156101-11327 30000


Turbine Shaft 3822504-3 12P48850 30000


3840310-3 11-156101-06693 30000


3840165-4 12-156101-01380 30000


Turbine Shaft 3822504-3 12P49117 30000


3840310-3 12-156101-00694 30000


3840165-4 10-156101-04260 30000


Turbine Shaft 3822504-3 12P49754 30000


3840310-3 12-156101-00193 30000


3840165-4 12-156101-01265 30000


Turbine Shaft 3822504-3 12P49757 30000


3840310-3 11-156101-06966 30000


3840165-4 12-156101-01175 30000


Turbine Shaft 3822504-3 12P50430 30000


3840310-3 11-156101-13581 30000


3840165-4 12-156101-00338 30000


Turbine Shaft 3822504-3 12P50443 30000


3840310-3 11-156101-08023 30000


3840165-4 12-156101-02248 30000







Turbine Shaft 3822504-3 12P51053 30000


3840310-3 11-156101-07549 30000


3840165-4 12-156101-12230 30000


Turbine Shaft 3822504-3 12P51715 30000


3840310-3 11-156101-13473 30000


3840165-4 12-156101-03835 30000


Turbine Shaft 3822504-3 12P52094 30000


3840310-3 11-156101-08702 30000


3840165-4 12-156101-01187 30000


Turbine Shaft 3822504-3 12P52488 30000


3840310-3 11-156101-08701 30000


3840165-4 12-156101-04868 30000


Turbine Shaft 3822504-3 12P52780 30000


3840310-3 11-156101-08733 30000


3840165-4 12-156101-05914 30000


Turbine Shaft 3822504-3 12P52776 30000


3840310-3 11-156101-04273 30000


3840165-4 12-156101-05055 30000


Turbine Shaft 3822504-3 12P52972 30000


3840310-3 11-156101-08735 30000


3840165-4 12-156101-05497 30000


Turbine Shaft 3822504-3 12P53471 30000


3840310-3 12-156101-05775 30000


3840165-4 12-156101-01906 30000


Turbine Shaft 3822504-3 12P53625 30000


3840310-3 11-156101-07325 30000


3840165-4 12-156101-08122 30000







Turbine Shaft 3822504-3 12P54015 30000


3840310-3 12-156101-06086 30000


3840165-4 12-156101-07331 30000


Turbine Shaft 3822504-3 13P54911 30000


3840310-3 12-156101-09174 30000


3840165-4 12-156101-07603 30000


Turbine Shaft 3822504-3 13P55600 30000


3840310-3 11-156101-03793 30000


3840165-4 12-156101-09517 30000


Turbine Shaft 3822504-3 13P55537 30000


3840310-3 12-156101-11164 30000


3840165-4 12-156101-09190 30000


Turbine Shaft 3822504-3 13P55878 30000


A321 LANDING GEAR LIFE LIMITED PARTS

( IAW ALS Part 1 Rev: 02 Issue: MAY 13/11 & ALS Part 4 Rev: 01 Issue: JUN 15/12)

ISSUE: SEP 2013

SECSION 3 - A321 LDG LLP PAGE: 1

A321 LDG LLP SUB-PART 1-2

(IN CASE OF INCONSISTENCY BETWEEN THIS TABLE AND THE ALS PART 1, THE ALS PART 1 IS THE REFERENCE.)

Explanation notes are located under the assembly title. LIFE

LIMITS LIFE LIMITS

APPLICABILITY

IT Nomenclature Part Number LDG A321-200

ATA 32-11-00 MAIN LANDING GEAR (FIG. 01 to 05) X

BASIC SIDE STAY (FIG. 01 & 03) X

(6) This limit applies to parts fitted to A321-200 WV001, WV002, WV003, WV010 and WV011. (8) This limit applies to parts fitted to A321-200 NOT identified in note (6) above.

1 Lower side stay 201525301 51400 X (6)

2 Lower side stay 201525301 60000 X (8)

3 Upper side stay 201525300 51400 X (6)

4 Upper side stay 201525300 60000 X (8)


(IN CASE OF INCONSISTENCY BETWEEN THIS TABLE AND THE ALS PART 1, THE ALS PART 1 IS THE REFERENCE.)

Explanation notes are located under the assembly title. DEMONSTRATE

D FATIGUE

LIVES

DEMONSTRATED

FATIGUE LIVES

APPLICABILITY

IT Nomenclature Part Number LDG A321-200

ATA 32-11-00 MAIN LANDING GEAR (FIG. 01 to 05 & 08) X

(1) ‘xx’ at the end of the PNR stands for any number between 00 and 99, including unused digits.

1 Rear pintle pin (1) D32156005000xx 60000 X




5 Rear pintle pin nut SLN40851 60000 X

6 Rear pintle pin nut SLN41194 60000 X

MAIN STRUT AND DRESSINGS (FIG. 01, 03 & 04) X

(1) This PNR is submitted to an inspection. Refer to CN 2000-428-153(B) latest approved revision. (2) Bolt PNR NAS6610D43 must be replaced by a new one every time it is removed from the main fitting.

7 Aft pintle spherical bearing 201042415 60000 X







ISSUE: SEP 2013











20 Forward pintle pin 201522600 60000 X

21 Forward pintle pin lock bolt 201383628 (1) 60000 X

22 Forward pintle pin stub bolt 201587602 60000 X




26 Cardan bracket (LH) 201383304 60000 X

27 Cardan bracket (RH) 201383305 60000 X

28 Cardan bracket bolt NAS6610D43 (2) X

29 Main fitting (LH) 201522300 60000 X

30 Main fitting (LH) 201522351 60000 X

31 Main fitting (RH) 201522301 60000 X

32 Main fitting (RH) 201522352 60000 X

33 Upper torque link pin 201383604 60000 X

34 Upper torque link 201522302 60000 X

35 Upper torque link 201587303 60000 X

36 Torque link apex pin 201383606 60000 X

37 Torque link apex pin nut 201383615 60000 X

38 Torque link apex pin nut 201587612 60000 X

39 Lower torque link 201522303 60000 X

40 Lower torque link 201587304 60000 X

41 Lower torque link pin 201383605 60000 X

42 SHOCK ABSORBER SUBASSEMBLY (FIG. 01 & 02) X

(2) Upper bearing locking screw PNR NAS1802-3-8 must be replaced by a new one every time it is removed from the upper bearing. PNR applicable to Aircraft landing gear POST MOD 24218.

43 Sliding tube 201522350 60000 X

44 Sliding tube 201522353 60000 X

45 Upper diaphragm tube 201522651 60000 X

46 Upper bearing locking screw NAS1802-3-8 (2) X

COMPLETE SIDE STAY (FIG. 01 & 03) X

BASIC SIDE STAY (FIG. 01 & 03) X

47 Lower cardan nut 201525612 60000 X




ISSUE: SEP 2013


48 Lower cardan nut 201661611 60000 X

49 Lower cardan 201525302 60000 X

50 Side stay lower cardan pin 201525620 60000 X



53 Lower side stay 201661301 60000 X

54 Side stay pivot pin 201525605 60000 X

55 Side stay pivot pin 201661601 60000 X

56 Upper side stay 201661300 60000 X

57 Side stay upper cardan pin 201525618 60000 X

58 Upper cardan 201525607 60000 X

59 Upper cardan nut 201525619 60000 X

60 Upper cardan nut 201661610 60000 X

61 Upper pin (Springs) 201057611 60000 X

62 Upper pin (Springs) 201661607 60000 X

63 Lower pin (Springs) 201057625 60000 X

64 Lower pin (Springs) 201661606 60000 X

65 Triangulation link pin 201057624 60000 X

66 Triangulation link pin 201661609 60000 X

67 Triangulation link 201057306 60000 X

68 Triangulation link 201661307 60000 X

69 Banana link 201057304 60000 X

70 Banana link 201661304 60000 X

71 Banana link 201661306 60000 X

72 Cuff pin 201057623 60000 X

73 Cuff pin 201661612 60000 X

74 Cuff 201057634 60000 X

75 Cuff 201163309 60000 X

76 Cuff 201661302 60000 X

77 Cuff 201661305 60000 X

78 Cuff 201661602 60000 X

79 Cuff 201661613 60000 X

80 Pin (Lock link/Banana link) 201057644 60000 X

81 Pin (Lock link/Banana link) 201661605 60000 X

82 Lock link lower pin 201057627 60000 X

LOCK LINK (FIG. 03) X

83 Lower lock link 201403300 60000 X

84 Lock link center pin 201058608 60000 X

85 Upper lock link 201531300 60000 X

86 Upper lock link 201531600 60000 X

87 Lock link upper pin 201058611 60000 X




ISSUE: SEP 2013


88 Lock stay cardan 201058304 60000 X

89 Lock stay cardan 201058306 60000 X

90 Lock stay cardan pin 201056909 60000 X

ATA 32-21-00 NOSE LANDING GEAR (FIG. 06) X

NOSE LANDING GEAR LEG (FIG. 06) X

LEG STRUCTURE (FIG. 06) X

91 Hinge pin (Barrel/Structure) D65588 60000 X

92 Hinge pin (Barrel/Structure) D65588-1 60000 X

93 Barrel D65233 60000 X

94 Barrel D67583 60000 X

95 Pin (Retraction actuator/ Lock link/Barrel) D65589 60000 X

96 Pin (Retraction actuator/ Lock link/Barrel) D65589-1 60000 X

97 Pin (Forestay/Barrel) D65599 60000 X

98 Pin (Forestay/Barrel) D65599-1 60000 X

SHOCK ABSORBER (FIG. 06) X

(3) One-piece sliding tube (integrating the wheel axle). (4) Sliding tube with a separate wheel axle.

99 Cylinder D65519 60000 X

100 Sliding tube D65236 (3) 60000 X

101 Sliding tube D66679 (4) 60000 X

102 Wheel axle D66680 60000 X

FORESTAY ASSEMBLY (FIG. 06) X

FORESTAY (FIG. 06) X

103 Forestay lower link D65238 60000 X

104 Forestay lower link D67802 60000 X

105 Pin (Lower link/U-joint) D65773 60000 X

106 Lock link lower pin D65631 60000 X

107 Lock link lower pin D65631-1 60000 X

108 Lock link lower pin D67928 60000 X

109 Cross pin D65628 60000 X

110 Cross pin D65628-1 60000 X

111 Cross pin D67932 60000 X

112 Universal joint D59638 60000 X

113 Pin (Upper panel/U-joint) D65887 60000 X

114 Forestay upper panel D59416 60000 X

115 Forestay upper panel D65237 60000 X

116 Pin (Upper panel/Structure) D65616 60000 X

LOCK LINK (FIG. 06) X

117 Lock link lower link D59635 60000 X

118 Lock link center pin D60054 60000 X

119 Lock link upper link D59636-1 60000 X




ISSUE: SEP 2013


ATA 57-00-00 WING STRUCTURE (FIG. 07 & 08) X

(1) This item is not transferable from an aircraft to another: Traceability at aircraft level is authorized. (2) ‘xx’ at the end of the PNR stands for any number between 00 and 99, including unused digits.

120 Gear support rib (LH) (1) (2) D57255510000xx 48000 X





125 Gear support rib (RH) (1) (2) D57255510001xx 48000 X





130 Forward pintle fitting (LH) (1) (2) D57259192002xx 48000 X

131 Forward pintle fitting (RH) (1) (2) D57259192003xx 48000 X

132 Sidestay fitting (LH) (1) (2) D57259172000xx 48000 X




136 Sidestay fitting (RH) (1) (2) D57259172001xx 48000 X




140 Retraction Jack fitting (LH) (1) (2) D57259162000xx 48000 X

141 Retraction Jack fitting (RH) (1) (2) D57259162001xx 48000 X


(IN CASE OF INCONSISTENCY BETWEEN THIS TABLE AND THE ALS PART 4, THE ALS PART 4 IS THE REFERENCE)

ATA 32-10-00 MAIN LANDING GEAR

RETRACTION ACTUATOR (FIG 04) PART NUMBER

LIFE LIMITATIONS

(LDG)

LIFE LIMITS

APPLICABILITY

A321-200

Retraction actuator pin (main fitting side) 114193637 60000 X


Retraction actuator piston rod 114193601 60000 X

Retraction actuator piston rod 201590908 60000 X

Retaining ring (retraction actuator piston rod)

114193606 (1) X

Retraction actuator piston head 114193603 60000 X

Retraction actuator piston head 201590909 60000 X

Retraction actuator piston head nut 114193604 60000 X

Retraction actuator piston head nut 201590910 60000 X

Retraction actuator gland 114193602 60000 X






ISSUE: SEP 2013



Retaining ring (retraction actuator gland) 114193643 (2) X

Retraction actuator cylinder 114193600 60000 X








Retraction actuator pin (rear spar side) 114193610 60000 X

Retraction actuator pin (rear spar side) 201590901 60000 X


(1) Retaining ring P/N 114094611 and P/N 114193606 must be replaced by a new one every time it is removed from the piston head.

(2) Retaining ring P/N 114193643 must be replaced by a new one every time it is removed from the gland.


A321 TIME CONTROLLED ITEMS LIST

(*) For new parts: Current task interval is applied.

For used parts: Current task interval or CRS (certificate release to service) part interval is applied, whichever comes first. ISSUE: SEP 2013 SECSION 3 - A321 TIME CONTROLLED ITEMS LIST PAGE 1 OF 10

ITEM MPD/AMS

REF. DESIGNATION PART No CMM

SOURCE REF.

SERVICE DESCRIPTION INTERVAL(*)

1 215141-01-1 OZONE FILTER (OZONE

CONVERTER)

20499003 20499004 20499005 20499006 44018003 44018004

21-11-04 21-11-15

MPD FUNCTIONAL CHECK 9000 FH OR 60 MO

2 215200-01-1 PRIMARY HEAT EXCHANGER

753A0000-03 753A0000-04 753B0000-02 753C0000-01 753C0000-02

21-52-11 MPD CLEANING 12000 FH OR 80 MO

3 215200-01-1 MAIN HEAT EXCHANGER 754A0000-03 754B0000-02 754C0000-01

21-52-11 MPD CLEANING 12000 FH OR 80 MO

4 212141-01-1 CARTRIDGE FILTER (RECIRCULATION FILTER)

424B200-3 424B200-4 424B200-6 424B200-7 QA06423 QA06423-01

21-21-02 21-21-23

MPD DISCARD & REPLACE 5000 FH OR 36 MO

5 213100-08-1 VALVE-SAFETY 9024-15704-2 9024-15704-03

21-31-40 MPD RESTORATION 50000 FH OR 210 MO

6 215200-02-2 REHEATER 755A0000-04 755B0000-02 755C0000-01

21-52-08 MPD

CLEANING

12000 FH OR 80 MO

7 215200-04-1 CONDENSER 756A0000-05 756A0000-06

21-52-10 MPD RESTORATION (LEAK TEST) 18000 FH OR 120 MO





ITEM MPD/AMS


SOURCE REF.


8

237135-01-1 237135-02-1 313300-01-1 313300-03-1

UNDERWATER ACOUSTIC BEACON (ULD/ULB)

ELP362D DK100 DK120 266E0305-00 266E0305-01 266E0305-02

23-70-44 31-31-36 23-70-04

VR (CMM)

BEACON CLEANING AND/OR TESTING: ULB BATTERY (AND ORING) REPLACEMENT:

2 YEAR 6 YEAR

9 243851-01-1 BATTERY 2758 24-38-51 VR (MPD) GENERAL OVERHAUL IAW CMM

01 YE

10 243851-02-1 BATTERY 2758 24-38-51 VR (MPD)

* CLEANING, CHARGE BATTERY, ADJUST ELECTROLYTE LEVEL ** CLEANING, CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL

* 1000 FH ** 2000 FH OR 06 MO

11 212652-01-1 SKIN AIR INLET VALVE VFT210B00 VFT210A2

REMOVE SKIN AIR INLET VALVE FOR OVERHAUL

18000 FH OR 120 MO

12 212653-02-1 SKIN AIR OUTLET VALVE VFT300B00 REMOVE SKIN AIR OUTLET VALVE FOR OVERHAUL

18000 FH OR 120 MO

13 256241-02-1 EVACUATION SLIDE/RAFT D18309-XXX

25-65-17 VR (CMM)

DOT -SP 8162 DOT-SP 10945

* HYDROSTATIC TEST OF GAS CYLINDER ** DISCARD RESERVOIR

* 5 YEAR ** 15 YEAR

14 256241-03-1 EVACUATION SLIDE/RAFT D30664-XXX D30665-XXX

25-61-20 25-65-17

VR (CMM) DOT-SP 8162

DOT-SP 10945

* EVERY 3 YEARS: FOR EVACUATION SYSTEMS UP TO AND INCLUDING 15 YEARS OF AGE OR IF INFLATABLE, RESERVOIR, HOSE AND APPLICABLE LIFE-LIMITED ITEMS ARE REPLACED AT 15 YEARS FOR THE NEXT 15 YEARS:

* 03 YEAR ** 01 YEAR *** 15 YEAR:





ITEM MPD/AMS


SOURCE REF.


CHECK/TEST INCL. HYDROSTATIC TEST ** EVERY YEAR: FOR EVACUATION SYSTEMS AFTER 15 YEARS OF IN-SERVICE LIFE: CHECK/TEST INCL. HYDROSTATIC TEST * EVERY 3 YEARS UP AND INCLUDING 15 YEARS : PERFORM A SYSTEM CHECK OF INFLATION SYSTEM *** 15 YEARS: DISCARD RESERVOIR

15 VN256600-01 SURVIVAL KIT

60128-103 60128-101 60128-303

25-61-20 VR (CMM) VISUAL CHECK IAW CMM

THE FIRST OVERHAUL CONFORM TO THE EXPIRE DATE ON PLACARD’S KIT

03 YEARS.: BEFORE 15 YEARS OF AGE, AFTER THE FIRST OVERHAUL

01 YEAR.: AFTER 15 YEARS OF AGE

16 256247-01-1 A321 DOOR 2 /3 EVACUATION SLIDE SYSTEMS

62292-XXX 62293-XXX

25-66-10 25-66-11

VR (CMM)

* EVERY 3 YEARS FOR EVACUATION SYSTEMS UP TO AND INCLUDING 15 YEARS OF AGE OR IF INFLATABLE, RESERVOIR, HOSE AND APPLICABLE LIFE-LIMITED ITEMS ARE REPLACED AT 15 YEARS FOR THE NEXT 15 YEARS: CHECK/TEST INCL. HYDROSTATIC TEST ** EVERY YEAR FOR EVACUATION SYSTEMS AFTER 15 YEARS OF IN-SERVICE LIFE:

* 03 YEAR ** 01 YEAR





ITEM MPD/AMS


SOURCE REF.


CHECK/TEST INCL. HYDROSTATIC TEST * EVERY 3 YEARS UP AND INCLUDING 15 YEARS: PERFORM A SYSTEM CHECK OF INFLATION SYSTEM IAW CMM AT EVERY SCHEDULED MAINTENANCE CHECK: PERFORM A HOSE INTEGRITY TEST

17 256249-01-1 A321 EVACUATION SYSTEMS RESERVOIR AND VALVE ASSEMBLY

61639-XXX 25-65-21

VR (CMM) DOT-SP 8162 DOT-SP 10945 DOT-SP 11194

* EVERY 3 YEARS PERFORM INFLATION SYSTEM * * EVERY 5 YEARS UP AND INCLUDING 15 YEARS: PERFORM HYDROSTATIC TEST AND INSPECTION IAW CMM. *** DISCARD RESERVOIR

* 3 YEAR **5 YEAR *** 15 YEAR

18 256600-01-1 25 PERSON LIFE RAFT 65025-XXX 25-62-23 VR (CMM)

* 3 YEARS: PERFORM A SYSTEM CHECK OF INFLATION SYSTEM AND EVERY 6 YEARS UP AND INCLUDING 12 YEARS AND ** AFTER 15 YEARS AND THEN EACH YEAR THEREAFTER: PERFORM A FUNCTIONAL TEST, AN INFLATABLE INTEGRITY VERIFICATION TEST INCLUDING OVERPRESSURE TEST AND LEAK TEST, HOSE INTEGRITY CHECK, LIGHT SYSTEM TEST (IF






ITEM MPD/AMS


SOURCE REF.


APPLICABLE). DISSEMBLE SYSTEM TO EXTEND NECESSARY TO COMPLY WITH CHECK SECTION.

19 256532-01-1 PORTABLE EMERGENCY LOCATOR TRANSMITTER (ELT)

1151324-1 25-60-10 VR (CMM) EVERY 5 YEARS: PERFORM BATTERY TEST / INSPECTION IAW CMM

05 YEAR

S1823502-03 S1823502-02

25-63-05 VR (CMM) EVERY 6 YEARS: REPLACE BATTERY

06 YEAR

20 256535-02-1 ELT IN REAR FUSELAGE

95N6088 25-60-04 VR (CMM) REPLACE BATTERY 03 YEAR

DISCARD O-RING 08 YEAR

S1821502-02 25-63-05 VR (CMM) REPLACE BATTERY 06 YEAR

21 256551-01-1 ELECTRONIC MEGAPHONE A12SA 25-65-04 VR CMM) REPLACE BATTERIES 01 YEAR

22 256652-01-1 LIFE VESTS

0P0723-111WC P0723-103WC P0723E105P P0723E105PW P0640-103

25-60-07 25-60-07 25-60-12 25-60-12 25-60-15

VR (CMM)

EVERY 60 MONTHS: AFTER ENTRY INTO SERVICE, BUT NOT LATER THAN 63 MONTH AFTER DATE OF MANUFACTURE PERFORM MAINTENANCE INSPECTION IAW CMM

05 YEAR





ITEM MPD/AMS


SOURCE REF.


23 262141-02-1 262141-02-1A

ENGINE FIRE EXTINGUISHER BOTTLES

34100005-1 472088-1

26-20-05 26-20-79

VR (CMM) SIL 26-0237D

SIL96-2

HYDROSTATIC TEST: WEIGHT CHECK:

10 YEAR 05 YEAR

86181007 26-21-41 NR/VR (CMM)

* EVERY 2 YEARS: PERFORM A TEST INCLUDING WEIGHT CHECK ** EVERY 5 YEARS: PERFORM AN OVERHAUL INCLUDING HYDROSTATIC TEST OF EXTINGUISHER BOTTLE DOT 4A-700


24 262142-01-1 ENGINE FIRE EXTIR BOTTLE CARTRIDGES

30903886 446158

26-20-05 26-21-34

VR (CMM) DISCARD CARTRIDGE 10 YEAR

86182008 26-21-41 VR (CMM)

DISCARD CARTRIDGE LIFE LIMITS OF CARTRIDGE: 7 YEARS MAXIMUM LIFE 5 YEARS OPERATING LIFE

05 YEAR

25 262241-01-1 262241-01-1A

APU FIRE EXTINGUISHER BOTTLE

33600005-3 26-20-03 NR/VR (CMM) SIL 26-0237D

HYDROSTATIC TEST: WEIGHT CHECK:

10 YEAR 05 YEAR

26 262242-01-1 APU FIRE EXTINGUISHER BOTTLE CARTRIDGES

30903827 26-20-05 VR (CMM) DISCARD CARTRIDGE 10 YEAR

27 262541-02-1 LAVATORY FIRE EXTINGUISHER BOTTLE

BA24320A1 BA21758

26-25-36 26-25-12

MPD WEIGHT CHECK 72 MO





ITEM MPD/AMS


SOURCE REF.


28 262441-02-1 PORTABLE FIRE EXTINGUISHER

74-20 0074-20

26-24-05 VR (CMM)

* PERIODICAL CHECK EVERY 2 YEARS (VISUAL INSPECTION/WEIGHT CONTROL/SCALE…REF: CMM 26-24-05) ** AFTER EXPIRATION OF 5 YEARS, INCASE OF FILLING/REFILLING, THE CONTAINER OF FIRE EXT HAS TO BE INSPECTED INSIDE. SHOULD DEFECTS BE DETECTED, THE FIRE EXT HAS TO BE HYDROSTATICALLY PRESSURE TEST *** HYDROSTATIC TEST **** DISCARD EXTINGUISHER

* 2 YEAR ** 5 YEAR *** 10 YEAR **** 20 YEAR

29

262341-02-2

CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE

34600049-1

26-23-42 VR (CMM)

SIL 26-0237D HYDROSTATIC TEST & CHECK OF PRESSURE SWITCH SETTING

10 YE

262341-01-2 26-23-42 MPD WEIGHT CHECK 22500 FH OR 72 MO

30 262300-04-3 CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CARTRIDGES

30903898 26-23-42 VR (CMM) DISCARD CARTRIDGE 10 YEAR

31 261600-05-1 CARGO COMPARTMENT SMOKE DETECTOR

PPA1102-00 PPA1101-00 PPC1100-00 PPA1103-00

26-16-16 26-16-16 26-18-18

MPD CLEANING IN THE WORKSHOP 18000 FH OR 120 MO

32 261700-04-1 LAVATORY SMOKE DETECTOR

PPA1202-00 PPC1200-00

26-16-16 26-18-18

MPD CLEANING IN THE WORKSHOP 12000 FH OR 80 MONTH





ITEM MPD/AMS


SOURCE REF.


33 275117-01-1 FLAP/SLAT COMMAND SENSOR UNIT

780A0000-01 780A0000-02 780B0000-01

27-09-02 MPD CHECK OF FRICTION BRAKE IN WORKSHOP

40 MONTH

34 292000-11-1 RAT AND ACTUATOR

759998 761618 762308 762308A 762308B 766352 766352A 766352B

764711A 764711B 764711C

29-21-03 29-21-42 29-21-44

ALS PART 4 (ASM)

OVERHAUL AND REPLACE WITH NEW OR REPAIRED UNITS

20 YEAR

35 321111-01-2 MAIN LANDING GEAR ALL 32-12-13 32-12-21 32-12-22

MPD OVERHAUL 120 MO OR 20000 FC

36 322111-01-1 NOSE LANDING GEAR ALL

32-27-19 32-27-22 32-27-24 32-27-40

MPD OVERHAUL 120 MO OR 20000 FC

37 351141-01-1 CREW OXYGEN CYLINDER 89794077 35-21-93 VR (CMM) SIL-35-103

DOT-SP 8162

HYDROSTATIC TEST 05 YEAR

DISCARD CYLINDER 15 YEAR

38 351241-02-1 CREW OXYGEN MASK MF10-05-11 MF20-534

35-13-61 35-13-60

MPD FUNCTIONAL CHECK IN WORKSHOP 06 YEAR





ITEM MPD/AMS


SOURCE REF.


39 352142-01-1 OXYGEN GENERATORS 117042-02 117042-03 117042-04

35-21-73 MPD DISCARD OXYGEN GENERATORS 180 MO

40 353000-02-1 PORTABLE OXYGEN CYLINDER ASSEMBLIES

9700C1AF23AN 9800-2D1AF23AM

35-31-55 VR (CMM) EVERY 5 YEARS: PERFORM AN OVERHAUL INCLUDING HYDROSTATIC TEST

05 YEAR

3552AAADAACXCD 35-35-52 VR (CMM) HYDROSTATIC TEST: DISCARD:

05 YEAR 15 YEAR

41 353000-06-1 PBE-PROTECTIVE BREATHING EQUIPMENT (SMOCKE HOODS)

E28180 E28180-10 E28180-20-001

35-10-25 VR (CMM) DISCARD: 10 YEÁR

42 470000-02-1 AIR SEPARATION MODULE (ASM)

2060017-101 2060017-102

47-10-43 MPD FAL

REPLACEMENT 27000 FH

43 383155-01-1 VACUUM TOILET RINSE VALVE

15800-348 REV.A 15800-348 REV.B 15800-348 REV.C

MPD REMOVE, CLEAN AND INSPECT TOILET RINSE VALVES FROM ALL TOILETS

48 MONTH

44 215800-01-1 AIR COOLING AND TEMPERATURE CONTROL

MPD REMOVE CSAS OZONE CONVERTER FOR RESTORATION

6000 FH OR 48 MONTH

45 215800-02-1 AIR COOLING AND TEMPERATURE CONTROL

MPD REMOVE CSAS HEAT EXCANGER FOR CLEANING

12000 FH OR 80 MONTH

46 212653-01-1 SKIN AIR OUTLET VALVE VFT300A1 REMOVE SKIN AIR OUTLET VALVE FOR OVERHAUL

12000 FH OR 80 MO





ITEM MPD/AMS


SOURCE REF.


34 262441-02-1-A PORTABLE FIRE EXTINGUISHER

74-20 0074-20

26-24-05 VR (CMM)

PERIODICAL CHECK EVERY 2 YEARS (VISUAL INSPECTION/WEIGHT CONTROL/SCALE…REF: CMM 26-24-05)

2 YEAR

A320 AIRCRAFT MAINTENANCE schedule

SECTION 4

SCHEDULED AIRCRAFT MAINTENANCE

LIST OF EFFECTIVE PAGES SECTION MVT PAGE ISSUE

4-LEP R 1 AUG 2012 4-TOC R 1 AUG 2012 4-GENERAL R 1 JUL 2013 4- ALI SUB-SECTION R JUL 2013 4- CMR SUB-SECTION R JUL 2013 4- SYS SUB-SECTION R JUL 2013 4- FAL SUB- SECTION R JUL 2013 4- ASM SUB-SECTION R JUL 2013 4- STR SUB-SECTION R JUL 2013 4- ZNL SUB-SECTION R JUL 2013 4- ECO SUB-SECTION R JUL 2013

ISSUE: SEP 2013 SECTION 4 - LEP PAGE 1

s


SECTION 4

MAINTENANCE SCHEDULE

TABLE OF CONTENTS

SUBJECT SECTION

GENERAL INTRODUCTION 4

AIRWORTHINESS LIMITATION ITEM 4

CERTIFICATION MAINTENANCE REQUIREMENTS 4

SYSTEM 4

FUEL AIRWORTHINESS LIMITATIONS

4

AGEING SYTEMS MAINTENANCE 4

STRUCTURE 4

ZONAL 4

ECO 4

ISSUE: SEP 2013 SECTION: 4-TOC

PAGE: 1


ISSUE SEP 2013 SECTION 4 PAGE: 1

SECTION 4


1. GENERAL

This section includes all the scheduled tasks related to

General Visual Inspection (GVI) require-ments for each aircraft zone to check system and Power plant installations and structure for security and general condition (Zonal tasks).

Aircraft Systems and Components.

Auxiliary Power Unit (APU)

Power Plants.

Detailed and Special Detailed Inspection tasks and tasks for re-application of temporary protections applicable to the aircraft structure (Structure tasks)

2. CONTENTS

This Section includes 6 sub-sections:

Airworthiness Limitation Items (ALI)

Certification Maintenance Requirements (CMR)

Systems and Components (SYS)

Fuel Airworthiness Limitations (FAL )

Ageing Systems Maintenance (ASM)

Structure Program (STR)

Zonal Program (ZNL)

Fuel saving (ECO)

3. REMARK

This Aircraft Maintenance Schedule is printed out from AMASIS.

A321 Aircraft Maintenance Schedule


Date : SEP 2013

LIST OF EFFECTIVE PAGES - ALI Page : 1


LEP R 1 SEP 2013

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 52 DOORS

Task Number Zone Task Title Taskcode

Threshold Interval

Ctrl References Eff

ALI 521103-01-1AMM 521100/6AMT 521100-210-002

T 14 800 CYI 14 800 CY

ALL521103-01-1 FWD PAX/CREW DOOR SKIN EXTERNAL SURFACE831 GVI841

Y

GENERAL VISUAL INSPECTION OF FORWARD PASSENGER/CREWDOOR SKIN, EXTERNAL SURFACE, LH/RH

Skills :AF1 0.40 MHrsB21 0.00 MHrs

ALI 521303-01-1AMM 521300/6AMT 521300-210-002

T 14 800 CYI 14 800 CY

ALL521303-01-1 AFT PAX/CREW DOOR SKIN EXTERNAL SURFACE832 GVI842

Y

GENERAL VISUAL INSPECTION OF AFT PASSENGER/CREW DOORSKIN, EXTERNAL SURFACE, LH/RH


ALI 522201-01-1AMM 522211/6AMT 522211-200-005

T 4 500 CYI 4 500 CY

ALL522201-01-1 FORWARD EMERGENCY EXITS EXTERNAL SURFACE833 GVI843

N

GENERAL VISUAL INSPECTION OF FORWARD EMERGENCY EXITS,EXTERNAL SURFACE, LH/RH


Date ATA 52Date 22/01/2014Amendment NoIssue No Page ALI - 52 [1 / 6] :

: : :

: :

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Threshold Interval

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ALI 522203-01-1AMM 522211/6AMT 522211-200-006

T 24 000 CYI 4 500 CY

ALL522203-01-1 FWD EMERGENCY EXIT DOORS STOP ASSEMBLIES833 GVI843

N

GENERAL VISUAL INSPECTION OF DOOR STOP ASSEMBLIES ANDLOCKING HOOK ON FORWARD EMERGENCY EXIT DOORS, LH/RHAccess panels :

833 8430.04Total access time : Hrs

Skills :AF1 0.40 MHrs

ALI 522204-01-1AMM 522211/6AMT 522211-200-007

T 4 500 CYI 4 500 CY

ALL522204-01-1 AFT EMERGENCY EXITS EXTERNAL834 GVI844

N

AFT EMERGENCY EXITS EXTERNALGENERAL VISUAL INSPECTION OF AFT EMERGENCY EXITS,EXTERNAL SURFACE, LH/RH


ALI 522206-01-1AMM 522211/6AMT 522211-200-008

T 24 000 CYI 4 500 CY

ALL522206-01-1 AFT EMERGENCY EXITS INTERNAL834 GVI844

N

GENERAL VISUAL INSPECTION OF DOOR STOP ASSEMBLIES ANDLOCKING HOOK ON AFT EMERGENCY EXIT DOORS, LH/RHAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 523101-01-1AMM 523111/6AMT 523111-200-011

T 25 000 FHT 12 500 CYI 25 000 FHI 12 500 CY

ALL523101-01-1 FWD CARGO COMPARTMENT DOOR SKIN825 GVI N

GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE


ALI 523108-01-1AMM 523111/6AMT 523111-200-004MRB 523108-01-1

T 102 400 FHT 51 200 CYT 12 YEI 29 000 FHI 14 500 CYI 12 YE

ALL523108-01-1 FWD CARGO DOOR FITTINGS EXTERNAL AREA825 DI Y

DETAILED INSPECTION OF FORWARD CARGO COMPARTMENTDOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNALNOTE 1: APPLICATION OF TPS IS LIMITED ON THE INNER SIDE OF HINGE FITTINGSTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : DOOR OPENEDNOTE 2: 100% LIMIT = 12 YE OR 36500 FCNOTE 3: SAMPLING 20%NOTE 4: CPCPNOTE 5: RII TASKAccess panels :

8250.22Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 523109-02-1AMM 523111/6AMT 523111-200-013

T 20 700 FHT 10 300 CYI 20 700 FHI 10 300 CY

ALL523109-02-1 FWD CARGO DOOR LOCKING HOOKS825 GVI Y

GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORKFITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALLFRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)

Access panels :



ALI 523111-01-1AMM 523211/6AMT 523211-200-011

T 25 000 FHT 12 500 CYI 25 000 FHI 12 500 CY

ALL523111-01-1 AFT CARGO DOOR SKIN826 GVI Y

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENTDOOR SKIN, EXTERNAL SURFACE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 523118-01-2AMM 523211/6AMT 523211-200-005MRB 523118-01-2


ALL523118-01-2 AFT CARGO DOOR FITTINGS EXTERNAL AREA826 DI Y

DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,HINGE FITTINGS AND ATTACHMENT AREA, EXTERNALNOTE 1: APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF HINGE FITTINGSTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE 2: 100% LIMIT = 12 YE OR 33800 FCNOTE 3: SAMPLING 20%NOTE 4: CPCPNOTE 5: RII TASKAccess panels :



ALI 523119-02-2AMM 523211/6AMT 523211-200-012

T 20 700 FHT 10 300 CYI 20 700 FHI 10 300 CY

ALL523119-02-2 AFT CARGO DOOR LOCKING HOOKS826 GVI Y

GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORKFITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 523301-01-1AMM 523311/6AMT 523311-200-004

T 7 500 CYI 7 500 CY

ALL523301-01-1 BULK CARGO DOOR SKIN EXTERNAL827 GVI Y

BULK CARGO DOOR SKIN EXTERNALGENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENTDOOR SKIN, EXTERNAL SURFACE


ALI 528107-01-1AMT 528100-210-801

T 49 100 CYI 2 800 CY

ALL528107-01-1 MAIN GEAR DOORS730 GVI740

N

GENERAL VISUAL INSPECTION OF MLG DOOR FWDFITTING JOINT TO HINGE FITTING, LH/RHNOTE: FOR PRE 24428 OR PRE 24903 AIRCRAFTRETROFITTED, THRESHOLD IS TO BE COUNTED FROMSB 52-1058 OR SB 52-1073 EMBODIMENTAccess panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 53 FUSELAGE


Threshold Interval

Ctrl References Eff

ALI 531101-01-1AMT 531100-220-802

T 36 500 CYI 3 800 CY

ALL531101-01-1 FWD PAX/CREW DOOR 220 DI N

DETAILED INSPECTION OF FWD PASSENGER/CREW DOORCUTOUT, INTERCOSTALS FITTINGS N°7 BETWEEN FR15-16AND FR20-21, LH/RHPREPARATION:CEILING PANELS REMOVED;INSULATION REMOVED;LINING REMOVED;Access panels :



ALI 531102-01-1AMM 531100/6AMT 531100-210-001MRB 531102-01-1

T 22 000 CYT 6 YEI 13 600 CYI 6 YE

ALL531102-01-1 FWD PAX / CREW DOOR220 DI Y

DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOORFRAME, UPPER CORNERS, EXTERNAL SURFACE, LH/RHNOTE : CPCP

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531110-01-2AMT 531100-220-803MRB 531110-01-2NTM 53-11-10

T 60 000 FHT 30 000 CYI 28 900 FHI 14 400 CY

ALL531110-01-2 NOSE FORWARD FUSELAGE125 SDI126

N

SPECIAL DETAILED INSPECTION (ROTO) OF CROSSBEAMSPLICING, FR16 AND FR20, LH/RH.PREP. : AIR CONDITIONING DUCTS REMOVED; BOLTS REMOVED; INSULATION REMOVED;NOTE 1: 100% THRESHOLD = 38900 FC OR 77900 FHNOTE 2: SAMPLING 20%.Access panels :


Skills :NDT1 0.26 MHrs

ALI 531111-01-1AMM 531100/6AMT 531100-210-809

T 1 500 CYI 1 500 CY

ALL531111-01-1 AVIONICS DOORS SURROUND100 GVI Y

GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENTDOORS, SURROUND CORNERS, EXTERNAL SURFACE (4 DOORS)


ALI 531112-01-1AMM 531100/6AMT 531100-210-005

T 32 600 FHT 16 300 CYI 32 600 FHI 16 300 CY

ALL531112-01-1 FUSELAGE LOWER PANEL EXTERNAL SURFACE100 DI Y

DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT NLGBAY AFT CORNERS, EXTERNAL SURFACE, LH/RH



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531113-01-1AMT 531100-210-818

T 41 400 CYI 7 400 CY

ALL531113-01-1 FUSELAGE SKIN ATTACHMENT200 GVI N

GENERAL VISUAL INSPECTION OF ATTACHMENT TO SKINPANEL, FR16, STG 3 LH/RH


ALI 531114-01-1AMM 531100/6AMT 531100-210-006

T 5 700 CYI 5 700 CY

ALL531114-01-1 FUSELAGE SKIN EXTERNAL SURFACE200 DI Y

DETAILED INSPECTION OF FUSELAGE SKIN ABOVEWINDSHIELD, BETWEEN FR 4 AND FR 12, EXTERNAL SURFACE,LH/RH


ALI 531117-01-1AMM 531100/6AMT 531100-210-810

T 14 500 CYI 14 500 CY

ALL531117-01-1 FUSELAGE SIDE PANEL200 GVI Y

GENERAL VISUAL INSPECTION OF FUSELAGE SIDE PANEL,BELOW COCKPIT SIDE WINDOWS, BETWEEN FR 1 AND FR 12,EXTERNAL SURFACE, LH/RH


ALI 531118-01-1AMM 531100/6AMT 531100-210-811

T 4 300 CYI 4 300 CY

ALL531118-01-1 FUSELAGE SIDE PANEL200 GVI Y

GENERAL VISUAL INSPECTION OF AREA FORWARD OFWINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR 4,EXTERNAL SURFACE, LH/RH



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531119-01-2AMM 531100/6AMT 531100-210-007MRB 531119-01-2

T 30 000 CYI 11 700 CY

ALL531119-01-2 LOWER LAP JOINT EXTERNAL SURFACE100 DI Y

DETAILED INSPECTION OF UPPER SKIN OF LOWERLONGITUDINAL LAP JOINT, BETWEEN FR 9 AND FR 20,EXTERNAL SURFACE, LH/RHNOTE 1 : 100% LIMIT = 35300 FCNOTE 2 : SAMPLING 20%


ALI 531124-01-2AMM 531100/6AMT 531100-210-011

T 33 600 CYI 7 900 CY

ALL531124-01-2 SPLICE AT FR 20127 DI128

Y

DETAILED INSPECTION OF FR 20 SPLICE, BETWEEN STRINGER30 AND STRINGER 32, LH/RHPREP. : INSULATION DISPLACED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531127-01-1AMT 531100-220-807MRB 531127-01-1NTM 53-11-27

T 30 000 CYI 9 900 CY

ALL531127-01-1 MAIN STRUCTURE211 SDI212

N

SPECIAL DETAILED INSPECTION (HFEC) OF LATERALSPLICING, FR11, LH/RHPREPARATION:INSULATION REMOVED;LINING REMOVED;NOTE 1: 100% THRESHOLD =42400 FCNOTE 2: SAMPLING 20%

Skills :AVI1 1.20 MHrs

ALI 531129-02-3AMT 531100-220-001NTM 53-11-29

T 34 600 CYI 9 000 CY

ALL531129-02-3 WINDSHIELD CTR POST LWR ATTACHMENT211 SDI212

N

SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELDCENTER POST, LOWER ATTACHMENT AREA, INTERNAL SIDEPREP.: - LH/RH WINDSHIELDS REMOVED; - DISPLAY UNIT 4WT1 REMOVED; - ANCHOR NUT SHIMS REMOVED;Access panels :

211LW 211MW0.00Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531133-02-1AMT 531100-210-029

T 26 700 CYI 5 700 CY

ALL531133-02-1 WINDSHIELD SIDE POST LWR ATTACHMENT211 SDI212

N

SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD SIDEPOST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-1PREPARATION: SLIDING WINDOW OPENED;Access panels :

211NW 211PW 212NW 212PW0.00Total access time : Hrs


ALI 531135-01-2AMM 531100/6AMT 531100-210-026NTM 53-11-35

T 28 800 CYI 11 000 CY

ALL531135-01-2 WINDSHIELD SIDE POST UPR ATTACHMENT211 SDI212

Y

SPECIAL DETAILED INSPECTION (ROTO) OF WINDSHIELD SIDEPOST AT FR 4, UPPER ATTACHMENT, INTERNAL SIDE, LH/RHPREP. : BOLTS REMOVED SLIDING WINDOW OPENEDAccess panels :

211BC 211KC 211LC 211NW 212BC 212KC 212LC212NW




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531155-02-1AMM 531100/6AMT 531100-210-027NTM 53-11-55

T 22 700 CYI 10 300 CY

ALL531155-02-1 DOOR STOPS AT FR20221 SDI222

Y

SPECIAL DETAILED INSPECTION (HFEC AND ROTO) OF DOORFR 20, AT DOUBLE JOGGLE AREA IN OUTER FLANGE OF FR,AT DOOR STOPS NUMBER 1 AND 7 LOCATION, LH/RHPREP. : BOLTS REMOVED LINING REMOVED INSULATION REMOVEDAccess panels :



ALI 531157-01-2AMM 531100/6AMT 531100-210-021

T 24 000 CYI 7 000 CY

ALL531157-01-2 CONTINUITY AND ANGLE FITTINGS127 DI128

Y

DETAILED INSPECTION OF CONTINUITY FITTING BETWEEN FR20 AND FR 21, AND ANGLE FITTING, BOTH SIDES OF FR 21,AT STRINGER 41 LOCATION, LH/RHPREP : FLOOR PANELS REMOVED;LADDER.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531170-01-2AMM 531100/6AMT 531100-210-038MRB 531170-01-2

T 30 000 CYI 5 500 CY

ALL531170-01-2 COCKPIT WINDSHIELD LOWER FRONT FTG200 DI Y

DETAILED INSPECTION OF COCKPIT WINDSHIELD, LOWERFRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNALSURFACE, LH/RHPREP. : LOWER RETAINERSNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-2NOTE 2: 100% LIMIT = 36700 FCNOTE 3: SAMPLING 20%


ALI 531170-02-2AMM 531100/6AMT 531100-210-039MRB 531170-02-2NTM 53-11-70

T 24 000 CYI 15 000 CY

ALL531170-02-2 COCKPIT WINDSHIELD LOWER FRONT FTG200 SDI Y

SPECIAL DETAILED INSPECTION (HFEC) OF COCKPITWINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWERATTACHMENT, EXTERNAL SURFACE, LH/RH.PREP. : LOWER RETAINERSNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-2NOTE 2: 100% LIMIT = 36700 FCNOTE 3: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 531184-01-2AMT 531100-210-045

T 34 000 CYI 13 500 CY

ALL531184-01-2 FWD PRESSURE BULKHEAD VERTICAL POSTS211 DI212

N

DETAILED INSPECTION OF CENTRAL AND ADJACENT VERTICALPOSTS OF FORWARD PRESSURE BULKHEAD AND WEB ASSEMBLY,UPPER PORTIONPREPARATION: INSULATION REMOVED;Access panels :



ALI 532104-01-1AMT 532100-220-802NTM 53-21-04

T 86 900 FHT 43 400 CYI 71 200 FHI 35 600 CY

ALL532104-01-1 FLOOR STRUCTURE131 SDI132

N

SPECIAL DETAILED INSPECTION (ROTO) OF ATTACHMENTAREA OF FR25 LH TO FR34 LH AND FR29 RH TO FR34 RHTO CABIN FLOOR BEAMS, INTERNAL STRUCTUREPREPARATION:BOLTS REMOVED;CEILING PANELSREMOVED;INSULATIONDISPLACED;LINING REMOVED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532132-01-1AMM 532100/6AMT 532100-200-027

T 24 000 CYI 13 800 CY

ALL532132-01-1 FWD CARGO DOOR HINGE FITTING100 DI132

Y

DETAILED INSPECTION OF FUSELAGE FORWARD CARGO DOORHINGE FITTING AND EXTERNAL ATTACHMENT AREANOTE : CPCPAccess panels :



ALI 532135-01-2AMM 532100/6AMT 532100-210-002MRB 532135-01-1


ALL532135-01-2 FWD CARGO DOOR CUTOUT LATERAL FRAMES132 GVI Y

GENERAL VISUAL INSPECTION OF FORWARD CARGO DOORCUTOUT, VISIBLE PART OF LATERAL FR 24A AND FR 28TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532137-01-1AMM 532100/6AMT 532100-200-004

T 19 400 FHT 9 700 CYI 19 400 FHI 9 700 CY

ALL532137-01-1 FWD CARGO DOOR CUTOUT PANELS100 DI132

Y

DETAILED INSPECTION OF FORWARD CARGO DOOR CUTOUTPANELS, UPPER AND LOWER CORNERS, EXTERNAL SURFACE

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532150-01-1AMM 532100/6AMT 532100-200-022MRB 532150-01-1


22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532150-01-1 FWD EMERGENCY EXIT CUTOUT UPR CORNERS231 DI YR

DETAILED INSPECTION OF FORWARD EMERGENCY EXIT SKINCUT OUT, UPPER CORNERS, EXTERNAL SURFACE, LH.NOTE : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532150-01-2AMM 532100/6AMT 532100-200-022MRB 532150-01-2


29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155343

5427

54695709

5994

532150-01-2 FWD EMERGENCY EXIT CUTOUT UPR CORNERS231 DI YR

DETAILED INSPECTION OF FORWARD EMERGENCY EXIT SKINCUT OUT, UPPER CORNERS, EXTERNAL SURFACE, LH.NOTE : CPCP

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532151-01-1AMM 532100/6AMT 532100-220-004MRB 532151-01-1


22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532151-01-1 FWD EMERG. EXIT SKIN CUTOUT232 DI YR

DETAILED INSPECTION OF FORWARD EMERGENCY EXIT SKINCUT OUT, UPPER CORNERS, EXTERNAL SURFACE, RHNOTE : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532151-01-2AMM 532100/6AMT 532100-220-004MRB 532151-01-2


29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

532151-01-2 FWD EMERG. EXIT SKIN CUTOUT232 DI YR

DETAILED INSPECTION OF FORWARD EMERGENCY EXIT SKINCUT OUT, UPPER CORNERS, EXTERNAL SURFACE, RH.NOTE : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :


ALI 532152-01-2AMM 532100/6AMT 532100-210-015

T 42 000 FHT 20 000 CYI 42 000 FHI 20 000 CY

ALL532152-01-2 FWD EMERG. EXIT SKIN CUTOUT200 GVI Y

GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUNDNFORWARD EMERGENCY EXIT SKIN CUT OUT BETWEEN FR 35 ANDFR 35.3 AND FROM STRINGER 8 TO STRINGER 23, EXTERNALSURFACE, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF ZONAL TASK ZL-200-02-4.


ALI 532155-01-2AMM 532100/6AMT 532100-200-012MRB 532155-01-2

T 32 400 CYI 10 500 CY

ALL532155-01-2 FRAME SPLICES FR 24-34131 DI Y

DETAILED INSPECTION OF FRAME SPLICES AT STRINGER 35LH, FROM FR 24 TO FR 34PREP. : CARGO FLOOR PANELS INSULATION REMOVED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532156-01-1AMM 532100/6AMT 532100-210-004

T 42 000 FHT 24 000 CYI 12 600 FHI 4 700 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532156-01-1 FUSELAGE SKIN BETWEEN FR 35.4 & FR 35.8200 GVI YR

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 35.4 AND FR 35.8 FROM STRINGER 8TO STRINGER 14 AND STRINGER 18 TO STRINGER 23, LH/RH


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALI 532156-01-2AMM 532100/6AMT 532100-210-004

T 42 000 FHT 24 000 CYI 11 800 FHI 4 400 CY

2974

3005

30133022

3198

33153355

3737

38623964

3966

41364213

4277

43114315

5164

52415247

5297

53435427

5469

57095994

532156-01-2 FUSELAGE SKIN BETWEEN FR 35.4 & FR 35.8200 GVI YR

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 35.4 AND FR 35.8 FROM STRINGER 8TO STRINGER 14 AND STRINGER 18 TO STRINGER 23, LH/RH


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532165-01-3AMM 532100/6AMT 532100-210-005

T 3 600 CYI 3 600 CY

ALL532165-01-3 FUSELAGE SKIN BETWEEN FR 24 AND 35.8100 GVI Y

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE,EXCEPT AREAS COVERED BY BELLY FAIRINGNOTE: INSPECTION BETWEEN FR 24 AND FR 35.8.


ALI 532170-01-2AMM 532100/6AMT 532100-210-006MRB 532170-01-4

T 9 100 CYT 6 YEI 9 200 CYI 6 YE

ALL532170-01-2 FWD CARGO DOOR LOCK FITTINGS AND132 GVI Y

SURROUNDING STRUCTUREGENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR LOCKFITTINGS AND SURROUNDING STRUCTURE, EXTERNAL PORTIONNOTE: INSPECTION BETWEEN FR 25 AND FR 27A (6 PLACES)TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 532186-01-2AMT 532100-200-024MRB 532186-01-2NTM 53-21-86

T 60 000 FHT 30 000 CYI 34 400 FHI 13 300 CY

ALL532186-01-2 CIRCUMFERENTIAL JOINT AT FR 35200 SDI N

SPECIAL DETAILED INSPECTION (LFEC) OF CIRCUMFERENTIALJOINT AT FR 35, BETWEEN STRINGER 10 LH AND STRINGER10 RH, EXTERNAL SIDE.NOTE 1: 100 % THRESHOLD = 42700 FC OR 60000 FHNOTE 2: SAMPLING 20%



T 60 000 FHT 30 000 CYI 52 500 FHI 17 500 CY

ALL532187-01-1 CIRCUMFERENTIAL JOINT AT FR 35.8200 SDI Y

SPECIAL DETAILED INSPECTION (LFEC) OF CIRCUMFERENTIALJOINT AT FR 35.8 BETWEEN STRINGER 10 LH ANDSTRINGER 10 RH, EXTERNAL SIDENOTE : 100% LIMIT = 44300 FC OR 60000 FHNOTE 2 : SAMPLING 20%


ALI 532190-01-1AMM 532100/6AMT 532100-210-007

T 48 000 CYI 8 100 CY

ALL532190-01-1 FUSELAGE SKIN BETWEEN FR 25 AND FR 29100 GVI Y

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE AROUND WATER DRAIN PANEL CUTOUT, BETWEEN FR25 AND FR 29 AT STRINGER 43 LH



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533105-01-4AMM 533100/6AMT 533100-210-003MRB 533105-01-4


29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

533105-01-4 MLG BAY SIDE PANELS147 DI148

Y

DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELSINSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDINGSLANTED FRAMES AND SIDE BOX, LH/RHNOTE 1 : 100% LIMIT = 24 YE OR 23600 FC OR 60000 FHNOTE 2 : SAMPLING 20%NOTE 3 : CPCP

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533105-01-8AMT 533100-210-003MRB 533105-01-8

T 12 YEI 29 400 FHI 10 700 CYI 6 YE

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

533105-01-8 MLG BAY SIDE PANELS147 DI148

NR

DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELSINSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDINGSLANTED FRAMES AND SIDE BOX, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533105-01-2.NOTE 1: 100% THRESHOLD = 24 YE OR 27100 FC OR 60000 FHNOTE 2: SAMPLING 20%NOTE 3: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



ALI 533109-01-2AMM 533100/6AMT 533100-210-005

T 55 000 FHT 20 000 CYI 27 800 FHI 10 100 CY

ALL533109-01-2 PRESSURE DECK MEMBRANES UPR SURFACE145 DI146

Y

DETAILED INSPECTION OF UPPER SURFACES OF PRESSUREDECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS ANDSUPPORT RIBS, LH/RHPREP. : AIR DUCT CABIN FLOOR PANELS INSULATION REMOVEDAccess panels :

NONE1.50Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533111-01-2AMM 533100/6AMT 533100-210-006MRB 533111-01-2


ALL533111-01-2 PRESSURE DECK MEMBRANES LWR SURFACE147 DI148

Y

DETAILED INSPECTION OF LOWER SURFACE OF PRESSURE DECKMEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDINGCONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES,SUPPORT RIBS, REAR SPAR OF CENTER WING BOX ANDPRESSURE BULKHEAD, LH/RHNOTE 1 : 100% LIMIT = 24 YE OR 22000 FC OR 60500 FHNOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :



ALI 533122-01-2AMM 533100/6AMT 533100-210-019

T 33 000 CYI 9 200 CY

ALL533122-01-2 CIRCUMFERENTIAL SPLICE AT FR 47200 DI Y

DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICEAND STRINGER COUPLING AREA AT FR 47, FROM STRINGER10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACENOTE 1: 100% LIMIT = 33000 FCNOTE 2: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533130-01-3AMM 533100/6AMT 533100-210-010MRB 533130-01-3

T 27 800 CYT 12 YEI 13 500 CYI 12 YE

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

533130-01-3 ANTI COLLISION LIGHT SKIN CUTOUT200 DI YR

DETAILED INSPECTION OF SKIN AROUND ANTI COLLISIONLIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEENSTRINGER 1, LH/RH, EXTERNAL SURFACEPREP. : COVER OF ANTI-COLLISION LIGHT ANDANTI-COLLISION LIGHT REMOVEDNOTE 1: 100% LIMIT = 24 YE OR 27800 FCNOTE 2: SAMPLING 20%NOTE 3: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



ALI 533130-01-4AMM 533100/6AMT 533100-210-010MRB 533130-01-4

T 27 800 CYT 12 YEI 11 500 CYI 12 YE

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

533130-01-4 ANTI COLLISION LIGHT SKIN CUTOUT200 DI Y

DETAILED INSPECTION OF SKIN AROUND ANTI COLLISIONLIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEENSTRINGER 1, LH/RH, EXTERNAL SURFACEPREP. : COVER OF ANTI-COLLISION LIGHT ANDANTI-COLLISION LIGHT REMOVEDNOTE 1: 100% LIMIT = 24 YE OR 27800 FCNOTE 2: SAMPLING 20%NOTE 3: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 533100-210-011MRB 533131-01-5

T 26 300 CYT 12 YEI 15 700 CYI 12 YE

ALL533131-01-5 ADF1 ANTENNA SKIN CUTOUT200 DI N

DETAILED INSPECTION OF SKIN AROUND ADF 1 ANTENNACUTOUT, BETWEEN FR 44 AND FR 45 AND BETWEEN STRINGER1, LH/RH, EXTERNAL SURFACEPREPARATION:COVER OF ANTENNA AND ANTENNA REMOVED;NOTE 1: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533131-01-1.NOTE 2: 100% THRESHOLD=24 YE OR 26300 FCNOTE 3: CPCP


ALI 533132-01-2AMM 533100/6AMT 533100-210-020MRB 533132-01-2

T 30 000 CYI 9 300 CY

ALL533132-01-2 WINDOW FORGINGS FR 35.8-47200 DI Y

DETAILED INSPECTION OF VISIBLE PART OF WINDOWFORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA,LH/RH, EXTERNAL SURFACENOTE 1: INSPECTION BETWEEN FR 35.8 AND FR 47.NOTE 2: 100% LIMIT = 36300 FCNOTE 3: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533138-01-2AMT 533100-210-027MRB 533138-01-2

T 30 000 CYI 10 000 CY

ALL533138-01-2 LONGITUDINAL LAP JOINT AT FR 42241 DI242

N

DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAPJOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUTAREA AT FR 42, INTERNALNOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK533138-02-2PREPARATION: LINING AND INSULATION REMOVED;NOTE 1: 100% THRESHOLD = 40000 FCNOTE 2: SAMPLING 20%


ALI 533138-02-2AMT 533100-220-004MRB 533138-02-2NTM 53-31-38

T 30 000 CYI 12 000 CY

ALL533138-02-2 LONGITUDINAL LAP JOINT AT FR 42241 SDI242

N

SPECIAL DETAILED INSPECTION (HFEC) OF LOWER SKIN OFLONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER18 RH, IN RUNOUT AREA AT FR 42, INTERNALPREPARATION: LINING AND INSULATION REMOVED;NOTE 1: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK533138-01-2NOTE 2: 100% THRESHOLD= 40000 FCNOTE 3: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


T 30 000 CYI 17 000 CY

ALL533140-01-3 SPLICE PLATE AT FR 47200 SDI Y

SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER10, LH/RH, TO CROWN CENTER LINENOTE : 100% LIMIT = 40000 FCNOTE 2 : SAMPLING 20%


ALI 533141-01-2AMM 533100/6AMT 533100-210-025MRB 533141-01-2

T 60 000 FHT 30 000 CYI 19 600 FHI 9 800 CY

ALL533141-01-2 FUSELAGE SKIN BETWEEN FR 35.8 AND 36190 DI Y

DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 35.8AND FR 36 AND BETWEEN STRINGER 25 AND STRINGER 30,LH/RH, EXTERNAL SURFACENOTE : 100% LIMIT = 38600 FC OR 60000 FHNOTE 2 : SAMPLING 20%Access panels :

191BT 191EB 192BT 192EB0.32Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533143-01-1AMM 533100/6AMT 533100-210-029

T 80 000 FHT 40 000 CYI 21 200 FHI 10 600 CY

ALL533143-01-1 SIDE BOX BEAM IN AREA OF FR 46147 DI148

Y

DETAILED INSPECTION OF SIDE BOX BEAM IN AREA OFATTACHMENT TO FR 46, LH/RH

Access panels :



ALI 533144-01-1AMM 533100/6AMT 533100-210-030MRB 533144-01-1

T 66 200 FHT 33 100 CYI 25 600 FHI 12 800 CY

ALL533144-01-1 FRAME ATTACHMENTS TO PRESSURE FLOOR145 DI146

Y

DETAILED INSPECTION OF FRAME ATTACHMENTS TO PRESSUREFLOOR FROM FR 42 TO FR 46, LH/RHPREP. : LINING REMOVED INSULATION REMOVED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533152-01-3AMM 533100/6AMT 533100-210-012MRB 533152-01-3

T 31 000 CYT 12 YEI 9 100 CYI 6 YE

ALL533152-01-3 PRESSURE BULKHEAD AT FR 35.8 FWD FACE137 DI138

Y

DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACENOTE 1: INSPECTION AT FR 35.8 AND PRESSURE DECK UPPERSURFACE, BETWEEN FR 35.8 AND FR 36, INCLUDINGCONNECTIONS TO CENTER WING BOX AT FR35.8 AND FR 36.NOTE 2: CPCPTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : AIR DUCT RECIRCULATION FILTER REMOVED INSULATION REMOVEDAccess panels :

NONE 131NW 131PW 132PW0.58Total access time : Hrs



T 60 000 FHT 30 000 CYI 39 300 FHI 17 500 CY

ALL533155-03-1 KEEL BEAM BOX ELLIPTICAL CUTOUT147 SDI148

Y

SPECIAL DETAILED INSPECTION (HFEC) OF KEELBEAM BOXELLIPTICAL CUTOUT AT FR 46, LH/RHNOTE : 100% LIMIT = 38400 FC OR 60000 FHNOTE 2 : SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 533186-01-1AMT 533100-220-805NTM 53-31-86

T 80 000 FHT 40 000 CYI 30 000 FHI 15 000 CY

ALL533186-01-1 FR 35 FORWARD FACE TO PRESSURE BULKHEAD137 SDI138

N

ATTACHMENTSSPECIAL DETAILED INSPECTION (HFEC) OF FR 35 FORWARDFACE TO PRESSURE BULKHEAD ATTACHMENTS, AROUNDRIVETS AND HOLES BETWEEN STR 28 AND STR 31, LH/RH.PREPARATION:AIR CONDITIONING DUCTS REMOVED;RECIRCULATION FILTERREMOVED;INSULATION REMOVED;


ALI 533188-01-2AMT 533100-220-806

T 30 300 CYI 8 400 CY

ALL533188-01-2 PRESSURE BULKHEAD, AFT FACE, LOWER PART191 DI192

N

PRESSURE BULKHEAD, AFT FACE, LOWER PARTOF VERTICAL STRUTSDETAILED INSPECTION OF PRESSURE BULKHEAD, AFT FACE,LOWER PART OF VERTICAL STRUTS (200 MM FROM BOTTOM) ATY= +/-765 MM (2 PLACES)NOTE: PRESSURE BULKHEAD FR 35.8.Access panels :

191BB 191EB 192EB 192FB0.10Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534108-01-2AMM 534100/6AMT 534100-210-810

T 3 000 CYI 3 000 CY

ALL534108-01-2 FUSELAGE EXTERNAL SURFACE FR 47-70100 GVI Y

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 47 AND FR 70, FROM STRINGER 23,LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BYBELLY FAIRING


ALI 534111-01-2AMM 534100/6AMT 534100-210-002MRB 534111-01-2


ALL534111-01-2 ADF2 ANTENNA SKIN CUTOUT200 DI Y

DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNACUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACENOTE 1: INSPECTION BETWEEN FR 47.1 AND FR 47.2.FOR PRE 20053 AIRCRAFT RETROFITTED, THRESHOLDIS TO BE COUNTED FROM SB EMBODIMENT.NOTE 2: 100% LIMIT = 24 YE OR 28800 FC OR 60000 FHNOTE 3: SAMPLING 20%NOTE 4: CPCPPREP. :COVER OF ANTENNA AND ANTENNA REMOVEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534112-01-7AMT 534100-210-019MRB 534112-01-7


ALL534112-01-7 VHF3 ANTENNA SKIN CUTOUT200 DI N

DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNACUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: INSPECTION BETWEENFR 52 AND FR 53: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534112-01-1.PREPARATION: ANTENNA REMOVED;NOTE 1: 100% THRESHOLD=24 YE OR 31200 FC OR 60000 FHNOTE 2: SAMPLING 20%NOTE 3: CPCP


ALI 534113-01-2AMM 534100/6AMT 534100-210-020MRB 534113-01-2

T 30 000 CYI 10 900 CY

ALL534113-01-2 CIRCUMFERENTIAL SKIN SPLICE AT FR 64200 DI Y

DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICEAND STRINGER COUPLING AREAS AT FR 64, FROM STRINGER10, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACENOTE 1 : 100% LIMIT = 36000 FCNOTE 2 : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534121-01-4AMT 534100-220-010MRB 534121-01-4NTM 53-41-21

T 30 000 CYI 15 000 CY

ALL534121-01-4 REAR FUSELAGE200 SDI N

SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 64, FROM STRINGER10, LH/RH TO CROWN CENTERLINENOTE 1: 100% THRESHOLD = 40000 FCNOTE 2: SAMPLING 20%


AMT 534100-220-808NTM 53-41-24

T 60 000 FHT 30 900 CYI 14 400 FHI 7 200 CY

ALL534124-01-4 REAR FUSELAGE263 SDI264

N

SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8AND STRINGER 10, FRAME 68 WEB JOINT TO DOOR FRAME,AFT FACE, LH/RHPREP.: INSULATION REMOVED; LINING REMOVED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 534100-220-809NTM 53-41-25

T 60 000 FHT 30 000 CYI 7 000 FHI 3 500 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

4863

534125-01-4 REAR FUSELAGE100 SDI N

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKINEXTERNAL SURFACE AT WATER SERVICE PANEL CUTOUT,BETWEEN FRAME 65 AND FRAME 66 AT AND BELOW STRINGER37, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENTJOINT, LHNOTE 1 : 100% LIMIT = 41500 FC OR 60000 FHNOTE 2 : SAMPLING 20%NOTE 3 : ALI WFD TASK


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

4945

4971

51645241

5247

52515275

5297

53065340

5343

53855392

5418

54275438

5469

54955555


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 534100-220-810NTM 53-41-26

T 60 000 FHT 34 400 CYI 4 800 FHI 2 400 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

4863

534126-01-4 REAR FUSELAGE100 SDI N

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKINEXTERNAL SURFACE AT WASTE SERVICE PANEL CUTOUT,BETWEEN FRAME 65 AND FRAME 66 BELOW STRINGER 33,TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENTJOINT, RHNOTE: ALI WFD TASK


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

4945

4971

51645241

5247

52515275

5297

53065340

5343

53855392

5418

54275438

5469

54955555


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 534100-220-811NTM 53-41-27

T 52 800 FHT 26 400 CYI 11 200 FHI 5 600 CY


N

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGEINTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TO UPPERFRAME 68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RHPREP.: INSULATION REMOVED; LINING REMOVED;Access panels :



AMT 534100-220-812NTM 53-41-29

T 60 000 FHT 30 000 CYI 17 600 FHI 8 800 CY


N

SPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOP FITTINGS HOLESAT FRAME 66 WEB, LH/RHPREP.: BOLTS REMOVED; LINING REMOVED;NOTE 1 : 100% LIMIT = 42300 FC OR 60000 FHNOTE 2 : SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 534100-220-813NTM 53-41-30

T 60 000 FHT 30 000 CYI 17 600 FHI 8 800 CY


N

SPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOP FITTINGS HOLESAT FRAME 68 WEB, LH/RHPREP.: BOLTS REMOVED; LINING REMOVED;NOTE 1 : 100% LIMIT = 39800 FC OR 60000 FHNOTE 2 : SAMPLING 20%Access panels :



AMT 534100-210-814T 47 400 FHT 23 700 CYI 47 400 FHI 23 700 CY

ALL534131-01-4 FUSELAGE SKIN BETWEEN FR 65 AND 70100 GVI200

N

GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND AFTPASSENGER/CREW DOOR CUTOUTS, BETWEEN FR 65 AND FR 70AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE(EXCEPT AREA UNDER SCUFF PLATE), LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534131-01-1.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534132-01-5AMM 534100/6AMT 534100-210-010

T 31 800 FHT 15 900 CYI 10 000 FHI 20 000 CY

ALL534132-01-5 AFT PAX/CREW DOOR CUTOUT UPR CORNER260 DI Y

DETAILED INSPECTION OF AFT PASSENGER/CREW DOORCUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLYTHE VISIBLE PORTION OF THE INTERNAL DOUBLER, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534132-01-2.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534140-01-5AMM 534100/6AMT 534100-210-815

T 60 000 FHT 39 600 CYI 7 000 FHI 3 500 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

534140-01-5 FUSELAGE SKIN AROUND OUTFLOW VALVE100 GVI YR

GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUNDOUTFLOW VALVE CUTOUT, BETWEEN FR 65 AND FR 66 ANDFROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534140-01-7.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534140-01-7AMT 534100-210-815

T 60 000 FHT 39 500 CYI 7 000 FHI 3 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

4945

534140-01-7 FUSELAGE SKIN AROUND OUTFLOW VALVE100 GVI Y

CUTOUTGENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUNDOUTFLOW VALVE CUTOUT, BETWEEN FR 65 AND FR 66 ANDFROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534140-01-5.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534141-01-6AMM 534100/6AMT 534100-210-816

T 59 400 FHT 29 700 CYI 21 400 FHI 10 700 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

534141-01-6 FUSELAGE SKIN AROUND WATER SERVICE PANEL100 DI YR

CUTOUTDETAILED INSPECTION OF FUSELAGE SKIN AROUND WATERSERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNALSURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534141-01-3.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALI 534141-01-7AMM 534100/6AMT 534100-210-816

T 60 000 FHT 30 500 CYI 21 800 FHI 10 900 CY

2974

3005

30133022

3198

33153355

3737

38623964

3966

41364213

4277

43114315

534141-01-7 FUSELAGE SKIN AROUND WATER SERVICE PANEL100 DI Y

CUTOUTDETAILED INSPECTION OF FUSELAGE SKIN AROUND WATERSERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNALSURFACE


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534142-01-6AMM 534100/6AMT 534100-210-817MRB 534142-01-6

T 60 000 FHT 30 000 CYI 27 200 FHI 13 600 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

534142-01-6 FUSELAGE SKIN AROUND WASTE SERVICE PANEL100 DI YR

CUT OUTDETAILED INSPECTION OF FUSELAGE SKIN AROUND WASTESERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 ANDFROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACENOTE 1: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534142-1-3NOTE 2: 100% THRESHOLD: 35000 FC OR 60000 FHNOTE 3: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALI 534142-01-7AMM 534100/6AMT 534100-210-817MRB 534142-01-6

T 60 000 FHT 30 000 CYI 27 200 FHI 13 600 CY

2974

3005

30133022

3198

33153355

3737

38623964

3966

41364213

4277

43114315

5164

52415247

5297

53435427

5469

57095994

534142-01-7 FUSELAGE SKIN AROUND WASTE SERVICE PANEL100 DI YR

CUTOUTDETAILED INSPECTION OF FUSELAGE SKIN AROUND WASTESERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 ANDFROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACENOTE 1: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534142-1-3NOTE 2: 100% THRESHOLD: 35000 FC OR 60000 FHNOTE 3: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534145-01-1AMM 534100/6AMT 534100-220-012NTM 53-41-45

T 28 300 CYI 6 500 CY

ALL534145-01-1 SPLICE PLATE AT FR 47.5200 SDI Y

SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 47.5, FROM STRINGER16, LH/RH, TO CROWN CENTER LINE


ALI 534149-01-1AMM 534100/6AMT 534100-210-042

T 29 000 CYI 9 000 CY

ALL534149-01-1 CIRCUMFERENTIAL SPLICE 47.5200 DI Y

DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICEAND STRINGER COUPLING AREAS AT FR 47.5, FROM STRINGER16, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE


ALI 534157-01-6AMM 534100/6AMT 534100-210-038MRB 534157-01-1

T 11 400 CYT 6 YEI 11 400 CYI 6 YE

ALL534157-01-6 AFT CARGO DOOR LOCK FITTINGS152 GVI Y

GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCKFITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 53 ANDFR 55A, EXTERNAL PORTION (6 PLACES)TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 534100-210-031T 12 000 CYI 12 000 CY

ALL534159-01-3 AFT CARGO DOOR CUTOUT UPR/LWR CORNERS152 DI154252

N

DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPERAND LOWER CORNERS, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534159-01-1Access panels :



AMT 534100-220-803T 1 400 CYT 2 800 FHI 2 800 FHI 1 400 CY

ALL534160-02-1 AFT CARGO DOOR CUTOUT LATERAL FRAMES152 DI N

DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLEPART OF LATERAL FRAMESNOTE: INSPECTION OF FR 52A AND FR 56.

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534171-01-2AMT 534100-210-008NTM 53-41-71

T 42 100 FHT 21 000 CYI 42 100 FHI 21 000 CY

ALL534171-01-2 BULK CARGO DOOR CUTOUT UPR CORNERS162 SDI N

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKINOF BULK CARGO DOOR CUTOUT AT UPPER CORNERSNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISMENT OF TASK 534171-01-3.Access panels :



ALI 534172-01-2AMM 534100/6AMT 534100-210-804MRB 534172-01-1

T 30 600 FHT 15 300 CYI 30 600 FHI 15 300 CY

ALL534172-01-2 BULK CARGO DOOR CUTOUT SEALING PROFILE162 GVI Y

GENERAL VISUAL INSPECTION OF SEALING PROFILE OF BULKCARGO DOOR CUTOUT AT UPPER CORNERSNOTE : CPCP

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 534183-01-1AMM 534100/6AMT 534100-210-820

T 24 000 CYI 11 900 CY

ALL534183-01-1 CIRCUMFERENTIAL JOINT ABOVE AFT200 GVI Y

EMERGENCY EXIT DOORGENERAL VISUAL INSPECTION OF CIRCUMFERENTIAL JOINTABOVE AFT EMERGENCY EXIT DOOR AT FR 47.3 FROMSTRINGER 6 TO STRINGER 12, EXTERNAL SURFACE, LH/RH


AMM 535100/6AMT 535100-210-019MRB 535103-01-2

T 35 000 FHT 17 500 CYI 35 000 FHI 17 500 CY

ALL535103-01-2 FUSELAGE SKIN AROUND CUTOUT FOR TAIL300 GVI Y

COMPARTMENT ACCESS DOORGENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUNDCUTOUT FOR TAIL COMPARTMENT ACCESS DOOR, BETWEEN FR70 AND FR 73 AND BETWEEN STRINGER 25 RH AND BOTTOMCENTER LINE, EXTERNAL SURFACE


AMT 535100-210-012T 34 100 CYI 14 400 CY

ALL535162-01-2 FIN/FUSELAGE ATTACH FITTINGS OUTSIDE323 DI N

DETAILED INSPECTION OF FIN TO FUSELAGE, FORWARD, MIDAND AFT ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RHAccess panels :

323AL 323AR0.26Total access time : Hrs



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 54 NACELLES / PYLONS


Threshold Interval

Ctrl References Eff

ALI 545103-01-2AMM 545100/6AMT 545100-200-003MRB 545103-01-2

T 8 300 CYI 8 300 CY

ALL545103-01-2 PYLON FWD MOUNT FITTING415 DI425

Y

DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING,FORWARD OF RIB 1

Access panels :

437AL 438AR 447AL 448AR 451AL 452AR 461AL462AR



ALI 545130-01-3AMM 545100/6AMT 545100-200-016

T 13 000 CYI 13 000 CY

ALL545130-01-3 PYLON LATERAL PANELS EDGE OF CUTOUTS415 DI425

Y

DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THEEDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 5 AND RIB 6,LH/RHAccess panels :

415BL 415BR 425BL 425BR0.08Total access time : Hrs



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 55 STABILIZERS


Threshold Interval

Ctrl References Eff

ALI 552007-01-2AMT 552000-200-006NTM 55-20-07SIL 55-037

T 12 YEI 6 YE

22552261

2267

23032480

552007-01-2 ELEVATOR TOP AND BOTTOM SKIN PANELS335 SDI345

Y

SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OFELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH.NOTE 1: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT.NOTE 2: THIS TASK IS ALTERNATIVE TO THE TASK 552007-01-4.


ALI 552007-01-4AMT 552000-200-006NTM 55-20-07SIL 55-037

T 12 YEI 6 YE

22552261

2267

23032480

552007-01-4 ELEVATOR TOP AND BOTTOM SKIN PANELS335 SDI345

YR

SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OFELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH.NOTE 1: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT.NOTE 2: THIS TASK IS ALTERNATIVE TO THE TASK 552007-01-2.NOTE 3: RII TASKPREP. : ELEVATOR REMOVED;



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 57 WINGS


Threshold Interval

Ctrl References Eff

ALI 571170-01-3AMM 571000/6AMT 571000-220-006NTM 57-11-47

T 60 000 FHT 35 000 CYI 18 200 FHI 9 100 CY

ALL571170-01-3 INSPECTION OF CENTER WING BOX191 SDI192

Y

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX,CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME42. LH/RH

Access panels :

191DT 191ET 192DT 192ET0.40Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 571185-01-3AMM 571000/6AMT 571000-200-026NTM 57-11-85

T 52 900 FHT 20 000 CYI 14 600 FHI 5 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

571185-01-3 OUTER WING UPPER HALF OF VERTICAL TEE540 SDI640

YR

SPECIAL DETAILED INSPECTION OF OUTER WB- (HOLES ON)UPPER HALF OF VERTICAL TEE FITTING AT JUNCTION WITHRIB 1 AND REAR SPAR, LH/RHPREP. : SEALANT TO BE REMOVED


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

540AB 540AZ 540BZ 640AB 640AZ 640BZ0.20Total access time : Hrs


ALI 571185-01-4AMM 571000/6AMT 571000-200-026NTM 57-11-85

T 42 000 FHT 24 000 CYI 13 200 FHI 4 900 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

571185-01-4 OUTER WING UPPER HALF OF VERTICAL TEE540 SDI640

Y

SPECIAL DETAILED INSPECTION OF OUTER WB- (HOLES ON)UPPER HALF OF VERTICAL TEE FITTING AT JUNCTION WITHRIB 1 AND REAR SPAR, LH/RHPREP. : SEALANT TO BE REMOVED

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572004-01-2AMM 572000/6AMT 572000-200-004MRB 572004-01-2

T 49 700 FHT 30 000 CYI 24 800 FHI 15 000 CY

ALL572004-01-2 OUTER WING FRONT SPAR AFT FACE540 DI640

Y

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFTFACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREAINSIDE THE DRY BAYNOTE 2: SAMPLING 20%NOTE 3: 100% LIMIT = 44000 FC OR 60000 FHAccess panels :

540AB 540AZ 540BB 540CB 640AB 640AZ 640BB640CB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572007-01-4AMM 572000/6AMT 572000-200-005MRB 572007-01-4


22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572007-01-4 OUTER WING REAR SPAR AFT FACE571 DI671

YR

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFTFACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDINGREAR SPAR ANGLENOTE : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572007-01-5AMM 572000/6AMT 572000-200-005


29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

572007-01-5 OUTER WING REAR SPAR AFT FACE571 DI671

YR

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFTFACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDINGREAR SPAR ANGLENOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572011-01-4AMM 572000/6AMT 572000-200-008

T 60 000 FHT 30 000 CYI 19 000 FHI 11 600 CY

ALL572011-01-4 OUTER WING REAR SPAR FWD FACE540 DI640

Y

DETAILED INSPECTION OF OUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGESAccess panels :

540AB 540BB 540BZ 540CB 640AB 640BB 640BZ640CB




ALL572014-01-7 OUTER WING TOP SKIN500 GVI600

N

OUTER WING TOP SKINGENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN,UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERSBETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572020-01-5AMM 572000/6AMT 572000-200-010MRB 572020-01-5

T 55 000 FHT 30 000 CYI 23 200 FHI 12 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572020-01-5 OUTER WING TOP SKIN RIB 1 AND 8540 DI640

YR

DETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTSAND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER11, EXCLUDING THE AREA INSIDE THE DRY BAYNOTE 1: 100% LIMIT = 41800 CY OR 60000 FHNOTE 2: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

540AB 540AZ 540BB 540BZ 640AB 640AZ 640BB640BZ




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572020-01-5AMM 572000/6AMT 572000-200-010

T 60 000 FHT 33 000 CYI 22 800 FHI 11 800 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

572020-01-6 OUTER WING TOP SKIN RIB 1 AND 8540 DI640

Y

DETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTSAND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER11, EXCLUDING THE AREA INSIDE THE DRY BAY

Access panels :

540AB 540AZ 540BB 540BZ 640AB 640AZ 640BB640BZ




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572032-01-2AMM 572000/6AMT 572000-200-020

T 42 000 FHT 24 000 CYI 11 800 FHI 6 800 CY

ALL572032-01-2 OUTER WING BOTTOM SKIN/REAR SPAR500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING

ALI 572034-01-3AMM 572000/6AMT 572000-210-003

T 53 000 FHT 32 700 CYI 16 600 FHI 10 200 CY

ALL572034-01-3 OUTER WING BOTTOM SKIN LDG PLATE500 GVI600

Y

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE MLG REINFORCING PLATE


ALI 572036-01-3AMM 572000/6AMT 572000-200-022MRB 572036-01-3

T 42 000 FHT 24 000 CYI 18 400 FHI 10 600 CY

ALL572036-01-3 OUTER WING BOTTOM SKIN FLAP TRACK 2531 DI631

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAPTRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPARNOTE : SAMPLING 20%NOTE : 100% THRESHOLD = 35800 FC OR 60000 FHAccess panels :

531CB 531EB 631CB 631EB0.08Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572038-01-2AMM 572000/6AMT 572000-200-023

T 41 700 FHT 24 000 CYI 7 200 FHI 4 100 CY

ALL572038-01-2 OUTER WING BOTTOM SKIN RUNOUTS500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6),STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10(RIB BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) ANDSTRINGER 15 (RIB BAY 2-3)


ALI 572041-02-10AMT 572000-220-802MRB 572041-02-10

T 48 700 FHT 30 000 CYI 7 900 FHI 4 900 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

572041-02-10 OUTER WING500 DI600

N

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWERSURFACE AT ATTACHMENT TO RIBS AND STRINGERS(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FAIRINGS AND REINFORCING PLATES.NOTE 1: 100% THRESHOLD = 39600 FC OR 60000 FHNOTE 2: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


22552267

2303

24803600

4669

47034737

4783

48264863

4945

49715241

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572041-02-9 OUTER WING500 DI600

NR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWERSURFACE AT ATTACHMENT TO RIBS AND STRINGERS(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FAIRINGS AND REINFORCING PLATES.NOTE 1 : 100% LIMIT THRESHOLD = 42400 FC OR 60000 FHNOTE 2 : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572042-01-4AMM 572000/6AMT 572000-210-005

T 42 000 FHT 24 000 CYI 6 500 FHI 4 000 CY

ALL572042-01-4 OUTER WING BOTTOM SKIN LOWER SURFACE471 GVI481

Y

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, INAREA COVERED BY PYLON FAIRINGPREP. : PYLON FAIRINGS REMOVED


ALI 572044-01-5AMM 572000/6AMT 572000-210-004

T 47 100 FHT 29 000 CYI 7 500 FHI 4 600 CY


Y

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREASCOVERED BY REINFORCING PLATES AND FAIRINGS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572050-01-5AMT 572000-200-034

T 51 400 FHT 28 700 CYI 22 000 FHI 12 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572050-01-5 OUTER WING, DRY BAY AREA540 DI640

YR

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE 1:- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-5.- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTIONTHRESHOLD OF THIS TASK, THE INSPECTION SHOULD BEPERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OFSSI 572004 OR 572020 OR 572027 OR 572053. FROM THATTIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THISTASK.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

540AB 540BB 540CZ 540DZ 640AB 640BB 640CZ640DZ




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572050-01-5AMT 572000-200-034

T 51 400 FHT 28 700 CYI 22 000 FHI 11 800 CY

37373862

3964

39664136

4213

42774311

4315

51645241

5247

52975343

5427

54695709

5994

572050-01-6 OUTER WING, DRY BAY AREA540 DI640

YR

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE 1:- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-6.- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTIONTHRESHOLD OF THIS TASK, THE INSPECTION SHOULD BEPERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OFSSI 572004 OR 572020 OR 572027 OR 572053. FROM THATTIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THISTASK.

Access panels :

540AB 540BB 540CZ 540DZ 640AB 640BB 640CZ640DZ




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572050-02-5AMT 572000-220-011MRB 572050-02-5NTM 57-20-50

T 42 000 FHT 24 000 CYI 22 000 FHI 12 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572050-02-5 OUTER WING, DRY BAY AREA521 SDI621

YR

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTERWING, DRY BAY AREANOTE 1:- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-5.- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTIONTHRESHOLD OF THIS TASK, THE INSPECTION SHOULD BEPERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OFSSI 572004 OR 572020 OR 572027 OR 572053. FROM THATTIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THISTASK.NOTE 2: 100% THRESHOLD 28700 FC OR 51400 FHNOTE 3: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

521AZ 521BZ 521EB 621AZ 621BZ 621EB0.30Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572050-02-6AMT 572000-220-011NTM 57-20-50

T 51 400 FHT 28 700 CYI 22 000 FHI 11 800 CY

37373862

3964

39664136

4213

42774311

4315

51645241

5247

52975343

5427

54695709

5994

572050-02-6 OUTER WING, DRY BAY AREA521 SDI621

YR

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTERWING, DRY BAY AREANOTE 1:- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-6.- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTIONTHRESHOLD OF THIS TASK, THE INSPECTION SHOULD BEPERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OFSSI 572004 OR 572020 OR 572027 OR 572053. FROM THATTIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THISTASK.

Access panels :

521AZ 521BZ 521EB 621AZ 621BZ 621EB0.30Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572053-01-3AMM 572000/6AMT 572000-200-026

T 51 400 FHT 28 700 CYI 22 000 FHI 12 300 CY

ALL572053-01-3 OUTER WING BOTTOM SKIN STRINGERS540 DI640

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAINHOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 ANDSTRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAYAccess panels :

540AB 540AZ 540BB 540BZ 540CB 640AB 640AZ640BB 640BZ 640CB


ALI 572111-01-3AMM 572100/6AMT 572100-200-002MRB 572111-01-3


ALL572111-01-3 OUTER WING REAR SPAR AFT FACE RIB 8-11574 DI575674675

Y

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFTFACE, FROM RIB 8 TO RIB 11NOTE : CPCP

Access panels :

573CB 573EB 573FB 575AB 673CB 673EB 673FB675AB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572112-01-3AMM 572100/6AMT 572100-200-003MRB 572112-01-3


ALL572112-01-3 OUTER WING REAR SPAR AFT FACE RIB11-27575 DI675

Y

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFTFACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINTPLATE AT RIB 22NOTE : CPCP

Access panels :

575BB 575CB 575DB 575EB 575FB 575GB 575HB575JB 575KB 575LB 575MB 675BB 675CB 675DB675EB 675FB 675GB 675HB 675JB 675KB 675LB675MB



ALI 572114-01-5AMM 572100/6AMT 572100-200-010MRB 572114-01-5

T 49 200 FHT 30 000 CYI 19 000 FHI 11 600 CY

ALL572114-01-5 OUTER WING REAR SPAR FWD FACE RIB 8-11540 DI640

Y

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARDFACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP ANDBOTTOM FLANGESNOTE 1: 100% LIMIT = 38900 FC OR 60000 FHNOTE 2: SAMPLING 20%Access panels :

540CB 540DB 540EB 640CB 640DB 640EB0.35Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572115-01-3AMM 572100/6AMT 572100-200-011MRB 572115-01-3

T 48 900 FHT 30 000 CYI 20 200 FHI 12 400 CY

ALL572115-01-3 OUTER WING REAR SPAR FWD FACE RIB11-27NT DI Y

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARDFACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT ATRIB 22 AND TOP AND BOTTOM FLANGESNOTE 1 : 100% LIMIT = 35600 FC OR 58100 FHNOTE 2 : SAMPLING 20%NOTE 3 : WORKING ZONES: 540, 550, 560 640, 650, 660Access panels :

540FB 540GB 540HB 540JB 540KB 540LB 540MB540NB 540PB 540QB 540RB 550AB 550BB 550CB550DB 560AB 640FB 640GB 640HB 640JB 640KB640LB 640MB 640NB 640PB 640QB 640RB 650AB650BB 650CB 650DB 660AB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572129-01-2AMM 572100/6AMT 572100-200-015MRB 572129-01-2

T 52 100 FHT 30 000 CYI 11 300 FHI 6 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572129-01-2 OUTER WING BOTTOM SKIN ATTACH RIB 8-15500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BYPYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3FAIRINGNOTE : 100% LIMIT = 38000 FC OR 60000 FHNOTE 2 : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572129-01-3AMM 572100/6AMT 572100-200-015

T 56 300 FHT 32 400 CYI 8 500 FHI 4 900 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

572129-01-3 OUTER WING BOTTOM SKIN ATTACH RIB 8-15500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BYPYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3FAIRING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572130-01-4AMM 572100/6AMT 572100-200-016MRB 572130-01-4

T 52 100 FHT 30 000 CYI 11 300 FHI 6 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572130-01-4 OUTER WING BOTTOM SKIN ATTACH RIB15-22500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BYFLAP TRACK 4 FAIRINGNOTE 1 : 100% LIMIT = 38000 FC OR 60000 FHNOTE 2 : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572130-01-5AMM 572100/6AMT 572100-200-016MRB 572130-01-5

T 52 100 FHT 30 000 CYI 11 300 FHI 6 500 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

572130-01-5 OUTER WING BOTTOM SKIN ATTACH RIB15-22500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BYFLAP TRACK 4 FAIRINGNOTE 1 : 100% LIMIT = 36700 FC OR 60000 FHNOTE 2 : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572137-01-3AMM 572100/6AMT 572100-200-019

T 42 000 FHT 24 000 CYI 8 200 FHI 4 900 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572137-01-3 OUTER WING BOTTOM SKIN RUNOUTS500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY19-20) AND STRINGER 12 (RIB BAY 17-18)


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572137-01-5AMM 572100/6AMT 572100-200-019

T 42 000 FHT 24 000 CYI 7 600 FHI 4 500 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

572137-01-5 OUTER WING BOTTOM SKIN RUNOUTS500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY19-20) AND STRINGER 12 (RIB BAY 17-18)



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572142-01-3AMM 572100/6AMT 572100-210-002

T 42 000 FHT 24 000 CYI 6 800 FHI 4 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572142-01-3 OUTER WING BOTTOM SKIN CUTOUTS500 GVI600

YR

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REARSPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING ANDFLAP TRACK 3 FAIRING


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572142-01-5AMM 572100/6AMT 572100-210-002

T 60 000 FHT 42 700 CYI 6 800 FHI 4 000 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

572142-01-5 OUTER WING BOTTOM SKIN CUTOUTS500 GVI600

YR

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REARSPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING ANDFLAP TRACK 3 FAIRING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572143-01-3AMM 572100/6AMT 572100-200-022MRB 572143-01-3

T 51 000 FHT 30 000 CYI 16 600 FHI 9 800 CY

ALL572143-01-3 OUTER WING BOTTOM SKIN RIB/STGR ATTACH532 DI533632633

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREACOVERED BY FLAP TRACK 3 FAIRING AND FLAP TRACK 4FAIRING.NOTE 1 : SAMPLING 20%NOTE 2 : 100% THRESHOLD = 39200 FC OR 60000 FHAccess panels :

532CB 532EB 533CB 533EB 632CB 632EB 633CB633EB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572148-01-5AMM 572100/6AMT 572100-210-003

T 39 000 FHT 24 000 CYI 7 300 FHI 4 500 CY

22552261

2267

23032480

2974

36003737

4669

47034737

4783

48264863

4945

49715251

5275

53065340

5385

53925418

5438

54565495

5555

5699

572148-01-5 OUTER WING BOTTOM SKIN RIB/STGR ATTACH500 GVI600

YR

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDINGAREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3FAIRING


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572148-01-6AMM 572100/6AMT 572100-210-003

T 39 000 FHT 24 000 CYI 6 100 FHI 3 700 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994


YR

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE,SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572149-01-5AMM 572100/6AMT 572100-210-004

T 52 300 FHT 32 200 CYI 8 600 FHI 5 300 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958


YR

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TOFRONT SPAR AND REAR SPAR, EXCLUDING AREAS COVERED BYFLAP TRACK 4 FAIRING


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572149-01-6AMM 572100/6AMT 572100-210-004

T 53 300 FHT 32 200 CYI 6 100 FHI 3 700 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994


YR

OUTER WING BOTTOM SKIN RIB/STGR ATTACHGENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE,SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAPTRACK 4 FAIRING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572150-01-4AMM 572100/6AMT 572100-200-023

T 42 000 FHT 24 000 CYI 16 000 FHI 9 400 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572150-01-4 OUTER WING BOTTOM SKIN JOINTS RIB11-13532 DI632

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREASCOVERED BY FLAP TRACK 3 FAIRING


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572150-01-5AMM 572100/6AMT 572100-200-023

T 40 700 FHT 24 000 CYI 8 300 FHI 4 800 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994


YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREASCOVERED BY FLAP TRACK 3 FAIRING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572155-01-3AMM 572100/6AMT 572100-200-026

T 58 100 FHT 30 500 CYI 29 600 FHI 15 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572155-01-3 OUTER WING BOTTOM SKIN RIB 8-21540 DI640

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPERSURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,BETWEEN RIB 8 AND RIB 21


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

540CB 540DB 540EB 540FB 540GB 540HB 540JB540KB 540LB 540MB 540NB 540PB 540QB 640CB640DB 640EB 640FB 640GB 640HB 640JB 640KB640LB 640MB 640NB 640PB 640QB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572155-01-4AMM 572100/6AMT 572100-200-026

T 42 000 FHT 22 800 CYI 18 800 FHI 9 900 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

572155-01-4 OUTER WING BOTTOM SKIN RIB 8-21540 DI640

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPERSURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,BETWEEN RIB 8 AND RIB 21


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

540CB 540DB 540EB 540FB 540GB 540HB 540JB540KB 540LB 540MB 540NB 540PB 540QB 640CB640DB 640EB 640FB 640GB 640HB 640JB 640KB640LB 640MB 640NB 640PB 640QB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572158-01-4AMM 572100/6AMT 572100-200-028

T 42 000 FHT 24 000 CYI 19 800 FHI 9 800 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

572158-01-4 OUTER WING BOTTOM SKIN STGR RIB 8-18540 DI640

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 ANDRIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 & 13


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

540CB 540DB 540EB 540FB 540GB 540HB 540JB540KB 540LB 540MB 640CB 640DB 640EB 640FB640GB 640HB 640JB 640KB 640LB 640MB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 572158-01-8AMM 572100/6AMT 572100-200-028

T 57 900 FHT 28 600 CYI 44 100 FHI 21 800 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

572158-01-8 OUTER WING BOTTOM SKIN STGR RIB 8-18540 DI640

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 ANDRIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 & 13NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572158-01-4.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALI 572160-01-3AMM 572100/6AMT 572100-200-029

T 42 000 FHT 24 000 CYI 27 800 FHI 16 100 CY

ALL572160-01-3 OUTER WING BOTTOM SKIN STGR RIB 18-27540 DI550560640650660

Y

DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGERS BETWEEN RIB 18 AND RIB 27COMPRISING STRINGERS 7, 8 AND 11

Access panels :

540NB 540PB 540QB 540RB 550AB 550BB 550CB550DB 560AB 640NB 640PB 640QB 640RB 650AB650BB 650CB 650DB 660AB



ALI 575158-01-2AMM 575100/6AMT 575100-210-003

T 42 000 FHT 24 000 CYI 8 800 FHI 5 200 CY


Y

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGSAND PYLON FAIRINGS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 575159-01-2AMM 575100/6AMT 575100-200-007

T 34 900 FHT 21 800 CYI 12 500 FHI 7 800 CY

ALL575159-01-2 OUTER WING BOTTOM SKIN/REAR SPAR500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE, CURVED SKIN EDGE AFT OF REAR SPAR JUSTINBOARD OF MLG SUPPORT RIB 5



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 575160-01-3AMM 575100/6AMT 575100-200-008NTM 57-51-60

T 42 000 FHT 24 000 CYI 19 100 FHI 11 900 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

575160-01-3 TRAILING EDGE BOTTOM SKIN REAR SPAR574 SDI674

YR

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTERWING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,ABOVE MLG REINFORCINGPREP. : MLG SECONDARY HINGED FAIRING


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

574AB 674AB0.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 575160-01-4AMM 575100/6AMT 575100-200-008NTM 57-51-60

T 42 000 FHT 24 000 CYI 16 900 FHI 10 600 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

575160-01-4 TRAILING EDGE BOTTOM SKIN REAR SPAR574 SDI674

YR

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTERWING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,ABOVE MLG REINFORCINGPREP. : MLG SECONDARY HINGED FAIRING


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 575161-01-2AMM 575100/6AMT 575100-210-004

T 42 000 FHT 24 000 CYI 6 700 FHI 4 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

575161-01-2 TRAILING EDGE BOTTOM SKIN REAR SPAR500 GVI600

YR

GENERAL VISUAL INSPECTION OF OUTER WING, TRAILINGEDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROMRIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE ATRIB 9 AND SIGHTING ROD HOLE AT RIB 10


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 575161-01-3AMM 575100/6AMT 575100-210-004

T 42 000 FHT 24 000 CYI 6 100 FHI 3 600 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

575161-01-3 TRAILING EDGE BOTTOM SKIN REAR SPAR500 GVI600

YR

GENERAL VISUAL INSPECTION OF OUTER WING, TRAILINGEDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROMRIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE ATRIB 9 AND SIGHTING ROD HOLE AT RIB 10



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


T 46 500 FHT 30 000 CYI 5 500 FHI 3 600 CY

ALL575163-01-3 OUTER WING BOTTOM SKIN UND PYLON FAIR574 SDI674

Y

SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDERPYLON FAIRINGPREP. : PYLON FAIRINGS REMOVED;NOTE 1: 100% LIMIT = 41500 FC OR 60000 FHNOTE 2: SAMPLING 20%


ALI 575164-01-4AMM 575100/6AMT 575100-220-012NTM 57-51-64

T 42 000 FHT 24 000 CYI 6 400 FHI 3 900 CY

ALL575164-01-4 OUTER WING BOTTOM SKIN UND FLAP TRACK2531 SDI574631674

Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, AROUNDFLAP TRACK 2 FORWARD FITTINGS

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 575165-01-2AMM 575100/6AMT 575100-200-009MRB 575165-01-2

T 52 500 FHT 30 000 CYI 21 100 FHI 12 700 CY

ALL575165-01-2 OUTER WING BOTTOM SKIN UND FLAP 2 FAIR531 DI574631674

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE, AFT OF REAR SPAR, UNDER FLAP TRACK 2 FAIRINGAND FLAP TAB DRIVE 1A FAIRINGNOTE 1: 100% LIMIT = 35400 FC OR 58800 FHNOTE 2: SAMPLING 20%Access panels :

531EB 535AB 535BB 631EB 635AB 635BB0.44Total access time : Hrs


ALI 575221-01-1AMM 575200/6AMT 575200-210-009

T 4 800 CYI 4 800 CY

ALL575221-01-1 INBOARD FLAP END RIB500 GVI600

Y

GENERAL VISUAL INSPECTION OF INBOARD DOUBLE-SLOTTEDFLAP, EXTERNAL SURFACE OF UPPER AND LOWER SKIN, LH/RHPREP. : FLAP EXTENSION


ALI 575321-01-2AMM 575300/6AMT 575300-210-009

T 8 500 CYI 8 500 CY

ALL575321-01-2 OUTBOARD DOUBLE SLOTTED FLAP TAB500 GVI600

Y

GENERAL VISUAL INSPECTION OF OUTBOARD DOUBLE-SLOTTEDFLAP, INCLUDING TAB, EXTERNAL SURFACE OF UPPER ANDLOWER SKIN, LH/RHPREP. : FLAP EXTENSION



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 576103-01-1AMM 576000/6AMT 576000-200-002MRB 576103-01-1

T 30 000 CYT 12 YEI 15 800 CYI 12 YE

ALL576103-01-1 AILERON HINGE AND ACTUATOR FITTINGS575 DI675

Y

DETAILED INSPECTION OF AILERON, HINGE FITTINGS ANDACTUATOR ATTACHMENT FITTINGSNOTE 1: 100% THRESHOLD = 12YE OR 38700 FCNOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

575AT 575KB 575LB 575MB 675AT 675KB 675LB675MB




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 71 POWER PLANT - GENERAL


Threshold Interval

Ctrl References Eff

ALI 711300-03-1AMT 711300-210-010

T 3 000 CYI 3 000 CY

ALL711300-03-1 FAN COWL DOOR HINGE FITTING437 GVI438447448

Y

GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGEFITTINGSNOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 711300-01-3.

Skills :B21 0.00 MHrs

ALI 712111-03-2AMM 712112/6AMT 712112-200-010

T 9 000 FHT 4 500 CYI 9 000 FHI 4 500 CY

ALL712111-03-2 FORWARD ENGINE MOUNT435 DI436445446451461

Y

DETAILED INSPECTION OF FORWARD ENGINE MOUNTINSTALLATION

Access panels :



Skills :B21 0.00 MHrsEN1 0.60 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALL712111-06-1 FORWARD ENGINE MOUNT450 SDI460

N

SPECIAL DETAILED INSPECTION (TC) OF FWD ENGINE MOUNTPYLON BOLTS.NOTE: IN CASE TASK THRESHOLD IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT IS AT 2500 FC OR5000 FH SINCE 04/04/2012.Access panels :



ALI 712112-02-1AMM 712112-200-805

T 15 000 FHT 7 500 CYI 15 000 FHI 7 500 CY

ALL712112-02-1 FORWARD ENGINE MOUNT450 SDI460

N

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF FORWARDENGINE MOUNT LINK LUGS.NOTE: IN CASE TASK THRESHOLD IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT IS AT 2500 FC OR5000 FH SINCE 04/04/2012.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 712211/6AMT 712211-200-010

T 15 000 FHT 7 500 CYI 15 000 FHI 7 500 CY

ALL712211-04-1 AFT ENGINE MOUNT451 DI453454461463464

Y

DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION

Access panels :



Skills :EN1 0.60 MHrs


ALL712211-06-1 AFT ENGINE MOUNT450 SDI460

N

SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNTPYLON BOLTSNOTE: IN CASE TASK THRESHOLD IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT IS AT 2500 FC OR5000 FH SINCE 04/04/2012.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

ALI 712212-02-1AMT 712211-200-803

T 15 000 FHT 7 500 CYI 15 000 FHI 7 500 CY

ALL712212-02-1 AFT ENGINE MOUNT450 SDI460

N

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINEMOUNT LINK LUGSNOTE: IN CASE TASK THRESHOLD IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT IS AT 2500 FC OR5000 FH SINCE 04/04/2012.Access panels :



ALI 712213-02-1AMM 712211-200-804

T 15 000 FHT 7 500 CYI 15 000 FHI 7 500 CY


N

DETAILED INSPECTION OF AFT ENGINE MOUNT PINSNOTE: IN CASE TASK THRESHOLD IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT IS AT 2500 FC OR5000 FH SINCE 04/04/2012.Access panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 78 ENGINE EXHAUST


Threshold Interval

Ctrl References Eff

ALI 783200-03-1AMM 783200/6AMT 783200-200-011

T 3 000 CYI 3 000 CY

ALL783200-03-1 "C" DUCT HINGE FITTING451 GVI452461462

N

GENERAL VISUAL INSPECTION OF "C" DUCT HINGE FITTINGSNOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 783200-01-3.Access panels :

451AL 452AR 461AL 462AR0.12Total access time : Hrs



: : :

: :

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01



Date : SEP 2013 LIST OF EFFECTIVE PAGES - CMR Page : 1


LEP R 1 SEP 2013

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 21 AIR CONDITIONING / PRESSURIZATION


Threshold Interval

Ctrl References Eff

AMM 213100/5AMT 213100-720-001CMR 213100-00001-1-CCMR 213100-00001-2-CCMR 213100-00001-3-CMRB 213100/06

I 24 000 FHI 80 MO

ALL213100-05-1 PRESSURE CONTROL AND MONITORING210 FNT N

PRESSURE CONTROL AND MONITORINGFUNCTIONAL CHECK OF POSITIVE/NEGATIVE DELTA "P"PROTECTION OF THE SAFETY VALVES.NOTE:- THE FUNCTIONAL CHECK MAY ALTERNATIVELY BE ACCOMPLISHED AS AN OFF AIRCRAFTTASK.- THE CHECK OF POSITION INDICATION OF SAFETY VALVES IS PART OF THIS TASKAFTER THE FUNCTIONAL CHECK/RE-INSTALLION.PREP: ACCESS THROUGH REAR GALLEY WALL REQUIRED;Access panels :

312AR0.02Total access time : Hrs


Date ATA 21Date 22/01/2014Amendment NoIssue No Page CMR - 21 [1 / 1] :

: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 24 ELECTRICAL POWER


Threshold Interval

Ctrl References Eff

AMM 242800/5AMT 242800-710-001MRB 242000/17MRB 243000/10MRB 245000/08

I 750 FHI 6 MO

ALL242800-01-2 STATIC INVERTER210 OPT N

OPERATIONAL CHECK OF STATIC INVERTER CMR**

Skills :B21 0.00 MHrsEL1 0.10 MHrs


: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 26 FIRE PROTECTION


Threshold Interval

Ctrl References Eff

AMM 262300/5AMT 262300-720-001MRB 26.23.00/03

I 12 000 FHI 80 MO

ALL262300-02-3 CARGO COMPARTMENT FIRE EXTINGUISHING132 OPT N

CHECK FIRING CIRCUIT CONTINUITY. CMR**NOTE: CREDIT CAN BE TAKEN FROM DELETED TASK 262300-02-1Access panels :

132MW 8250.06Total access time : Hrs


AMM 262300/6AMT 262300-200-001MRB 262300/04

I 18 000 FHI 120 MO

ALL262300-03-3 CARGO COMPARTMENT FIRE EXTINGUISHING132 FUC N

CHECK FIRE EXTINGUISHER LINES FOR LEAKAGE AND CMR**OBSTRUCTIONNOTE: CREDIT CAN BE TAKEN FROM DELETED TASK 262300-03-1Access panels :


Skills :CA2 2.00 MHrs


: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 27 FLIGHT CONTROLS - GENERAL


Threshold Interval

Ctrl References Eff

AMM 279600/5AMT 279600-710-007MRB 271400/01

I 4 000 FHI 36 MO

ALL271400-01-1 AILERON AND HYDRAULIC ACTUATION210 OPT N

OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE CMR**


AMM 271400/6AMT 271400-220-002MRB 271400/02

I 15 000 FHI 100 MO

ALL271400-03-1 AILERON AND HYDRAULIC ACTUATION575 OPC675

Y

CHECK AILERON SERVO CONTROLS FLUID RESERVE CMR**PISTON POSITION WITH HYDRAULIC RESERVOIRDEPRESSURIZEDAccess panels :

575KB 675KB0.08Total access time : Hrs


AMM 279600/5AMT 279600-710-008MRB 273400/01

I 4 000 FHI 36 MO

ALL273400-01-1 ELEVATOR AND HYDRAULIC ACTUATION210 OPT N

OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE CMR**



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 273400/6AMT 273400-220-001MRB 273400/02

I 15 000 FHI 100 MO

ALL273400-03-1 ELEVATOR AND HYDRAULIC ACTUATION334 OPC344

Y

CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC CMR**RESERVOIR DEPRESSURIZED.Access panels :

334DB 344DB0.06Total access time : Hrs


AMM 274400/5AMT 274400-710-002MRB 274000/01

I 750 FH ALL274000-02-1 TRIMMABLE HORIZONTAL STABILIZER210 OPT N

OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL CMR**HYDRAULIC SYSTEMS


AMM 274400/5AMT 274400-710-001MRB 274000/02

I 4 000 FHI 80 MO

ALL274000-03-1 TRIMMABLE HORIZONTAL STABILIZER210 OPT N

OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION CMR**DEVICEAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 274451/6AMT 274451-280-001MRB 274000/16

I 12 000 FHI 80 MO

ALL274451-08-1 THS ACTUATOR310 CHK N

CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT CMR*(PRIMARY AND SECONDARY LOAD PATH)Access panels :



AMM 275100/5AMT 275100-710-001MRB 275000/04MRB 275001/04

I 7 500 FHI 50 MO

ALL275100-01-2 FLAPS210 OPT N

OPERATIONAL CHECK OF WTB/POB CMR**NOTE : FLAP SURFACES MOVE AUTOMATICALLY

Access panels :

575DB 575EB 575FB 675DB 675EB 675FB0.12Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 275400/6AMT 275400-210-002MRB 275000/04MRB 275001/04

I 7 500 FHI 50 MO

ALL275100-03-1 FLAPS575 DI675

Y

CHECK OF FLAPS TRANSMISSION SHAFTING INTEGRITY, CMR**INCLUDING INSPECTION OF SEAL WITNESS DRAINS.

Access panels :

571AB 573AB 573BB 573CB 575AB 575BB 575CB575DB 575EB 575FB 575GB 671AB 673AB 673BB673CB 675AB 675BB 675CB 675DB 675EB 675FB675GB 734 744



AMM 278100/5AMT 278100-710-001MRB 27.80.00/04

I 7 500 FHI 48 MO

ALL278100-03-1 SLATS520 OPT620

N

OPERATIONAL CHECK OF WTB/POB CMR**



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 278400-210-002MRB 27.80.00/04

I 7 500 FHI 48 MO

ALL278100-04-1 SLATS520 DI620

N

CHECK OF SLATS TRANSMISSION SHAFTING INTEGRITY, CMR**INCLUDING INSPECTION OF SEAL WITNESS DRAINSNOTE: CREDIT CAN BE GIVEN FOR PREVIOUS ACCOMPLISHMENT OF TASK 278100-03-1Access panels :

191EB 191KB 192EB 192KB 521AT 521CB 521EB521GB 521HB 522AB 522CB 522EB 522FB 522LB522NB 522QB 522SB 522UB 621AT 621CB 621EB621GB 621HB 622AB 622CB 622EB 622FB 622LB622NB 622QB 622SB 622UB 734 744



AMM 279600/5AMT 279600-710-018MRB 27.90.00/02MRB 27.90.00/05

I 400 FHI 80 DY

ALL279000-05-1 ELECTRICAL FLIGHT CONTROL SYSTEM210 OPT B2

OPERATIONAL CHECK : CMR*- OF LOGICS ACTIVATING ELAC 1, ELAC 2, AND SEC.1STANDBY POWER SUPPLIES- TO CONFIRM ABILITY OF SEC.1 AND SEC.2 TO ACHIEVEPITCH CONTROL- TO CONFIRM ABILITY OF SIDESTICK PRIORITY FUNCTION

Skills :AV2 0.80 MHrsB21 0.00 MHrs


: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 29 HYDRAULIC POWER


Threshold Interval

Ctrl References Eff

AMM 291000/6AMT 291000-220-002MRB 29.10.00/05MRB 29.10.00/12

I 7 500 FHI 50 MO

ALL291900-02-1 GROUND INTERNAL LEAK TEST BLUE SYSTEM210 FNT Y

FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF CMR*BLUE HYDRAULIC SYSTEM


AMM 292200/5AMT 292200-720-003MRB 24.50.00/10MRB 29.10.00/29

I 3 600 FHI 18 MO

ALL292000-04-1 AUXILIARY HYDRAULIC POWER190 FUC Y

OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND CMR*FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT,FOLLOWED BY CHECK OF FILTER INDICATORAccess panels :

195BB 197EB0.04Total access time : Hrs


AMM 292200/5AMT 292200-710-006MRB 291000/08

I 3 600 FHI 18 MO

ALL292000-05-1 AUXILIARY HYDRAULIC POWER210 OPT N

OPERATIONAL CHECK OF RAM AIR TURBINE (RAT) AUTOMATIC CMR*DEPLOYMENT.Access panels :

197EB0.02Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 292200-220-002MRB 29.10.00-34

I 3 600 FHI 18 MO

ALL292000-09-1 AUXILIARY HYDRAULIC POWER190 DI N

DETAILED INSPECTION OF RAT BLADES FOR EVIDENCE CMR*OF PLATING CRACKSNOTE: THIS TASK IS ONLY APPLICABLE FOR RAT WITH P/N: 762308Access panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 32 LANDING GEAR


Threshold Interval

Ctrl References Eff

AMM 324300/5AMT 324300-710-802MRB 324000/08

I 6 000 FHI 40 MO

See note

ALL324300-01-1 ALTERNATE BRAKING SYSTEM210 OPT N

OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEMNOTE: - TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE - ACCOMPLISHMENT OF THIS TASK WILL ALSO COVER 324300-01-2 ON AIRCRAFT PRE 26925.


AMT 324300-710-802I 5 600 FHI 40 MO

See note

2255

22612267

2303

2480

324300-01-2 ALTERNATE BRAKING SYSTEM210 OPT N

ALTERNATE BRAKING SYSTEMOPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEMNOTE: TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE.



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 35 OXYGEN


Threshold Interval

Ctrl References Eff

AMM 352300/5AMT 352300-710-001MRB 352000/01

I 8 500 FHI 80 MO

ALL352000-01-1 PASSENGER OXYGEN (CHEMICAL)200 OPT Y

OPERATIONAL CHECK OF MANUAL MASK RELEASE CMR**


AMM 352300/5AMT 352300-720-003MRB 352000/02

I 24 000 FHI 74 MO

ALL352000-02-1 PASSENGER OXYGEN (CHEMICAL)200 FNT N

FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE, CMR**DETAILED INSPECTION OF MASKS AND VISUAL CHECKOF CHEMICAL OXYGEN GENERATORS



: : :

: :

1412/09/2013

01



Date : SEP 2013 LIST OF EFFECTIVE PAGES - SYS Page : 1

SECTION MVT PAGE DATE

LEP R 1 SEP 2013

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : VN VIETNAM AIRLINES


Threshold Interval

Ctrl References Eff

TRCheck : ALLVN257000-01 SECURITY BOX160 CHK N

CARRY OUT A CHECK OF SECURITY BOX FORGENERAL CONDITION

AMT 324227-210-003I 750 FHI 4 MO

ACheck :

ALLVN320000-01 MAIN LDG BRAKES700 GVI N

INSPECTION/CHECK MAIN LANDING GEAR BRAKES.CARRY OUT THE WEAR INDICATOR PIN MEASUREMENT AND RECORD.


AMM 313600/2AMT 313600-740-015

I 1 500 FH2ACheck :

ALLVN491000-01 APU ENGINE - RECORD HOURS & CYCLES210 CHK N

APU ENGINE - RECORD HOURS & CYCLES


Date ATA VNDate 22/01/2014Amendment NoIssue No Page SYS - VN [1 / 1] :

: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 08 LEVELING / WEIGHING


Threshold Interval

Ctrl References Eff

AMT 081000-200-001T 4 YEI 4 YE

ALL080000-81-1 AIRCRAFT WEIGHING210 CHK N

CHECK AIRCRAFT WEIGHING

Date ATA 08Date 22/01/2014Amendment NoIssue No Page SYS - 08 [1 / 1] :

: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 20 STANDARD PRACTICE


Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-023MRB L/HIRF-20-00-01-2MRB L/HIRF-20-00-01-3MRB L/HIRF20-00-01-2MRB L/HIRF20-00-01-3

I 72 MO ALL200001-02-1 HIRF/LIGHTNING PROTECTION-WING511 CHK520611620

N

CHECK THAT THE CONNECTOR IS CORRECTLY TIGHTENEDBY MEASUREMENT OF THE RESISTANCE WITH A LOOPTESTER:- 4005VC, 4007VC, 4009VC, 4011VC, LH SIDE- 4013VC, 4015VC, 4017VC, 4019VC, LH SIDE- 4006VC, 4008VC, 4010VC, 4012VC, RH SIDE- 4014VC, 4016VC, 4018VC, 4020VC, RH SIDEPREP. : SLATS FULLY EXTENDEDAccess panels :

521EB 521GB 522AB0.27Total access time : Hrs

Skills :EL1 2.00 MHrs

AMM 249200/6AMT 249200-210-018MRB L/HIRF-20-00-02-1

I 36 MO ALL200002-01-1 HIRF/LIGHTNING PROTECTION-THS T/E334 GVI344

N

GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ONTHE FOLLOWING HARNESSES :- 405VB, 406VB, 407VB, 408VB, 409VB, LH SIDE- 400VB, 401VB, 402VB, 403VB, 404VB, RH SIDEAccess panels :

334AB 334BB 334CB 334DB 334EB 344AB 344BB344CB 344DB 344EB




: : :

: :

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01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-019MRB L/HIRF-20-00-03-1

I 72 MO ALL200003-01-1 HIRF/LIGHTNING PROTECTION-VERTICAL FIN321 GVI N

GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ONTHE FOLLOWING HARNESSES :- 4202VB, 4204VBAccess panels :

321AL0.35Total access time : Hrs


AMM 249200/6AMT 249200-210-020MRB L/HIRF-20-00-03-2



322BL0.37Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-021MRB L/HIRF-20-00-03-3



324AT0.18Total access time : Hrs


AMM 249200/7AMT 249200-100-004MRB 20.0.121/01

I 48 MO ALL200121-01-1 FORWARD AVIONIC COMPARTMENT121 RST122

N

CLEANING OF EWIS INSTALLED IN THE FORWARD AVIONICCOMPARTMENT (ONLY IF CONTAMINATED)(EWIS)Access panels :

121AF 121AL 121BF 121CF 122BF 8110.15Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-027MRB 20.0.121/02

I 48 MO ALL200121-02-1 FORWARD AVIONIC COMPARTMENT121 GVI122

N

GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEFORWARD AVIONIC COMPARTMENT (EWIS)Access panels :



AMM 249200/6AMT 249200-210-028MRB 20.0.121/03

I 72 MO ALL200121-03-1 FORWARD AVIONIC COMPARTMENT121 GVI122

N

GENERAL VISUAL INSPECTION OF 90, 108, 109 VUIN THE FORWARD AVIONIC COMPARTMENT (EWIS)Access panels :

121AL 811 812 8220.08Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-220-005MRB 20.0.121/04

I 72 MO ALL200121-04-1 FORWARD AVIONIC COMPARTMENT121 DI122

N

DETAILED INSPECTION OF G, E AND P ROUTES IN THEFORWARD AVIONIC COMPARTMENT (EWIS)PREP. : FLOOR PANELS FROM FR 1 TO FR 9 REMOVED;Access panels :



AMM 249200/7AMT 249200-100-031MRB 20.0.125/01

I 72 MO ALL200125-01-1 LATERAL AVIONIC COMPARTMENT125 RST126

N

CLEANING OF EWIS INSTALLED IN THE LATERAL AVIONICCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : 813 IF INSTALLED;Access panels :

812 822 824 8310.09Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-808MRB 20.0.125/03

I 48 MO ALL200125-03-1 LATERAL AVIONIC COMPARTMENT125 GVI126

N

GENERAL VISUAL INSPECTION OF EWIS INSTALLEDIN THE LATERAL AVIONIC COMPARTMENT (EWIS)PREP. : 813 IF INSTALLED;Access panels :



AMM 249200/6AMT 249200-210-030MRB 20.0.125/05

I 72 MO ALL200125-05-1 LATERAL AVIONIC COMPARTMENT125 GVI126

N

GENERAL VISUAL INSPECTION OF 105, 106, 103, 107AND 70 VUS INSTALLED IN THE LATERAL AVIONICCOMPARTMENT (EWIS)PREP. : 103VU; 105VU; 106VU; 107VU;Access panels :

812 822 8310.06Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-220-008MRB 20.0.125/06

I 72 MO ALL200125-06-1 LATERAL AVIONIC COMPARTMENT125 DI126

N

DETAILED INSPECTION OF G, E AND P ROUTES INSTALLEDIN THE LATERAL AVIONIC COMPARTMENT (EWIS)PREP. : FLOOR PANELS FROM FR 9 TO FR 16 REMOVED; 813 IF INSTALLED;Access panels :



AMT 249200-100-013MRB 20.0.127/02

I 72 MO ALL200127-02-1 REAR AVIONIC COMPARTMENT127 RST128

N

CLEANING OF EWIS INSTALLED IN THE REAR AVIONICCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)NOTE: CREDIT CAN BE TAKEN FROM DELETED TASK 200127-01-1Access panels :

127BF 127BG 127CF 127DF 128CF 128EG 131AW131BW 131CW 131DW 132BW 132EW 824 825




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 249200-210-033MRB 20.0.127/04


N

GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THEREAR AVIONIC COMPARTMENT (EWIS)NOTE: CREDIT CAN BE TAKEN FROM DELETED TASK 200127-03-1Access panels :




AMM 249200/6AMT 249200-210-034MRB 20.0.127/05

I 72 MO ALL200127-05-1 REAR AVIONIC COMPARTMENT127 GVI128

N

GENERAL VISUAL INSPECTION OF 80, 63, 187, 188 VUINSTALLED IN THE REAR AVIONIC COMPARTMENT (EWIS)PREP. : PARTITION WALL PANELS ON FR 24A; 63VU;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 249200-220-007MRB 20.0.127/07


N

DETAILED INSPECTION OF G, E AND P ROUTES INSTALLEDIN THE REAR AVIONIC COMPARTMENT (EWIS)PREP. : FLOOR PANELS FROM FR 20 TO FR 24;NOTE: CREDIT CAN BE TAKEN FROM DELETED TASK 200127-06-1Access panels :

127BF 127BG 127CF 127DF 128EG 128GF 131AW131BW 131CW 131DW 132BW 132EW 824 825



AMM 249200/7AMT 249200-100-025MRB 20.0.131/01

I 72 MO ALL200131-01-1 FORWARD CARGO COMPARTMENT131 RST132

N

CLEANING OF EWIS INSTALLED IN THE FORWARD CARGOCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : SIDEWALL AND CEILING PANELS REMOVED;



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-805MRB 20.0.131/02

I 144 MO ALL200131-02-1 FORWARD CARGO COMPARTMENT131 GVI132

N

GENERAL VISUAL INSPECTION OF G, E AND P ROUTESINSTALLED IN THE FORWARD CARGO COMPARTMENT (EWIS)PREP. : SIDEWALL AND CEILING PANELS REMOVED;Access panels :



AMM 249200/7AMT 249200-100-024MRB 20.0.133/01

I 72 MO ALL200133-01-1 UNDERFLOOR BAY OF FWD CARGO COMPARTMENT133 RST134

N

CLEANING OF EWIS INSTALLED INTHE UNDERFLOOR BAY OF FORWARD CARGOCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : FLOOR PANELS;Access panels :

133AL 134AR 8250.07Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-029MRB 20.0.137/01

I 72 MO ALL200137-01-1 BAY BEHIND FWD CARGO COMPARTMENT137 RST138

N

CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWDCARGO COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : ACT(S) NO.4 AND NO.6 REMOVED (IF INSTALLED);Access panels :

131NW 131PW 132PW 8250.11Total access time : Hrs


AMM 249200/6AMT 249200-210-026MRB 20.0.141/01

I 144 MO ALL200141-01-1 WING CENTRE BOX141 GVI142

N

GENERAL VISUAL INSPECTION OF EXPOSED EWISINSTALLED IN THE WING CENTRE BOX (EWIS)Access panels :

147AZ 148AZ 734 7440.10Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-015MRB 20.0.145/01

I 72 MO ALL200145-01-1 ZONE UNDER CABIN FLOOR145 RST146

N

CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABINFLOOR (ONLY IF CONTAMINATED) (EWIS)PREP. : FLOOR PANELS FROM FR 36 TO FR 46;Access panels :



AMM 249200/7AMT 249200-100-026MRB 20.0.151/01

I 72 MO ALL200151-01-1 AFT CARGO COMPARTMENT151 RST152

N

CLEANING OF EWIS INSTALLED IN THE AFT CARGOCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : SIDEWALL PANELS FROM FR 46 TO FR 59; ACT(S) REMOVED (IF INSTALLED);Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-806MRB 20.0.151/02

I 144 MO ALL200151-02-1 AFT CARGO COMPARTMENT151 GVI152

N

GENERAL VISUAL INSPECTION OF P ROUTES INSTALLED INAFT CARGO COMPARTMENT (EWIS)PREP. : ACT(S) REMOVED (IF INSTALLED); CEILING PANELS FROM FR 46 TO FR 59; SIDEWALL PANELS FROM FR 46 TO FR 59;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-046MRB 20.0.151/03

I 72 MO 29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

200151-03-1 AFT CARGO COMPARTMENT151 GVI152

N

GENERAL VISUAL INSPECTION OF EWIS INSTALLED AT THEACT(S) (EWIS)PREP.: ACT;NOTE : THIS TASK COULD BE PERFORMED AT THE OPPORTUNITY OF R/I THE INTERVAL IS 72 ATC MO



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-030MRB 20.0.161/01

I 72 MO ALL200161-01-1 BULK CARGO COMPARTMENT161 RST162

N

CLEANING OF EWIS INSTALLED IN THE BULK CARGOCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : SIDEWALL PANELS FROM FR 59 TO FR 65; ACT(S) REMOVED (IF INSTALLED);Access panels :



AMM 249200/7AMT 249200-100-001MRB 20.0.171/01

I 144 MO ALL200171-01-1 AFT CABIN UNDERFLOOR COMPARTMENT171 RST172

N

CLEANING OF EWIS INSTALLED IN THE AFT CABINUNDERFLOOR COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)PREP. : ACT NO.5 REMOVED (IF INSTALLED); CABIN FLOOR PANELS FROM FR 65 TO FR 70;Access panels :

161DW 162DW 171AL 172AR 8260.11Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-027MRB 20.0.191/01

I 72 MO ALL200191-01-1 AIR CONDITIONING COMPARTMENT & FAIRINGS191 RST192

N

CLEANING OF EWIS INSTALLED IN THE AIR CONDITIONINGCOMPARTMENT AND FAIRINGS (ONLY IF CONTAMINATED)(EWIS)Access panels :

191AB 191AT 191BT 191CT 191DT 191EB 191ET191GB 191HB 191JB 191KB 191LB 192AB 192AT192BT 192CT 192DT 192EB 192ET 192FB 192KB192LB 192MB



AMM 249200/7AMT 249200-100-016MRB 20.0.211/01

I 144 MO ALL200211-01-1 COCKPIT211 RST212

N

CLEANING OF EWIS INSTALLED IN THE COCKPIT(ONLY IF CONTAMINATED) (EWIS)Access panels :

211BC 211FC 211HC 8310.08Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-017MRB 20.0.211/02

I 72 MO ALL200211-02-1 COCKPIT211 RST212

N

CLEANING OF EWIS INSTALLED IN 49VU AND 120VU(ONLY IF CONTAMINATED) (EWIS)PREP. : 120VU; 49VU;Access panels :



AMM 249200/6AMT 249200-210-035MRB 20.0.211/03

I 144 MO ALL200211-03-1 COCKPIT211 GVI212

N

GENERAL VISUAL INSPECTION OF EWISOF 49VU AND THE 120VU (EWIS)PREP. : 120VU; 49VU;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-007MRB 20.0.221/01

I 144 MO ALL200221-01-1 FORWARD CABIN UTILITY AREA221 RST222

N

CLEANING OF EWIS INSTALLED IN THE FORWARDCABIN UTILITY AREA (ONLY IF CONTAMINATED) (EWIS)PREP. : DOOR FRAME LINING REMOVED; FLOOR PANELS FROM FR 12 TO FR 20; FURNISHINGS FROM FR 12 TO FR 20; GALLEYS AND TOILETS REMOVED; SEATS REMOVED;Access panels :



AMM 249200/7AMT 249200-100-010MRB 20.0.223/01

I 144 MO ALL200223-01-1 FORWARD CABIN OVERHEAD COMPARTMENT223 RST224

N

CLEANING OF EWIS INSTALLED IN THE FORWARDCABIN OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)PREP. : CEILING PANELS FROM FR 12 TO FR 20; GALLEYS AND TOILETS REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-029MRB 20.0.223/02

I 144 MO ALL200223-02-1 FORWARD CABIN OVERHEAD COMPARTMENT223 GVI224

N

GENERAL VISUAL INSPECTION OF EWISOF THE 2000VU (EWIS)PREP. : 2000VU;Access panels :



AMM 249200/7AMT 249200-100-012MRB 20.0.231/02

I 144 MO ALL200231-02-1 FORWARD PASSENGER COMPARTMENT231 RST232

N

CLEANING OF EWIS INSTALLED IN THE FORWARDPASSENGER COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)PREP. : DOOR FRAME LINING REMOVED; FURNISHINGS; GALLEYS; SEATS REMOVED; SIDEWALL PANELS FROM FR 20 TO FR 35.8; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-036MRB 20.0.231/03

I 72 MO ALL200231-03-1 FORWARD PASSENGER COMPARTMENT231 GVI232

N

GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEENSEAT AND A/C INSTALLED IN THE FORWARD PASSENGERCOMPARTMENT (EWIS)NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS AND WITH EWIS BETWEEN SEAT AND A/C ONLYAccess panels :



AMM 249200/7AMT 249200-100-011MRB 20.0.233/02

I 144 MO ALL200233-02-1 FORWARD PASSENGER COMPARTMENT OVERHEAD233 RST234

N

COMPARTMENTCLEANING OF EWIS INSTALLED IN THE FORWARDPASSENGER COMPARTMENT OVERHEAD COMPARTMENT(ONLY IF CONTAMINATED) (EWIS)PREP. : CEILING PANELS FROM FR 20 TO FR 35.8; GALLEYS AND TOILETS REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-811MRB 20.0.233/04

I 144 MO ALL200233-04-1 FORWARD PASSENGER COMPARTMENT OVERHEAD233 GVI234

N

COMPARTMENTGENERAL VISUAL INSPECTION OF ALL G & P ROUTESINSTALLED IN THE FORWARD PASSENGERCOMPARTMENT OVERHEAD COMPARTMENT (EWIS)PREP. : CEILING PANELS FROM FR 20 TO FR 35.8; GALLEYS AND TOILETS REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED;Access panels :



AMM 249200/7AMT 249200-100-008MRB 20.0.241/02

I 144 MO ALL200241-02-1 CENTER PASSENGER COMPARTMENT241 RST242

N

CLEANING OF EWIS INSTALLED IN THE CENTERPASSENGER COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)PREP. : FURNISHINGS; GALLEYS AND TOILETS REMOVED; SEATS REMOVED; SIDEWALL PANELS FROM FR 35.8 TO FR 47;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-031MRB 20.0.241/03

I 144 MO ALL200241-03-1 CENTER PASSENGER COMPARTMENT241 GVI242

N

GENERAL VISUAL INSPECTION OF G ROUTES INSTALLEDAT FR 47 (EWIS)PREP. : LINING AT FR 47, RH ONLY; GALLEY & TOILET IF INSTALLED;Access panels :



AMM 249200/6AMT 249200-210-037MRB 20.0.241/04

I 72 MO ALL200241-04-1 CENTER PASSENGER COMPARTMENT241 GVI242

N

GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEENSEATS AND A/C INSTALLED IN THE CENTER PASSENGERCOMPARTMENT (EWIS)NOTE : THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS BETWEEN SEAT AND A/C ONLYPREP.: SEAT COVERS REMOVED AS NECESSARY;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-014MRB 20.0.243/02

I 144 MO ALL200243-02-1 CENTER PASSENGER OVERHEAD COMPARTMENT243 RST244

N

CLEANING OF EWIS INSTALLED IN THE CENTERPASSENGER OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)PREP. : CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 35.8 TO FR 47.1; GALLEY & TOILET IF INSTALLED;Access panels :



AMM 249200/6AMT 249200-210-038MRB 20.0.243/04

I 144 MO ALL200243-04-1 CENTER PASSENGER OVERHEAD COMPARTMENT243 GVI244

N

GENERAL VISUAL INSPECTION OF G AND P ROUTESINSTALLED IN THE CENTER PASSENGER OVERHEADCOMPARTMENT (EWIS)PREP. : CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 35.8 TO FR 47.1;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-018MRB 20.0.251/01

I 144 MO ALL200251-01-1 AFT PASSENGER COMPARTMENT251 RST252

N

CLEANING OF EWIS INSTALLED IN THE AFT PASSENGERCOMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : DOOR FRAME LINING REMOVED; GALLEYS AND TOILETS REMOVED; SIDEWALL PANELS FROM FR 47 TO FR 64 REMOVED;Access panels :



AMM 249200/6AMT 249200-210-039MRB 20.0.251/03

I 72 MO ALL200251-03-1 AFT PASSENGER COMPARTMENT251 GVI252

N

GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEENSEATS AND A/C INSTALLED IN THE AFT PASSENGERCOMPARTMENT (EWIS)NOTE : THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS BETWEEN SEAT AND A/C ONLYPREP.: SEAT COVERS REMOVED AS NECESSARY;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-021MRB 20.0.253/01

I 144 MO ALL200253-01-1 AFT PASSENGER OVERHEAD COMPARTMENT253 RST254

N

CLEANING OF EWIS INSTALLED IN THE AFT PASSENGEROVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 47 TO FR 64 REMOVED; GALLEY & TOILET IF INSTALLED;Access panels :



AMM 249200/6AMT 249200-210-042MRB 20.0.253/02

I 144 MO ALL200253-02-1 AFT PASSENGER OVERHEAD COMPARTMENT253 GVI254

N

GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLEDIN THE AFT PASSENGER OVERHEAD COMPARTMENT (EWIS)PREP. : CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 47 TO FR 64 REMOVED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/7AMT 249200-100-022MRB 20.0.261/01

I 144 MO ALL200261-01-1 AFT CABIN UTILITY AREA261 RST262

N

CLEANING OF EWIS INSTALLED IN THE AFT CABINUTILITY AREA (ONLY IF CONTAMINATED) (EWIS)PREP. : SEATS REMOVED; SIDEWALL PANELS FROM FR 64 TO FR 70; GALLEY & TOILET IF INSTALLED;Access panels :



AMM 249200/6AMT 249200-210-044MRB 20.0.261/02

I 144 MO ALL200261-02-1 AFT CABIN UTILITY AREA261 GVI262

N

GENERAL VISUAL INSPECTION OF P ROUTES INSTALLEDIN THE AFT CABIN UTILITY AREA (EWIS)PREP. : LINING AT FR 67; GALLEY & TOILET IF INSTALLED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-040MRB 20.0.261/03

I 72 MO ALL200261-03-1 AFT CABIN UTILITY AREA261 GVI262

N

GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEENSEATS AND A/C INSTALLED IN THE AFT CABIN UTILITYAREA (EWIS)NOTE : THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C ONLYPREP.: SEAT COVERS REMOVED AS NECESSARY;Access panels :



AMM 249200/7AMT 249200-100-023MRB 20.0.263/01

I 144 MO ALL200263-01-1 AFT CABIN OVERHEAD COMPARTMENT263 RST264

N

CLEANING OF EWIS INSTALLED IN THE AFT CABINOVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)PREP. : CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 64 TO FR 70; GALLEY & TOILET IF INSTALLED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-043MRB 20.0.263/02

I 144 MO ALL200263-02-1 AFT CABIN OVERHEAD COMPARTMENT263 GVI264

N

GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLEDIN THE AFT CABIN OVERHEAD COMPARTMENT (EWIS)PREP. : CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 64 TO FR 70;Access panels :



AMM 249200/6AMT 249200-210-045MRB 20.0.263/03

I 144 MO ALL200263-03-1 AFT CABIN OVERHEAD COMPARTMENT263 GVI264

N

GENERAL VISUAL INSPECTION OF ALL EWIS OF 2001 VU(EWIS)PREP. : CIRCUIT BREAKER PANEL;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-025MRB 20.0.315/01

I 24 MO ALL200315-01-1 TAIL CONE AND APU ACCESSORY COMPARTMENT315 GVI316

N

GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLEDIN THE TAIL CONE AND APU ACCESSORY COMPARTMENT (EWIS)Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-220-001MRB 20.0.413/01

I 24 MO 22552261

2267

23032480

2974

30053013

3022

31983315

3355

200413-01-1 UPPER FORWARD PYLON413 DI414423424

N

DETAILED INSPECTION OF EWIS INSTALLEDIN THE UPPER FORWARD PYLON (EWIS)

Access panels :

413AL 413BL 413CL 413DL 413EL 414AR 414AZ414BR 414CR 414FR 423AL 423AZ 423BL 423CL423DL 423FL 424AR 424BR 424CR 424ER




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-220-001MRB 20.0.413/03

I 24 MO 36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385

200413-03-1 UPPER FORWARD PYLON413 DI414423424

NR

DETAILED INSPECTION OF EWIS INSTALLEDIN THE UPPER FORWARD PYLON (EWIS)


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :

413AL 413AR 413BL 413BR 413CL 413CR 413DT414AZ 423AL 423AR 423AZ 423BL 423BR 423CL423CR 423DT 471AL 471AR 481AL 481AR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-220-003MRB 20.0.435/01

I 24 MO ALL200435-01-1 FAN AND ACCESSORY GEAR BOX435 DI436445446

N

DETAILED INSPECTION OF EWIS IN THE FAN ANDACCESSORY GEAR BOX (EWIS)

Access panels :



AMM 249200/6AMT 249200-220-004MRB 20.0.453/01

I 24 MO ALL200453-01-1 HOT SECTION453 DI454463464

N

DETAILED INSPECTION OF EWIS INSTALLEDIN THE HOT SECTION (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-801MRB 20.0.540/02

I 144 MO ALL200540-02-1 WING FUEL TANK540 GVI640

N

GENERAL VISUAL INSPECTION OF EXPOSED EWISWITHIN THE WING FUEL TANK (EWIS)Access panels :

521AZ 521BZ 540AB 540AZ 540BB 540BZ 540CB540DB 540EB 540FB 540GB 540HB 540JB 540KB540LB 540MB 540NB 540PB 540QB 540RB 621AZ621BZ 640AB 640AZ 640BB 640BZ 640CB 640DB640EB 640FB 640GB 640HB 640JB 640KB 640LB640MB 640NB 640PB 640QB 640RB



AMM 249200/6AMT 249200-210-802MRB 20.0.550/01

I 144 MO ALL200550-01-1 VENT SURGE TANK550 GVI650

N

GENERAL VISUAL INSPECTION OF EXPOSED EWISWITHIN THE VENT SURGE TANK (EWIS)Access panels :

550AB 550BB 550CB 550DB 650AB 650BB 650CB650DB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-803MRB 20.0.560/01

I 144 MO ALL200560-01-1 DRY BAY (OUTBOARD)560 GVI660

N

GENERAL VISUAL INSPECTION OF EXPOSED EWISWITHIN THE DRY BAY (OUTBOARD) (EWIS)Access panels :



AMM 249200/6AMT 249200-210-804MRB 20.0.571/01

I 144 MO ALL200571-01-1 MLG BAY571 GVI671

N

GENERAL VISUAL INSPECTION OF P ROUTE PUMPFEEDER (EWIS)PREP. : PUMP WIRING FAIRINGS;



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-024SIL 20-020

I 24 MO ALL202800-01-1 ELECTRICAL BONDING300 DI500600700800

N

DETAILED INSPECTION OF BONDING LEADS LOCATED ON THEFOLLOWING MOVABLE SURFACES: ELEVATOR, RUDDER, FLAPS,FLAP TRACK FAIRINGS, SLATS, SPOILERS, AILERONS,LANDING GEAR DOORS AND PASSENGER/CREW DOORSAccess panels :

325BL 325BR 325CL 325CR 325DL 325DR 325EL325ER 334BB 334DB 334FB 334GB 334HB 344BB344DB 344FB 344GB 344HB 521AB 522AB 522FB522NB 522SB 571AB 573AB 573BB 573CB 575AB575AT 575BB 575CB 575DB 575EB 575FB 575GB575KB 575LB 575MB 590AB 590BB 621AB 622AB622FB 622NB 622SB 671AB 673AB 673BB 673CB675AB 675AT 675BB 675CB 675DB 675EB 675FB675KB 675LB 675MB 690AB 831FZ 831GZ 832FZ832GZ 841FZ 841GZ 842FZ 842GZ




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 212149/7AMT 212149-100-001MRB 212100/05

I 24 000 FHI 160 MO

ALL212100-01-1 AIR DISTRIBUTION AND RECIRCULATION131 RST N

CLEAN COCKPIT AIR SUPPLY DUCTING GRID

Access panels :

131MW 131PW 8250.09Total access time : Hrs


AMM 212000/6AMT 212000-210-001MRB 212100/04

I 12 YE ALL212100-02-1 AIR DISTRIBUTION AND RECIRCULATION200 GVI Y

GENERAL VISUAL INSPECTION OF RISER DUCTS INTHE PASSENGER COMPARTMENT


AMM 212141/3AMT 212141-920-002MRB 212100/02

See noteNTCheck :

ALL212141-01-1 RECIRCULATION FILTER130 DIS N

DISCARD FILTER ELEMENTS OF RECIRCULATION SYSTEMNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST"IN SECTION 3 OF AMSAccess panels :

131PW 132PW0.06Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 212000/6AMT 212000-210-002MRB 212300/02

I 12 YE ALL212300-01-1 LAVATORY AND GALLEY VENTILATIONNT GVI Y

GENERAL VISUAL INSPECTION OF LAVATORY AND GALLEYVENTILATION DUCTING IN ZONES 210 THROUGH 260NOTE: WORKING ZONES 210, 220, 230, 240, 250, 260


AMM 212300/3AMT 212300-600-001MRB 212300/03

I 1 000 FHI 12 MO

ALL212300-02-1 LAVATORY AND GALLEY VENTILATION200 DIS Y

DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENTNOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.


AMM 212600/5AMT 212600-710-001MRB 212600/02MRB 261500/01

I 750 FHI 6 MO

ALL212600-01-1 AVIONICS EQUIPMENT VENTILATION210 OPT N

OPERATIONAL CHECK OF SYSTEM VIA MCDU



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 212600/5AMT 212600-710-002MRB 212600/03

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


OPERATIONAL CHECK OF OVERRIDE FUNCTION (BLOWER ANDEXTRACT)


AMM 212600/5AMT 212600-710-003MRB 212600/04

I 7 500 FHI 50 MO


OPERATIONAL CHECK OF SMOKE CONFIGURATION CONTROLCIRCUIT


AMM 212600/5AMT 212600-710-004MRB 212600/05

I 15 000 FHI 100 MO


OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROLCIRCUIT



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 212642/6AMT 212642-200-003MRB 212600/06

I 24 000 FHI 160 MO

ALL212600-05-1 AVIONICS EQUIPMENT VENTILATION120 DI Y

DETAILED INSPECTION OF SKIN HEAT EXCHANGER DRAIN HOSECONNECTION AREAAccess panels :



AMM 212642/6AMT 212642-210-001MRB 212600/08

I 24 000 FHI 160 MO


DETAILED INSPECTION OF DEMISTER DRAIN HOSE CONNECTIONAREA


AMM 212642/6AMT 212642-210-002SIL 21-074

I 24 000 FHI 160 MO


DETAILED INSPECTION OF ELBOW DRAIN HOSECONNECTION AREA DOWNSTREAM OF BLOWER FANPREP. : ELBOW DUCT DOWNSTREAM OF BLOWER FANAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 212656/5AMT 212656-280-002MRB 212600/16

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


OPERATIONAL CHECK OF AIR INLET CHECK VALVE 2150 HM


AMM 122113/7AMT 122113-100-002MRB 212600/19

I 40 MO ALL212600-09-1 AVIONICS EQUIPMENT VENTILATION120 CLN N

CLEAN GRID OF RELAY BOX VU PANELSNOTE: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.


AMM 212643/3AMT 212643-600-016MRB 212600/21

I 3 600 FHI 24 MO

See note

ALL212600-11-1 AVIONICS EQUIPMENT VENTILATION127 DIS N

AVIONICS EQUIPMENT VENTILATIONDISCARD DEMISTER FILTER ELEMENT AND FILTER CARTRIDGE(LE BOZEC). APPLICABILITY WITH PN:402K200-XAccess panels :


Skills :B21 0.00 MHrsIN1 0.10 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 212641/6AMT 212641-210-001MRB 212600/07

I 6 YE ALL212641-01-1 AVIONICS EQUIPMENT VENTILATION128 DI Y

DETAILED INSPECTION OF CHECK VALVE FLAPPERS FORCONDITION AND OPERATIONAccess panels :



AMT 212652-000-802SIL 21-159

NTCheck : ALL212652-01-1 AVIONICS VENT SKIN AIR INLET VALVE 824 RST N

(SAOV)REMOVE SKIN AIR INLET VALVE FOR OVERHAULNOTE 1: TASK APPLICABILITY FOR AIRCRAFT INTALLED P/N VFT210B00 OR P/NVFT210A2NOTE 2: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOF AMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMSISS13 AMD 00 EFFECTIVE DATE IS NEXT C CHECK.Access panels :


Skills :MEC1 1.32 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 212653/4AMT 212653-000-001MRB 212600/23SIL 21-099

NTCheck : ALL212653-01-1 AVIONICS VENT SKIN AIR OUTL VLV(SAOV)126 OVH Y

REMOVE SKIN AIR OUTLET VALVE FOR OVERHAUL.NOTE 1: TASK APPLICABILITY FOR AIRCRAFT INSTALLED P/N: VFT300A1.NOTE 2: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOF AMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS14 AMD 00 EFFECTIVE DATE IS NEXT C CHECK.


AMT 212653-000-803SIL 21-159

NTCheck : ALL212653-02-1 AVIONICS VENT SKIN AIR OUTLET VALVE126 RST N

(SAOV)REMOVE SKIN AIR OUTLET VALVE FOR OVERHAUL.NOTE 1: TASK APPLICABILITY FOR AIRCRAFT INSTALLED P/N: VFT300B00.NOTE 2: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOF AMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS13 AMD 00 EFFECTIVE DATE IS NEXT C CHECK.


AMM 213100/5AMT 213100-710-002MRB 213100/02

I 9 000 FHI 60 MO

ALL213100-01-1 PRESSURE CONTROL AND MONITORING210 OPT N

OPERATIONAL CHECK OF SYSTEM VIA MCDU



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 213100/5AMT 213100-710-003MRB 213100/03

I 9 000 FHI 60 MO

ALL213100-02-1 PRESSURE CONTROL AND MONITORING210 FUC N

OPERATIONAL CHECK OF MANUAL MODE SELECTION AND MANUALMODE PRESSURE CONTROL AND FUNCTIONAL CHECK OF MANUALMODE CABIN ALTITUDE INDICATION AND OUTFLOW VALVEPOSITION INDICATION


AMM 213100/5AMT 213100-710-004MRB 213100/04

I 22 500 FHI 150 MO


OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING INDITCHING CONFIGURATION


AMM 213100/5AMT 213100-710-005MRB 213100/05

I 22 500 FHI 150 MO


OPERATIONAL CHECK OF OUTFLOW VALVE PARTIAL OPENING BYEMERGENCY RAM AIR SWITCH


AMM 213100/3AMT 213100-600-001MRB 21.31.00/07

NTCheck : ALL213100-08-1 PRESSURE CONTROL AND MONITORING260 RST N

REMOVE SAFETY VALVE FOR RESTORATIONPREP. : ACCESS THROUGH REAR GALLEY WALL REQUIRED;



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 215243/6AMT 215243-210-001MRB 215000/06

I 24 000 FHI 120 MO

ALL215000-02-1 AIR COOLING AND TEMPERATURE CONTROL130 DI190

Y

DETAILED INSPECTION OF PACK AIR CHECK VALVES FLAPPERSFOR CONDITION AND OPERATIONAccess panels :

131PW 132PW 191BB 192FB0.21Total access time : Hrs


AMM 216151/6AMT 216151-200-001MRB 215000/14

I 6 000 FHI 48 MO

ALL215000-03-2 PACK RAM AIR INLET190 DI Y

DETAILED INSPECTION OF ACTUATOR MECHANISM AND INLETFLAP FOR EXCESSIVE PLAY AND CHECK GAP BETWEEN INLETNOSE AND DIFFUSOR RAMP


AMM 215141/4AMT 215141-920-001MRB 215000/10

I 9 000 FHI 60 MO

See note

ALL215141-01-1 AIR COOLING AND TEMPERATURE CONTROL130 FUC N

REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECKNOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 215200/7AMT 215200-100-001MRB 215000/12SIL 21-067

See noteNTCheck :

ALL215200-01-1 AIR CONDITIONING PACK191 RST192

N

REMOVE PRIMARY AND MAIN HEAT EXCHANGERS FORCLEANING.NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.Access panels :



AMT 215200-100-002MRB 21.50.00/15SIL 21-067

NTCheck : ALL215200-02-2 AIR CONDITIONING PACK191 RST192

N

REMOVE REHEATER FOR CLEANINGNOTE : CREDIT CAN BE TAKEN FROM TASK 215200-06-1Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 215200/5AMT 215200-790-001MRB 215000/16SIL 21-067

NTCheck : ALL215200-04-1 AIR CONDITIONING PACK191 FUC192

N

REMOVE CONDENSER FOR LEAK CHECK

Access panels :



AMM 215200/4AMT 215200-920-001MRB 215000/17SIL 21-039SIL 36-047

I 12 000 FHI 48 MO

2255

2303215200-07-1 AIR COOLING AND TEMPERATURE CONTROL191 RAR

192N

DISCARD COMBO SEALS AND PERISEALS ON HOT AIR INLETDUCTING, PACK DUCTING AND TRIM AIR DUCTING..NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. - TASK MAY BE COMBINED WITH TASK 361100-05-1.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 215200-920-002MRB 21.50.00/17SIL 21-039SIL 36-047

I 12 000 FHI 48 MO

22552261

2267

23032480

2974

30053013

3022

215200-08-1 AIR COOLING AND TEMPERATURE CONTROL191 DIS192

ND

DISCARD O-RING SEALS ON HOT AIR INLET DUCTING, PACKDUCTING AND TRIM AIR DUCTING.NOTE1:- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE A HIGHER INITIAL INTERVAL MAY BE USED.NOTE2: TASK THRESHOLD IS NEXT C CHECK

Access panels :



AMM 215200/6AMT 215200-200-001MRB 215000/19SIL 21-067

I 12 000 FHI 80 MO

ALL215222-01-1 AIR CYCLE MACHINE191 DI192

Y

DETAILED INSPECTION OF INTERIOR AND EXTERIOROF PLENUM CHAMBER (10HM5 AND 11HM5)FOR SIGNS OF DELAMINATION.NOTE : TO BE ACCOMPLISHED WITH TASK 215200-01-1PREP.: REMOVE HEAT EXCHANGERAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 215200/6AMT 15200-200-012AMT 215200-200-012SIL 21-128

I 24 000 FHI 160 MO

ALL215242-01-1 INJECTOR - WATER191 GVI192

N

GENERAL VISUAL INSPECTION OF WATER INJECTOR NOZZLESFOR EROSION


AMM 215500/5AMT 215500-710-001MRB 215000/04

I 15 000 FHI 100 MO

ALL215500-01-1 EMERGENCY RAM AIR INLET210 OPT N

OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM


AMM 215500/5AMT 215500-710-002MRB 215000/11SIL 21-060

I 15 000 FHI 100 MO

ALL215500-02-1 EMERGENCY RAM AIR INLET210 OPT N

OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET AND FLOWCONTROL VALVE CLOSING IN DITCHING CONFIGURATION


AMM 215541/6AMT 215541-210-001MRB 215000/07

I 24 000 FHI 160 MO

ALL215541-01-1 EMERGENCY RAM AIR INLET CHECK VALVE137 DI Y

DETAILED INSPECTION OF EMERGENCY RAM AIR/LP GROUNDAIR CHECK VALVE FLAPPERS FOR CONDITION AND OPERATIONAccess panels :

131PW0.03Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 215800-200-001MRB 21.58.00/01

NTCheck : 46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

54385456

5469

54955555

5699

5709

215800-01-1 AIR COOLING AND TEMPERATURE CONTROL191 RST YR

REMOVE CSAS OZONE CONVERTER FOR RESTORATIONNOTE: IF SYSTEM IS DEACTIVATED WHEN TASK BECOMES DUE,TASK MAY BE POSTPONED UNTIL REACTIVATION.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

5994

Access panels :

191BB0.10Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 215800-100-001MRB 21.58.00/02

NTCheck : 46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

54385456

5469

54955555

5699

5709

215800-02-1 AIR COOLING AND TEMPERATURE CONTROL191 RST YR

REMOVE CSAS HEAT EXCANGER FOR CLEANING


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

5994

Access panels :



AMM 216317/6AMT 216317-210-001MRB 215000/02

I 7 500 FHI 50 MO

ALL216000-01-1 AIR COOLING AND TEMPERATURE CONTROL200 DI Y

DETAILED INSPECTION OF CABIN SENSOR DUCT ANDTEMPERATURE SENSOR FOR CONTAMINATIONAccess panels :

231CC 251CC0.04Total access time : Hrs


AMM 216300/5AMT 216300-710-002MRB 215000/03

I 9 000 FHI 60 MO

22552261

2267

23032480

216000-02-1 AIR COOLING AND TEMPERATURE CONTROL210 OPT N

OPERATIONAL CHECK OF ZONE CONTROLLER (BACK UPSWITCHING) VIA CFDS/MCDU



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 216300/3AMT 216300-920-001SIL 21-134

I 12 000 FHI 80 MO

ALL216000-03-2 TEMPERATURE CONTROL130 DIS N

DISCARD TRIM AIR PRESSURE REGULATING VALVE FILTERNOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITHOPERATORS EXPERIENCEAccess panels :

131NW 131PW0.05Total access time : Hrs


AMM 216342/6AMT 216342-210-001MRB 215000/05

I 9 000 FHI 60 MO

ALL216242-01-1 AIR COOLING AND TEMPERATURE CONTROL191 DI Y

DETAILED INSPECTION OF TRIM AIR CHECKVALVE FLAPPERS FOR CONDITION AND OPERATIONPREP. : CHECK VALVE;Access panels :

191BB 192FB0.15Total access time : Hrs



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 22 AUTO FLIGHT


Threshold Interval

Ctrl References Eff

AMM 221000/5AMT 221000-710-002MRB 221000/01

I 15 000 FHI 100 MO

ALL221000-01-1 AUTOPILOT/FLIGHT DIRECTOR210 OPT N

OPERATIONAL CHECK OF AP DISENGAGEMENT AND LOCKINGDEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS

Skills :IN1 0.25 MHrs

AMM 223000/5AMT 223000-710-003MRB 223000/01

I 22 500 FHI 150 MO

ALL223000-01-1 AUTOTHRUST210 OPT N

OPERATIONAL CHECK OF ENGINE/AUTOTHRUST SYSTEMISOLATION

Skills :INS1 0.25 MHrs

AMM 226000/5AMT 226000-710-002MRB 226000/01

I 750 FHI 6 MO

ALL226000-01-1 FLIGHT AUGMENTATION210 OPT N

OPERATIONAL CHECK OF AUTOMATIC CHANGEOVER (AFS TEST)

Skills :B21 0.00 MHrsINS1 0.25 MHrs

AMM 226000/5AMT 226000-710-001MRB 226000/02

I 7 500 FHI 50 MO


OPERATIONAL CHECK OF FAC 2 FUNCTIONS



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 22 AUTO FLIGHT


Threshold Interval

Ctrl References Eff

AMM 226000/5AMT 226000-710-003MRB 226000/03

I 7 500 FHI 50 MO


OPERATIONAL CHECK OF "RETURN TO LOWSPEED" FUNCTION



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 23 COMMUNICATI0NS


Threshold Interval

Ctrl References Eff

AMM 231300/5AMT 231300-710-002MRB 231300/01MRB 343600/01MRB 345100/01MRB 345300/01MRB 345500/01

I 7 500 FHI 50 MO

ALL231300-01-1 RADIO MANAGEMENT210 OPT N

OPERATIONAL CHECK OF RADIO NAVIGATION SELECTION INSTANDBY MODE USING RMP 1 AND 2

Skills :B21 0.00 MHrsRA1 0.10 MHrs

AMM 233600/5AMT 233600-710-007MRB 233300/01

I 15 000 FHI 100 MO

ALL233300-01-1 PASSENGER ENTERTAINMENT (MUSIC & VIDEO)200 OPC ND

OPERATIONAL CHECK OF IFES POWER SHUTDOWN FUNCTION BYUSING THE VCC MASTER SWITCHAccess panels :


Skills :RA1 0.17 MHrs

AMM 235100/5AMT 235100-710-003MRB 235000/01

I 15 000 FHI 100 MO

ALL235100-01-1 AUDIO MANAGEMENT210 OPT N

OPERATIONAL CHECK OF CAPT. AND F/O AUDIO CONTROLPANELS SWITCHING TO THIRD AUDIO CONTROL PANEL



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 236100/6AMT 236100-200-001MRB 236000/01

I 3 000 FHI 16 MO

4ACheck :

ALL236142-01-1 STATIC DISCHARGER RETAINER300 CHK500600

N

RESISTANCE CHECK TIP TO RETAINER. BONDING CHECKRETAINER TO STRUCTURE


AMM 237100/5AMT 23700-710-001MRB 237100/01

I 7 500 FHI 50 MO

ALL237100-01-1 COCKPIT VOICE RECORDER210 OPT N

OPERATIONAL CHECK OF CVR AND CVR-CHANNEL RECORDING


AMM 237100/5AMT 237100-710-002MRB 237100/02

I 15 000 FHI 100 MO

ALL237100-02-1 COCKPIT VOICE RECORDER210 OPT N

OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDINGTIME DELAY RELAY



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 237135/4AMT 237135-920-001MRB 237100/3

See noteNTCheck :

ALL237135-01-1 COCKPIT VOICE RECORDER312 RST Y

DISCARD ULB BATTERYNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 237100/5AMT 237100-720-001MRB 237100/04

See noteNTCheck :

ALL237135-02-1 CVR ULB OPERATIONAL TEST312 OPT Y

OPERATIONAL CHECK OF ULBNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 237300/5AMT 237300-710-002MRB 237300/01

I 22 500 FHI 150 MO

2255

2261

22672303

2480

237300-01-1 CABIN INTERCOMMUNICATION DATA SYSTEM210 OPT N

OPERATIONAL CHECK FOR SECONDARY POWER SUPPLY TODIRECTORS AND DECODER/ENCODER UNITS, ANDDECODER/ENCODER UNITS-A CUT OFF FUNCTION



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 237300-710-036MRB 23.73.00/03

I 7 500 FHI 50 MO

ALL237300-03-1 CABIN INTERCOMMUNICATION DATA SYSTEM200 OPC N

OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDUNOTE: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 13AMD 00 EFFECTIVE DATE IS NEXT 2A CHECK.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 237300-710-038MRB 23.73.00/04

I 22 500 FHI 150 MO

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715164

5241

5247

237300-04-1 CABIN INTERCOMMUNICATION DATA SYSTEM200 OPC NR

OPERATIONAL CHECK OF DECODER/ENCODER UNITS ESSENTIALPOWER SUPPLY, AND DECODER/ENCODER UNITS-A CUT OFFFUNCTION


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

55555699

5709

59165958

5994

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 237300-710-042MRB 23.73.00/08

I 15 000 FHI 100 MO

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

237300-08-1 CABIN INTERCOMMUNICATION DATA SYSTEM200 OPC N

OPERATIONAL CHECK OF BATTERY BUS POWERED PA

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-003SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL240000-04-1 ELECTRICAL POWER521 TPS621

N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN WING INBOARD LEADINGEDGENOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-521-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

471CL 482CR 521GB 621GB0.12Total access time : Hrs


AMM 249200/6AMT 249200-210-004SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN WING OUTBOARD LEADINGEDGENOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-522-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-014SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN MAIN LANDING GEAR BAYAND FALSE SPAR BOXNOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-574-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

574AB 574BB 674AB 674BB0.08Total access time : Hrs


AMM 249200/6AMT 249200-210-006SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN WING OUTBOARD TRAILINGEDGETPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

575BB 575CB 575DB 575EB 575FB 575GB 575HB575KB 575LB 575MB 675BB 675CB 675DB 675EB675FB 675GB 675HB 675KB 675LB 675MB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-013SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN FLAP TRACK NUMBER 2FAIRINGNOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-531-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

531AT 631AT0.06Total access time : Hrs


AMM 249200/6AMT 249200-210-005SIL 24-067

I 6 YE ALL240000-09-1 ELECTRICAL POWER534 TPS634

N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN WING TIPNOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-534-01-1 AND ZL-534-01-2TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-015SIL 24-067


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN DRY BAY (OUTBOARD)NOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-560-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :



AMM 249200/6AMT 249200-210-007SIL 24-067


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN AIR CONDITIONINGCOMPARTMENTNOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-191-02-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

191AB 191AT 191BB 191BT 191CB 191CT 191DB191DT 191EB 191ET 191GB 191HB 191JB 191KB191LB 192AB 192AT 192BT 192CT 192DT 192EB192ET 192FB 192KB 192LB 192MB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-010SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN FUSELAGE TAIL AREANOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-311-01-1, ZL-315-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

312AR 314AR 315AL 316AR0.07Total access time : Hrs


AMM 249200/6AMT 249200-210-008SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL240000-13-1 ELECTRICAL POWER325 TPS N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN VERTICAL STABILIZERTRAILING EDGENOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-325-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

325BL 325BR 325CL 325DL0.08Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 249200/6AMT 249200-210-012SIL 24-067


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN VERTICAL STABILIZERLEADING EDGENOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-321-01-1, ZL-322-01-1, ZL 324-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

321AL 322BL 324AT0.90Total access time : Hrs


AMM 249200/6AMT 249200-210-011SIL 24-067

I 7 500 FHI 5 000 CYI 24 MO

CCheck :


N

APPLY TEMPORARY PROTECTION TO END FITTINGS OFELECTRICAL CONDUITS IN TRIMMABLE HORIZONTALSTABILIZERNOTE : SAME INTERVAL AND ACCESS AS FOR TASKZL-334-01-1TPS: APPLICATION OF TPS TYPE 2 GRADE 2Access panels :

334CB 334DB 334EB 344CB 344DB 344EB0.34Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 240000/6AMT 240000-200-004SIL 20-017

T 24 MOI 36 MO

ALL240000-17-1 ELECTRICAL POWER100 OPC200

N

ELECTRICAL POWER, OPENING AND CLOSING OF ALL CIRCUITBREAKERS.PREP. : ELECTRICAL POWER OFF.


AMM 244100/5AMT 244100-740-002MRB 242000/19

I 750 FHI 6 MO

ALL242000-01-1 AC GENERATION210 OPC Y

OPERATIONAL CHECK OF GAPCU VIA CFDS

Skills :B21 0.00 MHrsEL1 0.10 MHrsENG1 0.00 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 242100/3AMT 242100-920-041CMP 24-2-0000-001MRB 24.20.00/20SIL SUN236

T 150 FHT 1 MOI 800 FHI 6 MO

ALL242000-22-1 AC GENERATION438 DIS448

Y

- REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER ELEMENTS,- DRAIN AND REPLENISH OIL SYSTEMNOTE: - REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT DELIVERY. THEREAFTER REFER TO INTERVAL. - INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH SIL SUN 236.Access panels :

438AR 448AR0.08Total access time : Hrs


AMM 242141/6AMT 242141-200-010MRB 242000/07

I 2 400 FHI 24 MO

ALL242100-06-1 INTEGRATED DRIVE GENERATOR438 CHK448

Y

CHECK TORQUE OF QUICK-ATTACH-DETACH (QAD) TENSION BOLT.

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 242151/6AMT 242151-200-010MRB 242000/05

I 150 FHI 1 MO

See note

ALL242100-07-1 INTEGRATED DRIVE GENERATOR438 DI448

Y

-CHECK OIL LEVEL OF INTEGRATED DRIVE GENERATOR (GREEN RANGE) AND REPLENISH IF NECESSARY-CHECK FILTER DIFFERENTIAL PRESSURE INDICATOR (POP OUT NOT PROTRUDING)NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USEDAccess panels :



AMM 242100/5AMT 242100-710-042MRB 242000/11

NTCheck : ALL242100-09-1 INTEGRATED DRIVE GENERATOR438 OPC448

Y

OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR(IDG) DISCONNECT AND RECONNECT FUNCTION.NOTE 1: TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE.NOTE 2: RII TASK



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 242142/7AMT 242142-100-040CMM 24-21-42MRB 242000/12

See noteNTCheck :

ALL242100-10-1 INTEGRATED DRIVE GENERATOR437 RST447

Y

CLEAN INTEGRATED DRIVE GENERATOR (IDG) OILCOOLER.NOTE: TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE SHOP VISIT.


AMM 242200/5AMT 242200-710-002MRB 242000/08

I 7 500 FHI 50 MO

ALL242200-01-1 AC MAIN GENERATION210 OPT N

OPERATIONAL CHECK OF TRANSFER INHIBITION


AMM 242400/5AMT 242400-710-002MRB 242000/10

I 15 000 FHI 100 MO

ALL242400-02-1 AC GENERATION210 OPT N

OPERATIONAL CHECK OF EMERGENCY GCU VIA CFDS


AMM 242500/5AMT 242500-710-001MRB 242000/09

I 7 500 FHI 50 MO

ALL242500-01-1 AC GENERATION210 OPT N

OPERATIONAL CHECK OF AC ESS GENERATION SWITCHING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 242600/5AMT 242600-710-002MRB 242000/14

I 15 000 FHI 100 MO

ALL242600-02-1 AC GENERATION210 OPC N

OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY ANDBUS SHEDDING


AMM 243200/5AMT 243200-710-001MRB 243000/04

I 6 000 FHI 48 MO

ALL243200-01-1 DC GENERATION210 OPT N

OPERATIONAL CHECK OF DC GENERATION SWITCHING


AMM 243400/5AMT 243400-710-001MRB 243000/06

I 7 500 FHI 50 MO

ALL243400-01-1 DC GENERATION210 OPT N

OPERATIONAL CHECK OF "DC EMERG. CONFIG" CAUTION


AMM 243800/5AMT 243800-710-001MRB 243000/03

I 750 FHI 6 MO

ALL243800-01-1 DC MAIN GENERATION210 OPT N

OPERATIONAL CHECK OF BATTERY CHARGE LIMITER NO 1 ANDNO 2 VIA CFDS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 243851/6AMT 243851-280-001MRB 243000/05

See noteNTCheck :

ALL243851-01-1 DC GENERATION126 RST N

REMOVE BATTERY FOR OVERHAULNOTE : INTERVAL IS IAW SAFT CMM 24-38-51 OR REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMT 243851-280-802NTCheck : ALL243851-02-1 DC GENERATION126 RST N

REMOVE BATTERY FOR CHECK IN WORKSHOPNOTE 1 : THE INTERVAL OF THIS TASK REFER TO "A321 TIMECONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.NOTE 2: CREDIT IS TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 243851-01-1Access panels :


Skills :AV1 0.30 MHrs

AMM 242200/5AMT 242200-710-001MRB 245000/04

I 15 000 FHI 100 MO

ALL245100-01-1 AC/DC ELECTRICAL LOAD DISTRIBUTION210 OPT N

OPERATIONAL CHECK OF GENERATOR LINE CONTACTOR OPENING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 245100/5AMT 245100-710-001MRB 245000/05

I 15 000 FHI 100 MO

ALL245100-02-1 AC/DC ELECTRICAL LOAD DISTRIBUTION210 OPC N

OPERATIONAL CHECK OF COMMERCIAL ELECTRIC LOADSHEDDING



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 25 EQUIPEMENT & FURNISHING


Threshold Interval

Ctrl References Eff

IPC 25-65-01-52WIPC 25-65-04-18U

See noteNTCheck :

ALLVN256600-01 SURVIVAL KITS200 OVH N

REMOVE SURVIVAL KITS FROM THE STOWAGE FOR OVERHAULNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.P/N OFF: 60128-103 S/N OFF:P/N ON: 60128-103 S/N ON: GRN:

AMM 251100/6AMT 251100-200-001MRB 251100/01

I 24 000 FHI 160 MO

ALL251100-01-1 COCKPIT SEATS210 DI Y

DETAILED INSPECTION OF SEAT STRUCTURE AND SEATATTACHMENT OF ALL FLIGHT DECK SEATS


AMM 251151/6AMT 251151-200-002MRB 251100/02

I 7 500 FHI 50 MO

ALL251100-02-1 COCKPIT SEATS210 CHK N

CHECK OF ADJUSTMENT OF SEAT CONTROL CABLES


AMM 252100/6AMT 252100-210-001MRB 252100/01

I 15 000 FHI 100 MO

ALL252100-01-1 PASSENGER COMPARTMENT SEATS200 VCK Y

DETAILED INSPECTION OF SEAT TO FLOOR ATTACHMENT ANDGENERAL VISUAL INSPECTION OF SEAT STRUCTURE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 252100/6AMT 252100-210-002MRB 252100/02

I 15 000 FHI 100 MO

ALL252100-02-1 PASSENGER COMPARTMENT SEATS200 DI Y

DETAILED INSPECTION OF SEAT BELT ATTACHMENT, SEATBELT AND LOCK. CHECK OF LOCK


AMM 252200/6AMT 252200-210-001MRB 252200/01

I 15 000 FHI 100 MO

ALL252200-01-1 CABIN ATTENDANT SEATS200 VCK Y

DETAILED INSPECTION OF SEAT ATTACHMENT AND GENERALVISUAL INSPECTION OF SEAT STRUCTURE


AMM 252200/6AMT 252200-210-002MRB 252200/02

I 15 000 FHI 100 MO

ALL252200-02-1 CABIN ATTENDANT SEATS200 DI Y

DETAILED INSPECTION OF SEAT BELT ATTACHMENT, SEATBELT AND LOCK. CHECK OF LOCK



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 252344/6AMT 252344-210-001SIL 25-085

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL252331-01-1 PANELS - LOWER SIDEWALL200 DI Y

DETAILED INSPECTION OF LOWER SIDE WALL PANELAND OF AREA BEHIND LOWER SIDE WALL PANELFOR FOREIGN MATERIAL ACCUMULATION.NOTE : - ONE LOWER SIDE WALL PANEL IN FWD, MID AND AFT PASSENGER CABIN SHOULD BE REMOVED, (APPROX 2.5 MH) - ALTERNATE SIDEWALL PANEL IS RECOMMENDED AT NEXT INSPECTION - INTERVAL MAY BE ADJUSTED ACCORDING TO OPERATOR EXPERIENCE


AMM 253000/6AMT 253000-210-001MRB 253000/01

I 6 YE ALL253000-01-1 BUFFET AND GALLEY200 DI Y

DETAILED INSPECTION OF ATTACHMENT POINTS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 253000/3AMT 253000-920-001MRB 253000/04

I 5 500 FHI 40 MO

ALL253000-02-1 BUFFET AND GALLEY200 RAD N

REMOVE AND DISCARD AIR FILTER ELEMENTNOTE 1: TASK APPLICABLE ONLY IF FILTER ELEMENTSARE INSTALLEDNOTE 2: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVALMAY BE USED.


AMM 253400/7AMT 253400-100-001MRB 25-34-00/01

I 1 500 FHI 12 MO

See note

2255

22612267

2303

2480

253400-01-1 GALLEY COOLING200 RST Y

CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES/FILTERS IN GALLEY CABINETNOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.


AMM 253400/7AMT 253400-100-002MRB 25.34.00/02

I 1 500 FHI 12 MO

See note

ALL253400-02-1 GALLEY COOLING200 RST Y

CLEAN AIR CHILLER CONDENSER AIR FILTERNOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 74-08-09AMM 254000/6AMT 254000-210-001MRB 254000/01

I 6 000 FHI 40 MO

ALL254000-01-1 LAVATORIES200 DI Y

DETAILED INSPECTION OF WASTE COMPARTMENT INCLUDINGWASTE FLAP AND OPERATIONAL CHECK OF WASTE FLAPNOTE: INTERVAL IS 1000 FH FOR OPERATOR FLYING UNDER FAA REGULATIONS AS PERFAA AD 74-08-09

Skills :B21 0.00 MHrsCA1 0.20 MHrs

AMM 254000/6AMT 254000-210-002MRB 254000/03

I 80 MO ALL254000-02-2 LAVATORIES200 DI Y

DETAILED INSPECTION OF ATTACHMENT POINTS


AMM 254000-210-004MRB 25.40.00/05

I 7 500 FH ALL254000-04-2 LAVATORIES200 DI Y

LAVATORIESDETAILED INSPECTION OF LAVATORY FLOOR PAN"

Skills :ACA1 1.50 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 255000/6AMT 255000-200-002MRB 255000/01

I 8 DY ALL255000-01-1 CARGO COMPARTMENTS130 VCK150160

Y

VISUAL CHECK OF CARGO COMPARTMENT DECOMPRESSION,LINING, FLOOR PANELS AND PRESSURE COMPENSATION VALVE(AS FAR AS VISIBLE, IF ACT(S) INSTALLED)Access panels :



AMM 255000/6AMT 255000-210-001MRB 255000/03

I 8 000 FHI 53 MO

ALL255000-02-1 LOWER DECK CARGO LOADING130 OPT150

Y

PERFORM OPERATIONAL CHECK AND DETAILED INSPECTION OFXZ-LATCHESAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 255000/6AMT 255000-210-002MRB 255000/02

I 4 000 FHI 12 MO

ALL255000-03-1 CARGO COMPARTMENTS130 OPT150

Y

PERFORM OPERATIONAL CHECK AND DETAILED INSPECTION OFYZ DOOR SILL LATCHESAccess panels :



AMM 255000/6AMT 255000-200-018SIL 25-099

I 2 000 FHI 400 DY

ALL255000-07-1 LOWER DECK CARGO LOADING130 DI150

Y

DETAILED INSPECTION OF PDU ROLLERS FOR WEARAND DAMAGENOTE : IT IS RECOMMENDED TO ENSURE CLEANLINESS IN THE VICINITY OF THE PDU ROLLERSAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 255000/6AMT 255000-200-012MRB 255000/14

I 24 000 FHI 160 MO

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

255000-08-1 LOWER DECK CARGO LOADING150 DI YR

REMOVE XZ-ENDSTOPS AND YZ-LATCHES FOR DETAILED INSPECTION.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 255000/6AMT 255000-200-013MRB 255000/15

I 24 000 FHI 160 MO

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

255000-09-1 LOWER DECK CARGO LOADING150 DI Y

REMOVE XZ-SINGLE LATCH 32 ACT FOR DETAILED INSPECTION



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 255000-200-015I 24 000 FHI 160 MO

51645241

5247

53435427

5469

57095994

255000-10-1 LOWER DECK CARGO LOADING150 DI YR

LOWER DECK CARGO LOADINGREMOVE FIXED XZ - LATCHES ACT FOR DETAILED INSPECTION


AMM 255000/6AMT 255000-200-016MRB 255000/17

I 750 FHI 6 MO

ALL255000-11-1 LOWER DECK CARGO LOADING130 DI150 VCK

Y

VISUAL CHECK OF XZ-LATCHES AND DOOR SILL LATCHESNOTE: FOR A319 DOOR SILL LATCHES ONLY TO BE CHECKED IN FWD CCAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 255000-200-025MRB 25.50.00/04

I 750 FHI 6 MO

ALL255000-16-1 CARGO COMPARTMENTS130 DI150160

Y

DETAILED INSPECTION OF DIVIDER NETS, DOOR NETSAND NET ATTACHMENT POINTSNOTE: THE NUMBER OF AFFECTED ZONES MAY VARY ACCORDING TO THE CARGO SYSTEMS INSTALLED.


AMT 255000-200-802I 24 000 FHI 160 MO

ALL255000-25-1 CARGO COMPARTMENTS130 DI150

Y

REMOVE XZ-LATCHES FOR DETAILED INSPECTIONNOTE: : IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOF AMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS14 AMD 00 EFFECTIVE DATE IS NEXT C CHECKAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 256141/6AMT 256141-200-001MRB 256141/01

I 6 YE ALL256141-01-1 DESCENT DEVICE EMERGENCY210 DI Y

DETAILED INSPECTION OF EMERGENCY ESCAPE ROPE AND ROPEATTACHMENTAccess panels :

211EC 212EC0.04Total access time : Hrs


AMM 256200/6AMT 256200-210-001MRB 256200/01

I 750 FHI 6 MO

ALL256241-01-1 DOOR ESCAPE SLIDES800 CHK N

CHECK DOOR AND OFFWING ESCAPE SLIDE/RAFT INFLATION RESERVOIR PRESSURENOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS /EMERGENCY EXITS.DEPENDING ON AIRCRAFT CONFIGURATION, ALTERNATIVE ACCESSPANELS ARE:-151CW AND 152CW (A320 & A321) OR-151SW AND 152SW (A319 & A318) ORACCESS TO OVERHEAD STOWAGE COMP. (FOR A/C WITH ACT) SEE AMM FORACCESS PANELS TO BE OPENED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 256200/6AMT 256200-750-001MRB 256200/02

See noteNTCheck :

ALL256241-02-1 DOOR ESCAPE SLIDE831 RAI832841842

Y

REMOVE DOOR ESCAPE SLIDE/RAFT FOR HYDROSTATICTEST OF INFLATION RESERVOIRNOTE :- TASK TO BE PERFORMED WITH 256241-03-1. TASK IS NOT APPLICABLE FORDEACTIVATED PASSENGER/CREW DOORS / EMERGENCY EXITS - THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 256244/4AMT 256244-920-001MRB 256200/03

See noteNTCheck :

ALL256241-03-1 DOOR ESCAPE SLIDE831 RST832841842

Y

REMOVE DOOR ESCAPE SLIDE/RAFT FOR RESTORATIONNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.-TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS / EMERGENCYEXITS.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 256200/5AMT 256200-710-001MRB 256200/04

I 18 MO ALL256241-04-1 DOOR ESCAPE SLIDE831 OPT832841842

Y

OPERATIONAL CHECK OF FWD AND AFT PAX/CREWDOOR ESCAPE SLIDES/RAFT DEPLOYEMENT.NOTE : - DEPLOYMENT OF EITHER FWD DOOR 831 OR 841 SLIDE/RAFT AND DEPLOYEMENT OF EITHER AFT DOOR 832 OR 842 SLIDE/RAFT - ONE SAMPLE PER OPERATOR FLEET (COMBINED A320/A321 FLEET). - INTERVAL 18 MONTHS - TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS - ALTERNATE DOOR POSITION AT NEXT INTERVALE RECOMMENDED


AMM 531100/6AMT 531100-210-034MRB 521000/07SIL 53-054

I 1 110 CYI 400 DY

ALL256241-05-1 DOOR ESCAPE SLIDE221 CLN222261262

N

CLEAN DOOR GIRT BAR FITTING STOP LEVERSNOTE : TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORSINTERVAL TO BE ADJUSTED ACCORDING TODOOR USAGE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 256247/4AMT 256247-920-001MRB 256200/03

See noteNTCheck :

ALL256247-01-1 DOOR 2/3 ESCAPE SLIDE131 RST132151152

N

REMOVE DOOR 2/3 ESCAPE SLIDE FOR RESTORATIONNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 256200/5AMT 256200-710-003MRB 256200/04

I 18 MO ALL256247-02-1 DOOR 2/3 ESCAPE SLIDE833 OPT834843844

N

OPERATIONAL CHECK OF FWD AND AFT EMERGENCY EXITDOOR ESCAPE SLIDE DEPLOYMENTNOTE : - DEPLOYMENT OF EITHER FWD DOOR 833 OR 843 SLIDE/RAFT AND DEPLOYMENT OF EITHER AFT DOOR 834 OR 844 SLIDE/RAFT - ONE SAMPLE PER OPERATOR FLEET - ALTERNATE DOOR POSITION AT NEXT INTERVAL RECOMMENDED


AMM 256200/6AMT 256200-750-003MRB 256200/02

See noteNTCheck :

ALL256249-01-1 DOOR 2/3 ESCAPE SLIDE231 RFT232251252

N

REMOVE DOOR 2/3 ESCAPE SLIDE INFLATION RESERVOIR FORHYDROSTATIC TESTNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 256300/5AMT 237300-710-026MRB 237300/05MRB 256300/01

I 22 500 FHI 150 MO

ALL256300-01-1 EVACUATION SIGNALLING EQUIPMENT200 OPT N

OPERATIONAL CHECK OF EVAC FUNCTIONNOTE : IF INSTALLED


AMM 256500/5AMT 256500-720-001MRB 256532/01

See noteNTCheck :

ALL256532-01-1 PORTABLE EMERGENCY BEACON TRANSMITTER200 VCK Y

REMOVE THE EMERGENCY LOCATOR TRANSMITTER FOR WORKSHOPTEST (BATTERY CHECK & FUNCTIONAL CHECK)NOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 256500/5AMT 256500-710-001MRB 256535/01

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL256535-01-1 ELT (REAR FUSELAGE)200 OPT N

OPERATIONAL CHECK OF ELT SYSTEM BY MANUAL ACTIVATION



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 256500/5AMT 256500-720-004MRB 256535/02

See noteNTCheck :

ALL256535-02-1 ELT (REAR FUSELAGE)200 RAR N

REMOVE ELT FOR BATTERY REPLACEMENT AND DURINGREINSTALLATION PERFORM FUNCTIONAL CHECK OF ELT SYSTEMINCLUDING AUTOMATIC ACTIVATIONNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 256551/2AMT 256551-920-001MRB 256551/01

See noteNTCheck :

ALL256551-01-1 MEGAPHONE BATTERIES200 DIS Y

DISCARD MEGAPHONE BATTERIESNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 256551/2AMT 256551-710-002MRB 256551/02

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL256551-02-1 MEGAPHONE200 OPT N

OPERATIONAL CHECK OF MEGAPHONE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 256641/4AMT 256641-920-001MRB 256641/01

See noteNTCheck :

ALL256600-01-1 SUPPLEMENTAL LIFE RAFT200 RST N

REMOVE SUPPLEMENTAL LIFE RAFT FOR RESTORATIONAND HYDROSTATIC TEST OF INFLATION RESERVOIRNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 256652/4AMT 256652-920-001MRB 256652/01

See noteNTCheck :

ALL256652-01-1 LIFE VESTS200 RST Y

RESTORATION OF LIFE VESTSNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AD 2012-0134AMM 257100/6AMT 257100-290-001ISB 25A1555

T 20 000 CYI 500 CY

2255

22612267

2303

24802974

3005

30133022

257100-01-1 AVIONICS COMPARTMENT127 SDI128

Y

BORESCOPE INSPECTION OF THE 80VU RACK LOWER LATERALFITTINGS AND VISUAL INSPECTION OF THE UPPER FITTINGSAND CENTRAL SHELVE FITTINGS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2012-0134AMM 257100/6AMT 257100-290-002ISB 25A1555

T 20 000 CYI 500 CY

22552261

2267

23032480

2974

30053013

3022

257100-02-1 AVIONICS COMPARTMENT127 SDI128

Y

BORESCOPE INSPECTION OF THE 80VU RACK LOWER CENTRALSUPPORT AND VISUAL INSPECTION OF THE UPPER FITTINGS AND CENTRAL SHELVEFITTINGS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 261200-5AMT 261200-710-001MRB 261200/01MRB 262100/01

I 750 FH ALL261200-01-1 ENGINE FIRE AND OVERHEAT DETECTION210 OPT Y

OPERATIONAL CHECK OF LOOP/SQUIB


AMM 261300/5AMT 261300-710-001MRB 261300/01MRB 262200/01

I 750 FHI 6 MO

ALL261300-01-1 APU FIRE AND OVERHEAT DETECTION210 OPT Y

OPERATIONAL TEST OF THE APU FIRE AND OVERHEAT DETECTION SYSTEM


AMM 261500/6AMT 261500-100-001MRB 261500/03

I 11 000 FHI 73 MO

ALL261500-03-1 AVIONICS COMPARTMENT SMOKE DETECTION128 CLN N

CLEAN AVIONICS SMOKE DETECTION PICCOLO TUBESNOTE: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVALMAY BE USED.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 261600/5AMT 261600-710-001MRB 26.16.00/01MRB 26.23.00/02

I 750 FHI 6 MO

ALL261600-03-1 CARGO COMPARTMENT SMOKE DETECTION210 OPT N

OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKEDETECTION BY PTT


AMM 261600/5AMT 261600-710-003MRB 21.28.00/06MRB 26.16.00/02

I 750 FHI 6 MO

ALL261600-04-1 CARGO COMPARTMENT SMOKE DETECTION210 OPT N

OPERATIONAL TEST OF CARGO COMPARTMENT SMOKEDETECTION BY CFDS TO CONFIRM ISOLATION VALVELATCHING CIRCUIT INTEGRITY.


AMT 261615-100-001MRB 26.16.00/05

NTCheck : ALL261600-05-1 CARGO COMPARTMENT SMOKE DETECTION130 RST150160

N

REMOVE CARGO COMPARTMENT SMOKE DETECTORS FOR CLEANING

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 261700/5AMT 261700-710-001MRB 26.17.00/01

I 800 FHI 6 MO

ALL261700-03-1 LAVATORY SMOKE DETECTION210 OPT N

OPERATIONAL CHECK OF LAVATORY SMOKE DETECTION BY CFDSTO CONFIRM WARNINGS CAN BE DISPLAYED


AMM 261715/7AMT 261715-100-003CMM 261616MRB 261700/04

NTCheck : ALL261700-04-1 LAVATORY SMOKE DETECTION200 RST N

REMOVE SMOKE DETECTOR FOR CLEANING


AMM 262100/5AMT 262100-710-002MRB 262100/02

I 7 500 FHI 50 MO

ALL262100-02-1 ENGINE FIRE EXTINGUISHING210 OPT N

OPERATIONAL CHECK OF BOTTLE LOW PRESSURE INDICATINGCIRCUIT


AMM 262100/5AMT 262100-720-001MRB 262100/03

I 15 000 FHI 100 MO

ALL262100-03-1 ENGINE FIRE EXTINGUISHING415 CHK425

N

CHECK OF FIRING CIRCUIT CONTINUITY

Access panels :

415BR 425BR0.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 262100/5AMT 262100-720-003MRB 262100/09

I 7 000 FHI 48 MO

ALL262100-04-2 ENGINE FIRE EXTINGUISHING415 CHK425

Y

CHECK DISTRIBUTION PIPING FOR LEAKAGE AND OBSTRUCTION

Access panels :

415BL 415BR 425BL 425BR 437AL 438AR 447AL448AR 451AL 452AR 461AL 462AR



AMM 262100/5AMT 262100-710-004MRB 262100/08MRB 360000/06

I 15 000 FHI 100 MO

ALL262100-05-1 ENGINE FIRE EXTINGUISHING210 OPT N

OPERATIONAL CHECK OF FIRE CONTROL PUSH BUTTON SWITCHSUB FUNCTIONS RELATED TO ENGINE SHUTDOWN ANDISOLATIONAccess panels :

413DL 423DL0.16Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 262141/6AMT 262141-280-002MRB 262100/07

See noteNTCheck :

ALL262141-02-1 ENGINE FIRE EXTINGUISHER BOTTLES415 RAI425

N

HYDROSTATIC TEST OF BOTTLES INCLUDING CHECK SETTINGOF PRESSURE SWITCHNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 262141/6AMT 262141-280-001

See noteNTCheck :

ALL262141-02-1A ENGINE FIRE EXTINGUISHER BOTTLES415 CHK425

N

WEIGHT CHECK OF THE ENGINE FIRE EXTINGUISHERBOTTLE (6WE1,6WE2,8WE1,8WE2)NOTE: - THE FIRST ACCOMPLISHMENT OF THIS TASK IS NEXT 2A CHECK SINCE EFFECTIVE DATE OF AMS. - THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 262141/4AMT 262141-920-001MRB 262100/06

See noteNTCheck :

ALL262142-01-1 ENGINE FIRE EXTIR BOTTLE CARTRIDGES415 DIS425

Y

DISCARD CARTRIDGENOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 262200/5AMT 262200-710-002MRB 23.42.00/01MRB 26.22.00/02MRB 28.29.00/01MRB 28.29.00/03MRB 49.62.00/01-13MRB 49.62.00/01-32MRB 49.62.00/01-36MRB 49.62.00/03-13MRB 49.62.00/03-32MRB 49.62.00/03-36

I 3 000 FHI 20 MO

ALL262200-02-1 APU FIRE EXTINGUISHING210 OPT N

OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHINGCIRCUIT AND TEST APU LP FUEL VALVE OPERATION USINGEACH INDIVIDUAL MOTOR IN TURN AND TEST APU EMERGENCYSHUTDOWN CIRCUIT



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 262200/5AMT 262200-720-001MRB 262200/07

I 15 000 FHI 100 MO

ALL262200-03-1 APU FIRE EXTINGUISHING210 CHK N

CHECK FIRING CIRCUIT CONTINUITY

Access panels :



AMM 262200/6AMT 262200-210-001MRB 262200/05

I 15 000 FHI 100 MO

ALL262200-04-1 APU FIRE EXTINGUISHING313 DI N

DETAILED INSPECTION OF DISTRIBUTION PIPING

Access panels :



AMM 262200/5AMT 262200-710-003MRB 262200/06

I 15 000 FHI 100 MO


OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 262200/5AMT 262200-710-004MRB 26.22.00/09MRB 49.62.00/02-13MRB 49.62.00/02-32MRB 49.62.00/02-36

I 24 000 FHI 80 MO


OPERATIONAL CHECK OF APU FIRE PUSH BUTTON SWITCHFUNCTIONS (IN SINGLE CHANNEL CONFIGURATION) AND TESTAPU LP FUEL VALVE OPERATION USING EACH INDIVIDUALMOTOR IN TURN AND TEST APU EMERGENCY SHUTDOWN CIRCUIT


AMM 262241/6AMT 262241-280-002MRB 262200/03

See noteNTCheck :

ALL262241-01-1 APU FIRE EXTINGUISHER BOTTLE313 RAI N

HYDROSTATIC TEST OF BOTTLE INCLUDING CHECK OFPRESSURE SWITCH SETTINGNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 262200/4AMT 262200-040-004-1

See noteNTCheck :

ALL262241-01-1A APU FIRE EXTINGUISHER BOTTLE313 CHK N

WEIGHT CHECK OF THE APU FIRE EXTINGUISHERBOTTLE (11WF)NOTE : - THE FIRST ACCOMPLISHMENT OF THIS TASK IS NEXT 2A CHECK SINCE EFFECTIVE DATE OF AMS. - THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 262242/4AMT 262242-920-001MRB 262200/04

See noteNTCheck :

ALL262242-01-1 APU FIRE EXTIN BOTTLE CARTRIDGE313 DIS Y

DISCARD CARTRIDGENOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 262341/4AMT 262341-920-001MRB 262300/05

See noteNTCheck :

ALL262300-04-3 CARGO COMPARTMENT FIRE EXTINGUISHING132 DIS N

REMOVE AND DISCARD CARGO COMPARTMENT FIREEXTINGUISHER BOTTLE CARTRIDGESNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 262341/6AMT 262341-280-001MRB 26.23.00/01

I 22 500 FHI 72 MO

ALL262341-01-2 CARGO COMPARTMENT FIRE EXTIR BOTTLE132 FUC N

REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLEFOR WEIGHT CHECKAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 262341/6AMT 262341-280-002MRB 26.23.00/02MRB 26.23.00/06

See noteNTCheck :

ALL262341-02-2 CARGO COMPARTMENT FIRE EXTIR BOTTLE132 FUC N

REMOVE CARGO COMPARTMENT FIRE EXTINGUISHERBOTTLE FOR HYDROSTATIC TEST AND CHECK OFPRESSURE SWITCH SETTINGNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 262400/6AMT 262400-210-002MRB 262400/01

I 750 FHI 6 MO

See note

ALL262441-01-1 PORTABLE FIRE EXTINGUISHER BOTTLES200 CHK N

CHECK PRESSURE GAUGE READINGNOTE: IF EXTINGUISHER WITH PRESSURE GAUGE IS INSTALLED


AMM 262400/6AMT 262400-280-001MRB 262400/02

See noteNTCheck :

ALL262441-02-1 PORTABLE FIRE EXTINGUISHER BOTTLES200 RAI Y

HYDROSTATIC TEST OF BOTTLESNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.



: : :

: :

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01



Threshold Interval

Ctrl References Eff

CMM 26-24-05NTCheck : ALL262441-02-1A PERIODICAL CHECK200 CHK N

PERIODICAL CHECK EVERY 2 YEARSPERFORM PERIODICAL CHECK FOR FIRE EXTINGUISHER AS PER CMM 26-24-05NOTE: APPLICABILITY FOR PN: 74-20; 0074-20INCASE OF OVERDUE TASK WHEN AMS ISSUE 14 AMD 00 IS EFFECTIVE, THE TASKTHRESHOLD IS NEXT 2A CHECK.

AMM 262500/6AMT 262500-200-002MRB 262500/01

I 48 MO

2CCheck :

ALL262541-01-1 LAVATORY FIRE EXTINGUISHER200 GVI Y

GENERAL VISUAL INSPECTION OF LAVATORY FIREEXTINGUISHER FOR SIGNS OF LEAKAGE/DISCHARGE


AMM 262500/6AMT 262500-200-003MRB 262500/02

NTCheck : ALL262541-02-1 LAVATORY FIRE EXTINGUISHER BOTTLE200 FUC N

REMOVE LAVATORY FIRE EXTINGUISHER BOTTLEFOR WEIGHT CHECK


AMT 262500-200-005MRB 26.25.00/04

I 24 MO

CCheck :

ALL262541-04-1 LAVATORY FIRE EXTINGUISHING200 VCK N

VISUAL CHECK OF FIRE EXTINGUISHER BOTTLE PRESSUREREADING



: : :

: :

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01



Threshold Interval

Ctrl References Eff

AMM 271400/6AMT 271400-220-001MRB 271400/04

I 18 000 FHI 120 MO

ALL271400-02-2 AILERON AND HYDRAULIC ACTUATION575 CHK675

NR

CHECK AILERON SERVOCONTROL AND HINGE BEARINGSFOR EXCESSIVE PLAY AND CONDITIONNOTE: RII TASKAccess panels :

575KB 575MB 590AB 590BB 675KB 675MB 690AB690BB



AMM 272200/5AMT 272200-710-001MRB 272100/01

I 1 500 FHI 12 MO

ALL272100-01-1 RUDDER MECHANICAL CONTROL210 OPT N

OPERATIONAL CHECK OF RESET FUNCTION


AMM 272100/6AMT 272100-210-002MRB 272100/03

I 24 000 FHI 72 MO

ALL272100-02-1 RUDDER MECHANICAL CONTROL100 DI Y

DETAILED INSPECTION OF RUDDER MECHANICAL CONTROLCABLES -INCLUDING ZONE 311-Access panels :

131AC 131BC 131CC 131PW 151AC 151BC 151CC151DC 161AC 161BC 162DW 241FF 241KF 312AR812 824 825 826




: : :

: :

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01



Threshold Interval

Ctrl References Eff

AMM 272100/6AMT 272100-220-001MRB 272100/03

I 24 000 FHI 72 MO

ALL272100-03-1 RUDDER MECHANICAL CONTROL145 FUC NR

CHECK TENSION OF RUDDER MECHANICAL CONTROLCABLES USING TENSIOMETERNOTE: RII TASKAccess panels :

131BC 811 8250.10Total access time : Hrs


AMM 272641/6AMT 272641-280-001MRB 272100/04

I 24 000 FHI 156 MO

ALL272100-04-1 RUDDER MECHANICAL CONTROL325 RFT N

REMOVE YAW DAMPER SPRING ROD FOR WORKSHOP CHECK

Access panels :

325BL0.02Total access time : Hrs


AMM 272100/5AMT 272100-710-001MRB 272100/05

I 18 000 FHI 72 MO

ALL272100-05-1 RUDDER MECHANICAL CONTROL210 OPT Y

OPERATIONAL CHECK OF CENTERING SPRING ROD

Access panels :

325CL 325CR0.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 272100/6AMT 272100-210-003MRB 272100/07

I 18 000 FHI 72 MO

ALL272100-07-1 RUDDER MECHANICAL CONTROL325 DI Y

DETAILED INSPECTION OF MECHANICAL CONTROL LINKAGE INFINAccess panels :

325AL 325AR 325BL 325BR 325CL 325CR 325DL325DR



AMM 272143/3AMT 272143-600-001MRB 272100/09

I 20 MO ALL272100-08-1 RUDDER MECHANICAL CONTROL210 LUB N

LUBRICATION OF RUDDER PEDALS ADJUSTMENTMECHANISMNOTE: RII TASK


AMM 272149/6AMT 272149-200-001MRB 27.21.00/10

I 24 000 FHI 80 MO

ALL272100-10-1 RUDDER MECHANICAL CONTROL320 FUC N

FUNCTIONAL CHECK OF RUDDER SERVOCONTROL ACTUATINGSPRING RODSAccess panels :

325BL 325BR 325CL 325CR 325DL 325DR 325EL325ER




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 272100-220-004MRB 27.21.00/11

I 24 000 FHI 80 MO

ALL272100-11-1 RUDDER MECHANICAL CONTROL325 DI N

DETAILED INSPECTION OF RUDDER SERVOCONTROL ACTUATINGSPRING RODS AND RUDDER SERVOCONTROL FEEDBACK RODATTACHMENTSAccess panels :

325CL0.02Total access time : Hrs


AMM 272100/6AMT 272100-220-002MRB 272100/02

I 40 MO ALL272145-01-1 RUDDER CABLE TENSION REGULATOR125 CHK NR

CHECK TENSION REGULATOR POINTER IS WITHIN THE LIMITSNOTE: RII TASKAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 272400/5AMT 272400-710-002MRB 27.24.00/01MRB 29.10.00/15MRB 29.30.00/01MRB 29.30.00/02

I 750 FHI 6 MO

ALL272400-01-1 RUDDER HYDRAULIC ACTUATION210 OPT N

OPERATIONAL CHECK OF RUDDER SERVOCONTROLS WITHINDIVIDUAL HYDRAULIC SYSTEMS


AMM 272400/6AMT 272400-200-001MRB 272400/02

I 18 000 FHI 120 MO

ALL272400-02-1 RUDDER HYDRAULIC ACTUATION325 CHK N

CHECK RUDDER SERVO CONTROL AND HINGE BEARINGSFOR EXCESSIVE PLAY AND CONDITIONAccess panels :

325BL 325CL 325DL 325EL0.08Total access time : Hrs


AMM 122255-640-001AMT 122255/3MRB 272400/03

I 5 500 FHI 15 MO

ALL272400-03-1 RUDDER HYDRAULIC ACTUATION325 LUB N

LUBRICATION OF RUDDER HINGE BEARING NO 6NOTE: ALTERNATIVELY MPD TASK 272400-05-1 CAN BE APPLIED.Access panels :

325DL 325DR0.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2001-16-09AD 2010-02-09AMM 273400/6AMT 273400-200-001EAD 2007-0163MRB 273400/03

I 12 000 FHI 20 MO

ALL273400-02-1 ELEVATOR AND HYDRAULIC ACTUATION334 FUC344

N

CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGSFOR EXCESSIVE PLAY AND CONDITION

Access panels :

334BB 334DB 334FB 334HB 344BB 344DB 344FB344HB



AMM 273400/6AMT 273400-220-002MRB 273400/04

I 24 000 FHI 160 MO

ALL273400-04-2 ELEVATOR AND HYDRAULIC ACTUATION334 VCK344

Y

CHECK OF THE DIFFERENTIAL PRESSURE INDICATOR ANDPOSITION OF FLUID RESERVE PISTON OF ELEVATORSERVO CONTROLSAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 273400-200-003SIL 27-152

I 80 MO ALL273400-06-1 ELEVATOR AND HYDRAULIC ACTUATION334 CHK344

YR

CHECK OF ELEVATOR NEUTRAL POSITION AND SERVO CONTROLSINSTALLATIONNOTE: RII TASKAccess panels :



AD 2010-0046 01EAD 2010-0046FAD 2011-1904ISB 27A1186

I 5 000 CY ALL273400-07-1 ELEVATOR AND HYDRAULIC ACTUATION334 SDI344

Y

SPECIAL DETAILED INSPECTION OF ELEVATOR SERVOCONTROLROD EYE-ENDSNOTE 1: REFER TO EASA AD 2010-0046/FAA AD 2011-19-04 AND ISB27A1186 FOR IMPLEMENTATION PERIODS AND TIME UNTILFIRST REPEAT ON SERVICE AIRCRAFTNOTE 2: RII TASKAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 122253/3AMT 122253-640-001MRB 274000/04

I 5 500 FHI 15 MO

ALL274000-01-1 TRIMMABLE HORIZONTAL STABILIZER310 LUB N

LUBRICATE THS BEARINGS AND ATTACHMENT FITTINGS WITHGREASE MAT. NO. 04-004NOTE: ALTERNATIVE MPD TASK 274000-07-1 CAN BE APPLIED.Access panels :



AMM 279600/5AMT 279600-710-006MRB 274000/06

I 15 000 FHI 100 MO

ALL274000-04-1 TRIMMABLE HORIZONTAL STABILIZER210 OPT N

OPERATIONAL CHECK OF THS ACTUATOR WITH ELECTRICALMOTOR NO 3


AMM 274100/6AMT 274100-210-001MRB 274000/12

I 24 000 FHI 72 MO

ALL274100-01-1 THS MECHANICAL CONTROL100 DI310

Y

DETAILED INSPECTION OF THS MECHANICAL CONTROLPREP. : CEILING PANELS REMOVED; FLOOR PANELS REMOVED;



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 274100/6AMT 274100-220-002MRB 274000/13

I 24 000 FHI 72 MO

ALL274100-02-1 THS MECHANICAL CONTROL145 CHK N

CHECK THS MECHANICAL CONTROL CABLES FOR CORRECTTENSIONAccess panels :

241FF0.06Total access time : Hrs


AMM 122227/3AMT 122227-640-007MRB 274000/20

I 11 000 FHI 30 MO

ALL274100-03-1 THS MECHANICAL CONTROL120 LUB310

N

LUBRICATION OF THS MECHANICAL CONTROL CHAINS AND REAR CABLE (AREA OFTENSION REGULATOR).Access panels :

312AR 8110.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 274100/6AMT 274100-220-001MRB 274000/07

I 40 MO ALL274142-01-1 THS TRIM CTL CABLE TENSION COMPENSATOR310 CHK N

CHECK POINTER ON TENSION COMPENSATOR SCALE WITHINLIMITSAccess panels :



AMM 274454/5AMT 274454-720-001MRB 274000/14

I 24 000 FHI 160 MO

ALL274400-01-1 THS HYDRAULIC ACTUATION310 FNT N

FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE OFF BRAKE(APPLY TORQUE TO MANUAL CRANKING INPUT)Access panels :



AMM 274100/5AMT 274100-720-001MRB 274000/15

I 24 000 FHI 160 MO

ALL274400-02-1 THS HYDRAULIC ACTUATION310 FNT N

FUNCTIONAL CHECK OF THS ACTUATOR OVER FULL TRAVELRANGE BY REFERENCE TO MECHANICAL INDICATOR



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 274451/5AMT 274451-710-001MRB 274000/18

I 18 000 FHI 120 MO

ALL274400-03-1 THS ACTUATOR310 OPT Y

OPERATIONAL CHECK OF THS ACTUATOR NO-BACK DEVICE

Access panels :



AMM 122227/3AMT 122227-640-003MRB 274000/03

I 1 600 FHI 12 MO

ALL274451-01-1 THS ACTUATOR BALL SCREW NUT310 LUB Y

LUBRICATE THS ACTUATOR BALL SCREW NUT

Access panels :



AMM 274451/6AMT 274451-210-004MRB 274000/05

I 3 000 FHI 24 MO


CHECK OIL LEVEL OF THS ACTUATOR GEARBOX

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 274451/6AMT 274451-210-003MRB 274000/08

I 12 000 FHI 80 MO


CHECK INDICATOR OF THS ACTUATOR NO-BACK WEARDETECTION DEVICEAccess panels :



AMM 274451/6AMT 274451-220-001MRB 274000/09

I 12 000 FHI 80 MO

ALL274451-04-1 THS ACTUATOR310 DI Y

DETAILED INSPECTION OF THS ACTUATOR BALL SCREW NUTBODY AND SCREW AND CLAW STOPSAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 274451/6AMT 274451-220-002MRB 274000/10

I 12 000 FHI 40 MO

See note

ALL274451-05-1 THS ACTUATOR310 DI Y

DETAILED INSPECTION OF UPPER AND LOWER THS ACTUATORATTACHMENT (PRIMARY AND SECONDARY).NOTE: ENSURE THAT INSPECTIONS ACCORDING 274451-10-1 AND 274451-11-1 ARE CARRIED OUT PRIOR TO TASK 274451-05-1 (AND PRIOR TO ANY CLEANING), WHEN PLANNED AT THE SAME TIMEAccess panels :



AMM 274451/6AMT 274451-210-002MRB 274000/11

I 12 000 FHI 80 MO

ALL274451-06-1 THS ACTUATOR310 VCK Y

VISUAL CHECK OF THS ACTUATOR THREADED NUT (FAIL SAFENUT)Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 274451/6AMT 274451-200-001MRB 274000/17

I 15 000 FHI 100 MO

ALL274451-07-1 THS ACTUATOR310 VCK Y

CHECK BACKLASH BETWEEN THS ACTUATOR BALL SCREW NUTAND SCREWAccess panels :



AMM 274451/6AMT 274451-610-001MRB 274000/21

I 18 000 FHI 120 MO

ALL274451-09-1 THS ACTUATOR310 DRN N

DRAIN AND REFILL TRIMMABLE HORIZONTALSTABILIZER ACTUATOR GEAR BOXAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2007-06-02(FAA)AD 2008-0150(EASA)AMM 274451/6AMT 274451-220-003ISB 27-1164

I 20 MO ALL274451-10-1 THS ACTUATOR310 DI N

DETAILED INSPECTION OF THSA LOWER ATTACHMENTS FORSECONDARY LOAD PATH LOADINGNOTE: PERFORM INSPECTION PRIOR TO TASK 274451-05-1 (IF PLANNED AT THE SAME TIME) AND PRIOR TO ANY CLEANING.INTERVAL STARTING POINT IS THE AIRCRAFT FIRST FLIGHT AND NOT DELIVERYFLIGHTAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2007-06-02(FAA)AD 2008-0150(EASA)AMM 274451/6AMT 274451-220-004ISB 27-1164

I 10 MO ALL274451-11-1 THS ACTUATOR310 DI N

DETAILED INSPECTION OF THSA UPPER ATTACHMENTS FORSECONDARY LOAD PATH LOADINGNOTE: PERFORM INSPECTION PRIOR TO TASK 274451-05-1 (IF PLANNED AT THE SAME TIME) AND PRIOR TO ANY CLEANING.INTERVAL STARTING POINT IS THE AIRCRAFT FIRST FLIGHT AND NOT DELIVERYFLIGHTAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2012-0175AMT 274451-220-802ISB 27-1214

T 22 YEI 24 MO

ALL274451-12-1 THS ACTUATOR310 DI N

DETAILED INSPECTION OF THSA BALL SCREW SHAFT LOWERSPLINESNOTE :- TO BE ACCOMPLISHED BEFORE ACCUMULATING 22 YEARS,BUT NOT BEFORE 20 YEARS SINCE THSA FIRST FLIGHT.SEE EASA AD 2012-0175 FOR DETAILS OF COMPLIANCE.- TASK INTERVAL IS RELATED TO EQUIPMENT LEVEL(THSA MONTH BASED) AND NOT TO A/C LEVEL.Access panels :



AMM 275100/5AMT 275100-710-002MRB 275000/05MRB 275001/05

I 8 000 FHI 72 MO

ALL275100-02-1 FLAPS210 OPT N

OPERATIONAL CHECK OF FLAP INTERCONNECTING STRUT ANDFLAP DISCONNECT PROXIMITY SENSORS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 275400/6AMT 275400-220-006ISB 57-1133SIL 27-133

I 5 500 CY 22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

42134277

4311

4315

275100-07-1 FLAPS581 DI681

Y

VISUAL INSPECTION OF THE INNER FLAP DRIVE TRUNNIONCLAMP-TYPE STEEL RUBBING PADS FOR WEARNOTE: TASK MAY BE ACCOMPLISHED TOGETHER WITH 575221-02-1 IF INTERVAL NOT EXEEDED.PREP. : FLAPS EXTENDED;

Access panels :

193AB 193BB 194AB 194BB 734 7440.16Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 275117/6AMT 275117-280-001MRB 275000/07MRB 275001/07MRB 278000/05

NTCheck : 2255

2261

22672303

2480

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

4703

275117-01-1 FLAP/SLAT COMMAND SENSOR UNIT212 RAI Y

REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKENOTE : THE INTERVAL OF THIS TASK REFER TO "A321 TIMECONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 27.80.00/08AMT 275117-280-001MRB 27.50.00/16MRB 27.50.01/14

I 144 MO 47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

53855392

5418

54275438

5456

54695495

5555

56995709

5916

5958

275117-01-2 FLAP/SLAT COMMAND SENSOR UNIT212 FUC NR

REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5994


AMM 275144/6AMT 275144-200-001MRB 275000/06MRB 275001/06

I 8 000 FHI 72 MO

ALL275144-01-1 FLAP INTERCONNECTING STRUT580 DI680

Y

DETAILED INSPECTION OF INTERCONNECTING STRUT ANDATTACHMENTSPREP. : FLAP EXTENDED SLATS FULLY EXTENDED


AMM 275400/6AMT 275400-200-001MRB 275000/08MRB 275001/08

I 24 000 FHI 80 MO

ALL275400-01-1 FLAP TRANSMISSION ASSY570 DI670

Y

DETAILED INSPECTION OF TRANSMISSION ASSYPREP. : FLAP EXTENDED SLATS FULLY EXTENDEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 122227/3AMT 122227-640-004MRB 275000/02MRB 275001/02

I 1 800 CYI 10 MO

ALL275446-01-1 FLAP TRACKS530 LUB630

N

LUBRICATE ALL CARRIAGE ROLLERS ON ALL FLAP TRACKSPREP. : FLAP EXTENDED SLATS FULLY EXTENDED


AMM 275446-200-802MRB 27.50.01/09

I 22 000 FH ALL275446-04-1 FLAP TRACKS530 DI630

N

FLAP TRACKSDETAILED INSPECTION OF TRACKS, ROLLERS, SPHERICALBEARING AND TAB DRIVE KINEMATIC (AS FAR AS VISIBLE)NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 275446-02-1.PREPARATION:"FLAPS EXTENDED SLATS FULLY EXTENDED"


AMM 121327/3AMT 121327-612-005MRB 275000/13MRB 275001/12

I 24 000 FHI 72 MO

ALL275449-06-1 ACTUATOR ASSEMBLY575 SRV675

N

DRAIN AND REFILL FLAP ACTUATOR ASSEMBLIES WITHSEMI-FLUID



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 121327/3AMT 121327-612-002MRB 275000/03MRB 275001/03

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL275451-01-1 FLAP POWER CONTROL UNIT147 SVC N

REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL

Access panels :



AMM 122227/3AMT 122227-640-005MRB 276400/02

I 2 000 FHI 15 MO

ALL276400-01-1 SPOILER AND HYDRAULIC ACTUATION575 LUB675

N

LUBRICATE SPOILER NO 1 TO 5 ACTUATOR ATTACHMENTSPREP. : FLAP EXTENDED SLATS FULLY EXTENDED


AMM 276400/6AMT 276400-200-001MRB 276400/03

I 18 000 FHI 120 MO

ALL276400-02-1 SPOILER AND HYDRAULIC ACTUATION575 FUC675

N

CHECK SPOILER SERVOCONTROL BEARING AND HINGE BEARINGSFOR EXCESSIVE PLAY AND CONDITIONPREP. : FLAP EXTENDED SLATS FULLY EXTENDED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 278400/6AMT 278400-200-001MRB 278000/06

I 24 000 FHI 80 MO

ALL278400-01-1 SLAT TRANSMISSION ASSY147 DI190520620

Y

DETAILED INSPECTION OF TRANSMISSION ASSY

Access panels :

191BB 191BT 192BT 192FB 521BT 522AB 522CB522FB 522JB 522KB 522LB 522NB 522QB 522SB522UB 621BT 622AB 622CB 622FB 622JB 622KB622LB 622NB 622QB 622SB 622UB 734



AMM 121327/3AMT 121327-612-003MRB 278000/03

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL278451-01-1 SLAT POWER CONTROL UNIT147 SVC N

REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 122227/3AMT 122227-640-006MRB 278000/02

I 4 500 CYI 20 MO

ALL278468-01-1 SLAT TRACKS520 LUB620

N

LUBRICATE ALL TRACK ROLLERS AND PINIONS

Access panels :

521AB 521CB 521EB 522AB 522CB 522FB 522KB522LB 522NB 522QB 522SB 522UB 621AB 621CB621EB 622AB 622CB 622FB 622KB 622LB 622NB622QB 622SB 622UB



AMM 278400/6AMT 278400-210-001MRB 27.80.00/07MRB 574206-01-1MRB 574306-01-1MRB 574406-01-1MRB 574506-01-1MRB 574606-01-1

I 22 000 FHI 6 YE

ALL278468-02-1 SLAT TRACKS520 DI620

Y

DETAILED INSPECTION OF SLAT TRACKS, ROLLER BEARINGS,PINION BEARINGS AND CURVED RACK GEARS - AS VISIBLE.PREP. : FLAP EXTENDED SLATS FULLY EXTENDED

Access panels :





: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 28 FUEL


Threshold Interval

Ctrl References Eff

AMM 123228/3AMT 123228-281-001MRB 281100/01

I 36 HR ALL281100-01-2 TANKS190 SRV500600

Y

DRAIN WATER CONTENTNOTE : DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR'S EXPERIENCE A LESS FREQUENT INITIAL INTERVAL MAY BE USEDAccess panels :

195BB 196BB0.04Total access time : Hrs


AMM 281100/6AMT 281100-200-002MRB 281100/02MRB 281300/02MRB 282100/01MRB 282500/01

I 750 FHI 6 MO

ALL281100-02-1 TANKS196 CHK N

CHECK LEAK MONITOR FOR EVIDENCE OF FUEL LEAKAGE ANDCORRECT CLOSURE OF THE VALVE


AMM 123228/3AMT 123228-281-003SIL 28-079

I 1 500 FHI 8 MO

2ACheck :

ALL281100-04-2 FUEL TANK MICROBILOGICAL CONTAMINATION190 SVC500600

N

SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATIONANALYSISNOTE : INTERVAL DEPENDING ON EACH INDIVIDUAL OPERATOR´S ENVIRONMENT



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 281100/6AMT 281100-200-001MRB 281100/03

I 160 MO ALL281142-01-1 TANK FLAP VALVES540 CHK640

N

CHECK FOR FULL AND FREE MOVEMENT OF CLACK VALVESPREP. : TANK DEFUELINGAccess panels :



AMM 281200/02AMM 281200/06AMT 281200-210-001

I 750 FH ALL281200-01-1 TANK VENTING SYS500 VCK600

N

VISUAL CHECK OF VENT SURGE TANK BURST DISC (EXTERNAL)


AMM 281247/6AMT 281247-200-001MRB 281200/01

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL281247-01-1 NACA VENT INTAKE550 GVI650

Y

VISUAL CHECK OF NACA INTAKE FOR SIGNS OF BLOCKAGE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 281300/6AMT 281300-200-001MRB 281300/01MRB 282200/03

I 4 MO ALL281343-01-1 DRAIN MAST148 VCK N

VISUAL CHECK OF DRAIN MAST FOR OBSTRUCTION


AMT 281800-200-002MRB 28.18.00/01

I 144 MO ALL281800-03-1 IGNITION PREVENTION140 DI540550640650

Y

DETAILED INSPECTION OF TANK BONDING LEADS (SFAR88)PREP. : 147AZ

Access panels :

148AZ 540AB 540BB 540CB 540DB 540EB 540FB540GB 540HB 540JB 540KB 540LB 540MB 540NB540PB 540QB 540RB 550AB 550BB 550CB 550DB640AB 640BB 640CB 640DB 640EB 640FB 640GB640HB 640JB 640KB 640LB 640MB 640NB 640PB640QB 640RB 650AB 650BB 650CB 650DB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 281844-210-001MRB 28.18.00/02

I 144 MO ALL281800-04-1 IGNITION PREVENTION140 GVI540550640650

Y

GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING ANDPROBE ATTACHMENTS (SFAR88)PREP. : 147AZ

Access panels :

148AZ 540AB 540BB 540CB 540DB 540EB 540FB540GB 540HB 540JB 540KB 540LB 540MB 540NB540PB 540QB 540RB 550AB 550BB 550CB 550DB640AB 640BB 640CB 640DB 640EB 640FB 640GB640HB 640JB 640KB 640LB 640MB 640NB 640PB640QB 640RB 650AB 650BB 650CB 650DB



AMT 281852-210-001MRB 28.18.00/05


Y

GENERAL VISUAL INSPECTION OF CENTER TANK FWD CARGOBAY ISOLATION MATS (SFAR88)Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 281842-210-001MRB 28.18.00/06


Y

GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVECENTER TANK (SFAR88)PREP. : FLOOR PANELS FROM FR 36 TO FR 46;


AMM 281841/6AMT 281841-210-001MRB 28.18.00/07


Y

GENERAL VISUAL INSPECTION OF WING LEADING EDGE ANDTRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS(SFAR88)Access panels :

521AB 521BB 521BT 521CB 521EB 521GB 521HB522AB 522AT 522CB 522EB 522FB 522HB 522JB522KB 522LB 522NB 522QB 522SB 522UB 572AB572BB 573AB 573BB 573CB 573DB 573EB 573FB574AB 574BB 575AB 575AT 575BB 575CB 575DB575EB 575FB 575GB 575HB 575KB 575LB 575MB621AB 621BB 621BT 621CB 621EB 621GB 621HB622AB 622AT 622CB 622EB 622FB 622HB 622JB622KB 622LB 622NB 622QB 622SB 622UB 672AB672BB 673AB 673BB 673CB 673DB 673EB 673FB674AB 674BB 675AB 675AT 675BB 675CB 675DB675EB 675FB 675GB 675HB 675KB 675LB 675MB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 281843-210-001MRB 28.18.00/08


Y

GENERAL VISUAL INSPECTION OF WING FUEL PUMPELECTRICAL CONNECTIONS AND UNDERWING ELECTRICALSUPPLY CABLE (SFAR88)PREP. : FUEL PUMP FAIRINGS;


AMT 281851-210-001MRB 28.18.00/09


Y

GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS(SFAR88)Access panels :

147AZ 148AZ 540AB 640AB0.18Total access time : Hrs


AMM 282100/5AMT 282100-710-002MRB 282100/04

I 24 000 FH ALL282100-01-1 MAIN FUEL PUMP SYSTEM210 OPT N

OPERATIONAL CHECK OF WING TANK PUMP PRESSURE SENSELINE CHECK VALVES



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282100/5AMT 282100-710-008MRB 282100/08

I 15 000 FHI 100 MO

ALL282100-03-1 MAIN FUEL PUMP SYSTEM210 OPT Y

OPERATIONAL CHECK OF AIR RELEASE VALVES TO ENSUREADEQUATE FUEL FLOW UNDER SUCTION FEED CONDITIONS


AMM 282100/5AMT 282100-790-002MRB 282100/02

I 7 500 FHI 50 MO

22552261

2267

23032480

2974

30053013

3022

31983315

3355

282100-05-1 FUEL PUMP SYSTEM410 CHK420520620

N

VISUAL CHECK OF PIPES, COUPLINGS AND LP VALVEEXTERNAL TO TANK FROM FRONT SPAR TO DISCONNECT PANEL FORLEAKS WITH BOOSTER PUMP ON AND LP VALVE OPEN

Access panels :

413AL 413CL 413EL 414AZ 414FR 423AL 423AZ423CL 423FL 424ER 437AL 447AL 471AL 472AR481AL 482AR 522AB 622AB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282100/5AMT 282100-790-002MRB 282100/02

I 7 500 FHI 50 MO

36003737

3862

39643966

4136

42134277

4311

4315

282100-05-2 FUEL PUMP SYSTEM410 CHK420520620

N

VISUAL CHECK OF PIPES, COUPLINGS AND LP VALVEEXTERNAL TO TANK FROM FRONT SPAR TO DISCONNECT PANEL FORLEAKS WITH BOOSTER PUMP ON AND LP VALVE OPEN

Access panels :

413AL 413CL 414AZ 423AL 423AZ 423CL 423CR437AL 447AL 471AL 471AR 471BL 471BR 481AL481AR 481BL 481BR



AMM 282100/6AMT 282100-280-001MRB 282100/09

I 24 000 FHI 160 MO

ALL282100-06-1 MAIN FUEL PUMP SYSTEM540 CHK640

N

CHECK SUCTION VALVES FOR FULL AND FREEMOVEMENT



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282000/4AMT 282000-960-001SIL 28-073

I 24 000 FHI 18 000 CYI 80 MO

22552261

2267

23032480

2974

30053013

3022

31983315

3355

282100-07-1 MAIN FUEL PUMP SYSTEM470 DIS480

N

DISCARD "O" RINGS ON PYLON ENGINE FUEL FEED PIPECONNECTORS AND REPLACE BY NEW "O" RINGS

Access panels :

414FR 423FL 471AL 472AR 481AL 482AR0.27Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282000/4AMT 282000-960-001SIL 28-073

I 24 000 FHI 18 000 CYI 80 MO

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385

282100-07-2 MAIN FUEL PUMP SYSTEM470 DIS480

NR

DISCARD "O" RINGS ON PYLON ENGINE FUEL FEED PIPECONNECTORS AND REPLACE BY NEW "O" RINGS


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :

471AL 471AR 471BL 471BR 481AL 481AR 481BL481BR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 282100-720-802I 144 MO ALL282100-10-1 MAIN FUEL PUMP SYSTEM540 FUC640

N

REMOVE AIR RELEASE VALVE FOR FUNCTIONAL CHECK OFFLOATNOTE: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT C CHECK.Access panels :

540CB 640CB0.12Total access time : Hrs

AMM 282200/5AMT 282200-210-001MRB 282200/01

I 750 FH ALL282200-02-1 APU FUEL PUMP SYSTEM148 CHK N

CHECK FOR LEAKAGE FROM SHROUD DRAIN MAST AND APUCOMPARTMENT DRAIN MAST WITH APU FUEL PUMP RUNNING


AMT 282300-720-001MRB 28.23.00/01

I 7 500 FHI 50 MO

ALL282300-01-2 CROSSFEED SYSTEM210 OPT Y

CROSSFEED SYSTEMOPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUALMOTORS AND CHECK FUEL FLOW IN "OPEN" AND FUEL SHUTOFF IN "CLOSED" POSITIONSAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282400/5AMT 282400-790-003MRB 282400/01

I 15 000 FHI 100 MO

See note

ALL282400-01-1 ENGINE LOW PRESSURE SHUT OFF210 OPT N

OPERATIONAL CHECK OF LP SHUT OFF VALVES AND THEIRCONTROLS TO ENSURE NO FLOW WHEN SELECTED CLOSED WITHBOOSTER PUMP ONNOTE : TASK MAY BE PERFORMED AT OPPOTUNITY OF ENGINE REMOVAL PROVIDED INTERVAL NOT EXCEEDED


AMM 282541/6AMT 282541-200-001MRB 282500/02

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL282541-01-2 COUPLING REFUEL/DEFUEL522 DI622

Y

DETAILED INSPECTION OF COUPLING REFUEL/DEFUEL.

Access panels :

522HB 622HB0.06Total access time : Hrs


AMM 282600/6AMT 282600-210-001MRB 282600/01

I 66 MO ALL282600-01-1 MAIN TRANSFER SYSTEM540 CHK640

N

MANUALLY OPERATE THE TRANSFER SYSTEM DISCHARGECHECK VALVE ON RIB 1 AND CHECK FOR FULL ANDFREE MOVEMENT



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/6AMT 282800-200-003MRB 282800/01

I 750 FHI 6 MO

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

282800-01-1 ADDITIONAL CENTER TANK TRANSFER SYSTEM190 OPC N

OPERATIONAL CHECK OF LEAK MONITOR FOR EVIDENCE OFFUEL LEAKAGENOTE: IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 123228/3AMT 123228-281-005MRB 282800/03

I 4 MOSee note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

282800-03-1 ADDITIONAL CENTER TANK TRANSFER SYS190 OPT N

OPERATE WATER DRAIN VALVE IN ACT TO DRAINACCUMULATE WATERNOTE: DEPENDING ON OPERATING ENVIRONMENTAND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/5AMT 282800-710-002MRB 282800/4

I 22 500 FHI 150 MO

See note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315


OPERATE CHECK OF MOTOR 1 OF TRANSFER VALVENOTE: IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/5AMT 282800-710-001MRB 282800/13

I 22 500 FHI 150 MO

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

282800-05-2 ADDITIONAL CENTER TANK TRANSFER SYSTEM210 OPC N

OPERATIONAL CHECK OF THE ACT MANUAL TRANSFER SYSTEMNOTE:- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION. - TASK IS INCLUDED IN THE ACT INSTALLATION PROCEDURE. CREDIT CAN BE TAKEN FOR ACCOMPLISHMENT OF THE TASK AT THIS OPPORTUNITY



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282839/4AMT 282839-920-001MRB 282800/06

I 15 000 FHI 100 MO

See note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

282800-06-2 ADDITIONAL CENTER TANK TRANSFER SYS150 DIS N

REPLACE ACT AIR INLET FILTERNOTE : IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.

Access panels :

152YW0.02Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/5AMT 282800-720-001MRB 282800/7

I 22 500 FHI 150 MO

See note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

282800-07-1 ADDITIONAL CENTER TANK TRANSFER SYS150 FUC N

FUNCTIONAL CHECK OF ACT PRESSURE REDUCING VALVENOTE: IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/5AMT 282800-720-002MRB 282800/08

I 72 MOSee note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315


OPERATIONAL CHECK OF ACT INWARD RELIEF VALVENOTE:- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION. - ACT SERIAL NUMBER TO BE TRACKED SINCE TASK ACCOMPLISHMENT IS A FUNCTION OF ACT AGE AND NOT AIRCRAFT AGE.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/6AMT 282800-200-002MRB 282800/09

I 750 FHI 6 MO

See note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

282800-09-1 ADDITIONAL CENTER TANK TRANSFER SYS150 GVI N

GENERAL VISUAL INSPECTION OF THE INTEGRATED IMPACTWALL(S) (IF INSTALLED)



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 281100/5AMT 281100-790-011MRB 282800/12

I 5 YE 29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

282800-18-1 ADDITIONAL CENTER TANK TRANSFER SYSTEM150 FUC N

FUNCTIONAL CHECK OF THE VENT/TRANSFER PIPESHROUDS AND ACT DRAIN PIPE CONNECTORSNOTE: IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.

Access panels :

241EF 241JF0.12Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282900/5AMT 282900-710-002MRB 282900/02

I 24 000 FHI 160 MO

ALL282900-02-1 APU LOW PRESSURE FUEL SHUT OFF210 CHK N

OPERATIONAL CHECK OF APU LP FUEL VALVE FOR EVIDENCEOF INTERNAL LEAKAGE WITH LEFT WING TANK PUMP ONAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 291000/6AMT 291000-200-006MRB 291000/06MRB 291000/28

I 1 000 FHI 12 MO

ALL290000-03-1 HYDRAULIC POWER435 CHK445

Y

CHECK CLOGGING INDICATOR ON ENGINE DRIVEN PUMP (EDP) CASEDRAIN FILTER (POP OUT NOT PROTRUDING).

Access panels :

437AL 447AL0.04Total access time : Hrs


AMM 291000/6AMT 291000-210-002MRB 291000/28

I 1 000 FHI 12 MO

ALL290000-05-1 HYDRAULIC POWER100 VCK N

CHECK CLOGGING INDICATORS OF THE FOLLOWINGFILTERS(POP OUT NOT PROTRUDING)-HIGH PRESSURE DELIVERY-GROUND SERVICING (RESERVOIR FILLING)-RETURN (LOW PRESSURE)-BLUE HYDRAULIC SYSTEM ELECTRICAL PUMP CASEDRAIN-RESERVOIR PRESSURIZATION FILTER-WATER SEPARATORAccess panels :

195BB 196BB 197CB 197FB 7340.08Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 291000-200-025SIL 29-064

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL290000-07-1 HYDRAULIC SYSTEM SEALS100 VCK N

VISUAL CHECK OF HIGH AND LOW PRESSURE MANIFOLDS ANDGROUND SERVICE PANELS AND MANIFOLDS FOR SIGNS OFEXTERNAL LEAKAGE.


AMM 291000/6AMT 291000-200-001MRB 291000/01

I 750 FHI 6 MO

ALL291000-01-1 MAIN HYDRAULIC POWER100 VCK N

CHECK FLUID LEVEL ON RESERVOIR INDICATORS

Access panels :

196BB 197FB 7440.04Total access time : Hrs


AMM 291000/6AMT 291000-200-002MRB 291000/02

I 750 FHI 6 MO

ALL291000-02-1 MAIN HYDRAULIC POWER100 CHK N

CHECK RESERVOIR AIR PRESSURE ON RESERVOIR GAUGE

Access panels :

196BB 197FB 7440.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 292300/5AMT 292300-710-002MRB 291000/38

I 22 000 FHI 144 MO

ALL291000-04-1 MAIN HYDRAULIC POWER210 FUC N

FUNCTIONAL CHECK OF PTU GREEN TO YELLOW


AMM 291400/3AMT 291400-680-001MRB 291000/13

I 2 250 FHI 24 MO

ALL291000-05-1 MAIN HYDRAULIC POWER195 DRN Y

DRAIN WATER SEPARATOR

Access panels :



AMM 292300/5AMT 292300-710-003MRB 291000/37

I 7 500 FHI 50 MO


FUNCTIONAL CHECK OF PTU YELLOW TO GREEN


AMM 291000/5AMT 291000-720-002MRB 291000/19

I 36 000 FHI 144 MO

ALL291000-08-1 MAIN HYDRAULIC POWER210 FNT N

FUNCTIONAL CHECK OF PRIORITY VALVES IN GREEN, BLUEAND YELLOW SYSTEM



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 291000/5AMT 291000-710-001MRB 291000/14

I 10 000 FHI 72 MO

ALL291000-09-1 MAIN HYDRAULIC POWER210 OPT N

OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT OFFVALVES AND ASSOCIATED INDICATING SYSTEM.


AMM 291000/5AMT 291000-720-001MRB 291000/20

I 16 000 FHI 144 MO

See note

ALL291000-10-1 MAIN HYDRAULIC POWER574 FNT674

Y

FUNCTIONAL CHECK OF HYDRAULIC FIRE SHUT OFF VALVESNOTE : TASK MAY BE PERFORMED AT OPPOTUNITY OF ENGINE REMOVAL PROVIDED INTERVAL NOT EXCEEDEDAccess panels :



AMM 291000/6AMT 291000-200-008MRB 291000/22SIL 29-092

I 600 FHI 6 MO


CHECK NITROGEN CHARGE PRESSURE ON HYDRAULICPOWER ACCUMULATORS.

Access panels :

196BB 7440.02Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 123229/3AMT 123229-281-001MRB 291000/23SIL 29-081

I 7 500 FHI 24 MO

See note

ALL291000-15-1 MAIN HYDRAULIC POWER100 DI Y

ANALYZE HYDRAULIC FLUIDNOTE : DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESSFREQUENT OR MORE FREQUENT FREQUENT INITIAL INTERVAL MAY BE USEDAccess panels :



AMM 291700/3AMT 291700-680-001MRB 291000/32

I 1 500 FHI 12 MO

ALL291000-18-1 MAIN HYDRAULIC POWER148 SVC Y

DRAIN RECOVERY TANK

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 292300-710-006MRB 29.10.00/35

I 7 500 FHI 50 MO

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715251

5275

53065340

5385

53925418

5438

54565495

5555

56995916

5958

291000-19-1 MAIN/AUXILIARY POWER210 OPC YR

OPERATIONAL CHECK OF PTU INHIBITION LOGIC


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

196BB 734 7440.06Total access time : Hrs


AMT 291000-710-004MRB 29.10.00/36

I 24 MO ALL291000-20-1 MAIN/AUXILIARY POWER210 OPC Y

OPERATIONAL CHECK OF EDP DEPESSURIZATION


AMM 291200/5AMT 291200-710-001MRB 291000/10

I 7 500 FHI 50 MO

ALL291200-01-1 BLUE MAIN HYDRAULIC POWER210 FNT N

FUNCTIONAL CHECK OF BLUE ELECTRICAL PUMP PRESSURE BYREADING ECAM INDICATION


AMM 291000/6AMT 291000-220-001MRB 291000/18

I 24 000 FHI 144 MO

ALL291900-01-1 GROUND INTERNAL LEAK TEST SYSTEM210 FNT N

FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OFYELLOW AND GREEN HYDRAULIC SYSTEMS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 292200/5AMT 292200-280-002MRB 291000/27

I 72 MO ALL292000-07-1 AUXILIARY HYDRAULIC POWER190 FUC N

FUNCTIONAL CHECK OF ANTI-ICING DEVICE MAGNETS

Access panels :

197EB0.02Total access time : Hrs


AMM 292251/6AMT 292251-200-003MRB 291000/09

I 20 MO ALL292251-02-1 RAM AIR TURBINE195 DI Y

DETAILED INSPECTION OF RAM AIR TURBINE ( RAT )ASSEMBLY AND DOORS IN DEPLOYED POSITIONPREP. : RAM AIR TURBINE EXTENSIONAccess panels :



AMM 293100/5AMT 293100-710-001MRB 293000/05

I 24 000 FH ALL293100-01-1 HYDRAULIC FLUID QUANTITY INDICATING190 FNT N

FUNCTIONAL CHECK OF RESERVOIR LOW LEVEL WARNING

Access panels :

197CB 197EB 198CB0.06Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 293400/5AMT 293400-710-001MRB 293000/04

I 7 500 FHI 50 MO

ALL293400-01-1 RESERVOIR PRESSURIZATION INDICATING210 OPT N

OPERATIONAL CHECK OF RESERVOIR LOW AIR PRESSUREWARNING



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 30 ICE AND RAIN PROTECTION


Threshold Interval

Ctrl References Eff

AMM 301151/4AMT 301151-960-001MRB 301100/03

I 22 000 FH ALL301151-01-2 WING ANTI ICE CONTROL VALVE522 DIS622

N

REPLACE WING ANTI-ICING FILTERNOTE: APPLICABILITY TASK: AIRCRAF EQUIPTED WITH PART NUMBER:"P/N SAS911* OR P/N SAS912*OR P/N 38E93*"Access panels :



AMM 302100/5AMT 302100-710-001MRB 302100/02

I 48 MO

2CCheck :

ALL302100-01-1 ENGINE AIR INTAKE ICE PROTECTION210 OPT N

OPERATIONAL CHECK OF ENGINE ANTI-ICE SYSTEM FAULTWARNINGAccess panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 30 ICE AND RAIN PROTECTION


Threshold Interval

Ctrl References Eff

AMM 302149/6AMT 302149-200-010MRB 302100/01

I 6 000 FHI 40 MO

ALL302149-02-1 ENGINE AIR INTAKE ANTI-ICE DUCT438 DI448

N

DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLYDUCTS AND ASSOCIATED HARDWARE IN THE CORE COMPARTMENTAccess panels :

438AR 448AR 452AR 462AR0.04Total access time : Hrs


AMT 303100-720-001SIL 34-084

I 24 MO ALL303100-01-1 PROBE ICE PROTECTION120 FUC N

FUNCTIONAL CHECK OF THE INSULATION RESISTANCE OF THEPITOT PROBE HEATER



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 31 INDICATING & RECORDING SYSTEMS


Threshold Interval

Ctrl References Eff


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 313200/2AMT 313200-869-002MRB 212100/01MRB 212600/01MRB 212800/01MRB 213100/01MRB 215000/01MRB 233000/01MRB 242000/04MRB 244000/01MRB 261200/02MRB 261300/02MRB 275000/01MRB 275001/01MRB 278000/01MRB 281500/01MRB 282800/10MRB 284200/01MRB 284600/01MRB 293000/03MRB 303100/01MRB 304200/01MRB 324000/04MRB 360000/01MRB 494000/01MRB 494000/01-13MRB 494000/01-32MRB 494000/01-36MRB 495120/01MRB 495120/01-36MRB 496100/01MRB 496100/01-36

I 750 FHI 6 MO

ALL313000-01-1 CFDS AND DATA RECORDING SYSTEM210 OPC N

READ CENTRALIZED FAULT DISPLAY SYSTEM (CFDS)FOR CLASS 3 FAULTS.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

MRB 497000/01MRB 497000/01-32MRB 497000/01-36MRB 499000/01MRB 499000/01-32MRB 499100/01MRB 499120/01-13MRB 499300/01MRB 499300/01-36MRB 730000/03MRB 730000/03-C5MRB 732200/01-I2MRB 732534/01MRB 732534/01-C5MRB 732534/01-I2MRB 783100/01-I2MRB 793000/01MRB 793000/01-I2



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 313355/4AMT 313355-920-001MRB 313300/02MRB 313600/01

See noteNTCheck :

ALL313300-01-1 DFDR SYSTEM INTERCONNECTION312 DIS Y

DISCARD UNDERWATER LOCATOR BEACON BATTERYNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 313300/5AMT 313300-710-015MRB 313300/04MRB 313600/02

See noteNTCheck :

ALL313300-03-1 DFDR SYSTEM INTERCONNECTION312 OPT Y

OPERATIONAL CHECK OF ULBNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 313300/5AMT 313300-710-006MRB 313300/05MRB 313601/03

I 24 MO ALL313300-04-1 DFDR SYSTEM INTERCONNECTION210 OPC N

OPERATIONAL CHECK OF DFDR VIA MCDU



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 313300-710-803I 24 000 FHI 160 MO

46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

54385456

5469

54955555

5699

5709

313300-07-1 DFDR SYSTEM INTERCONNECTION121 OP NR

OPERATIONAL CHECK OF WGL-QAR INTERLOCK LOGICNOTE: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT C CHECK.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

5994

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 316000/5AMT 316000-740-005MRB 316001/02

I 7 500 FHI 50 MO

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715251

5275

5306

315000-01-1 CENTRAL WARNING SYSTEMS/ELECTRONIC210 OPC NR

INSTRUMENT SYSTEM (EIS)OPERATIONAL CHECK OF CORRECT OPERATION OF PFD-ND ANDECAM-ND MANUAL TRANSFER


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5340

5385

53925418

5438

54565495

5555

56995916

5958



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 316000/5AMT 316000-710-005MRB 316001/04

I 7 500 FHI 50 MO

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715251

5275

5306


INSTRUMENT SYSTEM (EIS)OPERATIONAL CHECK OF CORRECT OPERATION OF EFIS ANDECAM DMC AUTOMATIC AND MANUAL TRANSFER


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5340

5385

53925418

5438

54565495

5555

56995916

5958



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 316000/5AMT 316000-710-006MRB 316001/03

I 7 500 FHI 50 MO

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715251

5275

5306


INSTRUMENT SYSTEM (EIS)OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHENBUSBAR 101XP IS LOST


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5340

5385

53925418

5438

54565495

5555

56995916

5958


AMM 316000/5AMT 316000-710-002MRB 315000/01MRB 316000/01

I 6 000 FHI 48 MO

2255

2261

22672303

2480

316000-01-1 ELECTRONIC INSTRUMENT SYSTEM210 OPT N

OPERATIONAL CHECK OF EFIS/ECAM SWITCHING FUNCTIONS:- MANUAL DMC 1 + 2 TO DMC 3 SWITCHING- MANUAL PFD/ND TRANSFER- MANUAL ECAM/ND TRANSFER- AUTOMATIC UPPER DU/LOWER DU TRANSFER- AUTOMATIC PFD/ND TRANSFER



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 316000/5AMT 316000-740-002MRB 316000/02

I 7 500 FHI 50 MO

22552261

2267

23032480

316000-02-1 ELECTRONIC INSTRUMENT SYSTEM210 TST N

PERFORM ELECTRONIC INSTRUMENT SYSTEM ( EIS )INPUT TEST

AMM 316322/4AMT 316322-400-002SIL 31-025

I 2 400 FHI 24 MO

2255

2261

22672303

2480

316322-01-1 DISPLAY UNIT210 SWA N

REPOSITION ALL CATHODE RAY TUBES BY SWAPPINGALL DISPLAY UNITS FROM ONE POSITION(PFD,ND,UPPER ECAM,LOWER ECAM)TO ANOTHERNOTE:INTERVAL MAY BE ADJUSTED IN ACCORDANCE TOOPERATOR'S EXPERIENCE


AMM 316322/6AMT 316322-200-001SIL 31-030

T 6 000 FHT 48 MOI 1 200 FHI 12 MO

See note

22552261

2267

23032480

316322-02-1 DISPLAY UNIT210 FUC N

FUNCTIONAL CHECK OF DISPLAY UNITS BRIGHTNESSNOTE : INTERVAL MAY BE ADJUSTED IN ACCORDANCEWITH OPERATOR'S EXPERIENCE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 122232/3AMT 122232-640-001MRB 32.11.00/02MRB 32.11.00/18MRB 32.30.00/03

I 500 CYI 4 MO

ALL321000-01-1 MAIN LANDING GEAR AND DOORS731 LUB741

N

LUBRICATION OF MAIN LANDING GEAR AND DOORS

Access panels :



AMT 321100-220-006MRB 32.11.00/15

I 20 000 CYI 120 MO

ALL321100-15-1 MAIN GEAR731 SDI741

N

SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGSIN MLG AIRFRAME ATTACHMENT FITTINGSPREP. : AIRCRAFT JACKING; MAIN LANDING GEAR REMOVAL;Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 321111/4AMT 321111-920-001MRB 32.11.00/14MRB 32.11.00/19MRB 321105-03-1MRB 321107-03-1MRB 321109-02-1MRB 321110-03-1MRB 321111-02-1MRB 321113-02-1MRB 321116-02-1MRB 321125-02-1MRB 321128-03-1MRB 321135-01-1MRB 321135-02-1MRB 321136-02-1MRB 321140-01-1MRB 321141-01-1MRB 321142-01-1MRB 321151-01-1MRB 321152-01-1MRB 321155-01-1MRB 321155-01-2MRB 321160-01-1MRB 321162-01-1MRB 321164-01-1MRB 321165-01-1MRB 321167-01-1MRB 321168-01-1

NTCheck : ALL321111-01-2 MLG731 SDI741

N

SPECIAL DETAILED INSPECTION (OVERHAUL) OF MAIN GEAR(OFF AIRCRAFT)PREP. : AIRCRAFT JACKING; MAIN LANDING GEAR REMOVAL;NOTE: RII TASK


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 321111/6AMT 321111-200-001MRB 32.11.00/13

I 1 500 CYI 18 MO

ALL321111-03-1 MLG TORQUE LINK DAMPER RESERVOIR731 FUC741

N

CHECK OF MLG TORQUE LINK DAMPER FLUID LEVEL


AMM 121232/3AMT 121232-611-004MRB 321100/04

I 10 000 CYI 80 MO

ALL321113-03-1 MAIN LANDING GEAR SHOCK ABSORBER731 FUC741

N

CHECK OF MLG SHOCK ABSORBER FLUID LEVELPREP. : AIRCRAFT JACKING


AMM 121432/3AMT 121432-614-003MRB 321100/03

I 5 000 CYI 24 MO

ALL321113-04-1 MAIN LANDING GEAR SHOCK ABSORBER731 FUC741

N

CHECK OF MLG SHOCK ABSORBER CHARGE PRESSURE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 321127/6AMT 321127-200-001MRB 321100/05

I 10 000 CY ALL321127-01-1 MAIN LANDING GEAR TORQUE LINK731 CHK741

Y

CHECK OF MLG TORQUE LINKS FOR EXCESSIVE PLAY



I 500 CYI 4 MO

ALL322000-01-1 NOSE LANDING GEAR AND DOORS710 LUB N

LUBRICATION OF NOSE LANDING GEAR AND DOORS

Access panels :



AMT 322100-200-016MRB 32.21.00/07

I 20 000 CYI 120 MO

ALL322100-07-1 NOSE GEAR710 SDI N

SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGSIN NLG AIRFRAME ATTACHMENT FITTINGS.PREP. : NLG REMOVED; AIRCRAFT JACKING;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 322111/4AMT 322100-200-802MRB 32.21.00/05MRB 32.50.00/02MRB 322105-03-1MRB 322110-03-1MRB 322115-03-1MRB 322120-02-1MRB 322130-02-1MRB 322140-02-1MRB 322146-01-1MRB 322147-01-1MRB 322148-01-1MRB 322149-01-1MRB 322150-01-1MRB 322160-01-1MRB 322161-01-1

NTCheck : ALL322111-01-1 NOSE LANDING GEAR710 RST N

SPECIAL DETAILED INSPECTION (OVERHAUL) OF NOSE GEAR(OFF AIRCRAFT)PREP. : NLG REMOVED; AIRCRAFT JACKING;NOTE: RII TASK

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 121432/3AMT 121232-610-002MRB 322100/03

I 5 000 CYI 24 MO

CCheck :

ALL322113-01-1 NOSE LANDING GEAR SHOCK ABSORBER711 FUC N

CHECK OF NLG SHOCK ABSORBER CHARGE PRESSUREAND FLUID LEVEL.

Access panels :



AMM 322100/6AMT 322100-200-003ISB 32-1252MRB 322100/02

I 5 000 CYSee note

ALL322127-01-1 NOSE LANDING GEAR TORQUE LINK711 FUC Y

CHECK OF NLG TORQUE LINKS FOR EXCESSIVE PLAYNOTE: INCLUDING CHECK OF TORQUE LINK APEX PIN FOR CRACKS, WHERE APPLICABLE


ISB 32-1323I 4 500 CYI 20 MO

2255

2261

22672303

2480

322128-01-1 NOSE LANDING GEAR711 GVI Y

INSPECTION FOR BARREL WEAR



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 323000-200-002MRB 32.30.00/01

I 750 FHI 4 MO

ALL323000-01-1 NORMAL EXTENSION AND RETRACTION711 DI731741

N

VISUAL CHECK OF NLG AND MLG DOWNLOCK SPRINGS ANDATTACHMENTS.

Skills :AF1 0.40 MHrsMEC1 0.20 MHrs

AMT 528100-220-002MRB 32.30.00/16MRB 32.30.00/18

I 20 000 CYI 120 MO

ALL323000-16-1 NORMAL EXTENSION AND RETRACTION711 SDI731741

Y

SPECIAL DETAILED INSPECTION OF MLG AND NLG DOOR HINGEBEARINGS, ATTACHMENT LUG BUSHINGS AND PINS AND DOORACTUATING CYLINDERS ATTACHMENT LUG BUSHINGS AND PINS.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 323100-720-008MRB 32.30.00/17

I 4 000 FHI 26 MO

37373862

3964

39664136

4213

42774311

4315

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

5555

323000-17-1 NORMAL EXTENSION AND RETRACTION210 FUC YR

FUNCTIONAL CHECK OF LGCIU POWER SUPPLY RELAYS.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5699

5916

5958


AMT 323100-210-002MRB 32.30.00/19

I 750 FHI 6 MO

ALL323000-19-1 NORMAL EXTENSION AND RETRACTION711 GVI731741

Y

GENERAL VISUAL INSPECTION OF L/G EXTENSION /RETRACTION SYSTEM COMPONENTSAccess panels :



AMM 326900/5AMT 326900-740-001MRB 323000/02

I 750 FHI 6 MO

ALL323100-01-1 NORMAL EXTENSION AND RETRACTION210 VCK N

BITE CHECK OF LANDING GEAR CONTROL INTERFACE UNIT(LGCIU) USING MCDU (TO ENSURE THAT CONTINUOUS BITE ISOPERATIVE)



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 323100/6AMT 323100-200-001MRB 323000/07

I 3 500 CYI 24 MO

ALL323100-02-1 NORMAL EXTENSION AND RETRACTION711 DI731741

Y

DETAILED INSPECTION OF GEAR UPLOCK AND DOOR UPLOCKUNITS AND ROLLERS.Access panels :



AMM 323100/5AMT 323100-710-001MRB 323000/11

I 18 000 CYI 144 MO

ALL323100-03-1 NORMAL EXTENSION AND RETRACTION210 OPT N

OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK


AMM 323100/5AMT 323100-710-005MRB 323000/12

I 15 000 FHI 72 MO

ALL323100-04-1 NORMAL EXTENSION AND RETRACTION210 OPT Y

OPERATIONAL CHECK TO ENSURE SAFETY VALVE CLOSES AT260 KTSPREP : APU RUNNING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 323000/6AMT 323000-200-001MRB 32.30.00/06

I 5 000 CYI 24 MO

ALL323100-05-1 NORMAL EXTENSION AND RETRACTION120 DI Y

DETAILED INSPECTION OF NOSE GEAR DOOR OPERATINGMECHANISMAccess panels :



AMM 326100/5AMT 326100-710-001MRB 323000/05

I 7 500 FHI 50 MO

ALL323100-06-1 NORMAL EXTENSION AND RETRACTION210 OPT N

BITE CHECK USING MCDU TO ENSURE "GEAR NOT DOWN FORLANDING" WARNINGS OPERATIVE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 323122-920-001ISB 32-1307MRB 322152-01-1MRB 322153-01-1VSB 580-32-3160

I 20 000 CYI 10 YE

ALL323100-08-1 NORMAL EXTENSION AND RETRACTION711 RST N

SPECIAL DETAILED INSPECTION (OVERHAUL) OF THE NOSELANDING GEAR ACTUATING CYLINDER AND GEAR ATTACHMENT PIN (OFF AIRCRAFT).PREP. : ACTUATING CYLINDER - NLG;NOTE : REFER TO APPENDIX 7 OF MPD FOR LANDING GEAR OVERHAUL PROCEDURES DOCUMENTNOTE : CPCPAccess panels :



AMT 323100-220-002MRB 321147-01-1MRB 321148-01-1MRB 321171-01-1MRB 321172-01-1MRB 321173-01-1MRB 321174-01-1

I 20 000 CYI 10 YE

ALL323100-09-1 NORMAL EXTENSION AND RETRACTION731 SDI741

N

SPECIAL DETAILED INSPECTION (OVERHAUL) OF THE MAINLANDING GEAR RETRACTION ACTUATOR AND ATTACHMENT PINS(OFF AIRCRAFT)PREP. : RETRACTION ACTUATOR REMOVED.;NOTE : CPCPNOTE : REFER TO APPENDIX 7 OF MPD FOR LANDING GEAR OVERHAUL PROCEDURES DOCUMENTAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 323100/6AMT 323100-200-003ISB 32-1298

T 25 000 CYI 600 CY

See note

22552261

2267

23032480

323105-01-1 NORMAL EXTENSION AND RETRACTION - INSTL731 DI741

N

DETAILED INSPECTION OF RETRACTION ACTUATORNOTE: INITIAL ACCOMPLISHMENT IS RECOMMENDED AFTER 20000 FC BUT BEFORE 25000 FC FROM ENTRY INTO SERVICE (EIS)



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2011-0069AD 2011-13-11AOT 32A1390ISB 32-1390

T 800 CYI 425 CY

22672480

3005

30133022

3198

37373862

4136

42134311

4315

46694737

4783

48264863

4945

49715241

5247

52515275

5297

53065340

5343

5385

323105-02-1 NORMAL EXTENSION AND RETRACTION730 OPC740

NR

OPERATIONAL CHECK OF THE MLG DOOR ACTUATORNOTE 1: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOF AMSS ISS 13 AMD 04, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS13 AMD 04 EFFECTIVE DATE IS NEXT WEEKLY CHECK


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555


AOT 32A1390EAD 2011-0069

T 800 CYI 8 DY

See note

ALL323105-03-1 NORMAL EXTENSION AND RETRACTION210 VCK NR

NORMAL EXTENSION AND RETRACTIONCHECK CFDS (PFR) FOR SLOW DOOR OPENING/CLOSINGMESSAGES


AD 2007-0065ISB 32-1290

T 4 500 CYI 20 000 CYI 89 MO

See note

2255

2261

22672303

323112-01-1 SELECTOR VALVE - LG711 VCK N

INSPECTION OF SELECTOR VALVES.NOTE 1: THRESHOLD IS 4500 CY FROM THE EFFECTIVE DATE OF THE AD 2007-0065 (28/03/2007) BUT NOT EXCEEDING 20,800 CY FROM FIRST FLIGHT.NOTE 2: RII TASK



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 323300/6AMT 323300-200-002MRB 323000/09

I 72 MO ALL323300-01-1 LANDING GEAR FREE FALL EXTENSION100 DI200

Y

DETAILED INSPECTION OF FREE-FALL MECHANISM INCLUDINGCABLESAccess panels :

131AC 131BC 131CC 132PW 211FF 211JF 241EF241FF 241KF 241LF 241MF 242FF 242KF 242LF242MF 713 714 734 744 822 824825




I 15 000 CYI 80 MO

ALL323300-03-1 LANDING GEAR FREE FALL EXTENSION700 FNT N

FUNCTIONAL CHECK OF FREE-FALL SYSTEMPREP. : AIRCRAFT JACKING;

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 323300/6AMT 323300-200-001MRB 323000/15

I 72 MO ALL323300-04-1 LANDING GEAR FREE FALL EXTENSION100 VCK N

CHECK OF FREE-FALL MECHANISM CABLE TENSION

Access panels :

131AC 241EF 242FF 242LF 713 714 734744 822 825



AMM 323300/5AMT 323300-710-001MRB 323000/08

I 24 MO

CCheck :

ALL323300-05-1 LANDING GEAR FREE FALL EXTENSION210 OPT N

OPERATIONAL CHECK OF FREE-FALL MECHANICAL CONTROLNOTE: RII TASKAccess panels :



AMM 324200/5AMT 324200-720-004MRB 324000/14

I 5 000 CYI 48 MO

ALL324000-14-1 WHEELS AND BRAKES210 FUC730744

N

FUNCTIONAL CHECK OF THE AUTOMATIC REACTIVATION OF THENORMAL BRAKING MODE (PARKING BRAKE APPLIED)PREP. : HYDRAULIC GROUND POWER



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 324400-720-002MRB 32.40.00/17

I 7 500 FHI 5 000 CYI 50 MO

ALL324000-17-1 WHEELS AND BRAKES190 FUC N

FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM.


AMM 324100/6AMT 324100-210-003MRB 324000/01

I 3 DY ALL324100-01-1 WHEELS700 OPC Y

CHECK TIRE PRESSURE


AMT 324200-640-001SIL 32-130

I 2 000 CY ALL324100-05-1 WHEELS730 LUB740

Y

LUBRICATION OF MLG AXLE AND AXLE SLEEVESPREP. : BRAKE UNIT; MLG WHEEL;


ISB 32-1282T 7 500 CYI 2 000 CY

22552261

2267

23032480

324200-03-1 LANDING GEAR WHEELS AND BRAKES731 DI741

Y

DETAILED INSPECTION OF THE NORMAL BRAKE MANIFOLDPREP. : MLG FIXED LEG FAIRING;



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 324227/6AMT 324227-210-003MRB 324000/02

I 36 HR ALL324227-01-1 MAIN LANDING GEAR BRAKES731 FUC741

Y

FUNCTIONAL CHECK OF BRAKE HEAT PACK FOR WEAR BY USE OF THE WEAR INDICATOR(PARKING BRAKE APPLIED)NOTE : TASK ACCOMPLISHED AS PART OF OPERATORS ROUTINE MAINTENANCE PROGRAM. DEPENDENT ON OPERATORS EXPERIENCE, A HIGHER INITIAL INTERVAL MAY BE USED.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 324300-710-802MRB 32.40.00/08

I 7 500 FHI 50 MO

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715164

5241

5247

324300-01-3 ALTERNATE BRAKING SYSTEM210 OPC NR

OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEMNOTE: TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

55555699

5709

59165958

5994


AMM 324200/5AMT 324200-710-003MRB 324000/09

I 10 000 CY ALL324300-02-1 ALTERNATE BRAKING SYSTEM210 OPT N

OPERATIONAL CHECK OF ANTISKID INHIBITION



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 324311/6AMT 324311-210-001MRB 324000/06

I 1 500 CYI 18 MO

22552261

2267

23032480

324311-01-1 LOW PRESSURE BRAKE RESERVOIR122 FUC N

CHECK FLUID LEVEL OF LOW PRESSURE BRAKERESERVOIR

Access panels :



AMM 324314/6AMT 324314-200-002MRB 324000/12

I 13 MO 2255

2261

22672303

2480

324314-01-1 ALTERNATE BRAKE DIST. - DUAL VALVE148 RST N

DRAIN ACCUMULATED WATER FROM THE BRAKE DUALDISTRIBUTION VALVE (BDDV)

Access panels :

148FB 734 7440.20Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 324411/6AMT 324411-200-001CMP 32-2-0000-001MRB 32.40.00/05

I 750 FHI 4 MO

ALL324411-01-1 BRAKE ACCUMULATOR148 CHK N

FUNCTIONAL CHECK OF PARKING/EMERGENCY BRAKEACCUMULATOR BY READING THE CHARGE PRESSURE ON THEACCUMULATOR GAUGEAccess panels :



AMM 324500/5AMT 324500-710-001MRB 324000/13SIL 32-091

I 2 000 CYI 24 MO

ALL324500-01-1 PARKING/ULTIMATE EMERG. BRAKING SYSTEM148 OPT N

OPERATIONAL CHECK OF THE PARKING BRAKE SYSTEM


ISB 32-1279I 7 500 FHI 5 000 CY

2255

2261

22672303

2480

324500-04-1 PARKING/ULTIMATE EMERG. BRAKING SYSTEM190 FUC N

INSPECTION OF THE ACCUMULATOR OF THE ALTERNATEBRAKING SYSTEM FOR PRESSURE DECREASE.NOTE: CREDIT CAN BE TAKEN FROM TASK 324500-03-3



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 324900/5AMT 324900-720-001MRB 324000/03

I 750 CYI 9 MO

ALL324900-01-1 TIRE PRESSURE INDICATING SYSTEM210 FUC N

CROSSCHECK OF TPIS READING AND TIRE PRESSURE GAUGENOTE: A/C WITH TPIS INSTALLED



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 33 LIGHTS


Threshold Interval

Ctrl References Eff

AMM 331400/5AMT 331400-710-001MRB 231300/02MRB 279000/01MRB 315000/07MRB 331400/01MRB 344800/03

I 750 FHI 6 MO

ALL331400-01-1 ANNUNCIATOR LIGHT TEST AND DIMMING210 OPT N

OPERATIONAL CHECK OF LIGHTS TEST SYSTEM


AMM 335100/5AMT 335100-710-001MRB 335100/01

I 8 DY ALL335100-01-1 CABIN EMERGENCY LIGHTING210 OPT Y

OPERATIONAL CHECK OF EMERGENCY LIGHTS


AMM 335100/5AMT 335100-710-003MRB 335100/03SIL 33-033

I 400 DY ALL335100-03-1 CABIN EMERGENCY LIGHTING220 CHK Y

CHECK BATTERY CAPACITY



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 33 LIGHTS


Threshold Interval

Ctrl References Eff

AMM 335100/5AMT 335100-710-004MRB 335100/05

I 15 000 FHI 100 MO

ALL335100-05-1 CABIN EMERGENCY LIGHTING200 CHK N

CHECK MANUAL OPERATION FROM BOTH CONTROL PANELS ANDCHECK ALL CABIN LIGHTS AND SIGNS ILLUMINATED BYBATTERIES


AMM 335100/5AMT 335100-720-001MRB 335100/06

I 24 000 FH ALL335100-06-1 CABIN EMERGENCY LIGHTING220 CHK N

CHECK OF DOOR SWITCH POWER SUPPLIED BY EMERGENCYLIGHTS SYSTEM AND CHECK DOOR SWITCH OPERATION TOACTIVATE THE EXTERIOR LIGHTS



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 34 NAVIGATION


Threshold Interval

Ctrl References Eff

AMM 341300/5AMT 341300-710-002MRB 341300/01

I 15 000 FHI 100 MO

ALL341300-01-1 AIR DATA210 OPT N

OPERATIONAL CHECK OF OVERSPEED WARNING VMO/MMOUSING CFDS.


AMM 341300/5AMT 341300-710-001MRB 341300/02

I 15 000 FHI 100 MO


OPERATIONAL CHECK OF AIR DATA SWITCHING FUNCTION


AMM 341300/5AMT 341300-710-007MRB 341300/01

I 15 000 FHI 100 MO


OPERATIONAL CHECK OF OVERSPEED WARNINGS VFE/VLEUSING CFDS.


AMM 341300/5AMT 341300-710-003MRB 341300/04

I 7 500 FHI 50 MO


OPERATIONAL CHECK OF ALTITUDE COMPARISON WARNING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 341000/5AMT 341000-710-009MRB 341400/03

I 12 000 FHI 80 MO


OPERATIONAL CHECK OF THE 5-MINUTE TIME DELAY OF ADIRU2 AND 3 POWER DISCONNECTION IN EMERGENCYCONFIGURATION


AMM 341000/3AMT 341000-170-001MRB 341300/06SIL 34-3084

I 6 000 FHI 20 MO

ALL341300-07-1 AIR DATA120 RST N

FLUSHING OF TOTAL PRESSURE LINESNOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIALINTERVAL MAY BE USED.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 341300-710-009MRB 34.13.00/07

I 12 000 FHI 80 MO

46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

54385456

5469

54955555

5699

5709

341300-09-1 AIR DATA210 OPT NR

OPERATIONAL CHECK OF THE BACK UP SPEED SCALE DISPLAY


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

5994


AMT 303100-710-007ISB 34-1415

T 5 200 FHI 2 000 FH

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

341300-10-1 AIR DATA120 FUC N

FUNCTIONAL TEST OF THE HEATING OF THE THREE AOASENSORS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 341000-170-004SIL 34-084

T 5 200 FHI 750 FHI 4 MO

ALL341300-11-1 AIR DATA120 RST N

CLEANING OF 1 OUT OF 3 PITOT PROBES.NOTE: TASK TO BE PERFORMED ALTERNATELY ON PITOT 1, 2 AND 3.


AMM 341400/5AMT 341400-710-003MRB 341400/01

I 7 500 FHI 50 MO

ALL341400-01-1 ATTITUDE, HEADING AND POSITION210 OPT N

OPERATIONAL CHECK OF ATT/HDG SWITCHING FUNCTION


AMM 341400/5AMT 341400-710-004MRB 341400/02

I 7 500 FHI 50 MO

ALL341400-02-1 ATTITUDE, HEADING AND POSITION210 OPT N

OPERATIONAL CHECK OF ATTITUDE AND HEADING COMPARISONWARNING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 342225-710-001MRB 34.20.00/03

I 7 500 FHI 50 MO

38623964

3966

42134277

4311

43154669

4703

47374783

4826

48634945

4971

52515275

5306

53405385

5392

54185438

5456

54955555

5699

5916

342000-03-1 STANDBY NAVIGATION SYSTEM210 OPC NR

OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5958


AMM 342100/5AMT 342100-790-001MRB 342100/01SIL 34-084

I 12 000 FHI 80 MO

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

4136

342100-01-1 STANDBY ALTITUDE AND AIRSPEED120 TST N

LOW RANGE LEAK TEST OF STANDBY PNEUMATIC CIRCUITS

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 341000/3AMT 341000-170-003MRB 342100/02SIL 34-084

I 6 000 FHI 20 MO

22552261

2267

23032480

2974

30053013

3022

31983315

342100-02-1 STANDBY DATA ALTITUDE AND AIRSPEED120 DRN N

DRAINING AND FLUSHING OF STANDBY PNEUMATIC CIRCUITSNOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INTERVAL MAY BE USED.

Access panels :



AMM 342200/5AMT 342200-710-001MRB 342200/01

I 6 000 FHI 48 MO

ALL342200-01-1 STANDBY COMPASS210 DI Y

OPERATIONAL CHECK OF THE STANDBY COMPASS INCLUDINGLIGHT TEST AND VISUAL CHECK



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 342225-170-001MRB 34.20.00/02SIL 34-084

I 6 000 FHI 20 MO

38623964

3966

42134277

4311

43154669

4703

47374783

4826

48634945

4971

52515275

5306

53405385

5392

54185438

5456

54955555

5699

5916

342200-02-1 STANDBY ALTITUDE AND HEADING120 SVC NR

DRAINING AND FLUSHING OF STANDBY PNEUMATIC CIRCUITSNOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIALINTERVAL MAY BE USED.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5958

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 342225-790-001MRB 34.20.00/01SIL 34-084

I 12 000 FHI 80 MO

38623964

3966

42134277

4311

43154669

4703

47374783

4826

48634945

4971

52515275

5306

53405385

5392

54185438

5456

54955555

5699

5916

342200-05-1 STANDBY DATA - INTEGRATED STANDBY120 FUC NR

INSTRUMENT SYSTEM (ISIS)LOW RANGE LEAK TEST OF STANDBY PNEUMATIC CIRCUITS


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5958

Access panels :



AMM 344200/5AMT 344200-750-001MRB 344200/01

I 4 000 FHI 48 MO

ALL344200-01-1 RADIO ALTIMETER152 OPT N

OPERATIONAL CHECK AND DETAILED INSPECTION FORCONTAMINATION OF RADIO ALTIMETER FANNOTE: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MOREFREQUENT INITIAL INTERVAL MAY BE USED.Access panels :

152GW0.02Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 344211/4AMT 344211-920-001SIL 34-097

I 144 MO ALL344200-02-1 RADIO ALTIMETER150 DIS N

RADIO ALTIMETER ANTENNAS AND COAXIAL CABLESREPLACEMENT.Access panels :

151AG 151UF 152AG 152GW 152HW 152MF 152NF0.31Total access time : Hrs


AMT 344211-615-001SIL 34-099

I 6 MO ALL344200-03-1 RADIO ALTIMETER150 RST N

RADIO ALTIMETER ANTENNAS EXTERNAL SURFACE CLEANING


AMM 344800/5AMT 344800-710-001MRB 344800/01

I 7 500 FHI 50 MO

ALL344800-01-1 GROUND PROXIMITY WARNING SYSTEM210 OPT N

OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM


AMM 345200/5AMT 345200-720-006MRB 345200/02

I 15 000 FHI 100 MO

ALL345200-02-1 ATC SYSTEM210 FNT N

FUNCTIONAL CHECK OF ATC ANTENNAS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 351241/5AMT 351241-710-001FCO 3-03-06MRB 351000/01

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL351000-01-1 CREW OXYGEN SYSTEM210 OPT Y

OPERATIONAL CHECK OF FLIGHT CREW OXYGEN SYSTEM


AMM 351241/7AMT 351241-100-001MRB 351000/07

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL351000-07-1 CREW OXYGEN MASKS210 CLN Y

CLEANING OF OXYGEN MASKS


AMM 351000/5AMT 351000-720-001MRB 35.10.00/08

I 6 500 FHI 24 MO

ALL351000-08-1 CREW OXYGEN MASKS210 FUC Y

FUNCTIONAL CHECK OF ECAM OXYGEN CYLINDER CONTENTSINDICATION COMPARED WITH CYLINDER PRESSURE GAUGE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 351141/6AMT 351141-750-002MRB 351000/05

See noteNTCheck :

ALL351141-01-1 CREW OXYGEN CYLINDER125 RAI Y

HYDROSTATIC TEST OF OXYGEN CYLINDERNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.Access panels :



AMM 351241/6AMT 351241-200-001MRB 351000/03

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL351241-01-1 CREW OXYGEN MASKS210 DI N

DETAILED INSPECTION OF OXYGEN MASKS (OUT OF BOX)WITH HARNESS INFLATED


AMM 351241/6AMT 351241-750-001MRB 351000/04

NTCheck : ALL351241-02-1 CREW OXYGEN MASK REGULATORS210 FNT N

REMOVE FOR FUNCTIONAL CHECK OF MASK REGULATORASSEMBLY



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 351200/5AMT 351200-710-001MRB 351000/02

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL351351-01-1 OXYGEN SUPPLY VALVE210 OPT N

OPERATIONAL CHECK OF LP SOLENOID VALVE CONTROL(CLOSING MODE) AND LP INDICATION


AMM 352100/3AMT 352100-920-001MRB 352000/3

NTCheck : ALL352142-01-1 OXYGEN GENERATORS200 DIS Y

DISCARD OXYGEN GENERATORS


AMM 353000/6AMT 353242-210-002MRB 353000/1

I 4 MO ALL353000-01-1 PORTABLE OXYGEN CYLINDERS200 CHK N

CHECK PRESSURE ON CYLINDER PRESSURE GAUGES


AMM 353000/6AMT 353242-750-001MRB 353000/2

See noteNTCheck :

ALL353000-02-1 PORTABLE OXYGEN200 RAI Y

REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FORHYDROSTATIC TEST (INCLUDING FUNCTIONAL CHECK OFOXYGEN REGULATOR AND LP RELIEF VALVE)NOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 353000/6AMT 353242-210-001MRB 353000/03

I 24 000 FHI 160 MO

ALL353000-04-1 PORTABLE OXYGEN200 CHK N

VISUAL CHECK OF CYLINDER ATTACHMENTS


AMM 353000/6AMT 353000-210-006MRB 353000/04

I 100 DY ALL353000-05-1 PROTECTIVE BREATHING EQUIPMENT200 VCK N

VISUAL CHECK OF THE TAMPER SEAL/SERVICEABILITYINDICATION OF THE PROTECTIVE BREATHING EQUIPMENT


AMM 353000/6AMT 353000-920-001MRB 353000/05

See noteNTCheck :

ALL353000-06-1 PROTECT. BREATHING EQPT (CKPT & CABIN)200 DIS N

DISCARD PROTECTIVE BREATHING EQUIPMENTNOTE: THE INTERVAL OF THIS TASK REFER TO "A321 TIME CONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.


AMM 353000/6AMT 353000-220-001MRB 35.30.00/06

I 24 MO ALL353000-07-1 PORTABLE OXYGEN200 DI N

DETAILED INSPECTION OF PORTABLE OXYGEN MASK



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 36 PNEUMATIC


Threshold Interval

Ctrl References Eff

AMM 361153/5AMT 361153-720-001MRB 36.00.00/05

I 22 000 FHI 5 YE

ALL361100-01-1 ENGINE BLEED AIR SUPPLY SYSTEM450 FNT460

N

FUNCTIONAL CHECK OF OVERPRESSURE VALVE.

Access panels :




AMM 361100/5AMT 361100-790-002SIL 36-047

I 40 MO ALL361100-06-1 ENGINE BLEED AIR SUPPLY SYSTEM410 CHK420

N

PERFORM LEAK CHECK ON THE COMBO SEALS ON THEPYLON DUCT SLEEVES (DOWNSTREAM PRECOOLER).NOTE : DEPENDING ON OPERATING ENVIRONMENT ANDOPERATOR'S EXPERIENCE,A LESS OR A MOREFREQUENT INITIAL INTERVAL MAY BE USED


AMM 361141/6AMT 361141-200-010MRB 360000/16

I 6 000 FHI 40 MO

ALL361141-04-1 IP BLEED CHECK VALVE450 DI460

N

CHECK OF IP BLEED CHECK VALVE FOR CONDITION

Access panels :

437AL 447AL 451AL 461AL0.08Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 361143/7AMT 361143-100-001MRB 36.00.00/17SIL 36-055

I 6 000 FHI 40 MO

ALL361143-01-1 THERMOSTAT - FAN AIR VALVE CONTROL413 RST423

N

REMOVE THE THERMOSTAT-FILTER OF THE FAN AIRVALVE-CONTROL FOR CLEANING.NOTE:- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORSEXPERIENCE,A LESS OR A MORE FREQUENT INITIAL INTERVALMAY BE USEDAccess panels :

413DL 423DL0.16Total access time : Hrs


AMM 361200/5AMT 361200-710-002MRB 360000/03

I 50 MO ALL361200-01-1 AIR BLEED AIR SUPPLY & CROSSBLEED SYST210 OPT N

OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 361200/5AMT 361200-790-002MRB 360000/15SIL 36-047

I 22 000 FHI 144 MO

ALL361200-02-3 APU BLEED AIR SUPPLY & CROSSBLEED SYST150 FUC160190310

N

PERFORM LEAK CHECK ON APU BLEED AIR DUCTING(UPSTREAM THE APU BLEED CHECK VALVE)NOTE : TASK MAY BE COMBINED WITH TASKS 361148-01-1 AND 361200-03-1Access panels :

151BW 151CW 151DW 151EW 151HW 151JW 151RW161AW 161BW 161CW 161DW 197KB 312AR 314AR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 361200/5AMT 361200-790-003MRB 360000/11SIL 36-047

I 22 000 FHI 144 MO

ALL361200-03-1 APU BLEED AIR SUPPLY & CROSSBLEED SYST191 FUC192

N

PERFORM LEAK CHECK ON BLEED AIR DUCTING IN THEFUSELAGE AREA BETWEEN THE APU BLEED CHECKVALVE, AIR CONDITIONING PACK AND WING/FUSELAGECONNECTIONNOTE : - TASK MAY BE COMBINED WITH TASKS 361148-01-1 AND 361200-02-3 - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR'S EXPERIENCE,A LESS OR A MORE FREQUENT INITIAL INTERVAL MAY BE USEDAccess panels :



AMM 361251/6AMT 361251-200-001SIL 36-038

I 24 000 FHI 160 MO

ALL361251-01-1 APU BLEED CHECK VALVE192 DI N

REMOVE AND CHECK AUXILIARY POWER UNIT BLEEDCHECK VALVE FOR CONDITIONAccess panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 38 WATER / WASTE


Threshold Interval

Ctrl References Eff

AMM 381000/2AMT 381000-670-002MRB 38.10.00/01

I 750 FHI 4 MO

ACheck :

ALL381000-01-1 POTABLE WATER SYSTEM171 RST N

STERILIZATION OF POTABLE WATER SYSTEM AND DISCARD OFWATER FILTER ELEMENTS, IF INSTALLEDNOTE: -DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MOREFREQUENT INITIAL INTERVAL MAY BE USED. -PERFORM THIS TASK IN NEXT A CHECK FOR OVERDUED AIRCRAFTAccess panels :



AMM 383167/3AMT 383167-610-001MRB 383101/03SIL 38-020

I 6 000 FHI 24 MO

ALL383100-02-1 VACUUM TOILET SYSTEM170 DI N

INSPECT WATER SEPARATOR AND ASSOCIATED FILTERELEMENT, AND CLEAN AS NECESSARY

Access panels :

161DW 162DW0.04Total access time : Hrs

Skills :B21 0.00 MHrsUT2 1.00 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 383161/6AMT 383161-210-001MRB 383101/06SIL 38-020

I 6 000 FHI 24 MO

ALL383100-05-1 VACUUM TOILET SYSTEM172 DI N

DETAILED INSPECTION OF CLEANLINESS INSIDE WASTE TANKNOTE: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MOREFREQUENT INITIAL INTERVAL MAY BE USED.Access panels :

161DW 162DW0.04Total access time : Hrs

Skills :B21 0.00 MHrsUT1 0.50 MHrs

AMM 383100/7AMT 383100-100-018MRB 383101/05SIL 38-020

I 150 FHI 2 MO

ALL383100-06-1 VACUUM TOILET SYSTEM200 RST N

CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANINGAGENT AND CRUSHED ICENOTE: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MOREFREQUENT INITIAL INTERVAL MAY BE USED.


AMM 383100/7AMT 383100-100-004SIL 38-020

I 6 000 FHI 48 MO

ALL383100-07-1 VACUUM TOILET SYSTEM200 RST N

CORRECTIVE VACUUM WASTE LINE CLEANING.NOTE:INTERVAL MAY BE ADJUSTED ACCORDING TOOPERATOR EXPERIENCE.

Skills :B21 0.00 MHrsMEC2 10.00 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 383155-100-001SIL 38-031

NTCheck : ALL383155-01-1 VACUUM TOILET RINSE VALVE200 RST N

VACUUM TOILET RINSE VALVEREMOVE, CLEAN AND INSPECT TOILET RINSE VALVESFROM ALL TOILETS.NOTE1: TASK APPLICABILITY: AIRCRAFT EQUIPPED WITH P/N:P/N: 15800-348 REV.A OR P/N 15800-348 REV.B OR P/N 15800-348 REV.CNOTE2: TASK THRESHOLD IS NEXT C CHECK

Skills :UT1 0.35 MHrs

AMM 383200/7AMT 383200-100-002MRB 383200/02SIL 38-029

I 1 200 FHI 24 MO

ALL383200-01-1 WASTE WATER DRAIN200 RST N

CLEAN FILTER ELEMENT OF WASHBASIN DRAIN VALVESNOTE: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MOREFREQUENT INITIAL INTERVAL MAY BE USED.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 384100/3AMT 384100-610-001MRB 384000/01

I 24 000 FHI 72 MO

ALL384142-01-1 AIR FILTER171 DIS N

DISCARD SYSTEM FILTER ELEMENTNOTE : DEPENDING ON EACH INDIVIDUAL OPERATOR'SENVIRONMENT A MORE FREQUENT INTERVALMAY BE USEDAccess panels :

161DW 8260.04Total access time : Hrs


AMM 384200/6AMT 384200-210-001MRB 384000/03

I 12 000 FHI 80 MO

See note

ALL384241-01-2 AIR SUPPLY172 DI N

DETAILED INSPECTION OF COMPRESSOR INLET FILTER.NOTE: DEPENDING ON OPERATING ENVIRONMENT ANDOPERATORS EXPERIENCE, A LESS FREQUENT OR MOREFREQUENT INITIAL INTERVAL MAY BE USED.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 384200/3AMT 384200-610-001MRB 384000/02

I 24 000 FHI 72 MO

ALL384242-01-3 AIR SUPPLY171 DIS N

DISCARD COMPRESSOR OUTLET FILTER ELEMENT.

Access panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 47 INERT GAS GENERATION SYSTEM


Threshold Interval

Ctrl References Eff


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 471041-920-001MRB 47.00.00/01

I 7 000 FH 46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

54385456

5469

54955555

5699

5709

470000-01-1 INERT GAS GENERATION SYSTEM191 DIS NR

D-ULPA FILTER ELEMENT REPLACEMENTNOTE: IF SYSTEM IS DEACTIVATED WHEN TASK BECOMES DUE,TASK MAY BE POSTPONED UNTIL REACTIVATION.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

5994

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 471043-920-001MRB 47.00.00/02

NTCheck : 46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

54385456

5469

54955555

5699

5709

470000-02-1 INERT GAS GENERATION SYSTEM191 DIS NR

AIR SEPARATOR MODULE REPLACEMENTNOTE: IF SYSTEM IS DEACTIVATED WHEN TASK BECOMES DUE,TASK MAY BE POSTPONED UNTIL REACTIVATION.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

5994

Access panels :

191AB 191BB0.26Total access time : Hrs



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 49 AIRBORNE AUXILLIARY POWER UNIT


Threshold Interval

Ctrl References Eff

AMM 491200/6AMT 491200-210-004MRB 491200/02-32

I 80 MOSee note

ALL491200-A1-1 APU MOUNTS315 DI Y

DETAILED INSPECTION OF APU SUSPENSION RODS, VIBRATIONISOLATOR STRUCTURE INCLUDING BRACKETS AND VISIBLEPART OF STRUCTURE ATTACHMENT FITTINGSNOTE : TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF APU CHANGEAccess panels :



AMT 491200-210-005MRB 49.12.00/01-32

I 20 MO 37373862

3966

43114315

491200-A2-1 APU MOUNTS315 GVI316

Y

APU MOUNTSGENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEMFOR CONDITION AND SECURITY.NOTE: THIS TASK IS APPLIED TO A/C THAT IS EQUIPED WITH APS3200 APU SERIESONLYAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 491200/6AMT 491200-210-007MRB 491200/02-13

I 80 MOSee note

ALL491200-B1-1 APU MOUNTS315 DI Y

DETAILED INSPECTION OF APU SUSPENSION RODS, VIBRATIONISOLATOR STRUCTURE INCLUDING BRACKETS AND VISIBLEPART OF STRUCTURE ATTACHMENT FITTINGSNOTE : TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF APU CHANGENOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :



AMT 491200-210-804MRB 49.12.00/01-13MRB 49.12.00/01-32

I 20 MO ALL491200-B2-1 APU MOUNTS315 GVI316

Y

APU MOUNTSGENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEMFOR CONDITION AND SECURITY.NOTE: THIS TASK IS APPLIED TO A/C THAT IS EQUIPED WITH 131-9(A)APU SERIESONLYAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 491300/6AMT 491300-200-002MRB 49.13.00/01-32

I 20 MO 37373862

3966

43114315

491300-A1-1 FIRE SEALS310 GVI Y

GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIREWALLS AND SEALS:- COMPARTMENT DOORS- FWD AND AFT FIRE WALLS- SIDE FIRE WALLS- UPPER FIRE WALLAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 491300/6AMT 491300-200-003MRB 49.13.00/01-13

I 20 MO ALL491300-B1-1 FIRE SEALS310 GVI Y

GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIREWALLS AND SEALS:- COMPARTMENT DOORS- FWD AND AFT FIRE WALLS- SIDE FIRE WALLS- UPPER FIRE WALLNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :



AMM 491600/6AMT 491600-210-002MRB 491600/03-32

I 40 MO 37373862

3966

43114315

491600-A1-1 AIR INTAKE SYSTEM310 DI Y

DETAILED INSPECTION OF APU AIR INTAKE,DIFFUSER ELBOW, SEALS AND FELT METAL

Access panels :

314AR 315AL 316AR0.05Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2006-0153AD 2007-13-08AMM 491600/7AMT 491600-100-002ISB 49-1068

I 2 400 FH 22552261

2267

23032480

491600-A4-1 AIR INTAKE SYSTEM310 RST Y

CLEANING OF APU AIR INTAKENOTE: APPLY FOR APU APIC(APS 3200) PRE 35803 (49-1070)

Access panels :



AD 2006-0153AD 2007-13-08AMM 491600/6AMT 491600-210-005ISB 49-1068

I 600 FH 3737

38623966

4311

4315

491600-A5-1 AIR INTAKE SYSTEM310 GVI Y

GENERAL VISUAL INSPECTION OF APU AIR INLET PLENUMAND APU AIR INTAKE.

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 491600/6AMT 491600-200-002MRB 49.16.00/01-13

I 40 MO ALL491600-B1-1 AIR INTAKE SYSTEM313 DI315

Y

DETAILED INSPECTION OF APU AIR INTAKE,DIFFUSER ELBOW, SEALS AND FELT METALNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :



AD 2006-0153 02 01AD 2007-13-08AMM 491600/6AMT 491600-210-802EAD 2006-0153ISB 49-1068

I 600 FH ALL491600-B6-1 AIR INTAKE SYSTEM310 GVI YD

GENERAL VISUAL INSPECTION OF APU AIR INLET PLENUMAND APU AIR INTAKE.NOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APU AND PRE MOD 35936

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 492100-920-007MRB 49.21.00/05-13

See noteNTCheck :

ALL492100-B5-1 POWER SECTION315 DIS317

Y

DISCARD LIFE LIMITED PARTS OF THE APU POWERSECTION IN ACCORDANCE WITH OEM RECOMMENDATIONNOTE : REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.NOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUPREP. : APU REMOVED;Access panels :

315AL 316AR 317AL0.04Total access time : Hrs

AMT 493241-920-001MRB 49.30.00/02-13

I 8 500 FHI 72 MO

ALL493000-B1-1 ENGINE FUEL AND CONTROL315 DIS Y

DISCARD FUEL INLET FILTER ELEMENTNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 493100/5AMT 493100-710-002MRB 493400/01-32

I 24 MO 37374311

4315

493400-A1-1 APU FUEL LOW PRESSURE WARNING210 OPT N

OPERATIONAL CHECK OF APU FUEL LOW PRESSURE CIRCUITNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH APIC 3200 APU


AMT 493100-710-003MRB 49.34.00/01-13

I 24 MO ALL493400-B1-1 APU FUEL LOW PRESSURE WARNING210 OPC N

OPERATIONAL CHECK OF APU FUEL LOW PRESSURE CIRCUITNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 494141/6AMT 494141-920-001MRB 494000/02-32

I 2 250 FHI 24 MO

37374311

4315

494000-A1-1 IGNITION AND STARTING316 DI Y

REMOVE AND DISCARD IGNITER PLUGSNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH APIC 3200 APUAccess panels :



AMT 494141-220-001MRB 49.40.00/02-13

I 6 000 FHI 40 MO

ALL494000-B2-1 IGNITION AND STARTING315 VCK Y

DETAILED INSPECTION OF IGNITER PLUGNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2007-13-08AMT 494251-200-008EAD 2006-0153ISB 49-1068

I 600 FH 22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

42134277

4311

4315

494000-B3-1 IGNITION AND STARTING315 VCK YD

CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH NOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APU

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 494251-200-008SIL 49-043

I 750 FHI 6 MO

46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

54385456

5469

54955555

5699

5709

494000-B3-2 IGNITION AND STARTING315 VCK YR

CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

5994

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2007-13-08AMT 494251-700-002EAD 2006-0153ISB 49-1068

I 600 FH 22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

42134277

4311

4315

494000-B4-1 IGNITION AND STARTING315 OPT YD

TEST OF CLUTCH OF APU STARTER MOTORNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APU

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2006-0153AD 2007-13-08AMM 494251/6AMT 494251-200-006ISB 49-1068

I 600 FH 2255

2261

22672303

2480

494251-A1-1 STARTER MOTOR315 VCK N

CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH

Access panels :



AMM 494251/6AMT 494251-200-006SIL 49-043

I 750 FHI 6 MO

3737

43114315

494251-A2-1 STARTER MOTOR315 VCK N

CHECK WEAR INDICATOR OF STARTER MOTOR BRUSHNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH APIC 3200 APUAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 498100-200-016MRB 49.80.00/04-32

I 24 MO 37374311

4315

498000-A4-1 EXHAUST310 VCK N

VISUAL CHECK OF APU COMPARTMENT EXHAUST MUFFLERINSULATION COVERS AND BELLOWSNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH APIC 3200 APU


AMT 498100-200-017MRB 49.80.00/01-13

I 24 MO ALL498000-B1-1 EXHAUST310 VCK N

VISUAL CHECK OF APU COMPARTMENT EXHAUST MUFFLERINSULATION COVERS AND BELLOWSNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 490000-790-007SIL 49-032

I 7 500 FHI 50 MO

ALL499000-A2-1 OIL SYSTEM310 VCK N

CHECK APU COMPARTMENT AND AIR INTAKE DUCT FOROIL CONTAMINATIONNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH APIC 3200 APUAccess panels :



AMT 499141-200-002SIL 49-051

I 3 000 FHI 24 MO

ALL499100-B2-1 STORAGE AND DISTRIBUTION315 DIS N

REMOVE AND DISCARD OIL FILTER ELEMENTS (8069KM)AND (8076KM).NOTE : DEPENDING ON OPERATING ENVIROMENT AND OPERATORS EXPERIENCE A HIGHER INITIAL INTERVAL MAY BE USEDNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 490000-790-008SIL 49-032

I 7 500 FHI 50 MO

ALL499100-B4-1 STORAGE AND DISTRIBUTION310 VCK N

CHECK APU COMPARTMENT AND AIR INTAKE DUCT FOROIL CONTAMINATIONNOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APUAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 521000/6AMT 521000-210-004MRB 521000/01

I 8 DY ALL521000-01-1 PASSENGER/CREW DOOR831 CHK832841842

Y

CHECK EMERGENCY CYLINDER/ACCUMULATOR PRESSURENOTE : TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORS


AMM 521000/5AMT 521000-720-001MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO

ALL521000-02-1 PASSENGER/CREW DOOR831 FNT832841842

N

FUNCTIONAL CHECK OF DOOR SUSPENSION

Access panels :

831 831FZ 831GZ 832 832FZ 832GZ 841841FZ 841GZ 842 842FZ 842GZ



AMM 521000/6AMT 521000-220-006MRB 52.10.00/06

I 15 000 FHI 10 000 CYI 48 MO

2CCheck :

ALL521000-03-1 PASSENGER/CREW DOOR831 DI832841842

Y

DETAILED INSPECTION OF DOOR SEALSNOTE: TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORS

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 521000/6AMT 521000-200-002MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO

ALL521000-04-1 PASSENGER/CREW DOOR831 DI832841842

Y

DETAILED INSPECTION OF PASSENGER/CREWDOOR FOR INTEGRITY AND GOOD ADJUSTMENT OFMECHANISMS (INCLUDING GIRT BAR)PREP. : INSULATION REMOVEDNOTE: RII TASKAccess panels :

831AZ 831BZ 831CZ 831DZ 831EZ 831FZ 831GZ832AZ 832BZ 832CZ 832DZ 832EZ 832FZ 832GZ841AZ 841BZ 841CZ 841DZ 841EZ 841FZ 841GZ842AZ 842BZ 842CZ 842DZ 842EZ 842FZ 842GZ



AMM 521000/5AMT 521000-720-003MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO


N

FUNCTIONAL CHECK OF LOCKING MECHANISM

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 521000/5AMT 521000-720-005MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO


N

FUNCTIONAL CHECK OF ESCAPE SLIDE RELEASEMECHANISMNOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY DEACTIVATED)


AMM 521000/5AMT 521000-200-001MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO

ALL521000-07-1 PASSENGER/CREW DOOR831 CHK832841842

N

CHECK OF DOOR STOPS ADJUSTMENT

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 521000/5AMT 521000-710-002MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO

ALL521000-08-1 PASSENGER/CREW DOOR831 OPT832841842

N

OPERATIONAL CHECK OF INTERLOCK MECHANISM TOENSURE THAT EMERGENCY ESCAPE HANDLE STAYS INDISARMED POSITION WHEN DOOR IS UP AND OUTSIDEOF FRAMENOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY DEACTIVATED)Access panels :



AMM 521000/5AMT 521000-720-004MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO


N

FUNCTIONAL CHECK OF MECHANICAL LOCKINGINDICATION

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 521000/5AMT 521000-710-001MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO


N

OPERATIONAL CHECK OF DAMPING DURINGOPENING/CLOSINGNOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY DEACTIVATED)Access panels :



AMM 521000/5AMT 521000-710-003MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO


N

OPERATIONAL CHECK OF STRIKER MECHANISMNOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY DEACTIVATED)Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 521000/5AMT 521000-720-002MRB 52.10.00/02MRB 52.10.00/08

I 15 000 FHI 10 000 CYI 80 MO


N

OPERATIONAL CHECK OF ESCAPE SLIDE DISARMINGWHEN DOOR IS OPENED FROM THE OUTSIDENOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY DEACTIVATED)Access panels :



AMM 122252/3AMT 122252-640-016MRB 521000/05SIL 53-076

I 20 MO ALL521000-14-1 PASSENGER/CREW DOOR831 LUB832841842

N

PASSENGER/CREW DOORLUBRICATION OF HINGE ARM SUPPORT FITTING BEARINGSNOTE : TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORS


AMM 122252/3AMT 122252-640-006MRB 521000/03

I 20 MO ALL521121-01-1 PAX/CREW DOOR831 LUB832841842

N

LUBRICATION OF EXTERIOR CONTROL HANDLE AND TELESCOPICARMNOTE : TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 122252/3AMT 122252-640-014AOT 52A1103MRB 521000/04

I 36 MO ALL521121-02-1 PAX/CREW DOOR831 LUB832841842

N

LUBRICATION OF SAFETY PIN GUIDE FITTING AND DOORARMING/DISARMING MECHANISMNOTE : TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORSAccess panels :

831BZ 831CZ 831DZ 832BZ 832CZ 832DZ 841BZ841CZ 841DZ 842BZ 842CZ 842DZ



AMM 522200/5AMT 522200-710-001MRB 522200/01

I 8 000 FHI 53 MO

ALL522200-01-1 PASSENGER COMPARTMENT EMERGENCY EXIT833 OPC834843844

Y

OPERATIONAL CHECK- OF DOOR LOCKING/UNLOCKING AND DOOR OPENING/CLOSINGFROM INSIDE AND OUTSIDE AND DOOR LATCHING AND UNLATCHING,- TO ENSURE THAT DOOR CANNOT BE LOWERED AND LOCKEDWHEN OPEN,- OF DOOR DAMPING MECHANISM,- OF ESCAPE SLIDE DISARMING WHEN DOOR IS OPENED FROMOUTSIDE,- TO ENSURE THAT ESCAPE SLIDE ARMING LEVER IS LOCKEDIN "DISARMED" POSITION WHEN DOOR IS OPEN, ANDFUNCTIONAL CHECK- OF LOCKING MECHANISM, HAND FORCE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 522200/5AMT 522200-720-001MRB 522200/02

I 8 000 FHI 53 MO

ALL522200-02-1 PASSENGER COMPARTMENT EMERGENCY EXIT833 OPC834843844

N

OPERATIONAL CHECK- OF DOOR UNLOCKING FROM INSIDE AND OUTSIDE IN"ARMED" POSITION,- OF ESCAPE SLIDE RELEASE MECHANISMARMING/DISARMING, AND FUNCTIONAL CHECK- OF SLIDE RELEASE CABLE MOVEMENT


AMM 122252/3AMT 122252-640-013MRB 522200/03

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL522200-03-1 PASSENGER COMPARTMENT EMERGENCY EXIT833 LUB834843844

N

LUBRICATION OF EXTERIOR CONTROL HANDLE AND TELESCOPICARM


AMM 522211/6AMT 522211-200-004MRB 522200/04

I 8 000 FHI 53 MO

ALL522200-04-1 PASSENGER COMPARTMENT EMERGENCY EXIT833 DVI834843844

N

DOOR DETAILEDINSPECTION OF CYLINDER ASSEMBLY



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 522200/6AMT 522200-200-001MRB 522200/06

I 8 DY ALL522200-08-1 PASSENGER COMPARTMENT EMER EXIT DOOR833 VCK834843844

N

DOORCHECK EMERGENCY CYLINDER/ACCUMULATOR PRESSURE ONPRESSURE GAUGE


AMM 122252/3AMT 122252-640-002MRB 523100/01

I 4 500 CYI 18 MO

ALL523000-01-1 CARGO COMPARTMENT DOOR825 LUB826

N

LUBRICATION OF FWD AND AFT CARGO DOOR

Access panels :

825 825AR 826 826AR0.15Total access time : Hrs


AMM 122252/3AMT 122252-640-009MRB 523100/01

I 4 500 CYI 18 MO

ALL523000-03-1 CARGO COMPARTMENT DOOR825 LUB826

N

LUBRICATION OF EXTERIOR CARGO DOOR HANDLENOTE : INTERVAL MAY NEED TO BE MORE FREQUENTWHEN OPERATING IN HOSTILE ENVIRONMENTS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 523100/5AMT 523100-720-001MRB 523100/02

I 18 000 CYI 72 MO

ALL523100-01-1 FORWARD CARGO COMPARTMENT DOOR825 FUT N

FUNCTIONAL CHECK OF FORWARD CARGO COMPARTMENTDOOR, COMPRISING FUNCTIONAL CHECKS OF:- LOCKING MECHANISM- INTERLOCK MECHANISM- DRIFT PIN MECHANISM- SAFETY MECHANISMAccess panels :

825 825AR0.08Total access time : Hrs


AMM 523200/5AMT 523200-720-001MRB 523100/02

I 18 000 CYI 72 MO

ALL523200-01-1 AFT CARGO COMPARTMENT DOOR826 FUT N

FUNCTIONAL CHECK OF AFT CARGO COMPARTMENTDOOR, COMPRISING FUNCTIONAL CHECKS OF:- LOCKING MECHANISM- INTERLOCK MECHANISM- DRIFT PIN MECHANISM- SAFETY MECHANISMAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 122252/3AMT 122252-640-007MRB 523300-01-1

I 4 500 CYI 18 MO

ALL523300-01-1 BULK CARGO COMPARTMENT DOOR827 LUB N

LUBRICATION OF BULK CARGO COMPARTMENT DOOR HANDLE ANDHINGE ARM BEARINGSNOTE: INTERVAL MAY NEED TO BE MORE FREQUENT WHEN OPERATING IN HOSTILE ENVIRONMENTS


AMM 523500/5AMT 523500-710-001MRB 523500/01

I 10 000 CYI 72 MO

ALL523500-01-1 CARGO COMPARTMENT DOOR - ELECTRICAL100 OPT Y

CARGO COMPARTMENT DOOR ELECTRICAL CONTROL SYSAND HYD SYSTEMOPERATIONAL CHECK OF DOOR CLOSING INHIBITION BY DOORSILL LATCH SWITCHAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 524100/6AMT 524100-210-001MRB 524100/01

I 15 000 FHI 10 000 CYI 48 MO

2CCheck :

ALL524100-01-1 ACCESS DOORS811 DI812822824

Y

DETAILED INSPECTION OFDOOR SEALS

Access panels :



AMM 122252/3AMT 122252-640-008MRB 524100/02

I 20 MO ALL524100-02-1 ACCESS DOORS811 LUB812822824

N

LUBRICATION OF EXTERIOR AVIONIC COMPARTMENTDOOR HANDLE.NOTE : INTERVAL MAY NEED TO BE MORE FREQUENTWHEN OPERATING IN HOSTILE ENVIRONMENTSAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 525100/6AMT 525100-220-001MRB 525111/01

I 15 000 FHI 100 MO

ALL525111-01-1 COCKPIT DOOR220 DI N

DETAILED INSPECTION OF MECHANICAL PARTS OF DOORLOCKING SYSTEMS


AMM 525100/5AMT 525100-720-002MRB 525111/02

I 15 000 FHI 48 MO

ALL525111-02-1 COCKPIT DOOR220 OPC N

OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELSFOR RAPID DECOMPRESSION.


AMM 525100/5AMT 525100-710-005MRB 525111/02

I 15 000 FHI 48 MO


OPERATIONAL CHECK OF DOOR OPENING IN CASE OFPOWER OFF.


AMM 525100/5AMT 525100-710-006MRB 525111/02

I 15 000 FHI 48 MO


OPERATIONAL CHECK OF DOOR OPENING BY USING THEEMERGENCY CODE.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 525100-710-008MRB 52.51.11/04

I 12 000 FHI 80 MO

42134277

4315

525111-07-1 COCKPIT DOOR220 OPC N

OPERATIONAL CHECK OF DEADBOLT


AMT 525100-710-010MRB 52.51.11/05

I 72 MO ALL525111-08-1 COCKPIT DOOR220 OPC N

OPERATIONAL CHECK OF MANUAL RELEASE OF PIP-PINS


AMM 527100/5AMT 527100-710-001MRB 527100/01

I 7 500 FHI 40 MO

ALL527100-01-1 DOOR WARNING210 OPT N

OPERATIONAL CHECK OF DOOR WARNING SYSTEMNOTE: TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORS / EMERGENCY EXITS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 122252/3AMT 122252-640-005MRB 527100/02

I 18 MO ALL527100-02-1 DOOR WARNING831 LUB832841842

N

LUBRICATION OF DOOR WARNING PROXIMITY SWITCHACTUATING MECHANISMNOTE: TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORSAccess panels :



AMM 527300/5AMT 527300-710-003MRB 527300/01

I 7 500 FHI 40 MO

ALL527300-01-1 EMERGENCY ESCAPE SLIDE RELEASE210 OPT N

AND OVERPRESSURE WARNING SYSTEMSOPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASEWARNINGNOTE: TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORS / EMERGENCY EXITS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 527300/5AMT 527300-720-003MRB 527300/02

I 18 000 CYI 80 MO

ALL527300-02-1 EMERGENCY ESCAPE SLIDE RELEASE AND122 OPT N

OVERPRESSURE WARNING SYSTEMSOPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNINGAND FUNCTIONAL CHECK OF DIFFERENTIAL PRESSURE SWITCHNOTE: TASK IS NOT APPLICABLE FOR DEACTIVATEDPASSENGER/CREW DOORSAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 530000/6AMT 530000-210-001MRB 531900/03

I 6 YE ALL530000-01-1 FUSELAGE DRAINAGE100 DVI N

REMOVE AND DETAILED INSPECTION OF PISTON TYPEDRAIN VALVES IN LOWER FUSELAGE SHELL


AMM 531900/6AMT 531900-210-001MRB 531900/06

I 4 MO ALL531900-01-1 FUSELAGE DRAINAGE220 DI N

INSPECTION OF FUSELAGE DRAINAGE


AMM 531900/6AMT 531900-710-001MRB 531900/07

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL531900-02-1 FUSELAGE DRAINAGE120 OPT Y

OPERATIONAL CHECK OF THE FUSELAGE DRAINAGE

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531900/6AMT 531900-710-003MRB 531900/08

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL531900-03-1 FUSELAGE DRAINAGE120 OPC130150

Y

OPERATIONAL CHECK OF PISTON TYPE DRAIN VALVES INLOWER FUSELAGE SHELL FROM OUTSIDE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-013MRB 532180-01-3

T 5 YEI 5 YE

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

532180-01-3 FUSELAGE FR 24-35.8133 DI134137138

Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREBETWEEN FR 24 AND FR 35.8, INCLUDING FORWARD FACE OFPRESSURE BULKHEAD, FROM STRINGER 38 LH/RH TO BOTTOMCENTERLINENOTE 1: TII TPS MAY BE LIMITED TO FUSELAGE INTERNAL STRUCTURE FROM FR 35.7 TO FR 35.8, AND FORWARD FACE OF PRESSURE BULKHEAD, FROM STRINGER 38, LH/RH TO BOTTOM CENTERLINETPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: CARGO FLOOR PANELSNOTE 2: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOFAMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT C CHECK.

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 533900/6AMT 533900-210-001MRB 531900/01

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL533900-01-1 FUSELAGE DRAINS140 INS Y

OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE HOLES INPRESSURE FLOOR FROM MLG BAY


AMM 535900/6AMT 535900-210-001MRB 531900/02

I 8 MO ALL535900-01-1 FUSELAGE DRAINS310 INS Y

OPERATIONAL CHECK OF SINGLE DRAIN PIPE AFT OF FR 70FROM OUTSIDE


AMM 535900/6AMT 535900-210-002MRB 531900/05

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL535900-02-1 FUSELAGE DRAINS827 OPC N

OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE ATBULK CARGO COMPARTMENT DOOR FROM OUTSIDE



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545000/6AMT 545000-200-001MRB 545000/01

I 24 MO

CCheck :

ALL545000-01-1 PYLONS410 GVI420

Y

GENERAL VISUAL INSPECTION OF COMPARTMENT A AND FPYLON DRAIN SYSTEMNOTE: ACCESS 482AR 482BR 486AR OR 471CL 481BR 481CR485AR OR 425BL ARE ALTERNATIVE DEPENDING ONCONFIGURATION.Access panels :

413AL 415AL 415BL 423AL 425AR 425BL 425BR471AL 471BL 471CL 475AL 481BR 481CR 482AR482BR 485AR 486AR



AMM 545000/6AMT 545000-200-002MRB 545000/02

I 72 MO ALL545000-02-1 PYLONS410 CHK420

N

FLOW CHECK OF INDIVIDUAL DRAIN LINES OF PYLON SYSTEM

Access panels :

413AL 423AL 471AL 471BL 482AR 482BR0.16Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545000/6AMT 545000-220-001ISB 54-029

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL545000-03-1 PYLON DRAINAGE410 DI420

Y

DETAILED INSPECTION OF THE CAF4 SEALANT IN PYLONCANTILEVER ZONE "A"

Access panels :



AMT 545000-220-002MRB 54.50.00/03

I 24 MO ALL545000-04-1 PYLONS410 DI420

Y

PYLONSDETAILED INSPECTION OF PYLON COMPARTMENT C DRAINSYSTEM.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 552600-200-002SIL 55-035

T 12 YEI 12 YE

ALL552600-01-1 ELEVATOR ATTACH FITTINGS335 CHK345

YR

CHECK OF ELEVATOR ATTACHMENT FITTINGS FOR WEAR,LH/RHPREP. : ELEVATOR REMOVED;NOTE: RII TASKAccess panels :




AMT 554600-200-802SIL 55-038

I 6 YE ALL553600-01-1 RUDDER ATTACH FITTINGS325 CHK NR

CHECK OF RUDDER ATTACHMENT FITTINGS FOR WEARNOTE: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 13AMD 00 EFFECTIVE DATE IS NEXT 6Y CHECK.NOTE 1: RII TASKAccess panels :

325BL 325BR 325CL 325CR 325DL 325DR 325EL325ER




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 56 WINDOWS


Threshold Interval

Ctrl References Eff

AMM 561000/6AMT 561000-200-003SIL 56-017

I 4 MO ALL561000-01-1 COCKPIT WINDOWS210 DI Y

DETAILED INSPECTION OF ALL COCKPIT WINDOWS FROMINSIDE.


AMM 561000/6AMT 561000-200-005SIL 56-017

I 20 MO ALL561000-02-1 COCKPIT WINDOWS210 DI Y

DETAILED INSPECTION OF ALL COCKPIT WINDOWS FROMOUTSIDE


AMM 561200/6AMT 561200-220-001MRB 561200/02SIL 56-017

I 48 MO

2CCheck :

ALL561200-01-1 SLIDING WINDOWS210 DI Y

DETAILED INSPECTION OF WINDOW SEALS


AMM 122256/3AMT 122256-600-001MRB 561200/01

I 20 MO ALL561200-02-1 SLIDING WINDOWS210 LUB N

LUBRICATION OF COCKPIT SLIDING WINDOW TRACKS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572900/6AMT 572900-210-002MRB 572900/01

I 80 MO ALL572900-01-1 MISCELLANEOUS (DRAINS) FOR OUTER WING500 CHK600

Y

CHECK OF DRAIN HOLES AND HOSES FOR CLOGGING


AMM 573900/6AMT 573900-200-002MRB 573900/01

I 80 MO ALL573900-01-1 MISCELLANEOUS (DRAINS) FOR WING TIP530 CHK630

Y

CHECK OF DRAIN HOLES FOR CLOGGING


AMM 575900/6AMT 575900-200-002MRB 575900/01

I 80 MO ALL575900-01-1 MISCELLANEOUS (DRAINS)500 CHK600

Y

FOR LEADING/TRAILING EDGE ANDLEADING/TRAILING EDGE DEVICES.CHECK OF DRAIN HOLES FOR CLOGGING



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 711300/5AMT 711300-800-010MRB 71.13.00/06-I2

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALL711300-I2-1 FAN COWL430 OPT440

N

FUNCTIONAL CHECK OF FAN COWL LATCH TENSIONS.

Access panels :



AMT 711300-210-803I 6 000 FHI 40 MO

ALL711300-I4-1 FAN COWL430 GVI440

N

FAN COWLGENERAL VISUAL INSPECTION OF INNER SURFACE OF DOORSAND SEALSAccess panels :



AMT 711300-220-801I 24 MO ALL711300-I5-1 FAN COWL430 GVI440

N

FAN COWLFUNCTIONAL CHECK OF PRESSURE RELIEF DOOR LATCHASSEMBLY



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 711300-210-802I 7 500 FHI 24 MO

ALL711300-I6-1 FAN COWL430 GVI440

N

FAN COWLGENERAL VISUAL INSPECTION OF FAN COWL LATCHES ANDSURROUNDING STRUCTURE



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 72 ENGINE


Threshold Interval

Ctrl References Eff

AMM 723281/4AMT 723281-920-010MRB 723280/01MRB 723280/01-I2

See noteNTCheck :

ALL723000-I1-1 COMPRESSOR SECTION430 DIS440

N

DISCARD BOOSTER DISCNOTE : REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.PREP.: ENGINE REMOVED;

AMM 724110/4AMT 724110-920-010MRB 724100/01MRB 724100/01-I2

See noteNTCheck :

ALL723000-I2-1 COMPRESSOR SECTION450 DIS460

N

DISCARD LIFE LIMITED HP COMPRESSOR MODULE ROTATINGPARTSNOTE : REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.PREP.: ENGINE REMOVED;

AMM 723100/4AMT 723100-920-010MRB 723100/01MRB 723100/01-I2

See noteNTCheck :

ALL723100-I1-1 LP COMPRESSOR (FAN) SECTION430 DIS440

N

DISCARD FAN DISCNOTE : REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.PREP.: ENGINE REMOVED;

AMM 720000/6AMT 720000-200-011ISB V2500-ENG-72-0297

I 1 500 CY ALL723100-I3-1 LP COMPRESSOR (FAN) SECTION430 DI440

N

TAP TEST OF ENGINE FAN BLADESNOTE : REFER TO SB V2500-ENG-72-0297



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 723111/6AMT 723111-200-013MRB 723100/03-I2

I 5 000 CYI 72 MO

ALL723100-I4-1 LP COMPRESSOR (FAN) MODULE430 DI440

N

DETAILED INSPECTION OF FAN BLADES LEADING EDGE FOREROSION


AMT 723111-200-010AMT 723111-300-014ISB V2500-ENG-72-0386VSB V2500-ENG-72-0386 07 01

See noteNTCheck :

ALL723100-I6-1 LP COMPRESSOR (FAN) SECTION430 DI440

N

DOVETAIL ROOT FLANK ULTRASONIC INSPECTION ANDAPPLICATION OF DRY FILM LUBRICANTNOTE : REFER TO SB V2500-ENG-72-0386


AMM 720000/6AMT 720000-200-013MRB 724000/01MRB 724000/01-I2

I 2 400 FHI 1 200 CYI 72 MO

ALL724000-I1-1 COMBUSTION SECTION450 BSI460

N

BORESCOPE INSPECTION OF INSIDE OF COMBUSTION CHAMBERAND HP TURBINE STAGE 1 VANES

Access panels :



Skills :B21 0.00 MHrsENG1 2.00 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 720000/6AMT 720000-200-018MRB 724500/01MRB 724500/01-I2

I 2 400 FHI 1 200 CYI 72 MO

ALL725000-I1-1 TURBINE SECTION450 BSI460

N

BORESCOPE INSPECTION OF HP TURBINE BLADE AEROFOILSINTERVAL NOTE: 4A OR 1200CY

Access panels :



Skills :B21 0.00 MHrsENG1 2.00 MHrs

AMM 724500/4AMT 724500-920-010MRB 724500/02

See noteNTCheck :

ALL725000-I2-1 TURBINE SECTION450 DIS460

N

DISCARD HP TURBINE DISCS, ROTATING AIRSEALS ANDRETAINING PLATESNOTE : REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.PREP.: ENGINE REMOVED;

AMM 725000/4AMT 725000-920-010MRB 725000/01MRB 725000/01-I2

See noteNTCheck :

ALL725000-I3-1 TURBINE SECTION450 DIS460

N

DISCARD LPT SHAFT, DISCS AND ROTATING AIRSEALSNOTE : REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.PREP.: ENGINE REMOVED;


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

VSB V2500-ENG-72-0461 06I 6 000 FH ALL725000-I4-1 TURBINE SECTION450 DI460

N

INSPECTION OF THE NUMBER 5 BEARING COMPARTMENT (OILJET) AND OIL TUBES FOR COKING


AMM 726000/6AMT 726000-200-011MRB 726000/01-I2

I 10 000 FHI 9 000 CYI 100 MO

ALL726000-I1-1 ACCESSORY DRIVES (EXTERNAL GEARBOX)430 GVI440

Y

GENERAL VISUAL INSPECTION OF GEARBOX MOUNTINGLINKS AND ATTACHMENT FEATURES

Access panels :



AMM 723251/4AMT 723251-920-010MRB 723226/01MRB 723226/01-I2

See noteNTCheck :

ALL726000-I2-1 INTERNAL GEARBOX AND DRIVE SYSTEM430 DIS440

N

DISCARD LP STUB SHAFTNOTE : REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.PREP.: ENGINE REMOVED;


: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 73 ENGINE FUEL CONTROL


Threshold Interval

Ctrl References Eff

AMM 732200/5AMT 732200-740-042SIL 73-017

I 600 FH ALL730000-I4-1 ENGINE FUEL & CONTROL-GENERAL210 OPC B1

CORRECT FAULTS OF THE ENGINE SCHEDULED MAINTENANCEREPORT (SMR)


AMM 731242/4AMT 731242-920-010MRB 731000/01-I2SIL 73-024

T 1 500 FHT 750 FHT 150 FHI 6 000 FHI 40 MO

ALL731000-I1-1 FUEL DISTRIBUTION435 RAR445

N

REMOVE, INSPECT FOR CONTAMINATION AND REPLACE MAINFUEL FILTERNOTE 1: - REMOVE AND REPLACE FILTER ELEMENT AT 150 FH, 750 FH AND 1500 FH AFTER A/C DELIVERY THEREAFTER SEE INTERVAL. - REMOVE AND REPLACE FILTER ELEMENT AT 150 FH AND 750 FH AFTER MAJOR TANK INTERVENTION THEREAFTER SEE INTERVAL.NOTE 2: INCASE TASK THRESHOLD IS OVERDUE WHEN APLYING NOTE 1, THE FIRSTTIME OF TASK ACCOMPLISHMENT IS NEXT A CHECK.NOTE 3: RII TASKAccess panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 73 ENGINE FUEL CONTROL


Threshold Interval

Ctrl References Eff

AMM 732200/5AMT 732200-710-043SIL 73-022

I 30 000 FH ALL732500-I1-1 FUNCTIONAL INTERFACES210 CHK N

CHECK FOR ERRONEOUS SIGNAL POSITIONS TO THEZONES CONTROLLER FROM THE BLEED AND WING/NACELLE ANTI-ICE VALVES WITH ENGINES, APUAND PACKS OPERATING



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 75 ENGINE AIR


Threshold Interval

Ctrl References Eff

AMM 752100/6AMT 752100-200-010MRB 752100/01-I2

I 48 MO ALL752100-I1-1 NACELLE COMPT AND ACCESSORY COOLING430 CHK440

Y

CHECK ZONE 1 VENTILATION INLET AND EXIT FOR BLOCKAGE

Access panels :



AMM 752100/6AMT 752100-200-011MRB 752100/02MRB 752100/02-I2

I 7 500 FHI 50 MO

ALL752100-I2-1 NACELLE COMPT AND ACCESSORY COOLING450 CHK460

Y

CHECK ZONE 2 VENTILATION INTAKE HOLES (IN THRUSTREVERSER C-DUCTS) AND EXIT FOR BLOCKAGE

Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 752200/6AMT 752200-200-010MRB 752200/01MRB 752200/01-I2

I 1 200 FHI 12 MO

ALL752200-I1-1 BEARING COMPT COOLING AND SEALING450 GVI460

Y

GENERAL VISUAL INSPECTION OF NO 4 BEARING COOLING AIRTUBES FOR DAMAGE AND SECURITY AND OF THE NO 4 BEARINGCOOLER AND ASSOCIATED INLET IN THE LEFT THRUSTREVERSER C-DUCTS FOR DAMAGE OR BLOCKAGENOTE: APPLICABILITY ONLY IAE WITH ACAC P/N D1876-1000AAccess panels :




AMT 752200-200-010I 3 000 FHI 20 MO

ALL752200-I1-2 BEARING COMPT COOLING AND SEALING450 GVI460

N

GENERAL VISUAL INSPECTION OF NO 4 BEARING COOLING AIRTUBES FOR DAMAGE AND SECURITY AND OF THE NO 4 BEARINGCOOLER AND ASSOCIATED INLET IN THE LEFT THRUSTREVERSER C-DUCTS FOR DAMAGE OR BLOCKAGENOTE 1: APPLICABILITY WITH ACAC P/N D1876-5000ANOTE 2: THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT 2A CHECK.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 752451/6AMT 752451-200-010MRB 752400/01MRB 752400/01-I2

I 7 500 FHI 50 MO

ALL752400-I1-1 HP/LP TURBINE ACC SYSTEM454 CHK464

Y

CHECK THE ACC VALVE POSITION AND ACC VALVE ROD ENDBEARING FOR LOSSENESS

Access panels :

438AR 448AR 452AR 462AR0.04Total access time : Hrs


AMM 753242/2AMT 753242-640-010CMP 72-2-0401-015SIL IAE-128

I 1 500 FH ALL753200-I1-1 HPC AIRFLOW CONTROL SYSTEM450 LUB460

N

LUBRICATION OF HPC VARIABLE STATOR VANE (VSV) MECHANISM.NOTE : TASK IS ONLY APPLICABLE TO ENGINE PRE SB V2500-ENG-72-0564Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 781000/6AMT 781000-200-010MRB 781000/01-I2

I 24 000 FHI 160 MO

See note

ALL781000-I1-1 MIXED EXHAUST SYSTEM455 GVI465

Y

GENERAL VISUAL INSPECTION OF THE EXHAUST SYSTEMFIRE SEALSNOTE : TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE REMOVAL PROVIDED INTERVAL NOT EXCEEDED.


AMM 781000/6AMT 781000-200-011MRB 781000/02-I2

I 24 000 FHI 160 MO

See note

ALL781000-I2-1 MIXED EXHAUST SYSTEM455 GVI465

Y

GENERAL VISUAL INSPECTION OF THE COMMON NOZZLEASSEMBLY FIREPROOF BULKHEAD (ENGINE OR CNA REMOVED) NOTE: -THIS TASK IS AN ALTERNATIVE TO TASK 78100-I3-1 -TASK MAY BE PERFORMED AT OPPOTUNITY OF ENGINE REMOVAL PROVIDED INTERVAL NOT EXCEEDED


AMM 781000/6AMT 781000-200-014MRB 781000/07-I2

I 24 000 FHI 160 MO

ALL781000-I3-1 MIXED EXHAUST SYSTEM455 SDI465

Y

BORESCOPE INSPECTION OF THE COMMON NOZZLE ASSEMBLYFIREPROOF BULKHEAD (ENGINE/CNA INSTALLED)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 781000-I2-1



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 783200/5AMT 783200-700-001MRB 7832AA/04MRB 783200/04-I2

I 15 000 FHI 10 000 CYI 100 MO

ALL783100-I1-1 THRUST REVERSER CONTROL & INDICATING450 OPC460

Y

OPERATIONAL CHECK OF THE THRUST REVERSER LOWERACTUATOR LOCK MECHANISM.

Access panels :



AMM 783200/6AMT 783200-200-014MRB 7832AA/02MRB 7832AA/02-I2MRB 783200/02MRB 783201/01-I2

I 2 500 FHI 30 MO

ALL783200-I2-1 THRUST REVERSER HALVES450 GVI460

Y

DETAILED INSPECTION OF THRUST REVERSER BLOCKER DOORSAND LINKAGES FOR CONDITION AND SECURITY (REQUIRESPARTIAL MANUAL DEPLOYMENT OF THRUST REVERSER)PREP. : BLOCKER DOORS DEPLOYMENT

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 783219/6AMT 783219-200-010MRB 7832BB/02MRB 783201/02-I2

I 2 500 FHI 30 MO

ALL783200-I3-1 THRUST REVERSER HALVES450 GVI460

Y

GENERAL VISUAL INSPECTION OF THE CASCADES ANDTHEIR ATTACHMENTS (REQUIRES FULL DEPLOYMENTOF THRUST REVERSER )PREP. : BLOCKER DOORS DEPLOYMENT


AMM 783200/6AMT 783200-200-013MRB 78.32.01/05-I2

I 6 000 FH ALL783200-I5-1 THRUST REVERSER COWLING SYSTEM450 GVI460

Y

GENERAL VISUAL INSPECTION OF INNER BARREL HEATSHIELDAND FIRE SEALSAccess panels :



AMT 783200-210-802I 24 MO ALL783201-I8-1 THRUST REVERSER COWLING SYSTEM450 GVI460

Y

THRUST REVERSER COWLING SYSTEMGENERAL VISUAL INSPECTION OF THRUST REVERSERCROSSOVER BEAMS, HINGES AND LATCHES



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 79 ENGINE OIL


Threshold Interval

Ctrl References Eff

AMM 790000/6AMT 790000-200-013MRB 790000/01-I2

I 600 FHI 6 MO

ALL792000-I1-1 OIL DISTRIBUTION435 CHK445

N

CHECK MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OFMETALLIC DEBRISAccess panels :

437CL 447CL0.04Total access time : Hrs


AMM 792244/4AMT 792244-920-010MRB 791000/02

I 1 200 FHI 12 MO

ALL792000-I2-1 OIL DISTRIBUTION FILTER435 DIS445

N

REMOVE INSPECT AND REPLACE SCAVENGE FILTERNOTE: RII TASKAccess panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 79 ENGINE OIL


Threshold Interval

Ctrl References Eff

AMM 792144/4AMT 792144-920-010MRB 791000/03

I 6 000 FHI 40 MO

ALL792000-I3-1 OIL DISTRIBUTION FILTER435 DIS445

N

REMOVE INSPECT AND REPLACE WITH A NEWOR CLEANED PRESSURE FILTERNOTE: RII TASKAccess panels :



SIL IAE261I 5 000 CY ALL792000-I5-1 OIL DISTRIBUTION435 DI447

N

DETAILED INSPECTION OF IDG FCOC AND ENGINE FCOCNOTE: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 13AMD 00 EFFECTIVE DATE IS NEXT C CHECKAccess panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 80 STARTING


Threshold Interval

Ctrl References Eff

AMM 801341/6AMT 801341-200-010MRB 800000/01MRB 800000/01-I2

I 600 FHI 750 CYI 6 MO

ALL801300-I1-1 ENGINE STARTING SYSTEM436 DI446

N

INSPECTION OF STARTER MAGNETIC CHIP DETECTOR

Access panels :



AMM 121380/3AMT 121380-600-011MRB 800000/02MRB 800000/02-I2SIL IAE052


ALL801300-I3-1 ENGINE STARTING SYSTEM436 SER446

B1

DRAIN AND REPLENISH OIL SYSTEM

Access panels :




: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 80 STARTING


Threshold Interval

Ctrl References Eff

AMM 801351/7AMT 801351-100-010MRB 800000/03MRB 800000/03-I2

I 5 000 CYI 60 MO

ALL801300-I4-1 ENGINE STARTING SYSTEM436 CLN446

N

CLEAN PNEUMATIC STARTER VALVE FILTER

Access panels :




: : :

: :

1412/09/2013

01



Date : SEP 2013 LIST OF EFFECTIVE PAGES - FAL Page : 1


LEP R 1 SEP 2013



Threshold Interval

Ctrl References Eff

AMT 281800-700-001AMT 281800/5FAL 281800-00001-1-FMRB 28.13.00/03MRB 28.13.00/05MRB 28.18.00/04

I 72 MO ALL281800-01-1 CENTER TANK137 FUC138

Y

FUNCTIONAL CHECK OF TANK VAPOUR SEAL AND VENT DRAINSYSTEM (SFAR88)PREP. : 241AF OR 131NW


AMM 281800/6AMT 281800-200-001FAL 281800-00002-1-FMRB 28.18.00/03

I 72 MO ALL281800-02-1 CENTER TANK191 DI192

Y

DETAILED INSPECTION OF VAPOUR SEAL (SFAR88)

Access panels :



Date ATA 28Date 22/01/2014Amendment NoIssue No Page FAL - 28 [1 / 1] :

: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 472143-700-001FAL 470000-00001-1-F

I 12 000 FH 46694703

4737

47834826

4945

49715251

5275

53065340

5385

53925418

5438

54565495

5555

56995916

5958

470000-03-1 INERT GAS GENERATION SYSTEM191 OP NR

OPERATIONAL CHECK OF DUAL FLOW SHUT OFF VALVE(DFSOV), DUAL FLAPPER CHECK VALVES (DFCV) ANDNITROGEN ENRICHED AIR (NEA) LINE FOR LEAKS.

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 472043-700-001FAL 470000-00002-1-F

I 60 000 FH 46694703

4737

47834826

4945

49715164

5241

52475251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

55555699

5709

5916

470000-04-1 INERT GAS GENERATION SYSTEM137 OP138

NR

OPERATIONAL CHECK OF BOTH DUAL FLAPPER CHECK VALVES(DFCV) FOR LEAKS.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5958

5994

Access panels :




: : :

: :

1412/09/2013

01



Date : SEP 2013 LIST OF EFFECTIVE PAGES – ASM Page : 1


LEP R 1 SEP 2013



Threshold Interval

Ctrl References Eff

AMT 292200-960-001ASM 292200-00001-1-E

T 20 YENTCheck :

ALL292000-11-1 AUXILIARY HYDRAULIC POWER195 RST N

REMOVE RAT AND ACTUATOR FOR OVERHAUL ANDREPLACE WITH NEW OR RECONDITIONED UNITS.NOTE 1 : CHECK THE PART NUMBERS OF RAT AND ACTUATOR FOR EFFECTIVITY BEFORE PERFORM THE TASKNOTE 2 : THE INTERVAL OF THIS TASK REFER TO "A321 TIMECONTROLLED ITEMS LIST" IN SECTION 3 OF AMS.NOTE 3: RII TASKAccess panels :

147BB 147CB 195BB 7340.16Total access time : Hrs


Date ATA 29Date 22/01/2014Amendment NoIssue No Page ASM - 29 [1 / 1] :

: : :

: :

1412/09/2013

01



Date : SEP 2013 LIST OF EFFECTIVE PAGES - STR Page : 1


LEP R 1 SEP 2013



Threshold Interval

Ctrl References Eff

AMM 282800/6AMT 282800-200-004

T 6 YEI 6 YE

See note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

282801-01-1 ACT EXTERNAL SURFACE151 DI152

NR

DETAILED INSPECTION OF ADDITIONAL CENTER TANK(ACT), EXTERNAL SURFACENOTE: ACT SERIAL NUMBER TO BE TRACKED SINCE TASK ACCOMPLISHMENT IS A FUNCTION OF ACT AGE AND NOT OF AIRCRAFT AGENOTE: ACT INTERGRATED WALL IMPACT REMOVED


Date ATA 28Date 22/01/2014Amendment NoIssue No Page STR - 28 [1 / 3] :

: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/6AMT 282800-200-005MRB 282802-01-1

T 12 YEI 12 YE

See note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

282802-01-1 ACT INTERNAL STRUCTURE151 DI152

NR

DETAILED INSPECTION OF ADDITIONAL CENTER TANK (ACT),INTERNAL STRUCTURENOTE: ACT SERIAL NUMBER TO BE TRACKED, SINCE TASK ACCOMPLISHMENT IS A FUNCTION OF ACT AGE AND NOT OF AIRCRAFT AGE (THRESHOLD AND INTERVAL ARE 10 ACT YEARS)PREP: ACT ACCESS PANEL ACT REMOVED; BLADDER TANK REMOVED INTEGRATED IMPACT WALL REMOVED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 282800/6AMT 282800-200-008MRB 282803-01-1NTM 282803

T 32 000 CYI 13 300 CY

See note

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

282803-01-1 ACT EXTERNAL SURFACE151 SDI152

NR

SPECIAL DETAILED INSPECTION (HFEC) OF ADDITIONALCENTER TANK (ACT), EXTERNAL SURFACE, IN AREA OFTANKPLATE PROFILESNOTE: ACT SERIAL NUMBER TO BE TRACKED, SINCE TASK ACCOMPLISHMENT IS A FUNCTION OF ACT USAGE PARAMETER (ACT FC) AND NOT OF AIRCRAFT USAGE PARAMETER (THRESHOLD & INTERVAL ARE 32000 ACT CY & 13300 ACT CY)PREP: ACT INTEGRATED IMPACT WALL



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 321100/6AMT 321100-200-008MRB 321101-01-2

T 6 YEI 6 YE

ALL321101-01-2 MAIN GEAR731 DI741

Y

DETAILED INSPECTION OF MAIN LANDING GEAR, SLIDINGTUBE (TWIN WHEEL), BRAKE ATTACHMENT FLANGE, UPPER ANDLOWER TORQUE LINKS, UPPER AND LOWER TORQUE LINK PINSAND APEX PIN & NUT - EXTERNAL SURFACES, EXCEPT WHERECOVERED BY DRESSINGS AND BUSH FLANGES.TPS : TPS MUST NOT BE APPLIEDPREP.: AIRCRAFT JACKED, SLIDING TUBE FULLY EXTENDED.;NOTE : CPCP


AMM 321100/6AMT 321100-200-009MRB 321103-01-1

T 6 YEI 6 YE

ALL321103-01-1 MAIN GEAR731 DI741

Y

DETAILED INSPECTION OF MAIN LANDING GEAR, MAINFITTING, FORWARD PINTLE PIN, FORWARD PINTLE PIN LOCK/STUB BOLTS, REAR PINTLE PIN & NUT, RETRACTIONACTUATOR ATTACHMENT PINS & UPPER DIAPHRAGM CROSS PIN- EXTERNAL SURFACES, EXCEPT WHERE COVERED BYDRESSINGS & BUSH FLANGES.NOTE : CPCP



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Threshold Interval

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AMT 321100-200-018MRB 321146-01-1

T 6 YEI 6 YE

ALL321146-01-1 MAIN LANDING GEAR PARTS731 DI741

Y

DETAILED INSPECTION OF MAIN LANDING GEAR, RETRACTIONACTUATOR - EXTERNAL SURFACE, EXCEPT WHERE COVERED BYDRESSINGS & BUSH FLANGES.NOTE : CPCP


AMT 321100-200-019MRB 321156-01-1

T 6 YEI 6 YE

ALL321156-01-2 MAIN LANDING GEAR PARTS731 DI741

Y

DETAILED INSPECTION OF MAIN LANDING GEAR, UPPER &LOWER SIDESTAY, UPPER & LOWER CARDANS AND NUTS, UPPER& LOWER LOCK LINKS, LOCKSTAY CARDAN, LOCKSTAY CARDANBRACKET & BOLTS, CUFF, TRIANGULATION LINK, BANANALINKS, UPPER & LOWER CARDAN PINS, SIDESTAY PIVOT PIN,UPPER PIN (SPRINGS), LOCKSTAY CARDAN PIN, UPPER &LOWER LOCK LINK PINS, LOCK LINK CENTER PIN,TRIANGULATION LINK PINS, LOCK LINK/BANANA LINK PIN,CUFF PINS & LOWER (SPRINGS) PIN - EXTERNAL SURFACES,EXCEPT WHERE COVERED BY DRESSINGS, BUSH FLANGES &FITTINGS.NOTE : CPCP



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01



Threshold Interval

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AMT 322100-200-018MRB 322141-01-1

T 6 YEI 6 YE

ALL322141-01-1 NOSE LANDING GEAR PARTS711 DI Y

DETAILED INSPECTION OF NOSE LANDING GEAR, BARREL,SLIDING TUBE AND TURNING TUBE EXTERNAL SURFACES,EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES.PREP.: AIRCRAFT JACKED, SLIDING TUBE FULLY EXTENDED.;NOTE : CPCP


AMT 322100-200-013MRB 322142-01-1

T 6 YEI 6 YE


DETAILED INSPECTION OF NOSE LANDING GEAR, TORQUELINKS - EXTERNAL SURFACES, EXCEPT WHERE COVERED BYDRESSINGS AND BUSH FLANGES.NOTE : CPCP


AMT 322100-200-014MRB 322143-01-1

T 6 YEI 6 YE


DETAILED INSPECTION OF NOSE LANDING GEAR, FORESTAYUPPER PANEL, LOWER LINK AND UNIVERSAL JOINT -EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGSAND BUSH FLANGES.NOTE : CPCP



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01



Threshold Interval

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AMT 322100-200-012MRB 322144-01-1

T 6 YEI 6 YE


DETAILED INSPECTION OF NOSE LANDING GEAR, LOCK LINKUPPER AND LOCK LINK LOWER - EXTERNAL SURFACES, EXCEPTWHERE COVERED BY DRESSINGS AND BUSH FLANGES.NOTE : CPCP


AMT 322100-200-009MRB 322145-01-1

T 6 YEI 6 YE


DETAILED INSPECTION OF NOSE LANDING GEAR, UPPERBARREL HINGE PINS, FORESTAY BARREL PIN, ACTUATINGCYLINDER PINS, RETAINING NUT SHOCK ASSY, TORQUE LINKPINS, TORQUE LINK APEX PIN AND NUT, UPPER PANEL TOSTRUCTURE PINS, UPPER PANEL TO UNIVERSAL JOINT PIN,LOCK LINK CENTRE PIN, LOWER LOCK LINK PIN, LOWER LOCKLINK TO UNIVERSAL JOINT PIN AND CROSS PIN - EXTERNALSURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSHFLANGES.NOTE : CPCP


AMT 322100-200-015MRB 322151-01-1

T 6 YEI 6 YE


DETAILED INSPECTION OF NOSE LANDING GEAR, ACTUATINGCYLINDER - EXTERNAL SURFACES, EXCEPT WHERE COVERED BYDRESSINGS AND BUSH FLANGES.NOTE : CPCP



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Threshold Interval

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AMM 361148/6AMT 361148-790-001MRB 360000/10SIL 36-047

I 22 000 FHI 144 MO

ALL361148-01-1 AIR BLEED DUCTS, WING500 CHK600

N

PERFORM LEAK CHECK ON BLEED AIR DUCTING IN THEWING AREA BETWEEN BLEED AIR PRECOOLER,WINGANTI ICE VALVE AND WING/FUSELAGE CONNECTIONNOTE : - TASK MAY BE COMBINED WITH TASKS 361200-02-3 AND 361200-03-1 - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR'S EXPERIENCE,A LESS OR A MORE FREQUENT INITIAL INTERVAL MAY BE USEDAccess panels :

521AB 521CB 521EB 621AB 621CB 621EB0.40Total access time : Hrs



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Threshold Interval

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AMM 521100/6AMT 521100-200-001MRB 521101-01-1

T 12 YEI 12 YE

ALL521101-01-1 FWD PAX/CREW DOOR STOP ASSEMBLIES831 DI841

Y

DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONFORWARD PASSENGER/CREW DOOR, LH/RHNOTE : CPCPAccess panels :



AMM 521100/6AMT 521100-200-002MRB 521104-01-1

T 12 YEI 6 YE

ALL521104-01-1 FWD PAX/CREW DOOR INTERNAL STRUCTURE831 DI841

Y

DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR,INTERNAL STRUCTURE, LH/RHTPS: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :




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: :

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01



Threshold Interval

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AMM 521300/6AMT 521300-200-001MRB 521301-01-1

T 12 YEI 12 YE

ALL521301-01-1 AFT PAX/CREW DOOR STOP ASSEMBLIES832 DI842

Y

DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON AFTPASSENGER/CREW DOOR, LH/RHNOTE : CPCPAccess panels :



AMM 521300/6AMT 521300-200-002MRB 521304-01-1

T 12 YEI 6 YE

ALL521304-01-1 AFT PAX/CREW DOOR INTERNAL STRUCTURE832 DI842

Y

DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR,INTERNAL STRUCTURE, LH/RHTPS: APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :




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01



Threshold Interval

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AMM 522211/6AMT 522211-200-001MRB 522202-01-1

T 12 YEI 6 YE

ALL522202-01-1 FWD EMERGENCY EXITS, INTERNAL833 DI843

N

DETAILED INSPECTION OF FORWARD EMERGENCY EXITS,INTERNAL STRUCTURE, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :



AMM 522211/6AMT 522211-200-002MRB 522205-01-1

T 12 YEI 6 YE

ALL522205-01-1 AFT EMERGENCY EXITS INTERNAL834 DI844

N

DETAILED INSPECTION OF AFT EMERGENCY EXITS, INTERNALSTRUCTURE, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 523111/6AMT 523111-200-001MRB 523103-01-1

T 12 YEI 6 YE

ALL523103-01-1 FWD CARGO DOOR INTERNAL STRUCTURE825 DI Y

DETAILED INSPECTION OF FORWARD CARGO COMPARTMENTDOOR, INTERNAL STRUCTURETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :



AMM 523111/6AMT 523111-200-022MRB 523105-01-3

T 5 300 CYI 5 300 CY

ALL523105-01-3 FWD CARGO COMPARTMENT DOOR ACTUATOR825 GVI Y

GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR, ACTUATOR ATTACH FITTINGSAccess panels :




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01



Threshold Interval

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AMM 523111/6AMT 523111-200-005MRB 523109-01-1


ALL523109-01-1 FWD CARGO DOOR LOCKING HOOKS825 DI Y

DETAILED INSPECTION OF LOCKING HOOKS AND FORKFITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALLFRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE 1: 100% LIMIT = 12 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :



AMM 523211/6AMT 523211-200-001MRB 523113-01-1

T 12 YEI 6 YE

ALL523113-01-1 AFT CARGO DOOR INTERNAL STRUCTURE826 DI Y

DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,INTERNAL STRUCTURETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :




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: :

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01



Threshold Interval

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AMM 523211/6AMT 523211-200-022MRB 523115-01-3

T 5 300 CYI 5 300 CY

ALL523115-01-3 AFT CARGO DOOR ACTUATOR ATTACH FITTINGS826 GVI Y

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENTDOOR, ACTUATOR ATTACH FITTINGSAccess panels :



AMM 523211/6AMT 523211-200-006MRB 523119-01-2


ALL523119-01-2 AFT CARGO DOOR LOCKING HOOKS826 DI Y

DETAILED INSPECTION OF LOCKING HOOKS AND FORKFITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE 1: 100% LIMIT = 12 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

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01



Threshold Interval

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AMM 523311/6AMT 523311-200-003MRB 523303-01-1

T 12 YEI 6 YE

ALL523303-01-1 BULK CARGO DOOR INTERNAL827 DI Y

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR,INTERNAL STRUCTURETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP : LINING REMOVED INSULATION REMOVEDNOTE : CPCPAccess panels :



AMM 523311/6AMT 523311-200-002MRB 523305-01-1

T 12 YEI 12 YE

ALL523305-01-1 BULK CARGO DOOR FITTINGS AREA827 DI Y

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOORSTOP FITTINGS AND ATTACHMENT AREA, EXTERNAL ANDINTERNALTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : LINING REMOVED INSULATION REMOVEDNOTE 1: 100 % LIMIT=12 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 524111/6AMT 524111-200-001MRB 524111-01-1

T 12 YEI 12 YE

ALL524111-01-1 FWD AVIONIC DOOR INTERNAL STRUCTURE811 DI Y

DETAILED INSPECTION OF FORWARD AVIONICS COMPARTMENTACCESS DOOR, INTERNAL STRUCTURE, INCLUDING HINGE ARMSTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: DOOR FLOOR PANEL REMOVEDNOTE: CPCPAccess panels :



AMM 524114/6AMT 524114-200-001MRB 524121-01-1

T 12 YEI 6 YE

ALL524121-01-1 AFT AVIONIC DOOR INTERNAL STRUCTURE824 DI Y

DETAILED INSPECTION OF AFT AVIONICS COMPARTMENTACCESS DOOR, INTERNAL STRUCTURETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 524113/6AMT 524113-200-001MRB 524131-01-1

T 12 YEI 6 YE

ALL524131-01-1 LATERAL RIGHT AVIONIC DOOR822 DI Y

DETAILED INSPECTION OF LATERAL RIGHT AVIONICSCOMPARTMENT ACCESS DOOR, INTERNAL STRUCTURETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :



AMM 524112/6AMT 524112-200-001MRB 524141-01-1

T 12 YEI 6 YE

ALL524141-01-1 LATERAL LEFT AVIONIC DOOR812 DI Y

DETAILED INSPECTION OF LATERAL LEFT AVIONICSCOMPARTMENT ACCESS DOOR, INTERNAL STRUCTURETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: LINING REMOVED INSULATION REMOVEDNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 528100/6AMT 528100-200-001MRB 528101-01-1

T 6 YEI 6 YE

ALL528101-01-1 MLG DOOR FWD AND AFT FITTING734 DI744

Y

DETAILED INSPECTION OF MLG DOOR, FORWARD AND AFTFITTINGS, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :



AMT 528100-280-801MRB 528106-01-1NTM 52-81-06

T 18 800 CYI 3 600 CY

ALL528106-01-1 MAIN GEAR DOORS734 NDT744

N

SPECIAL DETAILED INSPECTION (HFEC & US) OF MLG DOORACTUATOR LUGS, LH/RH.NOTE: FOR PRE 24903 AIRCRAFT RETROFITTED, THRESHOLDIS TO BE COUNTED FROM SB 52-1073 EMBODIMENTPREPARATION: ACTUATOR REMOVED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 528200/6AMT 528200-200-001MRB 528211-01-1

T 6 YEI 6 YE

ALL528211-01-1 NLG MAIN DOOR HINGES713 DI714

Y

DETAILED INSPECTION OF NLG, MAIN DOOR HINGES, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :



AMM 528200/6AMT 528200-200-002MRB 528221-01-1

T 6 YEI 6 YE

ALL528221-01-1 NLG SECONDARY DOOR HINGES715 DI716

Y

DETAILED INSPECTION OF NLG, SECONDARY DOOR HINGES,LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMT 528200-220-801MRB 528223-01-1

T 26 000 CYI 7 500 CY

ALL528223-01-1 NOSE GEAR DOORS715 DI716

N

DETAILED INSPECTION OF NLG AFT DOOR AFT FITTINGS,LH/RHAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 531100/6AMT 531100-210-002MRB 531104-01-1

T 96 000 FHT 48 000 CYI 16 000 FHI 8 000 CY

ALL531104-01-1 DOOR FRAME FWD LOWER CORNER220 DI Y

DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOORFRAME, FORWARD LOWER CORNER UNDERNEATH THE SCUFFPLATE, LH/RHPREP. : FWD CORNER SCUFF PLATE REMOVEDNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 531104-02-1NOTE 2: SAMPLING 20%


AMM 531100/6AMT 531100-210-028MRB 531104-02-1NTM 53-11-04

T 96 000 FHT 48 000 CYI 32 200 FHI 16 100 CY

ALL531104-02-1 DOOR FRAME EXTERNAL SURFACE220 SDI Y

SPECIAL DETAILED INSPECTION (US) OF FORWARDPASSENGER/CREW DOOR FRAME, FORWARD LOWER CORNERUNDERNEATH THE SCUFF PLATES, LH/RH.PREP. : FWD CORNER SCUFF PLATE REMOVEDNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 531104-01-1NOTE 2: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-003MRB 531107-01-1

T 30 000 CYI 20 000 CY

ALL531107-01-1 FWD PRESSURE BULKHEAD110 DI Y

DETAILED INSPECTION OF FORWARD FACE OF PRESSUREBULKHEAD, VERTICAL ANGLE (Y=675) AT CROSSING AREASWITH HORIZONTAL STIFFENERS (Z=1 AND Z=1329), LH/RHPREP.: UPPER PROTECTIVE SHIELDNOTE : SAMPLING 20%Access panels :



AMM 531100/6AMT 531100-210-008MRB 531120-01-1

T 30 000 CYI 18 500 CY

ALL531120-01-1 UPPER LAP JOINT EXTERNAL SURFACE200 DI Y

DETAILED INSPECTION OF UPPER SKIN OF UPPERLONGITUDINAL LAP JOINT, BETWEEN FR 15 AND FR 16 ANDFR 20 AND FR 24, EXTERNAL SURFACE, LH/RHNOTE : SAMPLING 20%


AMM 531100/6AMT 531100-210-009MRB 531121-01-1

T 30 000 CYI 16 600 CY

ALL531121-01-1 LAT LAP JOINT FR 11-14, FR 20-24100 DI Y

DETAILED INSPECTION OF OUTER SKIN OF LATERALLONGITUDINAL LAP JOINT, BETWEEN FR 11 AND FR 14 ANDFR 20 AND FR 24, LH/RHNOTE : SAMPLING 20%



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: :

1412/09/2013

01



Threshold Interval

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AMM 531100/6AMT 531100-210-010MRB 531123-01-1

T 6 YEI 6 YE

ALL531123-01-1 LAT LAP JOINT FR 01-24100 DI Y

DETAILED INSPECTION OF OUTER SKIN OF LATERALLONGITUDINAL LAP JOINT, BETWEEN FR 1 AND FR 24, LH/RHNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCP


AMT 531100-220-805MRB 531125-02-1

T 33 000 CYI 29 800 CY

ALL531125-02-1 NOSE FORWARD FUSELAGE211 DI212

N

DETAILED INSPECTION OF CENTRAL/LATERAL WINDOW FRAMEAROUND FASTENER HOLE, UPPER AREA, LH/RHPREPARATION: SLIDING WINDOW OPENED;NOTE: SAMPLING 20%


AMM 531100/6AMT 531100-210-013MRB 531131-01-1

T 30 000 CYI 20 000 CY

ALL531131-01-1 WINDSHIELD CTR POST UPR ATTACHMENT211 DI212

Y

DETAILED INSPECTION OF WINDSHIELD CENTER POST, UPPERATTACHMENT AREA, INTERNAL SIDENOTE : SAMPLING 20%Access panels :

211LC 211MC 211MW 212LC0.08Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-015MRB 531141-01-1

T 30 000 CYI 9 200 CY

ALL531141-01-1 SIDE WINDOW STRUCTURE200 DI Y

DETAILED INSPECTION OF SIDE WINDOW STRUCTURE, UPPERJUNCTION, BETWEEN FORWARD AND REAR FR, EXTERNALSURFACE, LH/RHNOTE : SAMPLING 20%


AMM 531100/6AMT 531100-210-017MRB 531151-01-1

T 12 YEI 12 YE

ALL531151-01-1 DOOR STOP FITTINGS221 DI222

Y

DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 16AND FR 20, LH/RHPREP. : LINING REMOVEDNOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 531100/6AMT 531100-210-025MRB 531153-02-1NTM 53-11-53

T 30 000 CYI 17 700 CY

ALL531153-02-1 DOOR STOPS AT FR 16221 SDI222

Y

SPECIAL DETAILED INSPECTION (HFEC) OF DOOR FR 16, ATDOUBLE JOGGLE AREA IN OUTER FLANGE OF FR, AT DOORSTOPS NUMBER 1 AND 7 LOCATION, LH/RH.PREP.: BOLTS REMOVED LINING REMOVED INSULATION REMOVEDNOTE : SAMPLING 20%Access panels :



AMM 531100/6AMT 531100-210-803MRB 531161-01-1

T 6 YEI 6 YE

ALL531161-01-1 NLG BAY ALL PANELS123 GVI Y

GENERAL VISUAL INSPECTION OF NLG BAY, ALL PANELS,LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 531100/6AMT 531100-210-018MRB 531162-01-2

T 60 000 FHT 30 000 CYI 38 300 FHI 19 100 CY

ALL531162-01-2 NLG BAY127 DI128

Y

DETAILED INSPECTION OF NLG BAY, REAR PANEL AFT FACE,LOWER CORNERS, LH/RH.NOTE : SAMPLING 20%PREP.: LADDER REMOVED; FLOOR PANEL REMOVED;Access panels :



AMM 531100/6AMT 531100-210-019MRB 531163-01-1

T 6 YEI 6 YE

ALL531163-01-1 FWD PAX/CREW DOOR SURROUND221 DI222

Y

FORWARD PASSENGER/CREW DOOR, ABOVE CABIN FLOOR LEVEL,BETWEEN FR 15 AND FR 21 AND BETWEEN STRINGER 8 ANDSTRINGER 23, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: CEILING PANELS REMOVED LINING REMOVED INSULATION REMOVEDNOTE 1:CPCPNOTE 2:EXCLUDED AREA COVERED BY TASKS 531166-01-1 AND 531166-01-2Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-801MRB 531164-01-1

T 6 YEI 6 YE

ALL531164-01-1 FUSELAGE FR 15-21125 DI126

Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,BELOW FORWARD PASSENGER/CREW DOOR AND CABIN FLOORLEVEL, FROM FR 15 TO FR 21 AND BETWEEN STRINGER 28 LHAND STRINGER 28 RH.TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: INSULATION REMOVEDNOTE: CPCPAccess panels :



AMM 531100/6AMT 531100-220-006MRB 531166-01-2

T 6 YEI 6 YE

ALL531166-01-2 FUSELAGE FR 16-20221 DI222

Y

DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUTOUTLOWER CORNERS INTERNAL STRUCTURE ABOVE CABIN FLOORLEVEL, AT FR 16 AND FR 20 FROM STRINGER 22 TOSTRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RH.TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2NOTE:CPCPPREP: BLANKING PLATE REMOVED; GIRT BAR FITTING REMOVEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-036MRB 531167-01-1

T 6 YEI 6 YE

ALL531167-01-1 AREA BELOW BATTERIES126 DI Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,BELOW BATTERIES, BETWEEN FR 10 AND FR 16, RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :



AMM 531100/6AMT 531100-210-804MRB 531169-01-1

T 6 YEI 6 YE

ALL531169-01-1 FUSELAGE FR 12-15125 GVI126

Y

GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE, BELOW GALLEY AND TOILET, BETWEEN FR 12 ANDFR 15 AND BETWEEN STRINGER 23 LH AND STRINGER 23 RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: INSULATION REMOVEDNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-020MRB 531171-01-1

T 6 YEI 6 YE

ALL531171-01-1 NLG SECONDARY DOOR HINGE SUPPORTS123 DI124

Y

DETAILED INSPECTION OF NLG, SECONDARY DOOR HINGESUPPORTS ON FUSELAGE, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :



AMM 531100/6AMT 531100-210-032MRB 531172-01-1

T 30 000 CYI 14 000 CY

ALL531172-01-1 SKIN FR21-23 & FR17-18 FROM STGR 31-36100 DI Y

DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 21AND FR 23 LH AND FR 17 AND FR 18 RH, FROM STRINGER 31TO STRINGER 36NOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-040MRB 531175-01-1

T 12 YEI 12 YE

ALL531175-01-1 FWD FACE OF FRONT PRESSURE BULKHEAD110 DI Y

DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSUREBULKHEAD ATTACHED TO FR 1PREP. : PROTECTIVE SHIELDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :



AMM 531100/6AMT 531100-210-041MRB 531176-01-1

T 6 YEI 6 YE

ALL531176-01-1 COCKPIT SIDE WINDOWS FRAMEWORK200 DI Y

DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, EXTERNALVISIBLE PORTION OF FRAMEWORK, BETWEEN FR 4 AND FR 12,LH/RHNOTE : CPCP


AMM 531100/6AMT 531100-210-042MRB 531177-01-1

T 12 YEI 12 YE

ALL531177-01-1 COCKPIT WINDSHIELD FRAME200 DI Y

DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNALPORTION OF FRAMEWORK COVERED BY RETAINERSTPS : TPS MUST NOT BE APPLIEDPREP: WINDSHIELD RETAINERSNOTE: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-043MRB 531178-01-1

T 6 YEI 6 YE

ALL531178-01-1 COCKPIT WINDSHIELD RETAINERS200 DI Y

DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNALVISIBLE PORTION OF RETAINERSNOTE : CPCP


AMM 531100/6AMT 531100-210-044MRB 531180-01-1

T 12 YEI 12 YE

ALL531180-01-1 FWD PAX/CREW DOOR UNDER SCUFF-PLATE100 DI Y

DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOORCUTOUT, UNDERNEATH THE SCUFF-PLATE, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: SCUFF PLATE REMOVEDNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-035MRB 531181-01-1

T 6 YEI 6 YE

ALL531181-01-1 FUSELAGE INTL STRUCT FR15-21, STR23-28129 DI Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREAND LOWER SURFACE OF CABIN FLOOR STRUCTURE FROM FR 15TO FR 21, BETWEEN STRINGER 23 AND STRINGER 28 LH/RHNOTE 1: TII TPS MAY BE LIMITED TO LOWER SURFACE OF CABIN FLOOR STRUCTURE BETWEEN FR15 AND FR21TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP. : CABIN FLOOR PANELS REMOVED STAIRS DEPLOYED (IF INSTALLED)NOTE 2: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 531100-210-814MRB 531185-01-1

T 12 YEI 12 YE

ALL531185-01-1 FUSELAGE INTERNAL STRUCTURE211 GVI212221222223224231232233234

Y

GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FROM FR 1 TO FR 24, ABOVE CABIN FLOORLEVEL, AS FAR AS VISIBLE.PREP. : AIR CONDITIONING DUCTS REMOVED; GALLEYS AND TOILETS REMOVED; LINING AND CEILING PANELS REMOVED; INSULATION DISPLACED;NOTE 1: CPCPNOTE 2: SAMPLING 20%NOTE 3: 100% LIMIT = 24 YE


AMM 531100/6AMT 531100-210-046MRB 531186-01-1

T 12 YEI 12 YE

ALL531186-01-1 AFT FACE OF FWD PRESSURE BULKHEAD211 DI212

Y

DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSUREBULKHEAD, ABOVE COCKPIT FLOOR LEVEL, INCLUDING FR 1,AS FAR AS VISIBLEPREP. : INSULATION DISPLACED WIRING BUNDLES DISPLACEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-047MRB 531187-01-1

T 12 YEI 12 YE

ALL531187-01-1 COCKPIT WINDOW FRAMES211 DI212

Y

DETAILED INSPECTION OF COCKPIT WINDOW FRAMES ANDCLOSING PANELS, INTERNAL STRUCTURE (FR 12 ANDFORWARD).PREP. : - INSULATION DISPLACED - LINING REMOVED - ELECTRONIC DEVICES DISPLACEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :



AMM 531100/6AMT 531100-210-048MRB 531188-01-1

T 12 YEI 12 YE

ALL531188-01-1 COCKPIT FLOOR STRUCTURE211 DI212

Y

DETAILED INSPECTION OF COCKPIT FLOOR STRUCTURE,BETWEEN FR 1 AND FR 12TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: COCKPIT FLOOR PANELS RUBBER LEVELLING STRIPSNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-049MRB 531189-01-2

T 6 YEI 6 YE

ALL531189-01-2 FUSELAGE FR 12-21NT DI Y

DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BETWEENFR 12 AND FR 21TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: CABIN FLOOR PANELS GALLEYS TOILET REMOVAL/INSTALLATIONNOTE 1: CPCPNOTE 2: WORKING ZONES: 211, 212, 221, 222, 231, 232Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-805MRB 531190-01-2

T 12 YEI 12 YE

ALL531190-01-2 FLOOR STRUCTURE FR 21 TO FR 24NT GVI Y

GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,EXCLUDING AREAS BELOW GALLEYS AND TOILETS, BETWEEN FR21 AND FR 24TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP. : CABIN FLOOR PANELSNOTE 1: CPCPNOTE 2: WORKING ZONES 221, 222, 231, 232Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-220-002MRB 531191-01-1

T 12 YEI 12 YE

ALL531191-01-1 AFT FACE OF FWD PRESSURE BULKHEAD121 DI122

Y

DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSUREBULKHEAD, BELOW COCKPIT FLOOR LEVEL, INCLUDING FR 1AND STRINGER CONNECTIONS.NOTE 1: IF CORROSION IS FOUND ON THE PRESSURE BULKHEADABOVE THE AVIONICS FLOOR PANELS THE COMPLETE AFT FACE(UPPER AND LOWER AREAS) OF THE PRESSURE BULKHEAD ISTO BE INSPECTED.TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : - FORWARD AVIONICS BAY FLOOR PANELS REMOVED - INSULATION DISPLACED - WIRING BUNDLES DISPLACEDNOTE 2: CPCPAccess panels :

NONE 8112.32Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-806MRB 531192-01-1

T 12 YEI 12 YE

ALL531192-01-1 FUSELAGE FR 1 TO 12121 GVI122125126

Y

GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE AND FLOOR STRUCTURE, INCLUDING NLG BAYPANELS, BETWEEN FR 1 AND FR 12, BELOW COCKPIT FLOORPANELSNOTE 1: TPS MAY BE LIMITED TO FUSELAGE INTERNAL STRUCTURE BETWEEN FR1 AND FR12 AND AFT FACE OF PRESSURE BULKHEAD, FROM STRINGER 32, LH/RH TO BOTTOM CENTERLINETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : AIR DUCT. FORWARD AVIONICS BAY FLOOR PANELS REMOVED INSULATION REMOVEDNOTE 2: CPCPAccess panels :

NONE 811 812 8223.06Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-210-807MRB 531193-01-1

T 12 YEI 12 YE

ALL531193-01-1 FUSELAGE FR 21 TO 24127 GVI128

Y

GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE AND FLOOR STRUCTURE, INCLUDING NLG BAY AFTFACE, BETWEEN FR 21 AND FR 24, BELOW CABIN FLOORPANELSNOTE 1: TPS MAY BE LIMITED TO FUSELAGE INTERNAL STRUCTURE BETWEEN FR 21 AND FR 24, FROM STRINGER 32, LH/RH TO BOTTOM CENTERLINETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : AVIONICS BAY FLOOR PANELS REMOVEDNOTE 2: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 531100/6AMT 531100-220-003MRB 531194-01-2

T 6 YEI 6 YE

ALL531194-01-2 FLOOR STRUCTURE FR 21 TO 24221 DI222231232

Y

DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOWAND 0.5M AROUND GALLEYS AND TOILETS, BETWEEN FR 21AND FR 24TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: CABIN FLOOR PANELS GALLEYS TOILET REMOVAL/INSTALLATIONNOTE: CPCPNOTE: TASK ONLY APPLICABLE IF GALLEYS/TOILETS INSTALLED BETWEEN FR 21 AND FR 24Access panels :



ISB 53-1180T 10 000 CYI 500 CY

2267531197-01-1 NLG BAY123 DI124

YD

DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATORFITTING FASTENERSAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2013-0122ISB 53-1259

T 60 000 FHT 30 000 CYI 10 000 FHI 5 000 CY

ALL531259-01-1 TI-ANGLE CONNECTION BETWEEN BELLY140 DI N

DETAILED INSPECTION OF OF TI-ANGLE CONNECTIONBETWEEN BELLY FAIRING AND KEEL BEAM SIDE PANELFR41-FR42, RH/LH.NOTE: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT C CHECK.

AMM 532100/6AMT 532100-210-001MRB 532102-01-2

T 12 YEI 12 YE

ALL532102-01-2 FLOOR STRUCTURE FR 24-35.8231 GVI232

Y

GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,EXCLUDING AREAS BELOW GALLEYS AND TOILETS (IFINSTALLED) AND EMERGENCY EXIT ENTRANCE AREA, BETWEENFR 24 AND FR 35.8TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: CABIN FLOOR PANELSNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-220-001MRB 532105-01-2

T 6 YEI 6 YE

ALL532105-01-2 FLOOR STRUCTURE FR 24 TO FR 35.8231 DI232

Y

DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOWAND 0.5M AROUND GALLEYS AND TOILETS (IF INSTALLED)AND EMERGENCY EXIT ENTRANCE AREA, BETWEEN FR 24 ANDFR 35.8TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: CABIN FLOOR PANELS GALLEYS TOILET REMOVAL/INSTALLATIONNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-018MRB 532113-01-1

T 6 YEI 6 YE

ALL532113-01-1 FWD EMERGENCY EXIT CUTOUT SURROUNDS231 DI232

Y

DETAILED INSPECTION OF INTERNAL STRUCTURE AROUNDFORWARD EMERGENCY EXIT CUTOUTS, BETWEEN FR 35 AND FR35.3 FROM STRINGER 23 LH TO STRINGER 7 LH AND FROMSTRINGER 23 RH TO STRINGER 10 RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: CEILING PANELS REMOVED LINING REMOVED OVERHEAD STOWAGE COMPARTMENTS ON RH SIDE (IF REMOVED (IF INSTALLED) INSULATION REMOVEDNOTE: CPCPAccess panels :

NONE 833 8430.19Total access time : Hrs


AMM 532100/6AMT 532100-200-019MRB 532114-01-1

T 12 YEI 12 YE

ALL532114-01-1 DOOR STOP FITTINGS231 DI232

Y

DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 35.1AND FR 35.2A, LH/RHPREP.: LINING REMOVEDNOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-220-006MRB 532115-01-1

T 30 000 CYI 20 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532115-01-1 FR35.1 &.2A WEB/DOOR STOP INTERCOSTALS231 DI232

YR

DETAILED INSPECTION OF FR 35.1 AND FR 35.2A WEB ANDDOOR STOP INTERCOSTALS, AT JUNCTION AREA, BETWEENDOOR STOP NO1 AND NO8 (LH)/NO6 (RH), LH/RHPREP : LINING REMOVED INSULATION REMOVEDNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 532100/6AMT 532100-220-006MRB 532115-01-2

T 30 000 CYI 19 100 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

532115-01-2 FR35.1 &.2A WEB/DOOR STOP INTERCOSTALS231 DI232

Y

DETAILED INSPECTION OF FR 35.1 AND FR 35.2A WEB ANDDOOR STOP INTERCOSTALS, AT JUNCTION AREA, BETWEENDOOR STOP NO1 AND NO8 (LH)/NO6 (RH), LH/RHPREP : LINING REMOVED INSULATION REMOVEDNOTE : SAMPLING 20%

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-020MRB 532117-01-1

T 6 YEI 6 YE

ALL532117-01-1 ESCAPE CHUTE SLIDE COMPARTMENT131 DI132

Y

DETAILED INSPECTION OF ESCAPE CHUTE SLIDECOMPARTMENT, INTERNAL STRUCTURE, BETWEEN FR 35.1 ANDFR 35.2A, FROM STRINGER 24 TO STRINGER 28, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: ESCAPE CHUTE SLIDE ASSEMBLY REMOVEDNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-021MRB 532119-01-1


22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532119-01-1 FWD EMER EXIT CUTOUT UNDER SCUFF-PLATE100 DI YR

DETAILED INSPECTION OF FORWARD EMERGENCY EXIT CUT OUTUNDERNEATH THE SCUFF-PLATE, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP. : SCUFF PLATE REMOVEDNOTE 1: 100% LIMIT = 12 YENOTE 2: SAMPLING 20%NOTE 3: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 532100/6AMT 532100-200-021MRB 532119-01-2


2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

532119-01-2 FWD EMER EXIT CUTOUT UNDER SCUFF-PLATE100 DI Y

DETAILED INSPECTION OF FORWARD EMERGENCY EXIT CUT OUTUNDERNEATH THE SCUFF-PLATE, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP. : SCUFF PLATE REMOVEDNOTE 1: 100% LIMIT = 12 YENOTE 2: SAMPLING 20%NOTE 3: CPCP

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-001MRB 532120-01-1

T 30 000 CYI 9 500 CY

ALL532120-01-1 FRAME WEBS231 DI232

Y

DETAILED INSPECTION OF FRAME WEBS AT STRINGER 18LH/RH FOR FR 25, 26, 27, 28, 32, 33, 34PREP.: LINING INSULATION REMOVEDNOTE : SAMPLING 20%Access panels :



AMM 532100/6AMT 532100-200-002MRB 532125-01-1

T 60 000 FHT 30 000 CYI 20 800 FHI 10 400 CY

ALL532125-01-1 JUNCTION FR 24/PAX FLOOR BEAM128 DI132

Y

DETAILED INSPECTION OF FR 24 JUNCTION WITH CABINFLOOR BEAM AT STRINGER 23, INTERNAL SIDE, RHPREP.: INSULATION REMOVEDNOTE : SAMPLING 20%Access panels :

NONE 131HC 132BW 132EW 8250.23Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-027MRB 532132-01-3

T 12 YEI 12 YE

ALL532132-01-3 FWD CARGO DOOR HINGE FITTING100 DI132

Y

DETAILED INSPECTION OF FUSELAGE FORWARD CARGO DOORHINGE FITTING AND EXTERNAL ATTACHMENT AREANOTE 1: TPS APPLICATION IS LIMITED TO THE INNER SIDE OF THE HINGE FITTINGSTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : DOOR OPENED AND CLOSEDNOTE 2: CPCPAccess panels :



AMM 532100/6AMT 532100-200-016MRB 532140-01-1

T 60 000 FHT 30 000 CYI 14 200 FHI 7 100 CY

ALL532140-01-1 FR 25, 26 AND 27 LOWER FITTINGS132 DI232

Y

DETAILED INSPECTION OF INSIDE RADIUS OF CROSS BEAM ATFR 25, FR 26 AND FR 27 LOWER FITTINGS, LOCATED ABOVEFORWARD CARGO DOOR, RHNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 532140-02-1PREP. : ACTUATOR DISCONNECTED CEILING PANELS REMOVEDNOTE 2: SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-017MRB 532140-02-1NTM 53-21-40

T 60 000 FHT 30 000 CYI 34 800 FHI 17 400 CY

ALL532140-02-1 FR 25, 26 AND 27 LOWER FITTINGS132 SDI232

Y

SPECIAL DETAILED INSPECTION (HFEC) OF INSIDE RADIUSOF CROSS BEAM AT FR 25, FR 26 AND FR 27 LOWERFITTINGS, LOCATED ABOVE FORWARD CARGO DOOR, RH.NOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 532140-01-1PREP. : ACTUATOR DISCONNECTED CEILING PANELS REMOVEDNOTE 2: SAMPLING 20%Access panels :



AMM 532100/6AMT 532100-200-009MRB 532145-01-2

T 30 000 CYI 11 100 CY

ALL532145-01-2 FR 29 TO 34 ATTACHMENT AREA131 DI132

Y

DETAILED INSPECTION OF ATTACHMENT AREA OF FR 29 TO FR34, CARGO FLOOR BEAMS, LH/RHPREP:CARGO FLOOR PANELS REMOVED;NOTE : SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-220-007MRB 532147-01-1

T 30 000 CYI 15 400 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532147-01-1 FR35.1 & FR35.2A TO CABIN FLOOR BEAMS131 DI132

YR

DETAILED INSPECTION OF ATTACHMENT AREA OF FR 35.1 ANDFR 35.2A TO CABIN FLOOR BEAMS, LH/RHPREP.: LINING REMOVED INSULATION REMOVEDNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 532100/6AMT 532100-220-007MRB 532147-01-2

T 30 000 CYI 14 700 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

532147-01-2 FR35.1 & FR35.2A TO CABIN FLOOR BEAMS131 DI132

Y

DETAILED INSPECTION OF ATTACHMENT AREA OF FR 35.1 ANDFR 35.2A TO CABIN FLOOR BEAMS, LH/RHPREP.: LINING REMOVED INSULATION REMOVEDNOTE : SAMPLING 20%

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-220-005MRB 532153-01-1

T 60 000 FHT 30 000 CYI 22 500 FHI 8 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532153-01-1 FUSELAGE SKIN/WINDOW FORCING DOUBLERS200 DI YR

DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE PARTOF WINDOW FORGING DOUBLERS AROUND CABIN WINDOWS,BETWEEN FR 35.3 AND FR 35.8 AND BETWEEN STRINGER 14AND STRINGER 18, EXTERNAL SURFACE, LH/RHNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


AMM 532100/6AMT 532100-220-005MRB 532153-01-2

T 60 000 FHT 30 000 CYI 22 700 FHI 8 600 CY

2974

3005

30133022

3198

33153355

3737

38623964

3966

41364213

4277

43114315

532153-01-2 FUSELAGE SKIN/WINDOW FORCING DOUBLERS200 DI Y

DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE PARTOF WINDOW FORGING DOUBLERS AROUND CABIN WINDOWS,BETWEEN FR 35.3 AND FR 35.8 AND BETWEEN STRINGER 14AND STRINGER 18, EXTERNAL SURFACE, LH/RHNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-220-002MRB 532158-01-1

T 60 000 FHT 30 000 CYI 19 900 FHI 7 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532158-01-1 FUSELAGE SKIN BETWEEN FR 35 & FR 35.8200 DI YR

DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE,BETWEEN FR 35 AND FR 35.8 FROM STRINGER 8 TO CROWNCENTERLINE, LH/RH.NOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


AMM 532100/6AMT 532100-220-002MRB 532158-01-2

T 60 000 FHT 30 000 CYI 24 000 FHI 9 000 CY

2974

3005

30133022

3198

33153355

3737

38623964

3966

41364213

4277

43114315

532158-01-2 FUSELAGE SKIN BETWEEN FR 35 & FR 35.8200 DI Y

DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE,BETWEEN FR 35 AND FR 35.8 FROM STRINGER 8 TO CROWNCENTERLINE, LH/RH.NOTE : SAMPLING 20%

AMM 532100/6AMT 532100-200-008MRB 532160-01-1

T 48 000 CYI 13 000 CY

ALL532160-01-1 FUSELAGE SKIN BETWEEN FR 28 AND 35200 DI Y

DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE PARTOF WINDOW FORGING DOUBLERS AROUND CABIN WINDOWS,BETWEEN FR 28 AND FR 35 AND BETWEEN STRINGER 14 ANDSTRINGER 18, EXTERNAL SURFACE, LH/RH



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 532100-210-802MRB 532164-01-6

T 60 000 FHT 30 000 CYI 5 800 FHI 2 900 CY

ALL532164-01-6 FORWARD FUSELAGE200 GVI N

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, FROM STRINGER 23 LH/RH TO CROWN CENTERLINE,EXCEPT AREAS COVERED BY BELLY FAIRINGNOTE: INSPECTION BETWEEN FR 24 AND FR 35.8.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-220-003MRB 532168-01-1

T 30 000 CYI 9 600 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

532168-01-1 FUSELAGE SKIN COVERED BY BELLY FAIRING191 DI192

YR

DETAILED INSPECTION OF FUSELAGE SURFACE COVERED BYBELLY FAIRING, BETWEEN FR 35.5 AND FR 35.7 FROMSTRINGER 26 TO STRINGER 32, LH/RHNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 532100/6AMT 532100-220-003MRB 532168-01-2

T 30 000 CYI 9 100 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

532168-01-2 FUSELAGE SKIN COVERED BY BELLY FAIRING191 DI192

Y

DETAILED INSPECTION OF FUSELAGE SURFACE COVERED BYBELLY FAIRING, BETWEEN FR 35.5 AND FR 35.7 FROMSTRINGER 26 TO STRINGER 32, LH/RHNOTE : SAMPLING 20%

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-011MRB 532175-01-1

T 12 YEI 6 YE

ALL532175-01-1 FWD CARGO DOOR CUT OUT132 DI232

Y

DETAILED INSPECTION OF INTERNAL STRUCTURE AROUNDFORWARD CARGO DOOR CUTOUT, FROM FR 24 TO FR 29 ANDBETWEEN STRINGER 23 AND STRINGER 38, RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : CARGO FLOOR PANELS REMOVED * TBDFWD ACT(S) REMOVED (IF INSTALLED)LINING AND INSULATION REMOVEDNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 532100/6AMT 532100-200-013MRB 532180-01-4

T 6 YEI 6 YE

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

53855392

5418

5427

532180-01-4 FUSELAGE FR 24-35.8133 DI134137138

YR

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREBETWEEN INCLUDING FORWARD FACE OF PRESSURE BULKHEAD, FROM STRINGER 38 LH/RHTO BOTTOM CENTERLINENOTE 1: INSPECTION BETWEEN FR 24 AND FR 35.8. TYPE 2 TPS MAY BE LIMITED TOFUSELAGE INTERNAL STRUCTURE FROM FR 35.7 TO FR 35.8, AND FORWARD FACE OFPRESSURE BULKHEAD, FROM STRINGER 38, LH/RH TO BOTTOM CENTERLINENOTE 2: CPCPTPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP. : CARGO FLOOR PANELS


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Threshold Interval

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5438

5456

54695495

5555

56995709

5916

59585994

Access panels :



AMM 532100/6AMT 532100-210-008MRB 532195-01-1

T 16 700 CYI 16 700 CY

ALL532195-01-1 FWD CARGO DOOR ACTUATOR132 GVI Y

GENERAL VISUAL INSPECTION OF FORWARD CARGO DOORACTUATOR ATTACH BRACKETS, BETWEEN CABIN FLOOR BEAMS,FROM FR 25 TO FR 27Access panels :

131AC 8250.09Total access time : Hrs



: : :

: :

1412/09/2013

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Threshold Interval

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AMM 532100/6AMT 532100-200-005MRB 532196-01-1

T 37 400 CYT 12 YEI 9 300 CYI 12 YE

ALL532196-01-1 FWD CARGO DOOR ECCENTRIC BOLTS132 DI Y

DETAILED INSPECTION OF FORWARD CARGO DOOR ECCENTRICBOLTS OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEENFR 25 AND FR 27ATPS : TPS MUST NOT BE APPLIEDPREP. : ECCENTRIC BOLTS REMOVEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :



AMT 533100-210-002MRB 533101-01-3

T 60 000 FHT 30 000 CYI 37 600 FHI 18 800 CY

ALL533101-01-3 AFT PRESSURE BULKHEAD FWD FACE147 DI148

N

DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46,FORWARD FACE.NOTE 1: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533101-01-1.NOTE 2: SAMPING 20%Access panels :




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Threshold Interval

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AMT 533100-210-008MRB 533103-01-5


ALL533103-01-5 AFT PRESSURE BULKHEAD AFT FACE151 DI152

N

DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46,AFT FACE, INCLUDING VERTICAL BEAMS, ABOVE CARGO FLOORLEVEL.NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533103-01-1.PREPARATION:ACT(S) REMOVED (IF INSTALLED);INSULATION REMOVED;NOTE 1: 100% THRESHOLD = 12 YEARSNOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

151AW 151BW 152BW0.00Total access time : Hrs


AMM 533100/6AMT 533100-210-004MRB 533107-01-1

T 48 000 CYI 20 000 CY

ALL533107-01-1 MLG BAY SIDE PANELS OUTBOARD FACE147 DI148

Y

DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELS,OUTBOARD FACE, BETWEEN FR 42 AND FR 47, FROM STRINGER26 TO STRINGER 36, LH/RHNOTE : SAMPLING 20%Access panels :

191ET 192ET 193AT 194AT 734 7440.24Total access time : Hrs



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1412/09/2013

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Threshold Interval

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AMT 533100-220-003MRB 533110-01-2NTM 53-31-00

T 60 000 FHT 33 500 CYI 33 000 FHI 12 000 CY

ALL533110-01-2 LONGITUDINAL FLOOR BEAMS145 SDI146

N

SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF UPPERFLANGE OF LONGITUDINAL FLOOR BEAMS AT FR 42 AND FR46, AS FAR AS VISIBLEPREPARATION: CABIN FLOOR PANELS REMOVED;NOTE 1: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533110-01-1.NOTE 2: SAMPLING 20%


AMM 533100/6AMT 533100-210-018MRB 533121-01-2

T 30 000 CYI 20 000 CY

ALL533121-01-2 CIRCUMFERENTIAL SPLICE AT FR 35 & 35.8200 DI Y

DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICEAND STRINGER COUPLING AREA AT FR 35 AND FR35.8 FROMSTRINGER 10, LH/RH TO CROWN CENTERLINE, EXTERNALSURFACENOTE : SAMPLING 20%


AMT 533100-210-038MRB 533133-01-6

T 30 000 CYI 5 000 CY

ALL533133-01-6 CENTER FUSELAGE200 GVI N

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRINGNOTE: INSPECT FROM FR 35.8 TO FR 47.



: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 533100/6AMT 533100-210-031MRB 533135-01-1

T 12 YEI 12 YE

ALL533135-01-1 FUSELAGE FR 36-46145 GVI146

Y

GENERAL VISUAL INSPECTION OF FUSELAGE INTERNALSTRUCTURE BELOW CABIN FLOOR PANELS, INCLUDING CABINFLOOR STRUCTURE BETWEEN FR 36 AND FR 46NOTE 1: CAN BE PERFORMED AT SAME TIME AS TASK 571157-01-1TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : CABIN FLOOR PANELS INSULATION REMOVEDNOTE 2: CPCP


AMM 533100/6AMT 533100-210-023MRB 533136-01-1

T 6 YEI 6 YE

ALL533136-01-1 MAIN LANDING GEAR BAY147 GVI148

Y

GENERAL VISUAL INSPECTION OF MLG BAY, INCLUDING MLGDOOR HINGESTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

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Threshold Interval

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AMM 533100/6AMT 533100-210-007MRB 533151-01-2

T 48 000 CYT 6 YEI 10 000 CYI 6 YE

ALL533151-01-2 KEELBEAM BOXNT DI Y

DETAILED INSPECTION OF KEELBEAM BOXNOTE 1: INSPECTION BETWEEN FR 35.8 AND FR 47.NOTE 2: CPCPNOTE 3: WORKING ZONES: 147, 148, 191, 192, 195, 196TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3Access panels :

147AB 147BB 147EB 147FB 148DB 148FB 191BB191GB 191HB 191JB 191KB 192KB 195AB 196AB734 744



AMM 533100/6AMT 533100-210-032MRB 533153-02-2

T 6 YEI 6 YE

ALL533153-02-2 PRESSURE BULKHEAD AT FR 35.8 AFT FACE191 GVI192

Y

GENERAL VISUAL INSPECTION OF PRESSURE BULKHEAD AFTFACE AND LOWER SKIN OF RESSURE DECK LOWER SURFACENOTE 1: INSPECTION AT FR 35.8 AND LOWER SKIN OFPRESSURE DECK LOWER SURFACE, BETWEEN FR 35.8 AND FR36.NOTE 2: CPCPTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3Access panels :

191BB 191EB 192EB 192FB0.25Total access time : Hrs



: : :

: :

1412/09/2013

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Threshold Interval

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AMM 533100/6AMT 533100-210-014MRB 533154-01-1

T 6 YEI 6 YE

ALL533154-01-1 MLG DOORS FITTINGS147 DI148

Y

DETAILED INSPECTION OF HINGE AND ACTUATOR FITTINGSFOR MLG DOORS AT KEELBEAMTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :



AMT 533100-220-001EAD 2012-0118FAD 2009-20-05ISB 53-1195

NTCheck : ALL533154-03-1 MLG DOORS FITTINGS147 SDI148

N

SPECIAL DETAILED INSPECTION (US AND HFEC) OFACTUATOR FITTINGS FOR MLG DOORS AT KEEL BEAM LH/RH(FOR TWIN WHEEL A/C OR FOR BOGIE A/C)PREPARATION: ACTUATOR REMOVEDNOTE 1: FOR THRESHOLD AND INTERVAL, REFER TO AD 2012-0118.


AMT 533100-220-001EAD 2012-0118FAD 2009-20-05ISB 53-1196

NTCheck : ALL533154-04-1 MLG DOORS FITTINGS147 SDI148

N

SPECIAL DETAILED INSPECTION (HFEC) OF THE KEEL BEAM MLG DOOR FWD HINGEFITTING (FOR TWIN WHEEL A/C), OR OF THE KEEL BEAM MLG DOORCENTER-HINGE-FITTING (FOR BOGIE A/C), LH/RHNOTE: -FOR THRESHOLD AND INTERVAL, REFER TO AD 2012-0118.



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: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-016MRB 534103-01-2

T 44 300 CYI 20 000 CY

ALL534103-01-2 WINDOW FORGINGS FR 47-64200 DI Y

DETAILED INSPECTION OF VISIBLE PART OF WINDOWFORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA,BETWEEN FR 47 AND FR 64, LH/RH, EXTERNAL SURFACENOTE : SAMPLING 20%


AMM 534100/6AMT 534100-210-011MRB 534106-01-2

T 48 000 CYI 12 000 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

4315

534106-01-2 FRAME SPLICES FR 53-56252 DI Y

DETAILED INSPECTION OF FRAME SPLICES AND ADJACENTAREA LOCATED ABOVE STRINGER 18 RHNOTE 1: INSPECT AREA FROM FR 53 TO FR 56.THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK534106-02-2.NOTE 2: SAMPLING 20%PREP. : INSULATION REMOVED

Access panels :

252HW 252LW 252PW0.06Total access time : Hrs


: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-220-004MRB 534106-02-1NTM 53-41-06

T 48 000 CYI 20 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

534106-02-1 FRAME SPLICES FR 53-56252 SDI YR

SPECIAL DETAILED INSPECTION (US) OF FRAME SPLICES ANDADJACENT AREA FROMLOCATED ABOVE STRINGER 18NOTE: INSPECT AREA FROM FR 53 TO FR 56. THIS TASK IS AN ALTERNATIVEINSPECTION TO TASK 534106-01-5NOTE 2: SAMPLING 20%


: : :

: :

1412/09/2013

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Threshold Interval

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Access panels :



AMM 534100/6AMT 534100-220-004MRB 534106-02-2NTM 53-41-06

T 48 000 CYI 19 000 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

534106-02-2 FRAME SPLICES FR 53-56252 SDI Y

SPECIAL DETAILED INSPECTION (US) OF FRAME SPLICES ANDADJACENT AREA LOCATED ABOVE STRINGER 18NOTE 1: INSPECT AREA FROM FR 53 TO FR 56.THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK534106-01-2.NOTE 2: SAMPLING 20%PREP. : INSULATION REMOVED

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

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ALI 534107-01-1AMM 534100/6AMT 534100-210-014MRB 534107-01-1

T 6 YEI 6 YE

ALL534107-01-1 FUSELAGE INTERNAL STRUCTURE FR 46-65153 DI154

Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,BETWEEN FR 46 AND FR 65, INCLUDING AFT FACE OFPRESSURE BULKHEAD FROM STRINGER 38, LH/RH TO BOTTOMCENTER LINE.NOTE 1: CREDIT IS TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534107-01-4.NOTE 2: CPCPPREP.: CARGO FLOOR PANELS REMOVED; ACT(S) REMOVED (IF INSTALLED);Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-036MRB 534109-01-1

T 48 000 CYI 20 000 CY

ALL534109-01-1 UPPER SEGMENT OF FR 70263 DI264

Y

DETAILED INSPECTION OF UPPER SEGMENT OF FR 70, FIN TOFUSELAGE FORWARD ATTACHMENT FITTINGS AND AREA BETWEENFR 69 AND FR 70, FROM STRINGER 6, LH/RH TO CROWNCENTER LINE, INTERNAL STRUCTUREPREP.: GALLEYS INSULATION REMOVED TOILET REMOVAL/INSTALLATIONNOTE : SAMPLING 20%Access panels :



ALI 534110-01-1AMM 534100/6AMT 534100-210-018MRB 534110-01-1

T 48 000 CYI 20 000 CY

ALL534110-01-1 CIRCUMFERENTIAL SKIN SPLICE AT FR 70200 DI323

Y

DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICEAT FR 70, BETWEEN STRINGER 10, LH/RH AND CROWN CENTERLINE, INCLUDING CUTOUT CORNERS FOR FIN ATTACHMENTS,EXTERNAL SURFACENOTE : SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMT 534100-210-823T 30 000 CYI 3 000 CY

ALL534118-01-4 REAR FUSELAGE200 GVI N

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTERLINENOTE 1: INSPECTION FROM FR 47 TO FR 70.NOTE 2: THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT 2A CHECK

AMT 534100-220-802NTM 53-41-23

T 60 000 FHT 34 200 CYI 19 600 FHI 9 800 CY


N

SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGEINTERNAL STRUCTURE, FRAME 66 AND FRAME 68 INNER CAPJOINT TO GUSSETS PLATE FROM STRINGER 10 TO STRINGER16, LH/RHPREP.: BOLTS REMOVED; INSULATION REMOVED; LINING REMOVED;NOTE: SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-806MRB 534128-01-3

T 60 000 FHT 48 000 CYI 58 200 FHI 29 100 CY

22552261

2267

23032974

534128-01-3 FUSELAGE SKIN BETWEEN FR 64 AND 70200 DI Y

DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACEBETWEEN FRAME 64 AND FRAME 70 FROM STRINGER 6 TOCROWN CENTER LINE, LH/RHNOTE 1: CREDIT IS TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534128-01-4NOTE 2: SAMPLING 20%Access panels :



AMT 534100-210-021MRB 534133-01-6

T 60 000 FHT 48 000 CYI 47 600 FHI 23 800 CY

ALL534133-01-6 AFT PAX/CREW DOOR CUTOUT LWR CORNER832 DI842

N

DETAILED INSPECTION OF AFT PASSENGER/CREW DOORCUTOUT, LOWER CORNERS, INCLUDING SKIN AND DOUBLERUNDERNEATH THE SCUFF PLATE, LH/RHPREPARATION: CORNER SCUFF PLATES REMOVED;NOTE: SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 534100-220-008NTM 53-41-33

T 60 000 FHT 48 000 CYI 60 000 FHI 38 600 CY


N

SPECIAL DETAILED INSPECTION (HFEC & X-RAY) OF AFTPASSENGER/CREW DOOR CUTOUT, LOWER CORNERS, INCLUDINGSKIN AND DOUBLER UNDERNEATH THE SCUFF PLATE, LH/RHNOTE: SPECIAL DETAILED INSPECTION IS FOR DOUBLERWHICH IS NOT VISIBLE WITH DETAILED INSPECTION.PREP.: LINING AND INSULATION REMOVED; CORNER SCUFF PLATES REMOVED;Access panels :


AMM 534100/6AMT 534100-210-029MRB 534134-01-1

T 12 YEI 12 YE

ALL534134-01-1 DOOR STOP FITTINGS FR 66 AND 68261 DI262

Y

DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 66AND FR 68, LH/RHPREP.: LINING REMOVEDNOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-003MRB 534135-01-4

T 6 YEI 6 YE

ALL534135-01-4 AFT PAX/CREW DOOR CUTOUT261 DI262263264

Y

DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFTPASSENGER/CREW DOOR CUTOUT, ABOVE CABIN FLOOR LEVEL,BETWEEN FR 65 AND FR 69 AND FROM STRINGER 6 TOSTRINGER 23, LH/RH, EXCLUDING THE LOWER CORNERS OFTHE DOOR ENTRANCE AREA AT FR 66 AND FR 68, BETWEENSTRINGER 22 AND 23, LH/RHNOTE 1: EXCLUDED AREA COVERED BY TASKS 534143-01-1 OR534143-01-3.NOTE 2: CPCPTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: LINING AND INSULATION REMOVEDAccess panels :



AMM 534100/6AMT 534100-210-041MRB 534136-01-1

T 12 YEI 12 YE

ALL534136-01-1 AFT PAX/CREW DOOR UNDER SCUFF-PLATE100 DI Y

DETAILED INSPECTION OF AFT PASSENGER/CREW DOORCUTOUT, UNDERNEATH THE SCUFF PLATE, LH/RHPREP.: SCUFF PLATENOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMT 534100-220-009NTM 53-41-37

T 60 000 FHT 30 300 CYI 50 200 FHI 25 100 CY


SPECIAL DETAILED INSPECTION (LFEC) OF INTERNALDOUBLER, FORWARD AND AFT OF WASTE SERVICE PANELCUTOUT, BETWEEN STRINGER 35 AND STRINGER 39, RHNOTE: SAMPLING 20%


AMT 534100-220-007NTM 53-41-39

T 60 000 FHT 48 000 CYI 45 600 FHI 22 800 CY


SPECIAL DETAILED INSPECTION (LFEC) OF INTERNALDOUBLER, FORWARD AND AFT OF WATER SERVICE PANELCUTOUT, BETWEEN STRINGER 38 AND STRINGER 42, LH.NOTE 1 : CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENOF TASK 534139-01-1NOTE 2 : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-834MRB 534143-01-1

T 5 YEI 5 YE

22552261

2267

23032480

534143-01-1 FUSELAGE INTERNAL STRUCTURE FR 66-68261 DI262

Y

DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR CUTOUTLOWER CORNERS INTERNAL STRUCTURE, ABOVE CABIN FLOORLEVEL, AT FR 66 AND FR 68 FROM STRINGER 22 TOSTRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RHNOTE 1:CREDIT CAN BE TAKEN FORM PREVIOUS ACCOMPLISHMENT OF TASK 534135-01-4 IN CASE THIS INSPECTION WAS PERFORMED PRIOR JUNE 2004.TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP.:BLANKING PLATE REMOVED; GIRT BAR FITTING REMOVED LINING AND INSULATION REMOVEDNOTE 2: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMT 534100-210-834MRB 534143-01-3

T 6 YEI 6 YE

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715251

5275

5306

534143-01-3 FUSELAGE INTERNAL STRUCTURE FR 66-68261 DI262

YR

DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR CUTOUTLOWER CORNERS INTERNAL STRUCTURE, ABOVE CABIN FLOORLEVEL, AT FR 66 AND FR 68 FROM STRINGER 22 TOSTRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RHNOTE: CREDIT CAN BE GTAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASKS534135-01-4 OR 534143- 01-1.TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: BLANKING PLATE REMOVED; GIRT BAR FITTING REMOVED LINING AND INSULATION REMOVED;NOTE: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5340

5385

53925418

5438

54565495

5555

56995916

5958

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-030MRB 534144-01-1

T 6 YEI 6 YE

ALL534144-01-1 FUSELAGE INTERNAL STRUCTURE FR 65-70171 DI172

Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,BELOW CABIN FLOOR PANELS INCLUDING FLOOR STRUCTURE,FROM FR 65 TO FR 70TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: INSULATION REMOVEDNOTE: CPCPAccess panels :

161DW 162DW 8260.06Total access time : Hrs


AMM 534100/6AMT 534100-210-801MRB 534146-01-1

T 12 YEI 12 YE

ALL534146-01-1 FLOOR STRUCTURE FR 47-70251 GVI252261262

Y

GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,EXCLUDING AREAS BELOW GALLEYS AND TOILETS AND DOORENTRANCE AREA, FROM FR 47 TO FR 70TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: CABIN FLOOR PANELSNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-037MRB 534147-01-1

T 6 YEI 6 YE

ALL534147-01-1 FLOOR STRUCTURE FR 47 TO 70251 DI252261262

Y

DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOWAND 0.5M AROUND GALLEYS AND TOILETS, FROM FR 47 TOFR 70, EXCEPT AREA BETWEEN FR 66 AND FR 68 ANDLATERAL SHEAR PLATES BETWEEN FR 68 AND FR 70.NOTE: TASK ONLY APPLICABLE IF GALLEYS/TOILETSINSTALLEDPREP: CABIN FLOOR PANELS GALLEYS TOILET REMOVAL/INSTALLATIONNOTE: CPCPAccess panels :



AMM 534100/6AMT 534100-210-802MRB 534148-01-2

T 6 YEI 6 YE

ALL534148-01-2 FUSELAGE UNDER BELLY FAIRING190 GVI Y

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE, AND BELLY FAIRING SUPPORT STRUCTURE BETWEENFR 35.3 AND FR 48, UNDER THE BELLY FAIRINGTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : BELLY FAIRINGNOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-004MRB 534150-01-1

T 12 YEI 6 YE

ALL534150-01-1 AFT CARGO DOOR CUTOUT152 DI Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREAROUND AFT CARGO DOOR CUTOUTNOTE: INSPECTION FROM FR 52 TO FR 57 AND BETWEEN STRINGER 23 AND STRINGER38TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: ACT INSULATION REMOVEDAccess panels :

152DW 152EF 152FF 152HW 152MF 152NF0.34Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-005MRB 534152-01-3

T 12 YEI 12 YE

ALL534152-01-3 AFT CARGO DOOR HINGE FITTINGS INTERNAL252 DI Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE ATINTERNAL ATTACHMENT AREA OF AFT CARGO DOOR HINGEFITTINGS, FROM FR 52 TO FR 57, BETWEEN STRINGER 22AND STRINGER 23PREP. : REAR ACT REMOVED (IF INSTALLED) INSULATION REMOVEDNOTE 1: 100 % THRESOLD = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

252GW 252KW 252NW0.17Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-006MRB 534153-01-3

T 12 YEI 12 YE

ALL534153-01-3 AFT CARGO DOOR HINGE FITTINGS EXTERNAL152 DI Y

DETAILED INSPECTION OF FUSELAGE AFT CARGO DOOR HINGEFITTINGS AND EXTERNAL ATTACHMENT AREANOTE: APPLICATION OF TPS IS LIMITED TO THE INNER SIDEOF HINGE FITTINGSTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : ACTNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 534100/6AMT 534100-210-025MRB 534155-01-3

T 48 000 CYT 12 YEI 11 400 CYI 12 YE

ALL534155-01-3 AFT CARGO DOOR ECCENTRIC BOLTS154 DI Y

DETAILED INSPECTION OF AFT CARGO DOOR ECCENTRIC BOLTSOF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN FR 53AND FR 55 A (6 PLACES)PREP. : ECCENTRIC BOLTS REMOVEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-012MRB 534156-01-1

T 48 000 CYI 8 400 CY

ALL534156-01-1 AFT CARGO DOOR LOCK FITTING154 DI Y

DETAILED INSPECTION OF AFT CARGO DOOR LOCK FITTINGSAND SURROUNDING STRUCTURE, BETWEEN FR 53 AND FR 55 A,FROM STRINGER 41 RH TO DOOR SILL, INTERNAL PORTION (6PLACES)PREP. : REAR ACT CARGO FLOOR PANELSNOTE 1: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 534156-02-1NOTE 2: SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-220-011MRB 534156-02-1NTM 53-41-56

T 48 000 CYI 9 600 CY

ALL534156-02-1 AFT CARGO DOOR LOCK FITTINGS154 SDI Y

SPECIAL DETAILED INSPECTION (HFEC) OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR53 AND FR 55 A, FROM STRINGER 41 RH TO DOOR SILL,INTERNAL PORTION (6 PLACES)NOTE 1: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 534156-01-1PREP. : REAR ACT CARGO FLOOR PANELSNOTE 2: SAMPLING 20%Access panels :



AMM 534100/6AMT 534100-210-803MRB 534160-01-1

T 6 YEI 6 YE

ALL534160-01-3 AFT CARGO DOOR CUTOUT LATERAL FRAMES152 GVI Y

GENERAL VISUAL INSPECTION OF AFT CARGO DOOR CUTOUT,VISIBLE PART OF LATERAL FRAMES.NOTE: INSPECTION OF FR 52A AND FR 56Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-819MRB 534163-01-1

T 16 700 CYI 16 700 CY

ALL534163-01-1 AFT CARGO DOOR ACTUATOR ATTACH BRACKET152 GVI Y

GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATORATTACH BRACKET NOTE: INSPECTION BETWEEN FLOOR BEAMS AT FR 53, FR 54AND FR 55PREP. : ACTAccess panels :

151CC0.07Total access time : Hrs


AMM 534100/6AMT 534100-210-028MRB 534164-01-1

T 12 YEI 6 YE

ALL534164-01-1 BULK CARGO DOOR CUTOUT162 DI Y

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,AROUND BULK CARGO DOOR CUTOUT, FROM FR 59 TO FR 63AND BETWEEN STRINGER 23 AND STRINGER 38TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: INSULATION REMOVEDNOTE: CPCPAccess panels :

162BW 162EW0.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-805MRB 534167-02-1

T 6 YEI 6 YE

ALL534167-02-1 BULK CARGO DOOR STOP FITTING162 GVI Y

GENERAL VISUAL INSPECTION OF BULK CARGO DOOR STOPFITTINGS INCLUDING VISIBLE PART OF LATERAL FR 60 ANDFR 62.NOTE: TPS APPLICATION IS LIMITED TO THE VISIBLE PART OF THE LATERAL BULK CARGO DOOR FRAMES.TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP: INSULATION REMOVED;NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-007MRB 534169-01-1

T 12 YEI 12 YE

ALL534169-01-1 FUSELAGE SKIN UNDER SCUFF PLATE162 DI164

Y

DETAILED INSPECTION OF FUSELAGE SKIN UNDERNEATH BULKCARGO DOOR SCUFF PLATETPS : TPS MUST NOT BE APPLIEDPREP. : SCUFF PLATES REMOVEDNOTE 1: 100% LIMIT = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :



AMM 534100/6AMT 534100-210-044MRB 534176-01-1

T 40 000 CYI 11 600 CY

ALL534176-01-1 AFT EMERGENCY EXIT SKIN CUTOUTS100 DI200

Y

DETAILED INSPECTION OF AFT EMERGENCY EXIT SKINCUTOUTS, UPPER AND LOWER CORNERS, EXTERNAL SURFACE,LH/RHNOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-045MRB 534177-01-1

T 48 000 CYI 20 000 CY

ALL534177-01-1 AFT EMERGENCY EXIT ESCAPE CHUTE COMPT.100 DI Y

DETAILED INSPECTION OF AFT EMERGENCY EXIT ESCAPECHUTE COMPARTMENT SKIN CUTOUTS, UPPER AND LOWERCORNERS, EXTERNAL SURFACE, LH/RHNOTE : SAMPLING 20%


AMM 534100/6AMT 534100-210-049MRB 534187-01-1

T 6 YEI 6 YE

ALL534187-01-1 ESCAPE CHUTE SLIDE COMPARTMENT151 DI152

Y

DETAILED INSPECTION OF ESCAPE CHUTE SLIDE COMPARTMENTINTERNAL STRUCTURE, BETWEEN FR 47.2A AND FR 47.4 FROMSTRINGER 24 TO STRINGER 28, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: ESCAPE SLIDENOTE: CPCP


AMM 534100/6AMT 534100-210-048MRB 534190-01-1

T 12 YEI 12 YE

ALL534190-01-1 DOOR STOP FITTINGS ON FR 47.2A & 47.4251 DI252

Y

DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 47.2AAND FR 47.4, LH/RHNOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-046MRB 534191-01-1

T 48 000 CYI 9 500 CY

ALL534191-01-1 FUSELAGE SKIN AT WINDOW CUTOUT200 DI Y

DETAILED INSPECTION OF SKIN AT WINDOW CUTOUT BETWEENFR 47 AND FR 47.2, FROM STRINGER 14 TO STRINGER 18,EXTERNAL SURFACE, LH/RHNOTE : SAMPLING 20%


AMM 534100/6AMT 534100-210-047MRB 534192-01-1

T 48 000 CYT 12 YEI 20 000 CYI 6 YE

ALL534192-01-1 INTL STRUCT AROUND EMERG EXIT CUTOUTS251 DI252

Y

DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFTEMERGENCY EXIT CUTOUTS, ABOVE CABIN FLOOR LEVEL,BETWEEN FR 47.2 AND FR 47.5, AND FROM STRINGER 10 TOSTRINGER 23, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : LINING REMOVED INSULATION REMOVEDNOTE 1: 100% LIMIT = 12 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 534100/6AMT 534100-210-835MRB 534195-01-1

T 5 YEI 5 YE

22552261

2267

23032480

2974

30053013

3022

534195-01-1 CABIN FLOOR STRUCTURE AFT ENTRANCE AREA261 DI262

Y

DETAILED INSPECTION OF CABIN FLOOR STRUCTURE ANDSTRUCTURE BELOW AFT ENTRANCE AREA; BETWEEN FRAME 66AND FRAME 68 AND LATERAL SHEAR PLATES BETWEEN FRAME68 AND FRAME 70.NOTE: IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBSIS NOT POSSIBLE DUE TO GALLEY CONFIGURATION,THE GALLEY MUST BE REMOVED TO GET ACCESS TO THEINSPECTION AREA.PREP: CABIN ATTENDANT SEAT REMOVED; FLOOR PANELS FROM FR 66 TO FR 68; LATERAL GALLEY LINING REMOVED LOWER DOOR FRAME LINING REMOVEDNOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 534100-210-835MRB 534195-01-2

T 6 YEI 6 YE

31983315

3355

36003737

3862

39643966

4669

47034737

4783

48264863

4945

49715251

5275

53065340

5385

53925418

5438

54565495

5555

5699

534195-01-2 CABIN FLOOR STRUCTURE AFT ENTRANCE AREA261 DI262

YR

CABIN FLOOR STRUCTURE AFT ENTRANCE AREADETAILED INSPECTION OF CABIN FLOOR STRUCTURE ANDSTRUCTURE BELOW AFT ENTRANCE AREA; BETWEEN FRAME 66AND FRAME 68 AND LATERAL SHEAR PLATES BETWEEN FRAME68 AND FRAME 70.NOTE: IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBSIS NOT POSSIBLE DUE TO GALLEY CONFIGURATION,THE GALLEY MUST BE REMOVED TO GET ACCESS TO THEINSPECTION AREA.PREP: CABIN ATTENDANT SEAT REMOVED; FLOOR PANELS FROM FR 66 TO FR 68; LATERAL GALLEY LINING REMOVED; LOWER DOOR FRAME LINING REMOVED;NOTE :CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5916

5958

Access panels :



AMM 535100/6AMT 535100-210-001MRB 535101-01-1

T 6 YEI 6 YE

ALL535101-01-1 REAR PRESSURE BULKHEAD AFT FACE311 DI312

Y

DETAILED INSPECTION OF REAR PRESSURE BULKHEADCOMPLETE AFT FACE, AND FUSELAGE INTERNAL STRUCTURE,BETWEEN FR 70 AND FR 71, FROM STRINGER 26, LH/RH TOBOTTOM CENTER LINENOTE1 : TPS MAY BE LIMITED TO FUSELAGE INTERNAL STRUCTURE FROM FR 70 TO FR 71, AND AFT FACE OF PRESSURE BULKHEAD, FROM STRINGER 26, LH/RH TO BOTTOM CENTERLINETPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2PREP. : PROTECTIVE SHIELDNOTE 2: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 535100/6AMT 535100-210-014MRB 535105-01-3

T 48 000 CYI 13 800 CY

ALL535105-01-3 REAR PRESSURE BULKHEAD SPLICE311 DI312

Y

DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFTFACE, REINFORCEMENT SPLICE AT FORWARD FIN ATTACHMENTAREANOTE : SAMPLING 20%Access panels :



AMM 535100/6AMT 535100-210-003MRB 535107-01-2

T 60 000 FHT 30 000 CYI 27 000 FHI 9 000 CY

ALL535107-01-3 CIRCUMFERENTIAL JOINT AT FR70311 DI312

Y

DETAILED INSPECTION OF RING FRAME AT CIRCUMFERENTIALJOINT OF REAR PRESSURE BULKHEAD SKIN AT FR 70, AFTFACENOTE : SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 535100-210-004T 48 000 CYI 17 300 CY

ALL535113-01-5 FUSELAGE SKIN AT THS CUTOUT311 DI312

N

DETAILED INSPECTION OF FUSELAGE SKIN AT HORIZONTALSTABILIZER CUTOUT AT FORWARD, UPPER AND LOWERCORNERS, LH/RHNOTE 1 : CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 535113-01-1.NOTE 2 : CPCPNOTE 3 : 100% LIMIT THRESHOLD = 12YE, INTERVAL = 12YENOTE 4 : SAMPLING 20%Access panels :

333AB 333AT 343AB 343AT0.20Total access time : Hrs

AMM 535100/6AMT 535100-210-005MRB 535115-01-1

T 12 YEI 12 YE

ALL535115-01-1 FRAME 74 SPLICES311 DI312

Y

DETAILED INSPECTION OF FR 74, SPLICES AT STRINGER 12AND STRINGER 19, LH/RH, INTERNAL STRUCTURETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 535100-210-007T 48 000 CYI 18 000 CY

ALL535117-01-5 HORIZONTAL STABILIZER ATTACHMENT311 DI312

N

DETAILED INSPECTION OF HORIZONTAL STABILIZERATTACHMENT AND BACK UP STRUCTURE AT FR 77, FROMSTRINGER 8 TO STRINGER 21, LH/RHNOTE 1 : CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 535117-01-1.NOTE 2 : CPCPNOTE 3 : 100% LIMIT THRESHOLD = 12YE, INTERVAL = 12YENOTE 4 : SAMPLING 20%Access panels :


AMM 535100/6AMT 535100-210-002MRB 535121-01-1

T 6 YEI 6 YE

ALL535121-01-1 REAR PRESSURE BULKHEAD BLW CABIN FLOOR171 DI172

Y

DETAILED INSPECTION OF REAR PRESSURE BULKHEAD,FORWARD FACE, BELOW CABIN FLOOR LEVELTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :

162DW0.02Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 535100/6AMT 535100-210-008MRB 535123-01-1

T 12 YEI 12 YE

ALL535123-01-1 REAR PRESSURE BULKHEAD ABV CABIN FLOOR261 DI262

Y

DETAILED INSPECTION OF REAR PRESSURE BULKHEAD,FORWARD FACE, ABOVE CABIN FLOOR LEVELTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: GALLEYS INSULATION REMOVED TOILET REMOVAL/INSTALLATIONNOTE: CPCP


AMM 535100/6AMT 535100-210-018MRB 535126-01-1

T 12 YEI 12 YE

ALL535126-01-1 FUSELAGE AND VERT STAB ATTACH FITTINGS323 GVI Y

GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNALSURFACE AND VERTICAL STABILIZER ATTACHMENT FITTING,UNDERNEATH VERTICAL STABILIZER/FUSELAGE FAIRINGSTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP: FAIRINGSNOTE: CPCPACCESS : FAIRINGS REMOVED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 535100/6AMT 535100-210-009MRB 535151-01-1

T 12 YEI 12 YE

ALL535151-01-1 TAIL CONE ATTACH FITTINGS311 DI312313314

Y

DETAILED INSPECTION OF TAIL CONE ATTACHMENT FITTINGSAT FR 77 AND FR 78NOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 545100-200-001NTM 54-51-01

T 60 000 FHT 30 000 CYI 24 600 FHI 12 300 CY

ALL545101-01-5 PYLON FWD MOUNT FITTING415 SDI N

SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARDMOUNT FITTING AND SPIGOT FITTING.NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 545101-01-2PREP.: BOLTS REMOVED;NOTE: SAMPLING 20%Access panels :


AMM 545100/6AMT 545100-200-002NTM 54-51-02

T 60 000 FHT 30 000 CYI 45 400 FHI 22 700 CY

ALL545102-01-3 PYLON FWD MOUNT FITTING415 SDI425

Y

SSPECIAL DETAILED INSPECTION (US) OF PYLON FORWARDMOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,FORWARD AND AFT ATTACHMENT BOLT HOLES.NOTE: SAMPLING 20%Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-027MRB 545104-01-1

T 12 YEI 12 YE

ALL545104-01-1 PYLON LOWER SPAR UPPER SURFACE415 DI425

Y

DETAILED INSPECTION OF PYLON, LOWER SPAR, UPPERSURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASTASK 545104-02-1TPS : TPS MUST NOT BE APPLIEDNOTE: CPCPNOTE: SAMPLE 20%.NOTE: 100% LIMIT = 24YEAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-028MRB 545104-02-1NTM 54-51-04

T 12 YEI 12 YE

ALL545104-02-1 PYLON LOWER SPAR UPPER SURFACE415 SDI425

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,LOWER SPAR, UPPER SURFACE, BETWEEN RIB 1 AND RIB 2,AND RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.TPS : TPS MUST NOT BE APPLIEDNOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 545104-01-1NOTE 2: CPCPNOTE 3: SAMLE 20%NOTE 4: 100% LIMIT = 24YEAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-004MRB 545106-01-1

T 12 YEI 12 YE

ALL545106-01-1 PYLON LWR SPAR415 DI425

Y

DETAILED INSPECTION OF PYLON, LOWER SPAR, BETWEEN RIB1 AND RIB 10, LOWER SURFACETPS : TPS MUST NOT BE APPLIEDNOTE: CPCPNOTE: SAMLE 20%NOTE: 100% LIMIT = 24YEAccess panels :

437AL 438AR 447AL 448AR 451AL 452AR 461AL462AR 473AL 473AR 473BL 473CL 483AL 483AR483BL 483CL



AMT 545100-200-005T 60 000 FHT 30 000 CYT 12 YEI 30 200 FHI 15 100 CYI 12 YE

ALL545107-01-5 ENGINE AFT ATTACH BEAM415 DI425

N

DETAILED INSPECTION OF ENGINE AFT ATTACHMENT BEAM.NOTE 1 : CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 545107-01-1.NOTE 2 : CPCPNOTE 3 : 100% LIMIT = 24YENOTE 4 : SAMPLING 20%Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-006MRB 545114-01-3

T 60 000 FHT 30 000 CYI 28 400 FHI 14 200 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355

545114-01-3 PYLON/WING ATTACH FITTINGS LUGS RIB 4415 DI425

Y

DETAILED INSPECTION OF PYLON TO WING ATTACH FITTINGLUGS AT RIB 4NOTE : SAMPLING 20%

Access panels :

414FR 423FL 471AL 472AR 481AL 482AR0.24Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-006MRB 545114-01-6

T 60 000 FHT 30 000 CYI 28 400 FHI 14 200 CY

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385


YR



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-008MRB 545115-01-3

T 60 000 FHT 30 000 CYI 11 600 FHI 5 800 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355

545115-01-3 PYLON/WING RIB 4415 DI425

Y

DETAILED INSPECTION OF PYLON TO WING FORWARDATTACHMENT SHACKLES AT RIB 4NOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-3NOTE 2: SAMPLING 20%

Access panels :

414FR 423FL 471AL 472AR 481AL 482AR 521BT621BT




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-008MRB 545115-01-6

T 60 000 FHT 30 000 CYI 11 600 FHI 5 800 CY

36003737

3862

39643966

4136

42134277

4311

4315

545115-01-6 PYLON/WING RIB 4415 DI425

Y

DETAILED INSPECTION OF PYLON TO WING FORWARDATTACHMENT SHACKLES AT RIB 4NOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-6NOTE 2: SAMPLING 20%

Access panels :

471AL 471AR 471BL 471BR 481AL 481AR 481BL481BR 521BT 621BT




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-007MRB 545115-02-3NTM 54-51-15

T 60 000 FHT 30 000 CYI 22 000 FHI 11 000 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355

545115-02-3 PYLON/WING RIB 4415 SDI425

Y

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WINGFORWARD ATTACHMENT SHACKLES AT RIB 4.NOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 545115-01-3NOTE 2: SAMPLING 20%

Access panels :

414FR 423FL 471AL 472AR 481AL 482AR 521BT621BT




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-007MRB 545115-02-6NTM 54-51-15

T 60 000 FHT 30 000 CYI 22 000 FHI 11 000 CY

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385

545115-02-6 PYLON/WING RIB 4415 SDI425

YR

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WINGFORWARD ATTACHMENT SHACKLES AT RIB 4.NOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 545115-01-6NOTE 2: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :

471AL 471AR 471BL 471BR 481AL 481AR 481BL481BR 521BT 621BT




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-009MRB 545116-01-1

T 12 YEI 12 YE

ALL545116-01-1 PYLON/WING ATTACH FITTING RIB4415 DI425

Y

DETAILED INSPECTION OF SHACKLES, SLEEVES AND BOLTS OFPYLON TO WING ATTACHMENT FITTINGS AT RIB 4TPS : TPS MUST NOT BE APPLIEDPREP. : BOLTS REMOVED SHACKLES SLEEVES ENGINE REMOVEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMM 545100/6AMT 545100-200-010MRB 545117-01-1

T 12 YEI 12 YE

22552261

2267

23032480

545117-01-1 PYLON SPIGOT415 DI425

Y

DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPERSURFACE, INCLUDING FITTING BORE, AND UPPER SPARSURROUNDING SURFACETPS : TPS MUST NOT BE APPLIEDPREP: BALL JOINTNOTE: CPCPAccess panels :

415BL 415BR 425BL 425BR 471AL 471BL 472AR472BR 481AL 481BL 482AR 482BR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 545100-200-010MRB 545117-01-2

T 12 YEI 12 YE

29743005

3013

30223198

3315

3355

545117-01-2 PYLON SPIGOT415 DI425

Y

DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPERSURFACE, INCLUDING FITTING BORE, AND UPPER SPARSURROUNDING SURFACETPS : TPS MUST NOT BE APPLIEDPREP: BALL JOINTNOTE: CPCPNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%Access panels :

415BL 415BR 425BL 425BR 471AL 471BL 472AR472BR 481AL 481BL 482AR 482BR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 545100-200-010MRB 545117-01-4

T 12 YEI 12 YE

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385

545117-01-4 PYLON SPIGOT415 DI425

YR

DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPERSURFACE, INCLUDING FITTING BORE, AND UPPER SPARSURROUNDING SURFACETPS : TPS MUST NOT BE APPLIEDPREP: BALL JOINTNOTE: CPCPNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :

415BL 415BR 425BL 425BR 471BL 471BR 471CL471CR 481BL 481BR 481CL 481CR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-011MRB 545120-01-1

T 60 000 FHT 30 000 CYI 22 000 FHI 11 000 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355


Y


Access panels :

471CL 472BR 475BL 476BR 481BL 482CR 485BL486BR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-011MRB 545120-01-4

T 60 000 FHT 30 000 CYI 22 000 FHI 11 000 CY

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645251

5275

53065340

5385

53925418

5438

5456


YR



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5469

5495

55555699

5709

59165958

5994

Access panels :

471CR 471DL 475BL 475BR 481CL 481CR 485BL485BR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-220-001MRB 545123-01-1NTM 54-51-23

T 60 000 FHT 30 000 CYI 19 600 FHI 9 800 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355

545123-01-1 PYLON/WING AFT ATTACHMENT SHACKLES AT415 SDI425

Y

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING AFTATTACHMENT SHACKLES AT RIB 10.NOTE : SAMPLING 20%

Access panels :

471CL 472BR 475AL 475BL 476AR 476BR 481BL482CR 485AL 485BL 486AR 486BR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-220-001MRB 545123-01-5NTM 54-51-23

T 60 000 FHT 30 000 CYI 19 600 FHI 9 800 CY

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385

545123-01-5 PYLON/WING AFT ATTACHMENT SHACKLES AT415 SDI425

YR

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING AFTATTACHMENT SHACKLES AT RIB 10.NOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :

471CR 471DL 475AL 475AR 475BL 475BR 481CL481DR 485AL 485AR 485BL 485BR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-014MRB 545124-01-1

T 12 YEI 12 YE

ALL545124-01-1 PYLON/WING AFT ATTACH FITTING SLEEVES415 DI425

Y

DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENTFITTING, SLEEVES AND BOLTSTPS : TPS MUST NOT BE APPLIEDPREP. : BOLTS REMOVED SHACKLES SLEEVES ENGINE REMOVEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMM 545100/6AMT 545100-200-015MRB 545126-01-2

T 60 000 FHT 30 000 CYI 19 000 FHI 9 500 CY

ALL545126-01-2 PYLON LATERAL PANELS FASTENERS AREAS410 DI420

Y

DETAILED INSPECTION OF PYLON, LATERAL PANELS, IN THEAREAS OF FASTENERS SECURING THE SUPPORTS OF ACCESSDOORS, BETWEEN RIB 5 AND RIB 6, LH/RHNOTE : SAMPLING 20%


AMM 545100/6AMT 545100-200-017MRB 545131-01-2

T 60 000 FHT 30 000 CYI 19 400 FHI 9 700 CY

ALL545131-01-2 PYLON LATERAL PANELS CUTOUT CORNERS410 DI420

Y

DETAILED INSPECTION OF PYLON, LATERAL PANEL, IN AREASOF FASTENERS AT DOOR CUTOUT CORNERS, BETWEEN RIB 2AND RIB 3, EXTERNAL SURFACE, LH/RHNOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-018MRB 545133-01-1

T 60 000 FHT 30 000 CYI 26 200 FHI 13 100 CY

ALL545133-01-1 PYLON LWR SPAR RIB 1 AND 4415 DI425

Y

DETAILED INSPECTION OF PYLON, LOWER SPAR, IN AREAS OFFASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB1 AND RIB 4, LH/RHNOTE : SAMPLING 20%Access panels :



AMT 545100-200-019MRB 545134-01-6

T 60 000 FHT 30 000 CYI 19 800 FHI 9 900 CY

ALL545134-01-6 PYLON UPR SPAR RIB 4 AND 10415 DI425

N

DETAILED INSPECTION OF PYLON, UPPER SPAR, IN AREAS OFFASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB4 AND RIB 10, LH/RHNOTE: SAMPLE 20%Access panels :

471BL 471BR 471CL 471CR 471DL 481BL 481BR481CL 481CR 481DR


Skills :ENG1 1.00 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-021MRB 545156-01-1

T 10 YEI 10 YE

22552261

2267

23032480

545156-01-1 PYLON UPPER SPARS UPPER SURFACE415 DI425

Y

DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPERSURFACE, FROM FORWARD OF RIB 1 TO RIB 10TPS : TPS MUST NOT BE APPLIEDPREP: PRE-COOLERNOTE: CPCPAccess panels :

413CL 413DL 413EL 414CR 414FR 423CL 423DL423FL 424CR 424ER 471AL 471BL 471CL 472AR472BR 481AL 481BL 482AR 482BR 482CR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-021MRB 545156-01-3

T 12 YEI 12 YE

29743005

3013

30223198

3315

3355


Y

DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPERSURFACE, FROM FORWARD OF RIB 1 TO RIB 10TPS : TPS MUST NOT BE APPLIEDPREP: PRE-COOLERNOTE: CPCP

Access panels :

413CL 413DL 413EL 414CR 414FR 423CL 423DL423FL 424CR 424ER 471AL 471BL 471CL 472AR472BR 481AL 481BL 482AR 482BR 482CR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-021MRB 545156-01-6

T 12 YEI 12 YE

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385


YR

DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPERSURFACE, FROM FORWARD OF RIB 1 TO RIB 10TPS : TPS MUST NOT BE APPLIEDPREP: PRE-COOLERNOTE: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :

413CL 413CR 413DT 423CL 423CR 423DT 471AL471AR 471BL 471BR 471CL 471CR 471DL 481AL481AR 481BL 481BR 481CL 481CR 481DR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-022MRB 545161-01-1

T 10 YEI 10 YE

22552261

2267

23032480

545161-01-1 PYLON UPPER SPAR LOWER SURFACE415 DI425

Y

DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWERSURFACE, FORWARD OF RIB 1TPS : TPS MUST NOT BE APPLIEDNOTE: CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-022MRB 545161-01-2

T 12 YEI 12 YE

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715164

5241

5247


YR

DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWERSURFACE, FORWARD OF RIB 1TPS : TPS MUST NOT BE APPLIEDNOTE: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

55555699

5709

59165958

5994

Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-023MRB 545162-01-1

T 10 YEI 10 YE

22552261

2267

23032480


Y

DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWERSURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8NOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 545162-02-1TPS : TPS MUST NOT BE APPLIEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 545100-200-023MRB 545162-01-2

T 12 YEI 12 YE

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715164

5241

5247


YR

DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWERSURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8NOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 545162-02-2TPS : TPS MUST NOT BE APPLIEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

55555699

5709

59165958

5994

Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-024MRB 545162-02-1NTM 54-51-62

T 10 YEI 10 YE

22552261

2267

23032480

545162-02-1 PYLON UPPER SPAR LOWER SURFACE415 SDI425

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,UPPER SPAR, LOWER SURFACE, BETWEEN RIB 1 AND RIB 2,RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.NOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 545162-01-1TPS : TPS MUST NOT BE APPLIEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 545100-200-024MRB 545162-02-2NTM 54-51-62

T 12 YEI 12 YE

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715164

5241

5247

545162-02-2 PYLON UPPER SPAR LOWER SURFACE415 SDI425

YR

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,UPPER SPAR, LOWER SURFACE, BETWEEN RIB 1 AND RIB 2,RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.NOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 545162-01-2TPS : TPS MUST NOT BE APPLIEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

55555699

5709

59165958

5994

Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 545100/6AMT 545100-200-025MRB 545170-01-1

T 12 YEI 12 YE

ALL545170-01-1 PYLON PYRAMID MATING FACE415 DI425

Y

DETAILED INSPECTION OF PYLON, PYRAMID MATING FACEWITH THE ENGINE FORWARD MOUNT FITTINGTPS : TPS MUST NOT BE APPLIEDPREP. : ENGINE REMOVEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMM 545100/6AMT 545100-200-026MRB 545171-01-1

T 12 YEI 12 YE

ALL545171-01-1 PYLON ENGINE AFT ATTACHMENT BEAM415 DI425

Y

DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENTBEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTINGTPS : TPS MUST NOT BE APPLIEDPREP. : ENGINE REMOVEDNOTE 1: 100% LIMIT = 20 YENOTE 2: SAMPLING 20%NOTE 3: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 545400-220-002ISB 54-1022

T 6 YEI 6 YE

22552261

2267

23032480

2974

30053013

3022

31983315

3355

545172-01-1 PYLON FWD CORNER FITTINGS475 DI476485486

Y

DETAILED INSPECTION OF AFT PYLON SECONDARYTTACHMENTSTRUCTURE, FORWARD CORNER FITTINGSFT MOUNT FITTINGNOTE: FOR OVERDUED AIRCRAFT, PERFORM THIS TASK IN NEXT C CHECK

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2012-0100ISB 54A1026

I 3 000 FHI 2 250 CY

36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385

545500-01-1 PYLON AFT MOVABLE FAIRING470 DI480

NR

DETAILED INSPECTION OF AFT PYLON MOVEABLE FAIRING,LH/RHNOTE 1: THRESHOLD IN ACCORDANCE WITH EASA AD 2012-0100.NOTE 2: RII TASK


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 551634/6AMT 551634-200-001MRB 551001-01-1

T 6 YEI 6 YE

ALL551001-01-1 THS JACK FITTING333 DI343

Y

DETAILED INSPECTION OF HORIZONTAL STABILIZER, JACKFITTING AND SURROUNDING EXTERNAL STRUCTUREAccess panels :



AMM 551600/6AMT 551600-200-002MRB 551002-01-1

T 32 000 CYI 24 000 CY

ALL551002-01-1 THS UPR JOINT FITTING REAR AREA333 DI343

Y

DETAILED INSPECTION OF HORIZONTAL STABILIZER, UPPERAND LOWER JOINT FITTINGS, EXTERNAL SURFACES, 5REARMOST ROWS OF FASTENERSNOTE : SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 551600/6AMT 551600-200-001MRB 551010-01-1

T 6 YEI 6 YE

ALL551010-01-1 THS HINGE AND ATTACH FITTINGS333 DI343

Y

DETAILED INSPECTION OF HORIZONTAL STABILIZER, REARSUPPORT FITTINGS, UPPER AND LOWER ATTACH FITTINGS ANDSURROUNDING EXTERNAL STRUCTURE, LH/RHAccess panels :



AMM 551000/6AMT 551000-210-001MRB 551012-01-1

T 12 YEI 12 YE

ALL551012-01-1 THS SPARBOX INTERNAL STRUCTURE333 DI343

Y

DETAILED INSPECTION OF HORIZONTAL STABILIZER,INTERNAL STRUCTURE OF TORQUE BOX, IINBOARD OFFUSELAGE FAIRINGSPREPARATION: PEELABLE HOLE COVERS REMOVED;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 551000/6AMT 551000-210-002MRB 551019-01-1

T 12 YEI 12 YE

ALL551019-01-1 THS TORQUE BOX INTERNAL STRUCTURE333 DI343

Y

DETAILED INSPECTION OF HORIZONTAL STABILIZER,INTERNAL STRUCTURE OF TORQUE BOX, OUTBOARD OFFUSELAGE FAIRINGS, LH/RH PREPARATION : PEELABLE HOLE COVERS REMOVEDAccess panels :

331AB 331BB 331CB 332AB 334AB 334AT 334BB334BT 334CB 334CT 334DB 334DT 334EB 334FB334GB 334HB 341AB 341BB 341CB 342AB 344AB344AT 344BB 344BT 344CB 344CT 344DB 344DT344EB 344FB 344GB 344HB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 551600/6AMT 551600-200-004MRB 551020-01-1

T 6 YEI 6 YE

ALL551020-01-1 ELEVATOR HINGE SUPPORTS AND FITTINGS334 DI344

Y

DETAILED INSPECTION OF HORIZONTAL STABILIZER, HINGEFITTINGS AND SUPPORT RIBS AND ACTUATOR FITTINGS FORTHE ELEVATOR, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :

334AT 334BB 334BT 334CT 334DB 334DT 334FB334HB 344AT 344BB 344BT 344CT 344DB 344DT344FB 344HB



AMM 552000/6AMT 552000-200-003MRB 552002-01-1

T 6 YEI 6 YE

ALL552002-01-1 ELEVATOR HINGE SUPPORT AND ACT. FTG.335 DI345

Y

DETAILED INSPECTION OF ELEVATOR, HINGE FITTINGS ANDACTUATOR FITTINGS, LH/RHTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :

334BB 334DB 334FB 334HB 335AB 335BB 335CB335DB 344BB 344DB 344FB 344HB 345AB 345BB345CB 345DB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 552000/6AMT 552000-200-001MRB 552004-01-1NTM 51-10-03NTM 55-20-04

T 6 YEI 6 YE

ALL552004-01-1 ELEVATOR SKIN PANELS300 SDI Y

SPECIAL DETAILED (TAP TEST) INSPECTION OF ELEVATOR,TOP AND BOTTOM SKIN PANELS IN AREA OF HINGE SUPPORTS2, 3 AND 4 AND ACTUATOR FITTINGS 1 AND 2, LH/RH


AMM 552000/6AMT 552000-200-002MRB 552005-01-1

T 12 YEI 12 YE

ALL552005-01-1 ELEVATOR PANELS INTERNAL STRUCTURE335 DI345

Y

DETAILED INSPECTION OF ELEVATOR PANELS, INTERNALSTRUCTURE AS FAR AS VISIBLE, LH/RHPREP. : PEELABLE HOLE COVERS REMOVEDAccess panels :

334AB 334BB 334CB 334DB 334EB 334FB 334GB334HB 335AB 335BB 335CB 335DB 344AB 344BB344CB 344DB 344EB 344FB 344GB 344HB 345AB345BB 345CB 345DB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 552000/6AMT 552000-200-005MRB 552006-01-2

T 12 YEI 12 YE

ALL552006-01-2 ELEVATOR OUTBOARD RIB335 DI345

Y

DETAILED INSPECTION OF ELEVATOR OUTBOARD RIB,EXTERNAL SURFACE, LH/RHNOTE 1: CREDIT CAN BE TAKE FROM PREVIOUS ACCOMPLISHMENT OF TASK 552005-01-1 IN CASE THIS INSPECTION WAS PERFORMED PRIOR JUNE 2004.PREP. : ELEVATOR TIP;NOTE 2 : CPCPAccess panels :



AMM 553000/6AMT 553000-200-001MRB 553003-01-1

T 12 YEI 12 YE

ALL553003-01-1 VERT STABILIZER CENTER BOX321 DI322323324

Y

DETAILED INSPECTION OF VERTICAL STABILIZER, CENTERBOX, INTERNAL STRUCTURE AS FAR AS VISIBLE, FRONT SPARFORWARD FACE AND UPPER CLOSING RIB, UPPER SURFACEPREP. : PEELABLE HOLE COVERS REMOVEDAccess panels :

321AL 322AL 322BL 322CL 323AL 323AR 324AT325AL 325AR 325BL 325BR 325CL 325CR 325DL325DR 325EL 325ER




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 553600/6AMT 553600-210-001MRB 553004-01-1

T 6 YEI 6 YE

ALL553004-01-1 VERT STABILIZER ATTACH FITTINGS323 DI Y

DETAILED INSPECTION OF VERTICAL STABILIZER, ATTACHFITTINGS, INCLUDING LOAD INTRODUCTION AREA AT SKINPANELSAccess panels :



AMM 553000/6AMT 553000-210-001MRB 553005-01-1

T 6 YEI 6 YE

ALL553005-01-1 RUDDER HINGE ARMS AND ACTUATOR325 DI Y

DETAILED INSPECTION OF RUDDER HINGE ARM 1,2,3,4 AND 5AND FIN ACTUATOR FITTINGS (ACTUATOR 1, 2 AND 3)TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :

325BL 325CL0.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 553000/6AMT 553000-210-002MRB 553006-01-2

T 6 YEI 6 YE

ALL553006-01-2 RUDDER HINGE ARM 6 AND 7325 DI YR

DETAILED INSPECTION OF RUDDER HINGE ARM 6 AND 7TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE 1: CPCPNOTE 2: RII TASKAccess panels :

324AT 325DL 325EL 326CT0.37Total access time : Hrs


AMM 554000/6AMT 554000-210-001MRB 554003-01-1NTM 55-40-03NTM 55-40-03/PART5

T 6 YEI 6 YE

ALL554003-01-1 RUDDER SIDE PANELS300 SDI Y

SPECIAL DETAILED INSPECTION (US) OF RUDDER SIDEPANELS, IN AREA OF RUDDER BEARINGS, IN THE BOOSTERAREA AND AROUND TRAILING EDGE FASTENERS AND HOISTINGPOINTS, LH/RH.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 554000/6AMT 554000-210-003MRB 554004-01-1

T 12 YEI 12 YE

ALL554004-01-1 RUDDER SIDE PANELS INTERNAL SURFACES326 DI YR

DETAILED INSPECTION OF RUDDER SIDE PANELS, INTERNALSURFACESNOTE 1: ALTERNATIVE ACCESS: 325AR 325BR 325CR 325DR 325ER 326ATNOTE 2: RII TASKPREP: PEELABLE HOLE COVERS REMOVEDAccess panels :

325AL 325BL 325CL 325DL 325EL 326AT0.22Total access time : Hrs


AMM 554000/6AMT 554000-210-004MRB 554005-01-1

T 6 YEI 6 YE

ALL554005-01-1 RUDDER FITTINGS,ACT. ATTACH FITTINGS326 DI Y

DETAILED INSPECTION OF RUDDER ATTACH FITTING 1,2,3,4AND 5 AND RUDDER ACTUATOR ATTACH FITTINGS (ACTUATOR1, 2 AND 3)NOTE: NOTE: ON A/C POST SB 55-1030 ONLY RUDDER ACTUATOR ATTACH FITTINGS (ACTUATOR 1, 2 AND 3) TO BE INSPECTED.TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :

325BL 325CL0.04Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 554000/6AMT 554000-210-005MRB 554006-01-1

T 6 YEI 6 YE

ALL554006-01-1 RUDDER ATTACH FITTING 6 AND 7326 DI Y

DETAILED INSPECTION OF RUDDER ATTACH FITTING 6 AND 7TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE: CPCPAccess panels :

324AT 325DL 325EL0.22Total access time : Hrs


AMT 554000-220-001MRB 554008-01-1NTM 55-40-08

T 6 YEI 6 YE


SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF THEHONEYCOMB CORE OF THE RUDDER SIDE PANELS, LH / RH.NOTE: RUDDER WITH AN AGE OF 12 YE OR HIGHER, ATAPPROVAL DATE OF MRBR REVISION 16 (SEP 2011), SHOULDTO BE INSPECTED NOT LATER THAN 12 MONTH AFTERAPPROVAL DATE OF MRBR REVISION 16 (SEP 2011).RUDDER WITH AN AGE LOWER THAN 12 YE, AT APPROVAL DATEOF MRBR REVISION 16 (SEP 2011), SHOULD PERFORM THEINSPECTION WITHIN 24 MONTH AFTER APPROVAL DATE OFMRBR REVISION 16 (SEP 2011), OR AT THE RUDDERINSPECTION THRESHOLD DATE, WHICHEVER OCCURS THELATER.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 554000-210-006MRB 554009-01-1NTM 55-40-09

T 6 YEI 6 YE


SPECIAL DETAILED INSPECTION (ELCH TEST) OF THEBONDING LAYERS BETWEEN RUDDER SIDE PANEL HONEYCOMBSTRUCTURE AND EXTERNAL SKINS OF THE RUDDER SIDEPANELS, LH / RH.NOTE: RUDDER WITH AN AGE OF 12 YE OR HIGHER, ATAPPROVAL DATE OF MRBR REVISION 16 (SEP 2011), SHOULDTO BE INSPECTED NOT LATER THAN 12 MONTH AFTERAPPROVAL DATE OF MRBR REVISION 16 (SEP 2011).RUDDER WITH AN AGE LOWER THAN 12 YE, AT APPROVAL DATEOF MRBR REVISION 16 (SEP 2011), SHOULD PERFORM THEINSPECTION WITHIN 24 MONTH AFTER APPROVAL DATE OFMRBR REVISION 16 (SEP 2011), OR AT THE RUDDERINSPECTION THRESHOLD DATE, WHICHEVER OCCURS THELATER.



: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 56 WINDOWS


Threshold Interval

Ctrl References Eff

AMM 562113/6AMT 562113-200-001MRB 562101-01-1

T 6 YEI 6 YE

ALL562101-01-1 WINDOW PANELSNT DI Y

DETAILED INSPECTION OF CABIN WINDOW PANES, INCLUDINGWINDOW PANES IN DOORSTPS : TPS MUST NOT BE APPLIEDNOTE: WORKING ZONES: 221, 222, 231, 232, 241, 242 251, 252, 261, 262Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-220-002MRB 571106-01-3NTM 57-11-06

T 60 000 FHT 40 000 CYI 23 400 FHI 9 900 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

571106-01-3 CENTER WING BOX LWR SKIN141 SDI142

Y

SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOXAT ENDS OF LOWER SKIN STIFFENERS, 8 TO 15, LH/RH.PREP. : SEALANT TO BE REMOVEDNOTE 2 : SAMPLING 20%

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-220-002MRB 571106-01-5NTM 57-11-06

T 60 000 FHT 31 000 CYI 21 600 FHI 9 200 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

571106-01-5 CENTER WING BOX LWR SKIN141 SDI142

YR

SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOXAT ENDS OF LOWER SKIN STIFFENERS, 8 TO 15, LH/RH.PREP. : SEALANT TO BE REMOVEDNOTE 2 : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 571000/6AMT 571000-200-004MRB 571109-01-1

T 12 YEI 12 YE

ALL571109-01-1 CENTER WING BOX REAR SPAR147 DI148

Y

DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR,AROUND ACCESS DOOR CUTOUTSTPS : TPS MUST NOT BE APPLIEDNOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-006MRB 571120-01-3

T 60 000 FHT 48 000 CYI 18 000 FHI 7 600 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

571120-01-3 CENTER WING SPANWISE137 DI138

YR

DETAILED INSPECTION OF CENTER WING SPANWISE FORMEDANGLE, ALONG LOWER EDGE OF FRONT SPAR, FORWARD FACEPREP.: LINING REMOVED INSULATION REMOVEDNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 571000/6AMT 571000-200-006MRB 571120-01-5

T 60 000 FHT 48 000 CYI 15 600 FHI 6 600 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

571120-01-5 CENTER WING SPANWISE137 DI138

Y

DETAILED INSPECTION OF CENTER WING SPANWISE FORMEDANGLE, ALONG LOWER EDGE OF FRONT SPAR, FORWARD FACEPREP.: LINING REMOVED INSULATION REMOVEDNOTE : SAMPLING 20%

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-012MRB 571122-01-1

T 6 YEI 6 YE

ALL571122-01-1 CENTER WING BOX REAR SPAR147 DI148

Y

DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR AFTFACETPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2NOTE: CPCPAccess panels :


AMM 571000/6AMT 571000-200-013MRB 571134-01-3

T 60 000 FHT 30 000 CYI 42 000 FHI 18 900 CY

ALL571134-01-3 CENTER WING BOX SKIN STGR 11-15191 DI192195196

Y

DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKINLOWER SURFACE, FROM STRINGER 11 TO STRINGER 15,BETWEEN Y=+/-1292, AS FAR AS VISIBLENOTE : SAMPLING 20%Access panels :

191BB 191CT 191EB 191KB 191LB 192CT 192EB192FB 192KB 192LB 195AB 196AB 734 744




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-014MRB 571135-01-3

T 60 000 FHT 30 000 CYI 42 000 FHI 18 900 CY

ALL571135-01-3 CENTER WING BOX SKIN STGR 6-11, 11-15141 DI142

Y

DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKINUPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11TO STRINGER 15, BETWEEN Y=+/-1292NOTE : SAMPLING 20%Access panels :



AMM 571000/6AMT 571000-200-019MRB 571154-01-1

T 6 YEI 6 YE

ALL571154-01-1 CENTER WING BOX LOWER SKIN191 DI192195196

Y

DETAILED INSPECTION OF CENTER WING BOX, LOWER SKINLOWER SURFACE, FROM FR 36 TO FR 42, BETWEEN RIB 1 LHAND RIB 1 RH, INCLUDING LOWER SPLICE AT RIB 1, AS FARAS VISIBLETPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3NOTE : CPCPAccess panels :

191BB 191CT 191EB 191LB 192CT 192EB 192FB192LB 195BB 196BB 734 744



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-016MRB 571155-01-1

T 12 YEI 12 YE

ALL571155-01-1 CENTER WING BOX LOWER SKIN191 DI192195196

Y

DETAILED INSPECTION OF CENTER WING BOX, LOWER SKINLOWER SURFACE, FROM FR 36 TO FR 42 BETWEEN RIB 1 LHAND RIB 1 RH, COVERED BY VAPOR SEALPREP. : AIR CONDITIONING PACKS VAPOR SEAL (IF INSTALLED) HEAT SHIELDS REMOVEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

191BB 191CT 191EB 191KB 191LB 192CT 192EB192FB 192KB 192LB 195AB 196AB 734 744




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-020MRB 571156-01-1

T 12 YEI 12 YE

ALL571156-01-1 CENTER WING BOX FRONT SPAR137 DI138

Y

DETAILED INSPECTION OF CENTER WING BOX, FRONT SPAR,FORWARD FACEPREP. : FWD ACT(S) REMOVED (IF INSTALLED).LINING REMOVED INSULATION REMOVEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :



AMM 571000/6AMT 571000-200-021MRB 571157-01-1

T 12 YEI 12 YE

ALL571157-01-1 CENTER WING BOX UPPER SKIN145 DI146

Y

DETAILED INSPECTION OF CENTER WING BOX, UPPER SKINUPPER SURFACE AND BEAMS, INCLUDING FRAME FEET BETWEENFR 36 AND FR 42.NOTE :-CAN BE PERFORMED AT SAME TIME AS 533135-01-1 -TPS MAY BE LIMITED TO CENTER WING BOX, UPPER SKIN BEAMS, BETWEEN FR 36 AND FR 42NOTE : CPCPTPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3PREP. : CABIN FLOOR PANELS REMOVED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-023MRB 571181-01-3NTM 57-11-81

T 60 000 FHT 43 000 CYI 40 100 FHI 17 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

571181-01-3 CENTER WING BOX TRIFORM FITTING141 SDI142

YR

SPECIAL DETAILED INSPECTION (US) OF CWB, UPPERSURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERSFROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RHPREP. : SEALANT REMOVED;NOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-023MRB 571181-01-5NTM 57-11-81

T 60 000 FHT 43 000 CYI 37 300 FHI 15 900 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

571181-01-5 CENTER WING BOX TRIFORM FITTING141 SDI142

YR

SPECIAL DETAILED INSPECTION (US) OF CWB, UPPERSURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERSFROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RHPREP. : SEALANT REMOVED;NOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-024MRB 571182-01-3NTM 57-11-82

T 60 000 FHT 45 000 CYI 40 100 FHI 17 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

571182-01-3 OUTER WING TRIFORM FITTING540 SDI640

YR

SPECIAL DETAILED INSPECTION (US) OF OUTER WB, UPPERSURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERSFROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RHPREP. : SEALANT REMOVED;NOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 571000/6AMT 571000-200-024MRB 571182-01-5NTM 57-11-82

T 60 000 FHT 43 000 CYI 37 300 FHI 15 900 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

571182-01-5 OUTER WING TRIFORM FITTING540 SDI640

Y

SPECIAL DETAILED INSPECTION (US) OF OUTER WB, UPPERSURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERSFROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RHPREP. : SEALANT REMOVED;NOTE : SAMPLING 20%

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-025MRB 571183-01-3NTM 57-11-83

T 60 000 FHT 40 000 CYI 40 100 FHI 17 000 CY

ALL571183-01-3 CENTER WING BOX LOWER SPLICE AT RIB 1191 SDI192195196

Y

SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICEON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRALROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,LH/RHNOTE : SAMPLING 20%Access panels :

191LB 192LB 734 7440.33Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-017MRB 571189-01-2

T 60 000 FHT 30 000 CYI 42 000 FHI 19 000 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

571189-01-2 CENTER WING BOX STRINGER WEB141 DI142

YR

DETAILED INSPECTION OF CENTER WING BOX,STRINGER WEB AT JUNCTION WITH STRUT ATTACHFITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16NOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 571000/6AMT 571000-200-017MRB 571189-01-4

T 60 000 FHT 30 000 CYI 41 200 FHI 17 700 CY

2974

30053013

3022

31983315

3355

37373862

3964

39664136

4213

42774311

4315

571189-01-4 CENTER WING BOX STRINGER WEB141 DI142

Y

DETAILED INSPECTION OF CENTER WING BOX,STRINGER WEB AT JUNCTION WITH STRUT ATTACHFITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16NOTE : SAMPLING 20%

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 571000/6AMT 571000-200-022MRB 571199-01-1

T 12 YEI 12 YE

ALL571199-01-1 OUTER WING BOX EXTERNAL SURFACE540 DI640

Y

DETAILED INSPECTION OF OUTER WING BOX, EXTERNALSURFACE OF RIB 1 AND UPPER SURFACE OF TRIFORMFITTING, BETWEEN FRONT SPAR AND REAR SPARTPS : TPS MUST NOT BE APPLIEDNOTE : CPCPAccess panels :


AMM 572000/6AMT 572000-220-004MRB 572001-01-1

T 12 YEI 6 YE

ALL572001-01-1 OUTER WING FRONT SPAR FWD FACE521 DI621

Y

DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARDFACE, BETWEEN RIB 1 AND RIB 8, INCLUDING VICINITY OFCUTOUTS FOR SLAT TRACKS 1,2,3 AND 4NOTE : CPCPAccess panels :

521AB 521BT 521CB 521EB 521GB 621AB 621BT621CB 621EB 621GB



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-003MRB 572002-01-2


ALL572002-01-2 OUTER WING FRONT SPAR ROOT JOINT FTG540 DI640

Y

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFTFACE, UPPER AND LOWER ROOT JOINT FITTINGTPS : TPS MUST NOT BE APPLIEDNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :

540AB 540AZ 640AB 640AZ0.16Total access time : Hrs

AMM 572000/6AMT 572000-200-006MRB 572008-01-2NTM 572008

T 60 000 FHT 48 000 CYI 20 000 FHI 11 000 CY

ALL572008-01-2 OUTER WING REAR SPAR JOINT PLATE574 SDI674

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER WINGREAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6.NOTE : SAMPLING 20%

Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-007MRB 572010-01-2


ALL572010-01-2 OUTER WING REAR SPAR ROOT JOINT FTG540 DI640

Y

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARDFACE, UPPER AND LOWER ROOT JOINT FITTINGSTPS : TPS MUST NOT BE APPLIEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

540AB 540BZ 640AB 640BZ0.16Total access time : Hrs

AMM 572000/6AMT 572000-220-001MRB 572012-01-2

T 60 000 FHT 48 000 CYI 21 600 FHI 13 400 CY

ALL572012-01-2 OUTER WING TOP SKIN UPR SURFACE500 DI600

Y

DETAILED INSPECTION OF OUTER WING TOPSKIN UPPER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR BETWEEN RIB 1 AND RIB 8NOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-009MRB 572019-01-2

T 60 000 FHT 48 000 CYI 23 400 FHI 16 800 CY

ALL572019-01-2 OUTER WING TOP SKIN STGR CROWN FTG540 DI640

Y

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERCROWN FITTINGS AT ROOT JOINT, FROM FRONT SPAR TO REARSPARNOTE : SAMPLING 20%Access panels :



AMM 572000/6AMT 572000-200-011MRB 572022-01-1

T 12 YEI 12 YE

ALL572022-01-1 OUTER WING TOP SKIN LWR SURFACE521 DI540621640

Y

DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWERSURFACE PYLON REINFORCING PLATENOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

521BT 540BB 540CB 621BT 640BB 640CB0.40Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-013MRB 572024-01-2

T 60 000 FHT 42 000 CYI 24 600 FHI 17 600 CY

ALL572024-01-2 OUTER WING RIBS OUTBOARD FACE540 DI640

Y

DETAILED INSPECTION OF OUTER WING RIBS,OUTBOARD FACE OF RIB 2, RIB 3 AND RIB 4 ATSKIN ATTACHMENTS ( INCLUDING CLEATS ) SPARATTACHMENTS AND REGION OF STRINGER CUTOUTSNOTE : SAMPLING 20%Access panels :



AMM 572000/6AMT 572000-200-014MRB 572026-01-5

T 60 000 FHT 34 000 CYI 21 000 FHI 10 000 CY

ALL572026-01-5 OUTER WING BOLTED PANEL540 DI640

Y

DETAILED INSPECTION OF OUTER WING, RIB 5, AFT OFBOLTED PANELNOTE : SAMPLING 20%

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALL572027-01-4 OUTER WING RIB 5 AND RIB 6540 DI640

N

DETAILED INSPECTION OF OUTER WING, RIB 5 AND RIB 6 ATSKIN ATTACHMENTS (INCLUDING CLEATS) SPAR ATTACHMENTS,ACCESS CUTOUT SURROUNDS AND IN REGION OF STRINGERCUTOUTS, EXCLUDING THE AREA INSIDE THE DRY BAYNOTE 1: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572027-01-2NOTE 2: SAMPLING 20%Access panels :



ALL572028-01-2 OUTER WING RIB 7 AND 8540 DI640

N

DETAILED INSPECTION OF OUTER WING, RIB 7 AND RIB 8AND PYLON REAR FITTING EXCLUDING PICK-UP LUGNOTE: SAMPLING 20%

Access panels :

540BB 540CB 640BB 640CB0.24Total access time : Hrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-017MRB 572029-01-3

T 60 000 FHT 44 000 CYI 30 000 FHI 22 000 CY

ALL572029-01-3 OUTER WING BOTTOM SKIN RIB 1-7500 DI600

Y

DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 1 AND RIB 7 EXCLUDING AREA COVEREDBY PYLON FAIRING AND PYLON REINFORCINGNOTE : SAMPLING 20%


AMM 572000/6AMT 572000-200-019MRB 572031-01-2

T 60 000 FHT 48 000 CYI 22 900 FHI 16 400 CY

ALL572031-01-2 OUTER WING BOTTOM SKIN LWR SURFACE411 DI421500600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT FRONT SPAR MASKED BY PYLON FAIRING ANDVISIBLE PORTION OF PYLON REINFORCING PLATEPREP.: PYLON FAIRINGS REMOVEDNOTE : SAMPLING 20%


AMM 572000/6AMT 572000-200-021MRB 572033-01-2NTM 57-20-33

T 52 500 FHT 30 000 CYI 25 900 FHI 16 000 CY

ALL572033-01-2 OUTER WING BOTTOM SKIN LDG PLATE540 SDI640

Y

SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING,BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BYMLG REINFORCING PLATE INCLUDING ATTACHMENT TO REARSPAR.NOTE : SAMPLING 20%Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALL572037-02-5 OUTER WING471 DI481

N

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWERSURFACE ATTACHMENT TO REAR SPAR IN AREA COVERED BYPYLON FAIRINGPREP.: REMOVE PYLON FAIRINGS;NOTE: SAMPLING 20%

AMM 572000-200-001T 12 YEI 6 YE

ALL572040-01-2 OUTER WING BOTTOM SKIN CUTOUTS540 SDI640

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPERAND LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIBBAY 2-3 AND RIB BAY 6-7TPS : TPS MUST NOT BE APPLIEDNOTE: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-032NTM 57-20-40

T 51 300 FHT 30 000 CYI 25 600 FHI 15 000 CY

ALL572040-03-3 OUTER WING BOTTOM SKIN CUTOUTS500 SDI540600640

Y

SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF OUTERWING, BOTTOM SKIN, UPPER AND LOWER SURFACES, AROUNDACCESS DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7.NOTE : SAMPLING 20%Access panels :



AMT 572000-200-024MRB 572047-01-5NTM 57-20-47

T 44 900 FHT 30 000 CYI 16 600 FHI 11 100 CY

ALL572047-01-5 OUTER BOTTOM SKIN LOWER SURFACE471 SDI481

N

SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF OUTERWING, BOTTOM SKIN, LOWER SURFACE AROUND AFT PYLONATTACHMENT FITTING CUTOUTPREPARATION: PYLON FAIRINGS REMOVEDNOTE: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 574100-200-003MRB 572049-01-3

I 6 YE 22552261

2267

23032480

2974

30053013

3022

31983315

3355

3600

572049-01-3 OUTER WING BOTTOM SKIN DRAIN HOLES500 DI600

N

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWERSURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIBBAYS 1-2, 2-3, 4-5, 5-6) MAGNETIC LEVEL INDICATORHOLE ADJACENT TO RIB 6; MLG PICK UP RAIL HOLE FORWARDOF REAR SPAR INBOARD IF RIB 5.NOTE 1: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOF AMSS ISS 13 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS13 AMD 00 EFFECTIVE DATE IS NEXT 6YE CHECK.NOTE 2: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-003MRB 572049-01-4

T 6 YEI 6 YE

37373862

3964

39664136

4213

42774311

4315

46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

5392

572049-01-4 OUTER WING BOTTOM SKIN DRAIN HOLES500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWERSURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIBBAYS 1-2, 2-3, 4-5, 5-6), DRY BAY DRAIN HOLE IN RIBBAY 6-7; MAGNETIC LEVEL INDICATORHOLE ADJACENT TO RIB 6, MLG PICK UP RAIL HOLE FORWARDOF REAR SPAR INBOARD OF RIB 5.NOTE : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5418

5427

54385456

5469

54955555

5699

57095916

5958


AMM 572000/6AMT 572000-200-025MRB 572052-01-2

T 12 YEI 12 YE

ALL572052-01-2 OUTER WING BOTTOM SKIN ROOT JOINT FTG540 DI640

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ROOTJOINT FITTINGS ON STRINGER 8 AND STRINGER 11TPS : TPS MUST NOT BE APPLIEDNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-002MRB 572054-01-4


ALL572054-01-4 OUTER WING BOTTOM SKIN PUMP APERTURES500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT FUEL PUMP APERTURES BETWEEN RIB 1 AND RIB 2PREP. : FUEL PUMPNOTE 1: 100% THRESHOLD = 20YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMT 572000-220-805T 6 YEI 6 YE

ALL572054-02-1 OUTER WING BOTTOM SKIN PUMP APERTURES500 DI600

N

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWERSURFACE AT HOLES ADJACENT TO FUEL PUMP APERTURESBETWEEN RIB 1 AND RIB 2NOTE 1: CPCPNOTE 2: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGESOF AMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS14 AMD 00 EFFECTIVE DATE IS NEXT C CHECK.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-027MRB 572057-01-2NTM 57-20-57

T 60 000 FHT 43 500 CYI 33 200 FHI 20 600 CY

ALL572057-01-2 OUTER WING BOTTOM SKIN RIB BAY 7-8471 SDI481

Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,BOTTOM SKIN LOWER SURFACE, HOT FUEL RECIRCULATIONHOLE AT RIB BAY 7-8, BETWEEN STRINGER 4 AND STRINGER5.PREP.: PYLON FAIRINGS REMOVEDNOTE : SAMPLING 20%


AMM 572000/6AMT 572000-220-003MRB 572062-01-1

T 12 YEI 6 YE

ALL572062-01-1 OUTER WING FIXED TRAILING EDGE571 DI574671674

Y

DETAILED INSPECTION OF OUTER WING FIXEDTRAILING EDGE, REAR SPAR AFT FACE, BETWEEN GEARSUPPORT RIB 5 AND RIB 8NOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572000/6AMT 572000-200-031MRB 572063-01-1

T 6 YEI 6 YE

ALL572063-01-1 OUTER WING FIXED TRAILING EDGE500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWERSURFACE, AREA COVERED BY FUEL PUMP WIRING HARNESSFAIRINGS.PREP. : FUEL PUMP FAIRINGS WIRING HARNESS DISPLACEDNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMM 572100/6AMT 572100-200-006MRB 572101-01-2


ALL572101-01-2 OUTER WING FRT SPAR FWD FACE RIB 8-22522 DI622

Y

DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARDFACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTSNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCP

Access panels :

522AB 522CB 522EB 522FB 522HB 522JB 522KB522LB 522NB 522QB 622AB 622CB 622EB 622FB622HB 622JB 622KB 622LB 622NB 622QB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-007MRB 572106-01-4


ALL572106-01-4 OUTER WING FRT SPAR FWD FACE RIB 22-27522 DI622

Y

DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARDFACE, BETWEEN RIB 22 AND RIB 27, INCLUDING ALLCUTOUTSNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

522QB 522SB 522UB 622QB 622SB 622UB0.60Total access time : Hrs


AMM 572100/6AMT 572100-200-008MRB 572108-01-3

T 49 500 FHT 30 000 CYI 21 100 FHI 12 700 CY

ALL572108-01-3 OUTER WING FRT SPAR AFT FACE RIB 8-22540 DI640

Y

DETAILED INSPECTION OF OUTER WING FRONTSPAR AFT FACE BETWEEN RIB 8 AND RIB 22NOTE : SAMPLING 20%

Access panels :

540CB 540DB 540EB 540FB 540GB 540HB 540JB540KB 540LB 540MB 540NB 540PB 540QB 540RB640CB 640DB 640EB 640FB 640GB 640HB 640JB640KB 640LB 640MB 640NB 640PB 640QB 640RB



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-009MRB 572109-01-2

T 60 000 FHT 48 000 CYI 24 600 FHI 17 600 CY

ALL572109-01-2 OUTER WING FRT SPAR AFT FACE RIB 22-27550 DI560650660

Y

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFTFACE, BETWEEN RIB 22 AND RIB 27NOTE : SAMPLING 20%

Access panels :

550AB 550BB 550CB 550DB 560AB 650AB 650BB650CB 650DB 660AB




ALL572116-02-2 MAIN STRUCTURE500 DI600

N

DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPARBETWEEN RIB 8 AND RIB 22NOTE: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-001MRB 572122-01-1

T 60 000 FHT 48 000 CYI 32 100 FHI 20 000 CY

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

572122-01-1 OUTER WING TOP SKIN RIB 19-20500 DI600

Y

DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPERSURFACE AROUND MANUAL REFUELLING APERTURE, BETWEENRIB 19 AND RIB 20PREP.: ADAPTOR RINGNOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-032MRB 572122-02-1

T 6 YEI 6 YE

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

572122-02-1 OUTER WING TOP SKIN RIB 19-20500 DI600

Y

DETAILED INSPECTION OF OUTER WING TOPSKIN, UPPER SURFACE AROUND MANUAL REFUELLINGAPERTURE BETWEEN RIB 19 AND RIB 20NOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALL572123-01-3 OUTER WING TOP SKIN STGR RIB 8-13540 DI640

N

DETAILED INSPECTION OF OUTER WING, TOP SKIN,STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTSAND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8AND RIB 9 AND BUTT STRAP AT STRINGER 11NOTE 1: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572123-01-1NOTE 2: SAMPLING 20%Access panels :

540CB 540DB 540EB 540FB 540GB 640CB 640DB640EB 640FB 640GB



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-013MRB 572124-01-2

T 52 900 FHT 30 000 CYI 35 100 FHI 22 000 CY

ALL572124-01-2 OUTER WING TOP SKIN STGR RIB 13-27540 DI550560640650660

Y

DETAILED INSPECTION OF OUTER WING TOPSKIN STRINGERS BETWEEN RIB 13 AND RIB 27INCLUDING RUNOUTS, AIR TRANSFER HOLES ANDBUTTSTRAP AT STRINGER 11 INCLUDING RUNOUT ATFRONT SPAR AT RIB 18NOTE : SAMPLING 20%Access panels :

540HB 540JB 540KB 540LB 540MB 540NB 540PB540QB 540RB 550AB 550BB 550CB 550DB 560AB640HB 640JB 640KB 640LB 640MB 640NB 640PB640QB 650AB 650BB 650CB 650DB 660AB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 572100-270-001ISB 57-1154

I 40 MOSee note

NTCheck :

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

572125-01-1 TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 22575 SDI675

Y

AND RIB 27SPECIAL DETAILED INSPECTION OF OUTER WING, TOP SKINPANEL 2 OVERHANG BETWEEN RIB 22 AND RIB 27NOTE : - FOR THRESHOLD REFER TO ISB 57-1154. - REFER TO ISB 57-1154 FOR ALTERNATIVE TASK TERMINATING THIS INSPECTION.



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


ALL572126-01-3 OUTER WING RIB9-27 AT SKIN ATTACHMENTS540 DI550560640650660

N

DETAILED INSPECTION OF OUTER WING, RIB 9 TO RIB 27,AT SKIN ATTACHMENTS, INCLUDING CLEATS, SPARATTACHMENTS AND IN REGION OF STRINGER CUTOUTSNOTE: SAMPLING 20%

Access panels :

540CB 540DB 540EB 540FB 540GB 540HB 540JB540KB 540LB 540MB 540NB 540PB 540QB 540RB550AB 550BB 550CB 550DB 560AB 640CB 640DB640EB 640FB 640GB 640HB 640JB 640KB 640LB640MB 640NB 640PB 640QB 640RB 650AB 650BB650CB 650DB



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 572100-270-002ISB 1155

I 40 MOSee note

NTCheck :

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

572127-01-1 TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 4575 SDI675

Y

AND RIB 22SPECIAL DETAILED INSPECTION OF OUTER WING, TOP SKINPANEL 2 OVERHANG BETWEEN RIB 4 AND RIB 22NOTE : - FOR THRESHOLD REFER TO ISB 57-1155.- REFER TO ISB 57-1155 FOR ALTERNATIVE TASKTERMINATING THIS INSPECTION.


AMM 572100/6AMT 572100-200-017MRB 572131-01-5

T 59 100 FHT 34 000 CYI 34 300 FHI 19 700 CY

ALL572131-01-5 OUTER WING BOTTOM SKIN LWR SURFACE500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,BETWEEN RIB 22 AND RIB 27NOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-018MRB 572134-01-3

T 52 500 FHT 30 000 CYI 42 000 FHI 24 000 CY

ALL572134-01-3 OUTER WING BOTTOM SKIN TRACK 3 AND 4540 DI640

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPERSURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD ANDAFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REARSPARNOTE : SAMPLING 20%Access panels :

540FB 540GB 540NB 540PB 640FB 640GB 640NB640PB



AMT 572100-200-004MRB 572139-01-2

T 12 YEI 6 YE

ALL572139-01-2 OUTER WING BOTTOM SKIN RIB BAY CUTOUTS500 DI540600640

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPERAND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS IN RIBBAYS 8-9, 9-10, 10-11, 11-12 AND 12-13TPS : TPS MUST NOT BE APPLIEDNOTE: CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-020MRB 572139-02-2NTM 57-21-39

T 52 100 FHT 30 000 CYI 17 700 FHI 10 200 CY

ALL572139-02-2 OUTER WING BOTTOM SKIN RIB BAY CUTOUTS500 SDI540600640

Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESSDOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND12-13.NOTE : SAMPLING 20%Access panels :




AMM 572100/6AMT 572100-200-021MRB 572140-01-2

T 12 YEI 90 MO

ALL572140-01-2 OUTER WING BOTTOM SKIN CUTOUTSNT DI Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS,BETWEEN RIB 13 AND RIB 27NOTE 1: CPCPNOTE 2: WORKING ZONES: 500, 540, 550, 560 600, 640, 650, 660Access panels :

540HB 540JB 540KB 540LB 540MB 540NB 540PB540QB 540RB 550AB 550BB 550CB 550DB 560AB640HB 640JB 640KB 640LB 640MB 640NB 640PB640QB 640RB 650AB 650BB 650CB 650DB 660AB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-024MRB 572151-01-3

T 48 700 FHT 30 000 CYI 20 300 FHI 12 500 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958


YR

DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11 BETWEEN RIB 18 ANDRIB 20 IN AREA COVERED BY FLAP TRACK 4 FAIRINGNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-024MRB 572151-01-4

T 48 700 FHT 30 000 CYI 15 900 FHI 9 800 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994


YR

DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11 BETWEEN RIB 18 ANDRIB 20 IN AREA COVERED BY FLAP TRACK 4 FAIRINGNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 572100/6AMT 572100-200-025MRB 572153-01-1

T 6 YEI 6 YE

ALL572153-01-1 OUTER WING BOTTOM SKIN DRAIN HOLES500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT DRAIN HOLES FOR TRACK CANS 5,6,7,8,9,10,11,12(RIB BAYS 9-10,11-12,13-14,16-17,18-19,21-22,23-24,25-26)DRY BAY DRAIN HOLES IN RIB BAY 26-27 AND MAGNETIC LEVELINDICATOR POSITIONS ADJACENT TO RIB 9 AND RIB 12NOTE : CPCP


AMM 572100/6AMT 572100-200-027MRB 572157-01-2NTM 57-21-57

T 52 500 FHT 30 000 CYI 33 200 FHI 20 000 CY

ALL572157-01-2 OUTER WING BOTTOM SKIN RUNOUT500 SDI600

Y

SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING,BOTTOM SKIN, RUNOUT OF BUTTSTRAP AT STRINGER 8,BETWEEN RIB 20 AND RIB 21, ADJACENT TO FRONT SPAR ANDRUNOUT OF BUTTSTRAP AT STRINGER 11 ADJACENT TO RIB 21AT REAR SPAR.NOTE : SAMPLING 20%Access panels :

540PB 540QB 540RB 640PB 640QB 640RB0.51Total access time : Hrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572100/6AMT 572100-200-030MRB 572161-01-6


ALL572161-01-6 OUTER WING BOTTOM SKIN ACCESS DOORS540 DI550560640650660

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ACCESSDOORS, BETWEEN RIB 13 AND RIB 27TPS : TPS MUST NOT BE APPLIEDNOTE 1: 100% THRESHOLD = 12YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

540HB 540JB 540KB 540LB 540MB 540NB 540PB540QB 540RB 550AB 550BB 550CB 550DB 560AB640HB 640JB 640KB 640LB 640MB 640NB 640PB640QB 640RB 650AB 650BB 650CB 650DB 660AB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-005MRB 572164-01-2

T 6 YEI 6 YE

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

3964

572164-01-2 OUTER WING BOTTOM SKIN FUEL DRAIN500 DI600

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB22-23, AND MAGNETIC LEVEL INDICATOR POSITION BETWEENRIB 15-16NOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-005MRB 572164-01-3

T 6 YEI 6 YE

39664136

4213

42774311

4315

46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

53925418

5427

5438

572164-01-3 OUTER WING BOTTOM SKIN FUEL DRAIN500 DI600

YR

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWERSURFACE AT FUEL TANK WATER DRAIN HOLES RIB 22-23NOTE : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5456

5469

54955555

5699

57095916

5958

5994


AMM 572600/6AMT 572600-200-004MRB 572601-01-2

T 48 000 CYI 6 100 CY

ALL572601-01-2 FLAP TRACK BEAMS UPR FLANGE RADII531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS2,3,4 TRACK UPPER FLANGE RADIINOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572601-02-2PREP. : FLAP EXTENSIONNOTE : SAMPLING 20%Access panels :

531CB 531EB 532CB 532EB 533CB 533EB 631CB631EB 632CB 632EB 633CB 633EB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572600/6AMT 572600-220-003MRB 572601-02-2NTM 57-26-01

T 48 000 CYI 12 300 CY

ALL572601-02-2 FLAP TRACK BEAMS UPR FLANGE RADII531 SDI532533 DI631632633

Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,FLAP TRACK BEAMS 2,3,4 TRACK UPPER FLANGE RADIIPREP. : FLAPS EXTENDED;NOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 572601-01-2NOTE 2: SAMPLING 20%Access panels :



AMM 572600/6AMT 572600-200-005MRB 572604-01-3

T 48 000 CYI 6 100 CY

ALL572604-01-3 FLAP TRACK BEAMS LWR FLANGES531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS2,3,4 LOWER FLANGES AND LOWER CHANNELPREP.: FLAP EXTENSIONNOTE : SAMPLING 20%

Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572600/6AMT 572600-200-006MRB 572607-01-2

T 6 YEI 6 YE

ALL572607-01-2 FLAP TRACK BEAMS FWD SPIGOT ATTACH531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS2,3,4 FORWARD SPIGOT PINS, BOLTS AND FITTINGS.NOTE : CPCP

Access panels :




AMM 572600/6AMT 572600-220-004MRB 572607-02-2

T 48 000 CYI 7 300 CY

ALL572607-02-2 FLAP TRACK BEAMS FWD SPIGOT ATTACH531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS2,3,4 FORWARD SPIGOT PINS, BOLTS AND FITTINGSNOTE: REFER TO AMM FOR GAP CHECKNOTE 2 : SAMPLING 20%

Access panels :

531CB 531EB 532CB 532EB 533CB 533EB 631AB631BB 632AB 632BB 633AB 633BB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572600/6AMT 572600-220-005MRB 572610-01-2

T 48 000 CYI 12 300 CY

ALL572610-01-2 FLAP TRACK BEAMS AFT SPIGOT531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS2,3,4 AFT SPIGOTPREP. : FLAP EXTENSIONNOTE 1: REFER TO AMM FOR TORQUE CHECKNOTE 2: SAMPLING 20%Access panels :

531CB 532CB 533CB 631CB 632CB 633CB0.12Total access time : Hrs


AMM 572600/6AMT 572600-200-010MRB 572610-02-1

T 6 YEI 6 YE

ALL572610-02-1 FLAP TRACK BEAMS AFT SPIGOT531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS2,3,4 AFT SPIGOTPREP. : FLAP EXTENSIONNOTE : CPCPTPS: "NO" (TPS MUST NOT BE APPLIED)Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572600/6AMT 572600-200-008MRB 572650-01-1

T 12 YEI 12 YE

ALL572650-01-1 OUTER WING REAR SPAR SIDESTAY FITTING571 DI671

Y

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACESIDESTAY FITTINGNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMM 572600/6AMT 572600-200-007MRB 572651-01-1

T 6 YEI 6 YE

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

572651-01-1 OUTER WING REAR SPAR JACK FITTING571 DI671

Y

DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE, RETRACTION JACK FITTINGPREP.: RETRACTION ANCHORAGE ACTUATOR REMOVED; BEARING ASSEMBLY REMOVED;NOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 572600-200-007I 6 YE 41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715251

5275

53065340

5385

53925418

5438

54565495

5555

56995916

5958

572651-01-2 OUTER WING REAR SPAR JACK FITTING571 DI671

YR

OUTER WING REAR SPAR JACK FITTINGDETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACERETRACTION JACK FITTINGNOTE: REMOVAL OF ACTUATOR AND BEARING ASSEMBLY NOTREQUIRED FOR POST 39730 OR POST 150311 AIRCRAFT.


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


AMM 572600/6AMT 572600-200-001MRB 572653-01-2

T 48 000 CYT 12 YEI 16 400 CYI 12 YE

ALL572653-01-2 FLAP TRACK 2 AFT ATTACH FITTINGS531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING, FLAP TRACK 2, AFTATTACHMENT FITTINGS ON WING BOTTOM SKIN AT FALSE REARSPAR, AND FLAP TRACK 3 & 4, AFT ATTACHMENT FITTINGSAT REAR SPARNOTE 1: SAMPLING 20%NOTE 2: 100% THRESHOLD = 12YENOTE 3: CPCPTPS: "NO" (TPS MUST NOT BE APPLIED)Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572600/6AMT 572600-220-001MRB 572654-01-2NTM 57-26-54

T 60 000 FHT 48 000 CYI 22 900 FHI 16 400 CY

ALL572654-01-2 OUTER WING PYLON FWD ATTACH FITTING521 SDI621

Y

SPECIAL DETAILED INSPECTION (US AND EC) OF OUTERWING, PYLON FORWARD ATTACHMENT FITTINGSPREP.: BOLTS REMOVED; SHACKLES; SLEEVES; ENGINE REMOVED;NOTE : SAMPLING 20%Access panels :

521BT 621BT0.16Total access time : Hrs


AMM 572600/6AMT 572600-200-002MRB 572656-01-1

T 12 YEI 12 YE

ALL572656-01-1 OUTER WING PYLON SPIGOT500 DI600

Y

DETAILED INSPECTION OF OUTER WING, PYLON SPIGOTFITTINGPREP. : BALL JOINT REMOVED PYLON FAIRINGS REMOVED SLEEVE REMOVEDNOTE 1: SAMPLING 20%NOTE 2: 100% LIMIT = 24 YENOTE 3: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 572600/6AMT 572600-200-003MRB 572657-01-1

T 12 YEI 12 YE

ALL572657-01-1 OUTER WING PYLON AFT FITTING LUG500 DI600

Y

DETAILED INSPECTION OF OUTER WING, AFT PYLONATTACHMENT FITTING LUGTPS : TPS MUST NOT BE APPLIEDPREP: PYLON FAIRINGS REMOVEDNOTE: 100% THRESHOLD = 24YENOTE: SAMPLING 20%


AMM 572600/6AMT 572600-200-009MRB 572658-01-2

T 12 YEI 12 YE

ALL572658-01-2 OUTER WING BOTTOM SKIN TRACK BEAM FTG531 DI532533631632633

Y

DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE FORWARD ATTACHMENT FITTINGFOR FLAP TRACK BEAMS 2, 3 & 4NOTE 1: SAMPLING 20%NOTE 2: 100% THRESHOLD = 24YEAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 573000/6AMT 573000-200-001MRB 573101-01-2

T 60 000 FHT 48 000 CYI 17 200 FHI 12 300 CY

ALL573101-01-2 WING TIP BOTTOM SKIN LWR SURFACE JOINT534 DI634

Y

DETAILED INSPECTION OF WING TIP BOTTOMSKIN LOWER SURFACE JOINT OUTBOARD OF RIB 27NOTE : SAMPLING 20%


AMM 574100/6AMT 574100-200-012MRB 574101-01-2


ALL574101-01-2 FIXED LE ROLLER PIN HOLES521 DI522621622

Y

DETAILED INSPECTION OF OUTER WING, FIXED LEADINGEDGE, ROLLER PIN HOLES AND OTHER CUTOUTS IN TRACK RIB1 TO 12NOTE 1 : 100% LIMIT = 12 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-013MRB 574102-01-2NTM 57-41-02

T 60 000 FHT 48 000 CYI 18 000 FHI 12 900 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

574102-01-2 FIXED LE FWD UPR ROLLER PIN HOLES522 SDI622

YR

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,FIXED LEADING EDGE, FORWARD UPPER ROLLER PIN HOLES INTRACK RIBS 5,6,7,8,9,10,11 AND 12.PREP.: SLATS AND SLAT TRACKS REMOVEDNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

522AB 522CB 522FB 522KB 522LB 522NB 522QB522SB 522UB 622AB 622CB 622FB 622KB 622LB622NB 622QB 622SB 622UB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-013MRB 574102-01-3NTM 57-41-02

T 60 000 FHT 48 000 CYI 13 800 FHI 9 900 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

574102-01-3 FIXED LE FWD UPR ROLLER PIN HOLES522 SDI622

YR

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,FIXED LEADING EDGE, FORWARD UPPER ROLLER PIN HOLES INTRACK RIBS 5,6,7,8,9,10,11 AND 12.PREP.: SLATS AND SLAT TRACKS REMOVEDNOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :

522AB 522CB 522FB 522KB 522LB 522NB 522QB522SB 522UB 622AB 622CB 622FB 622KB 622LB622NB 622QB 622SB 622UB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-014MRB 574106-01-2


22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

574106-01-2 FIXED LE BOTTOM ATTACH JOINT521 DI522621622

YR

DETAILED INSPECTION OF OUTER WING, FIXED LEADINGEDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TO 12NOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-014MRB 574106-01-4


29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

54275469

5709

5994

574106-01-4 FIXED LE BOTTOM ATTACH JOINT521 DI522621622

YR

DETAILED INSPECTION OF OUTER WING, FIXED LEADINGEDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TO 12NOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCP


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Access panels :



AMM 574100/6AMT 574100-200-015MRB 574112-01-1

T 12 YEI 6 YE

ALL574112-01-1 FIXED LE MAIN BOTTOM WING SKIN521 DI522621622

Y

DETAILED INSPECTION OF OUTER WING, FIXED LEADINGEDGE, BOTTOM WING SKIN, UPPER AND LOWER SURFACES,FORWARD OF FRONT SPAR, FROM RIB 1 TO RIB 27,INCLUDING SIGHTING ROD HOLES IN RIB BAY 8-9 AND RIBBAY 26-27, LIFTING BEAM HOLES AND DRAIN HOLESNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-016MRB 574113-01-1

T 12 YEI 6 YE

ALL574113-01-1 FIXED LE TOP WING SKIN521 DI522621622

Y

DETAILED INSPECTION OF OUTER WING, FIXED LEADING EDGETOP WING SKIN, UPPER AND LOWER SURFACES, FORWARD OFFRONT SPAR, FROM RIB 1 TO RIB 27NOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-017MRB 574114-01-2NTM 57-41-14

T 60 000 FHT 48 000 CYI 17 800 FHI 12 800 CY

ALL574114-01-2 FIXED LE PINION FITTING521 SDI522621622

Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,FIXED LEADING EDGE PINION FITTING BOLTING ANDACTUATOR BOLTING LOWER BOLT HOLES ON RIB2,3,5,6,7,8,9,10,11 AND 12NOTE : SAMPLING 20%Access panels :

521CB 521EB 522AB 522CB 522FB 522KB 522LB522NB 522QB 522SB 522UB 621CB 621EB 622AB622CB 622FB 622KB 622LB 622NB 622QB 622SB622UB



AMM 574100/6AMT 574100-200-002MRB 574201-01-1

T 6 YEI 6 YE

ALL574201-01-1 SLAT 1, TRACKS 1-4500 DI600

Y

DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 :VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT ISFULLY EXTENDED, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574200/6AMT 574200-200-001MRB 574202-01-1

T 12 YEI 6 YE

22552261

574202-01-1 SLAT 1 TRACKS 1-4 ATTACHMENTS500 DI600

Y

DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: BOLTS SUCCESSIVELY REMOVED SLATS EXTENDEDNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 574200-200-001MRB 574202-01-2

T 12 YEI 6 YE

22672303

2480

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

574202-01-2 SLAT 1 TRACKS 1-4 ATTACHMENTS500 DI600

Y

DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: SLATS FULLY EXTENDED;NOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574200/6AMT 574200-200-004MRB 574204-01-1


ALL574204-01-1 SLAT 1 SKIN CONNECTIONS500 DI600

Y

DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS INAREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH.NOTE 1: DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 1.TPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 574200/6AMT 574200-200-005MRB 574204-02-1NTM 57-42-04

T 12 YEI 12 YE

ALL574204-02-1 SLAT 1 SKIN CONNECTIONS500 SDI600

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 1,SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIBSTATIONS, LH/RH.NOTE 1: SDET INSPECTION IS OF INTERNAL STRUCTURE OFSLAT 1 (ENDOSCOPE).TPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 574200-280-801NTM 57-42-04

T 78 000 FHT 39 000 CYI 32 000 FHI 16 000 CY

ALL574204-03-1 SLAT 1500 SDI600

N

SPECIAL DETAILED INSPECTION (HFEC) OF SLAT 1, SKINCONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIBSTATIONS 3 AND 4, LH/RHNOTE 1: SDET INSPECTION IS OF EXTERNAL STRUCTURE OFSLAT 1PREP.: SLAT FULLY EXTENDED;NOTE 2: SAMPLING 20%

AMM 574200/6AMT 574200-200-006MRB 574205-01-1

T 12 YEI 6 YE

ALL574205-01-1 SLAT 1 TRAILING EDGE500 DI600

Y

DETAILED INSPECTION OF SLAT 1, TRAILING EDGE, LOWERFACE, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE : CPCP


AMM 574100/6AMT 574100-200-008MRB 574301-01-1

T 6 YEI 6 YE

ALL574301-01-1 SLAT 2 TRACK 5-6 ROLLER CONTACT AREA500 DI600

Y

DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6 :VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT ISFULLY EXTENDED, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574300/6AMT 574300-200-008MRB 574302-01-1

T 12 YEI 6 YE

22552261

574302-01-1 SLAT 2 TRACK 5-6 ATTACHMENTS500 DI600

Y

DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: BOLTS SUCCESSIVELY REMOVED SLATS EXTENDEDNOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574300/6AMT 574300-200-008MRB 574302-01-2

T 12 YEI 6 YE

22672303

2480

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315


Y

DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: SLATS FULLY EXTENDEDNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574300/6AMT 574300-200-002MRB 574304-01-1

T 12 YEI 12 YE


Y

DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS INAREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RHNOTE 1: DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 2.TPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 574300/6AMT 574300-200-003MRB 574304-02-2NTM 57-43-04

T 12 YEI 12 YE


Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 2,SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIBSTATIONS, LH/RH.NOTE 1: SDET INSPECTION IS OF INTERNAL STRUCTURE OF SLAT 2.TPS : TPS MUST NOT BE APPLIEDPREP. : SLAT FULLY EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 574300-280-801NTM 57-43-04

T 78 000 FHT 39 000 CYI 32 000 FHI 16 000 CY


N

SPECIAL DETAILED INSPECTION (LFEC) OF SLAT 2, SKINCONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIBSTATIONS, LH/RH.NOTE: SDET INSPECTION IS OF EXTERNAL STRUCTURE OFSLAT 2.PREP.: SLATS FULLY EXTENDED;NOTE: SAMPLING 20%


AMM 574300/6AMT 574300-200-001MRB 574305-01-1

T 12 YEI 6 YE


Y

DETAILED INSPECTION OF SLAT 2, TRAILING EDGE, LOWERFACE, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP.: SLATS EXTENDEDNOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574100/6AMT 574100-200-009MRB 574401-01-1

T 6 YEI 6 YE


Y



AMM 574400/6AMT 574400-200-010MRB 574402-01-1

T 12 YEI 6 YE

22552261


Y

DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP. : BOLTS SUCCESSIVELY REMOVED SLATS EXTENDED NOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574400/6AMT 574400-200-010MRB 574402-01-2

T 12 YEI 6 YE

22672303

2480

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315


Y

DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: SLATS FULLY EXTENDEDNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574400/6AMT 574400-200-007MRB 574404-01-1NTM 57440



Y

DETAILED INSPECTION OF SLAT 3, SKINCONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIBSTATIONS, LH/RHNOTE 1: DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 3.TPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 574400/6AMT 574400-200-007MRB 574404-02-1NTM 57-44-04

T 12 YEI 12 YE


Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 3,SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIBSTATIONS, LH/RH.NOTE 1: SDET INSPECTION IS OF INTERNAL STRUCTURE OF SLAT 3.TPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574400/6AMT 574400-200-009MRB 574405-01-1

T 12 YEI 6 YE


Y

DETAILED INSPECTION OF SLAT 3, TRAILING EDGE, LOWER FACE, LH/RH TPS : TPS MUST NOT BE APPLIED NOTE : CPCP PREP. : SLATS EXTENDED


AMM 574100/6AMT 574100-200-010MRB 574501-01-1

T 6 YEI 6 YE


Y

DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 :VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT ISFULLY EXTENDED, LH/RHTPS : TPS MUST NOT BE APPLIEDNOTE : CPCPNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%PREP. : SLATS EXTENDED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574500/6AMT 574500-200-008MRB 574502-01-1

T 12 YEI 6 YE

22552261


Y

DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP.: BOLTS SUCCESSIVELY REMOVED SLATS FULLY EXTENDEDNOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574500/6AMT 574500-200-008MRB 574502-01-2

T 12 YEI 6 YE

22672303

2480

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315


Y

DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: SLATS FULLY EXTENDEDNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574500/6AMT 574500-200-005MRB 574504-01-1NTM 574504



Y

DETAILED INSPECTION OF SLAT 4, SKINCONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIBSTATIONS, LH/RHNOTE 1: DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 4.TPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 574500/6AMT 574500-200-006MRB 574504-02-1NTM 57-45-04

T 12 YEI 12 YE


Y




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574500/6AMT 574500-200-007MRB 574505-01-1

T 12 YEI 6 YE


Y

DETAILED INSPECTION OF SLAT 4, TRAILING EDGE, LOWERFACE, LH/RHTPS : TPS MUST NOT BE APPLIED NOTE : CPCP PREP. : SLATS EXTENDED


AMM 574100/6AMT 574100-200-011MRB 574601-01-1

T 6 YEI 6 YE


Y




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574600/6AMT 574600-200-008MRB 574602-01-1

T 12 YEI 6 YE

22552261


Y

DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP. BOLTS SUCCESSIVELY REMOVED SLATS EXTENDEDNOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574600/6AMT 574600-200-008MRB 574602-01-2

T 12 YEI 6 YE

22672303

2480

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315


Y

DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,BOLTS, LINKS AND SIDE PLATES, LH/RHTPS : TPS MUST NOT BE APPLIEDPREP: SLATS FULLY EXTENDEDNOTE: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574600/6AMT 574600-200-005MRB 574604-01-1



Y

DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS INAREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RHNOTE 1: DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 5.TPS : TPS MUST NOT BE APPLIEDPREP. : SLATS EXTENDEDNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 574600/6AMT 574600-200-006MRB 574604-02-1NTM 57-46-04

T 12 YEI 12 YE


Y




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 574600/6AMT 574600-200-007MRB 574605-01-1

T 12 YEI 6 YE


Y

DETAILED INSPECTION OF SLAT 5, TRAILING EDGE, LOWERFACE LH/RHTPS : TPS MUST NOT BE APPLIED NOTE 1 : 100% LIMIT = 12 YE NOTE 2 : CPCP PREP. : SLATS EXTENDED


AMM 575100/6AMT 575100-220-004MRB 575101-01-1

T 12 YEI 12 YE

ALL575101-01-1 TRAILING EDGE FLAP ACTUATOR BRACKETS531 DI532533631632633

Y

DETAILED VISUAL INSPECTION OF OUTER WINGTRAILING EDGE FLAP ACTUATOR BRACKETS AT FLAPTRACKS 2, 3 AND 4NOTE : CPCP

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-220-005MRB 575101-02-2NTM 57-51-01

T 48 000 CYI 16 400 CY

ALL575101-02-2 TRAILING EDGE FLAP ACTUATOR BRACKETS531 SDI532533631632633

Y

SPECIAL DETAILED INSPECTION (US) OF OUTER WING,TRAILING EDGE FLAP ACTUATOR BRACKETS AT FLAPTRACKS 2, 3 AND 4NOTE : SAMPLING 20%

Access panels :



AMT 575100-220-006MRB 575104-01-1

T 48 000 CYT 12 YEI 15 000 CYI 12 YE

ALL575104-01-1 TRAILING EDGE SPOILER 1 HINGE FITTINGS500 DI600

Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,SPOILER 1 ACTUATOR AND HINGE FITTINGSPREP.: FLAPS EXTENDED; SPOILERS EXTENDED;NOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-210-001MRB 575106-01-3

T 48 000 CYI 12 300 CY

ALL575106-01-3 TRAILING EDGE SPOILERS HINGE PINSNT DI Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,SPOILERS 1,2,3,4 AND 5 HINGE PINSPREP.: PINS REMOVEDNOTE : THIS TASK IS AN ALTERNATIVE TO TASK 575106-02-3NOTE : SAMPLING 20%NOTE : WORKING ZONES 574 ,575 ,582 ,583 ,584 ,585 ,586 674 ,675 ,682 ,683 ,684 ,685 ,686Access panels :

573BB 575BB 575DB 575EB 575GB 673BB 675BB675DB 675EB 675GB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-220-015MRB 575106-02-3NTM 575106

T 48 000 CYI 16 400 CY

ALL575106-02-3 TRAILING EDGE SPOILERS HINGE PINSNT SDI Y

SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING,TRAILING EDGE, SPOILERS 1,2,3,4,AND 5 HINGE PINSPREP. : PINS REMOVEDNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 575106-01-3NOTE 3: SAMPLING 20%NOTE 4: WORKING ZONES: 574, 575, 582, 583, 584, 585, 586 674, 675, 682, 683, 684, 685, 686Access panels :




AMM 575100/6AMT 575100-210-002MRB 575106-03-1

T 12 YEI 12 YE

ALL575106-03-1 TRAILING EDGE SPOILERS HINGE PINSNT SDI Y

DETAILED INSPECTION OF OUTER WING TRAILING EDGESPOILERS 1,2,3,4 AND 5 HINGE PINSNOTE 1: WORKING ZONES: 574, 575, 582, 583, 584, 585, 586 674, 675, 682, 683, 684, 685, 686NOTE 2: CPCPPREP. : PINS REMOVEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-220-009MRB 575107-01-1

T 12 YEI 6 YE

ALL575107-01-1 TRAILING EDGE SPOILER 2-5 FITTINGSNT DI Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,SPOILERS 2,3,4 AND 5 ACTUATOR AND HINGE FITTINGSPREP.: FLAP EXTENSION SPOILER EXTENSIONNOTE : WORKING WITH ZONE : 575, 583, 584, 585, 586 675, 683, 684, 685, 686


AMM 575100/6AMT 575100-220-010MRB 575107-02-2NTM 57-51-07

T 48 000 CYI 12 300 CY

ALL575107-02-2 TRAILING EDGE SPOILER 2-5 FITTINGSNT SDI Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,TRAILING EDGE, SPOILERS 2,3,4 AND 5 ACTUATOR ANDHINGE FITTINGSNOTE 1 : SAMPLING 20%NOTE 2 : WORKING WITH ZONE : 575, 583, 584, 585, 586 675, 683, 684, 685, 686PREP . : FLAPS EXTENDED; SPOILERS EXTENDED;



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-220-001MRB 575119-01-2

T 30 500 CYT 12 YEI 16 500 CYI 12 YE

ALL575119-01-2 TRAILING EDGE AILERON HINGE FITTINGS575 DI590675690

Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMESNOTE 1 : 100% LIMIT = 12 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :

575AT 575JB 575KB 575LB 575MB 675AT 675JB675KB 675LB 675MB



AMM 575100/6AMT 575100-220-002MRB 575120-01-3

T 48 000 CYI 12 300 CY

ALL575120-01-3 TRAILING EDGE AILERON HINGE PINS575 DI590675690

Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,AILERON HINGE PINS 1 TO 5PREP. : PINS REMOVEDNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 575120-02-2NOTE 2: SAMPLING 20%Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-220-013MRB 575120-02-2NTM 57-51-20

T 48 000 CYI 16 400 CY

ALL575120-02-2 TRAILING EDGE AILERON HINGE PINS575 SDI590675690

Y

SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING,TRAILING EDGE, AILERON HINGE PINS 1 TO 5PREP. : PINS REMOVEDNOTE 1: THIS TASK IS AN ALTERNATIVE TO TASK 575120-01-3NOTE 2: SAMPLING 20%Access panels :




AMM 575100/6AMT 575100-220-016MRB 575120-03-1

T 12 YEI 90 MO

ALL575120-03-1 TRAILING EDGE AILERON HINGE PINS575 DI590675690

Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,AILERON HINGE PINS 1 TO 5PREP.: PINS REMOVEDNOTE : CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-220-003MRB 575121-01-2

T 30 000 CYT 6 YEI 25 000 CYI 6 YE

ALL575121-01-2 TRAILING EDGE AILERON ACTUATOR FITTING575 DI590675690

Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,AILERON, INBOARD AND OUTBOARD ACTUATOR FITTINGSNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

575KB 575LB 675KB 675LB0.00Total access time : Hrs


AMM 575100/6AMT 575100-200-003MRB 575140-01-1

T 30 000 CYT 12 YEI 15 000 CYI 12 YE

ALL575140-01-1 FLAP TRACK 1147 DI148

Y

DETAILED INSPECTION OF FLAP TRACK 1, INCLUDINGATTACHMENT BRACKETS TO FUSELAGE, STRUT, CARRIAGE ANDSWINGING LINK (PENDULUM), LH/RHPREP. : FLAP EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

191ET 192ET 193AT 194AT 734 7440.24Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-200-004MRB 575142-01-1

T 24 000 CYT 10 YEI 15 000 CYI 10 YE

ALL575142-01-1 INBOARD FLAP ACTUATOR DRIVE ARM147 DI148

Y

DETAILED INSPECTION OF INBOARD FLAP, INBOARD ACTUATORDRIVE ARM, DRIVE STRUT AND OUTER PART OF TRUNNION, LH/RHPREP. : FLAP EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :



AMM 575100/6AMT 575100-200-005MRB 575150-01-2

T 12 YEI 6 YE

ALL575150-01-2 OUTER WING MLG SUPPORT RIBS571 DI671

Y

DETAILED INSPECTION OF OUTER WING, MLG SUPPORT RIB 5,OUTBOARD AND INBOARD FACESNOTE : CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-200-006MRB 575151-01-3

T 46 700 FHT 30 000 CYI 9 200 FHI 5 900 CY

ALL575151-01-3 TRAILING EDGE FALSE REAR SPAR573 DI574673674

Y

DETAILED INSPECTION OF OUTER WING, TRAILING EDGEFALSE REAR SPAR, FORWARD AND AFT FACESNOTE : SAMPLING 20%

Access panels :

573AB 573BB 573CB 574AB 574BB 673AB 673BB673CB 674AB 674BB



AMM 575100/6AMT 575100-200-010MRB 575166-01-3

T 60 000 FHT 48 000 CYI 10 000 FHI 5 900 CY

ALL575166-01-3 OUTER WING FALSE REAR SPAR LWR FLANGE574 DI674

Y

DETAILED INSPECTION OF OUTER WING, FALSE REAR SPAR,FORWARD FACE, LOWER FLANGE, BETWEEN RIB 7 AND RIB 9NOTE : SAMPLING 20%

Access panels :

573BB 573CB 573DB 573EB 673BB 673CB 673DB673EB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575100/6AMT 575100-200-011MRB 575167-01-1

T 6 YEI 6 YE

ALL575167-01-1 OUTER WING BOTTOM SKIN UPPER SURFACE574 DI674

Y

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN PANELNO. 3, UPPER SURFACE, BETWEEN REAR SPAR AND FALSEREAR SPAR, AND BETWEEN GEAR SUPPORT RIB 5 AND RIB 8.TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2NOTE: CPCPAccess panels :



AD 2012-0032ISB 57-1168

I 500 CY ALL575171-01-4 MAIN LANDING GEAR SUPPORT RIB 5 LUGS730 DI740

Y

MAIN LANDING GEAR SUPPORT RIB 5 LUGSDETAILED INSPECTION OF MAIN LANDING GEAR SUPPORTRIB 5 LUGS.NOTE 1: FOR THRESHOLD REFER TO ISB 57-1168.NOTE 2: RII TASKAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AD 2008-05-12AMM 575200/6AMT 575200-210-010EAD 2010-0209ISB 57-1133

I 4 000 FH 22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

42134277

4311

4315

575221-02-1 FLAPS581 DI681

Y

DETAILED INSPECTION OF INBOARD FLAP TRUNNION ANDSLIDING PANELPREP.: FLAPS EXTENDED;NOTE : CREDIT CAN BE TAKEN FROM LAST ACCOMPLISHMENT OF SB 57-1133

Access panels :

193AB 193BB 194AB 194BB 195AB 195BB 734744



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


AMM 575200/6AMT 575200-210-001MRB 575223-01-1

T 30 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575223-01-1 INBOARD DOUBLE SLOTTED FLAP TRUNNION581 DI681

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,TRUNNION ATTACHMENT BRACKET, INCLUDING INBOARDTRUNNION, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575223-02-1.TPS : TPS MUST NOT BE APPLIEDPREP. : RUBBER SEALS FLAP EXTENSIONNOTE 2: 100% LIMIT = 24 YENOTE 3: CPCPNOTE 4: SAMPLING 20%Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-220-009MRB 575223-02-1NTM 57-52-23

T 30 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575223-02-1 INBOARD DOUBLE SLOTTED FLAP TRUNNION581 SDI681

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARDDOUBLE-SLOTTED FLAP, TRUNNION ATTACHMENT BRACKET,INCLUDING INBOARD TRUNNION, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575223-01-1.TPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% LIMIT = 24 YENOTE 3: CPCPNOTE 4: SAMPLING 20%PREP. : FLAP EXTENSIONAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-210-002MRB 575225-01-1

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575225-01-1 INBOARD DOUBLE SLOTTED FLAP DRIVE531 DI581631681

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,DRIVE STRUT FOR FLAP AND DRIVE LEVER FOR FLAP TRACKFAIRING, INCLUDING ATTACHMENT BRACKETS TO THE FLAP ATTRACK 2, LH/RHPREP. : FLAP EXTENSIONNOTE 1: 100% LIMIT = 12 YENOTE 2: CPCPNOTE 3: SAMPLING 20%PREP. : FLAP EXTENSIONAccess panels :

531AT 531CB 631AT 631CB0.00Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-220-010MRB 575226-01-1NTM 57-52-26

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575226-01-1 INBD DOUBLE SLOTTED FLAP INTL BRACK581 SDI681

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARDDOUBLE-SLOTTED FLAP, INTERNAL BRACKETS AT TRACK 2,LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLESTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAPS EXTENDED;NOTE 2: 100% THRESHOLD = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :

531AT 531CB 581AB 631AT 631CB 681AB0.00Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-210-003MRB 575227-01-1

T 32 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575227-01-1 INBD DOUBLE SLOTTED FLAP FLAP/CARRIAGE531 DI581631681

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,FLAP TO CARRIAGE ATTACHMENT BRACKET AT TRACK 2, LH/RHPREP. : RUBBER SEALS FLAP EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPPREP. : FLAP EXTENSIONAccess panels :



AMM 575200/6AMT 575200-210-004MRB 575229-01-1

T 32 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575229-01-1 INBD DOUBLE SLOTTED FLAP PYLON FAIR AT477 DI487581681

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,ATTACHMENT BRACKET OF PYLON AFT FAIRING, INCLUDINGSURROUNDING SKIN, LH/RHPREP. : PYLON FAIRINGS REMOVEDNOTE 1: 100% LIMIT = 20 YENOTE 2: SAMPLING 20%NOTE 3: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-220-011MRB 575230-01-1NTM 57-52-30

T 32 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575230-01-1 INBD DOUBLE SLOTTED FLP INT SUPP BRACK581 SDI681

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) INBOARDDOUBLE-SLOTTED FLAP, INTERNAL SUPPORT BRACKETS PYLONAFT FAIRING ATTACHMENT, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLESTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 575200/6AMT 575200-210-005MRB 575231-01-1

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575231-01-1 INBOARD DOUBLE SLOTTED FLAP END RIB581 DI681

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,END RIB, INCLUDING INTERCONNECTION STRUT ATTACHMENTBRACKET AND LEVER, LH/RHPREP. : RUBBER SEALS FLAP EXTENSIONNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-210-006MRB 575233-01-1

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575233-01-1 INBOARD DOUBLE SLOTTED FLAP TAB DRIVE535 DI572635672

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,TAB DRIVE ASSEMBLY AND ARTICULATION AT RIB 3, LH/RHPREP. : FLAP EXTENSIONNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :



AMM 575200/6AMT 575200-210-007MRB 575235-01-1

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575235-01-1 INBOARD DOUBLE SLOTTED FLAP TAB ARTIC535 DI635

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,TAB ARTICULATION AT RIB 6, LH/RHPREP. : FLAP EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-210-008MRB 575237-01-1

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575237-01-1 INBOARD DOUBLE SLOTTED FLAP TAB DRIBE531 DI631

Y

DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,TAB DRIVE STRUT AND ARTICULATION AT RIB 9, LH/RHPREP. : FLAP EXTENSIONNOTE 1 : 100% LIMIT = 24 YENOTE 2 : SAMPLING 20%NOTE 3 : CPCPAccess panels :



AMM 575200/6AMT 575200-220-012MRB 575239-01-1NTM 57-52-39

T 48 000 CYT 10 YEI 20 000 CYI 10 YE

ALL575239-01-1 INBOARD DOUBLE SLOTTED FLAP RIB 3581 SDI681

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARDDOUBLE-SLOTTED FLAP, RIB 3, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLESTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-220-013MRB 575241-01-1NTM 57-52-41

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575241-01-1 INBOARD DOUBLE SLOTTED FLAP RIB 6581 SDI681

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARDDOUBLE-SLOTTED FLAP, RIB 6, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLESTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% LIMIT = 24 YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 575200/6AMT 575200-200-005MRB 575250-01-1

T 24 YEI 12 YE

ALL575250-01-1 INBOARD FLAP TRACK 2 CARRIAGE500 DI600

Y

DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK2 CARRIAGE FORGINGPREP. : FLAP EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMM 575200/6AMT 575200-220-004MRB 575250-02-2NTM 57-52-50

T 48 000 CYI 16 400 CY

ALL575250-02-2 INBOARD FLAP TRACK 2 CARRIAGE500 SDI600

Y

SPECIAL DETAILED INSPECTION (U/S) OF OUTER WING,INBOARD FLAP TRACK 2 CARRIAGE FORGINGNOTE : SAMPLING 20%PREP. : FLAP EXTENSION


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-200-001MRB 575251-01-2

T 36 000 CYI 7 000 CY

ALL575251-01-2 INBOARD FLAP TRACK 2 ROLLERS500 DI600

Y

DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK2 CARRIAGE ROLLERSPREP. : FLAP EXTENSIONNOTE : SAMPLING 20%


AMM 575200/6AMT 575200-220-007MRB 575252-01-2NTM 57-52-52

T 48 000 CYI 12 300 CY

ALL575252-01-2 INBOARD FLAP TRACK 2 BOLT ASSEMBLY531 SDI631

Y

SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING,INBOARD FLAP TRACK 2 FLAP PIVOT BOLT ASSEMBLYPREP.: INNER BOLT REMOVED FLAP EXTENSIONNOTE : SAMPLING 20%


AMM 575200/6AMT 575200-200-006MRB 575254-01-1

T 6 YEI 6 YE

ALL575254-01-1 INBOARD FLAP TRACK 2 DRIVE LEVER531 DI631

Y

DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK2, DRIVE LEVERTPS : TPS MUST NOT BE APPLIEDPREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%NOTE 3: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575200/6AMT 575200-220-005MRB 575254-02-2NTM 57-52-54

T 48 000 CYI 12 700 CY

ALL575254-02-2 INBOARD FLAP TRACK 2 DRIVE LEVER531 SDI631

Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,INBOARD FLAP TRACK 2, DRIVE LEVERPREP.: FLAP EXTENSION SPOILER EXTENSIONNOTE : SAMPLING 20%


AMM 575300/6AMT 575300-220-021MRB 575323-01-1NTM 57-53-23

T 30 000 CYT 12 YEI 15 000 CYI 12 YE

ALL575323-01-1 OUTBOARD DOUBLE SLOTTED FLAP TAB587 SDI687

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE SLOTTED FLAP TAB FRONT SPAR, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLESTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-001MRB 575327-01-1

T 30 000 CYT 12 YEI 17 100 CYI 12 YE

ALL575327-01-1 OUTBD DOUBLE SLOTTED FLAP INBOARD RIB587 DI687

Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,INBOARD RIB, INCLUDING INTERCONNECTION STRUTATTACHMENT BRACKET, LEVER AND ROLLER, INTERNAL ANDEXTERNAL, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575327-02-1.TPS : TPS MUST NOT BE APPLIEDPREP. : RUBBER SEALS FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 12YENOTE 3: SAMPLING 20%NOTE 4: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-014MRB 575327-02-1NTM 57-53-27

T 30 000 CYT 12 YEI 17 100 CYI 12 YE

ALL575327-02-1 OUTBD DOUBLE SLOTTED FLAP INBOARD RIB587 SDI687

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE-SLOTTED FLAP, INBOARD RIB, INCLUDINGINTERCONNECTION STRUT ATTACHMENT BRACKET, LEVER ANDROLLER, INTERNAL AND EXTERNAL, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES. THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575327-01-1.TPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED RUBBER SEALS FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 12YENOTE 3: SAMPLING 20%NOTE 4: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-002MRB 575329-01-1

T 30 000 CYT 12 YEI 17 900 CYI 12 YE

22552261

2267

23032480

575329-01-1 OUTBD DOUBLE SLOTTED FLAP INTL SUPP532 DI587632687

Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,INTERNAL SUPPORT FITTING AT TRACK 3, INCLUDINGATTACHMENT BRACKET, DRIVE BRACKET AND ATTACHMENTSTRUCTURE, INTERNAL AND EXTERNAL, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575329-02-1.TPS : TPS MUST NOT BE APPLIEDPREP. : FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-015MRB 575329-02-1NTM 57-53-29

T 30 000 CYT 12 YEI 17 900 CYI 12 YE

22552261

2267

23032480

575329-02-1 OUTBD DOUBLE SLOTTED FLAP INTL SUPP533 SDI587633687

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE-SLOTTED FLAP, INTERNAL SUPPORT FITTING ATTRACK 3 INCLUDING ATTACHMENT BRACKET, DRIVE BRACKETAND ATTACHMENT STRUCTURE, INTERNAL AND EXTERNAL,LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES. THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575329-01-1.TPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 575300-210-002MRB 575329-03-1

T 30 000 CYT 12 YEI 17 900 CYI 12 YE

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715164

5241

5247

575329-03-1 OUTBD DOUBLE SLOTTED FLAP INTL SUPP532 DI587632687

YR

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,INTERNAL SUPPORT FITTING AT TRACK 3 INCLUDINGATTACHMENT BRACKET, DRIVE BRACKET AND ATTACHMENTSTRUCTURE, INTERNAL AND EXTERNAL, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575329-04-1NOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPTPS : TPS MUST NOT BE APPLIEDPREP. : FLAPS EXTENDED;


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

55555699

5709

59165958

5994

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 575300-220-015MRB 575329-04-1NTM 57-53-29

T 30 000 CYT 12 YEI 17 900 CYI 12 YE

29743005

3013

30223198

3315

33553600

3737

38623964

3966

41364213

4277

43114315

4669

47034737

4783

48264863

4945

49715164

5241

5247

575329-04-1 OUTBOARD DOUBLE-SLOTTED FLAP532 SDI587632687

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE-SLOTTED FLAP, INTERNAL SUPPORT FITTING ATTRACK 3 INCLUDING ATTACHMENT BRACKET, DRIVE BRACKETAND ATTACHMENT STRUCTURE, INTERNAL AND EXTERNAL,LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES. THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575329-03-1.NOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED; FLAPS EXTENDED;


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5251

5275

52975306

5340

53435385

5392

54185427

5438

54565469

5495

5555

Access panels :

532AT 532CB0.10Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-003MRB 575331-01-1

T 30 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575331-01-1 OUTBD DOUBLE SLOTTED FLAP DRIVE LINK532 DI632

Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,DRIVE LINKAGE AND DRIVE FITTING AT TRACK 3, LH/RHPREP. : FLAP EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-004MRB 575333-01-1

T 30 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575333-01-1 OUTBD DOUBLE SLOTTED FLAP INTL SUPP533 DI587633687

Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,INTERNAL SUPPORT FITTING AT TRACK 4, INCLUDINGPENDULUM SUPPORT, DRIVE BRACKET AND ATTACHMENTSTRUCTURE, INTERNAL AND EXTERNAL, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575333-02-1.TPS : TPS MUST NOT BE APPLIEDPREP. : FLAP EXTENSIONNOTE 1: 100% THRESHOLD = 90MONOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

533AT 533CB 587BB 633AT 633CB 687BB0.16Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-016MRB 575333-02-1NTM 57-53-33

T 30 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575333-02-1 OUTBD DOUBLE SLOTTED FLAP INTL SUPP533 SDI587633687

Y

SPECIAL DETAILED INSPECTION (EN) OF OUTBOARDDOUBLE-SLOTTED FLAP, INTERNAL SUPPORT FITTING ATTRACK 4, INCLUDING PENDULUM SUPPORT, DRIVE BRACKETAND ATTACHMENT STRUCTURE, INTERNAL AND EXTERNAL,LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES. THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575333-01-1.NOTE 2: SAMPLING 20%NOTE 3: 100% THRESHOLD = 90MONOTE 4: CPCPTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONAccess panels :

533AT 533CB 587BB 633AT 633CB 687BB0.16Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-005MRB 575335-01-1

T 30 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575335-01-1 OUTBD DOUBLE SLOTTED FLAP DRIVE LINK533 DI633

Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,DRIVE LINKAGE AND DRIVE FITTING AT TRACK 4, LH/RHPREP. : FLAP EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-006MRB 575337-01-1

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575337-01-1 OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC537 DI538539587637638639687

Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,TAB ARTICULATION AT STATIONS 3 A, 3 B, 3 C, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575337-02-1.TPS : TPS MUST NOT BE APPLIEDPREP. : FLAP EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCPAccess panels :

537AB 537BB 537CB 538AB 538BB 538CB 539AB539BB 539CB 637AB 637BB 637CB 638AB 638BB638CB 639AB 639BB 639CB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-017MRB 575337-02-1NTM 57-53-37

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575337-02-1 OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC537 SDI538539587637638639687

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE-SLOTTED FLAP, TAB ARTICULATION AT STATIONS 3A, 3 B, 3 C, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES. THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575337-01-1.TPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :

537AB 537BB 537CB 538AB 538BB 538CB 539AB539BB 539CB 637AB 637BB 637CB 638AB 638BB638CB 639AB 639BB 639CB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-007MRB 575339-01-1

T 30 000 CYT 12 YEI 20 000 CYI 12 YE


Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,TAB ARTICULATION AT TRACK 3, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575339-02-1.TPS : TPS MUST NOT BE APPLIEDPREP. : FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-018MRB 575339-02-1NTM 57-53-39

T 30 000 CYT 12 YEI 20 000 CYI 12 YE


Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE-SLOTTED FLAP, TAB ARTICULATION AT TRACK 3,LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES. THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575339-01-1.TPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-210-008MRB 575341-01-1

T 30 000 CYT 12 YEI 20 000 CYI 12 YE


Y

DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,TAB ARTICULATION AT TRACK 4, LH/RHNOTE 1: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575341-02-1.TPS : TPS MUST NOT BE APPLIEDPREP. : FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-019MRB 575341-02-1NTM 57-53-41

T 30 000 CYT 12 YEI 20 000 CYI 12 YE


Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE-SLOTTED FLAP, TAB ARTICULATION AT TRACK 4,LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLES. THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK 575341-01-1.TPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCPAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-020MRB 575343-01-1NTM 57-53-43

T 48 000 CYT 12 YEI 20 000 CYI 12 YE

ALL575343-01-1 OUTBD DOUBLE SLOTTED FLAP RIB 2, 9, 12587 SDI687

Y

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARDDOUBLE-SLOTTED FLAP, RIB 2, 9 AND 12, LH/RHNOTE 1: INSPECTION IS THROUGH INSPECTION HOLESTPS : TPS MUST NOT BE APPLIEDPREP. : COVER TAPES FROM INSPECTION HOLES REMOVED FLAP EXTENSIONNOTE 2: 100% THRESHOLD = 24YENOTE 3: SAMPLING 20%NOTE 4: CPCP


AMM 575300/6AMT 575300-200-009MRB 575350-01-1

T 12 YEI 12 YE

ALL575350-01-1 OUTBOARD FLAP TACK 3-4 CARRIAGE532 DI533632633

Y

DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK3 AND 4 CARRIAGE FORGINGSPREP. : FLAP EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-220-006MRB 575350-02-2NTM 575350

T 48 000 CYI 16 400 CY

ALL575350-02-2 OUTBOARD FLAP TACK 3-4 CARRIAGE532 SDI533632633

Y

SPECIAL DETAILED INSPECTION (US) OF OUTER WINGOUTBOARD FLAP TRACK 3 AND 4 CARRIAGE FORGINGSPREP.: FLAPS EXTENDED;NOTE : SAMPLING 20%


AMM 575300/6AMT 575300-200-001MRB 575351-01-2

T 36 000 CYI 20 000 CY

ALL575351-01-2 OUTBOARD FLAP TRACK 3-4 ROLLERS500 DI600

Y

DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK3 AND 4 CARRIAGE ROLLERSPREP.: FLAP EXTENSIONNOTE : SAMPLING 20%


AMM 575300/6AMT 575300-220-007MRB 575352-01-2NTM 57-53-52

T 36 000 CYI 15 000 CY

ALL575352-01-2 OUTBOARD FLAP TRACK 3-4 BOLT ASSEMBLY532 SDI533632633

Y

SPECIAL DETAILED INSPECTION (MPI) OF OUTER WINGOUTBOARD FLAP TRACK 3 AND 4 FLAP PIVOT BOLT ASSEMBLYPREP.: INNER BOLT REMOVED FLAP EXTENSIONNOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 575300/6AMT 575300-200-010MRB 575354-01-1

T 6 YEI 6 YE

ALL575354-01-1 OUTBOARD FLAP TRACK 3-4 DRIVE LEVERS532 DI533632633

Y

DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK3 AND 4 DRIVE LEVERSTPS : TPS MUST NOT BE APPLIEDPREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%NOTE 3: CPCP


AMM 575300/6AMT 575300-220-008MRB 575354-02-2NTM 575354

T 48 000 CYI 16 400 CY

ALL575354-02-2 OUTBOARD FLAP TRACK3-4 DRIVE LEVERS532 SDI533632633

Y

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WINGOUTBOARD FLAP TRACK 3 AND 4 DRIVE LEVERSPREP.: FLAP EXTENSION SPOILER EXTENSIONNOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 576000/6AMT 576000-200-003MRB 576104-01-1

T 12 YEI 12 YE

22552261

2267

23032480

2974

30053013

3022

3198

576104-01-1 AILERON SKIN ATTACH TO TRAILING EDGE500 DI600

Y

DETAILED INSPECTION OF AILERON, UPPER AND LOWEREXTERNAL SKINS AT ATTACHMENT TO TRAILING EDGE,INBOARD AND OUTBOARD EDGES, SPARS AND RIBS


AMM 576000/6AMT 576000-210-001MRB 576106-01-1

T 12 YEI 12 YE

ALL576106-01-1 AILERON UPPER AND LOWER SKINS500 DI600

Y

DETAILED INSPECTION OF AILERON, UPPER AND LOWERSKINS, EXTERNAL SURFACENOTE : 100% THRESHOLD = 24YENOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 576000-200-005MRB 576107-01-1

T 6 YEI 6 YE

33153355

3600

37373862

3964

39664136

4213

42774311

4315

46694703

4737

47834826

4863

49454971

5164

52415247

5251

52755297

5306

5340

576107-01-1 AILERON UPPER AND LOWER EXTERNAL SKINS500 DI600

YR

DETAILED INSPECTION OF AILERON UPPER AND LOWEREXTERNAL SKINS AT ATTACHMENT TO TRAILING EDGE ANDOUTBOARD CLOSING RIB


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5343

5385

53925418

5427

54385456

5469

54955555

5699

57095916

5958

5994



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 577100/6AMT 577100-200-001MRB 577001-01-2

T 48 000 CYI 16 400 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

577001-01-2 SPOILER 1 FITTING500 DI600

YR

DETAILED INSPECTION OF SPOILER 1, CENTER HINGEFITTING AND ACTUATOR BRACKETNOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 577001-02-2PREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 2: 100% THRESHOLD = 20YENOTE 3: SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


AMM 577100/6AMT 577100-200-001MRB 577001-01-4

T 48 000 CYI 15 300 CY

2974

3005

30133022

3198

33153355

3737

38623964

3966

41364213

4277

43114315

5164

52415247

5297

53435427

577001-01-4 SPOILER 1 FITTING500 DI600

Y

DETAILED INSPECTION OF SPOILER 1, CENTER HINGEFITTING AND ACTUATOR BRACKETNOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 577001-02-3PREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 2: 100% THRESHOLD = 20YENOTE 3: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMT 577100-200-001T 24 YEI 12 YE

ALL577001-01-6 SPOILER 1 FITTING500 DI600

Y

SPOILER 1 FITTINGDETAILED INSPECTION OF SPOILER 1, CENTER HINGEFITTING AND ACTUATOR BRACKETPREP: FLAPS AND SPOILERS EXTENDED;



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 577100/6AMT 577100-220-001MRB 577001-02-2NTM 57-70-01

T 48 000 CYI 16 400 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

577001-02-2 SPOILERS 1 FITTING500 SDI600

Y

SPECIAL DETAILED INSPECTION (HFEC) OF SPOILER 1,ACTUATOR BRACKETNOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 577001-01-2PREP. : PINS REMOVED FLAP EXTENSION SPOILERS EXTENSIONNOTE 2: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 577100/6AMT 577100-220-001MRB 577001-02-3NTM 57-70-01

T 48 000 CYI 15 300 CY

29743005

3013

30223198

3315

33553737

3862

39643966

4136

42134277

4311

43155164

5241

52475297

5343

5427

577001-02-3 SPOILERS 1 FITTING500 SDI600

Y

SPECIAL DETAILED INSPECTION (HFEC) OF SPOILER 1,ACTUATOR BRACKETNOTE 1: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 577001-01-4PREP. : PINS REMOVED FLAP EXTENSION SPOILER EXTENSIONNOTE 2: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 577100/6AMT 577100-200-002MRB 577002-01-1

T 12 YEI 12 YE

ALL577002-01-1 SPOILER 1 SKINS OF CENTER FITTING500 DI600

Y

DETAILED INSPECTION OF SPOILER 1, UPPER AND LOWERSKINS, IN REGION OF CENTER HINGE FITTINGPREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%


AMM 577100/6AMT 577100-200-003MRB 577003-01-1

T 12 YEI 12 YE

ALL577003-01-1 SPOILER 1 SKINS AT TRAILING EDGE500 DI600

Y

DETAILED INSPECTION OF SPOILER 1, UPPER AND LOWERSKINS, AT TRAILING EDGE AND INBOARD AND OUTBOARDEDGESPREP. : SPOILER EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%


AMM 577200/6AMT 577200-200-002MRB 577006-01-1

T 12 YEI 12 YE

ALL577006-01-1 SPOILER 2-5 CENTRE FITTING500 DI600

Y

DETAILED INSPECTION OF SPOILER 2,3,4 AND 5, CENTERHINGE FITTINGSPREP.: FLAP EXTENSION SPOILER EXTENSIONNOTE : CPCP



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 577200/6AMT 577200-200-004MRB 577006-02-2NTM 57-70-06

T 48 000 CYI 16 400 CY

22552261

2267

23032480

3600

46694703

4737

47834826

4863

49454971

5251

52755306

5340

53855392

5418

54385456

5495

55555699

5916

5958

577006-02-2 SPOILER 2-5 CENTRE FITTING500 SDI600

YR

SPECIAL DETAILED INSPECTION (HFEC AND US) OF SPOILER2, 3, 4 AND 5, CENTER HINGE FITTINGSPREP. : PINS REMOVED; FLAPS EXTENDED; SPOILERS EXTENDED;NOTE : SAMPLING 20%


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

Skills :AF1 2.00 MHrsNDT1 2.00 MHrs

AMM 577200/6AMT 577200-200-004MRB 577006-02-3NTM 57-70-06

T 48 000 CYI 15 300 CY

2974

3005

30133022

3198

33153355

3737

38623964

3966

41364213

4277

43114315

5164

52415247

5297

53435427

577006-02-3 SPOILER 2-5 CENTRE FITTING500 SDI600

Y

SPECIAL DETAILED INSPECTION (HFEC AND US) OF SPOILER2, 3, 4 AND 5, CENTER HINGE FITTINGSPREP. : PINS REMOVED; FLAPS EXTENDED; SPOILERS EXTENDED;NOTE : SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 577500/6AMT 577500-200-001MRB 577007-01-1

T 12 YEI 12 YE

ALL577007-01-1 SPOILER 2-5 SKINS OF CENTER FITTING500 DI600

Y

DETAILED INSPECTION OF SPOILER 2,3,4 AND 5, UPPER ANDLOWER SKINS IN REGION OF CENTER HINGE FITTINGPREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 1: 100% THRESHOLD = 24YENOTE 2: SAMPLING 20%


AMM 577200/6AMT 577200-200-003MRB 577008-01-1

T 12 YEI 12 YE

ALL577008-01-1 SPOILER 2-5 SKINS AT TRAILING EDGE500 DI600

Y

DETAILED INSPECTION OF SPOILER 2,3,4 AND 5, UPPER ANDLOWER SKINS AT TRAILING EDGE AND INBOARD AND OUTBOARDEDGESPREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 577100/6AMT 577100-210-001MRB 577009-01-1

T 12 YEI 12 YE

ALL577009-01-1 SPOILERS 1 TO 5 EXTERNAL SURFACE500 DI600

Y

DETAILED INSPECTION OF SPOILERS 1 TO 5, UPPER ANDLOWER SKINS, EXTERNAL SURFACEPREP. : FLAP EXTENSION SPOILER EXTENSIONNOTE 1: 100% LIMIT = 24 YENOTE 2: SAMPLING 20%



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 712112/6AMT 712112-200-013MRB 712111-04-1

T 12 YEI 12 YE

See note

ALL712111-04-1 FORWARD ENGINE MOUNT435 DI436445446451461

Y

DETAILED INSPECTION OF FORWARD ENGINE MOUNTINSTALLATIONNOTE 1: ACCOMPLISHMENT OF THIS INSPECTION TO BE PERFORMED WITH A MAXIMUM INTERVAL OF 12 YEARS BETWEEN MOUNT DISASSEMBLYTPS : TPS MUST NOT BE APPLIEDPREP. : ENGINE MOUNT DISASSEMBLED ENGINE REMOVALNOTE 2: CPCPAccess panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 712211/6AMT 712211-200-012MRB 712211-02-1

T 12 YEI 12 YE

See note


Y

DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATIONNOTE 1: ACCOMPLISHMENT OF THIS INSPECTION TO BE PERFORMED WITH A MAXIMUM INTERVAL OF 10 YEARS BETWEEN MOUNT DISASSEMBLYTPS : TPS MUST NOT BE APPLIEDPREP. : ENGINE MOUNT DISASSEMBLED ENGINE REMOVALNOTE 2: CPCPAccess panels :





: : :

: :

1412/09/2013

01



Date : SEP 2013 LIST OF EFFECTIVE PAGES - ZNL Page : 1


LEP R 1 SEP 2013

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : ZL ZONAL CARD


Threshold Interval

Ctrl References Eff

AMT 052530-200-008I 24 MO ALLZL-535-01-2 FLAP TAB HINGE AND FAIRING NO. 1A535 GVI635

N

GENERAL VISUAL INSPECTION OF FLAP TAB HINGE ANDFAIRING NO. 1A (EWIS)NOTE: IN CASE TASK THRESHOLD/INTERVAL IS OVER DUE WHEN APPLYING CHANGES OFAMSS ISS 14 AMD 00, THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT 2A CHECK.Access panels :

535CB 635CB0.44Total access time : Hrs


AMT 052530-200-010I 24 MO ALLZL-537-01-2 FLAP TAB HINGE AND FAIRING NO. 3A537 GVI637

N

GENERAL VISUAL INSPECTION OF FLAP TAB HINGE ANDFAIRING NO. 3A (EWIS)NOTE: THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT 2A CHECK.Access panels :

537AB 537CB 637AB 637CB0.08Total access time : Hrs


Date ATA ZLDate 22/01/2014Amendment NoIssue No Page ZNL - ZL [1 / 2] :

: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : ZL ZONAL CARD


Threshold Interval

Ctrl References Eff

AMT 052530-200-011I 24 MO ALLZL-538-01-2 FLAP TAB HINGE AND FAIRING NO. 3B538 GVI638

N

GENERAL VISUAL INSPECTION OF FLAP TAB HINGE ANDFAIRING NO. 3B (EWIS)NOTE: THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT 2A CHECKAccess panels :



AMT 052530-200-012I 24 MO ALLZL-539-01-2 FLAP TAB HINGE AND FAIRING NO. 3C539 GVI639

N

GENERAL VISUAL INSPECTION OF FLAP TAB HINGE ANDFAIRING NO. 3C (EWIS)NOTE: THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMS ISS 14AMD 00 EFFECTIVE DATE IS NEXT 2A CHECKAccess panels :



Date ATA ZLDate 22/01/2014Amendment NoIssue No Page ZNL - ZL [2 / 2] :

: : :

: :

1412/09/2013

01

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 05 MAINTENANCE CHECKS


Threshold Interval

Ctrl References Eff

AMM 052100/6AMT 052100-200-002MRB ZL-100-02-3MRB 531109-01-2MRB 531115-01-1MRB 531116-01-1MRB 531119-02-1MRB 531172-02-1MRB 532137-02-1MRB 532165-01-6MRB 534108-01-1MRB 534131-01-2MRB 534176-02-1

I 4 MO ALLZL-100-02-3 LOWER HALF OF FUSELAGE100 GVI Y

GENERAL VISUAL INSPECTION OF LOWER HALF OF FUSELAGE.


AMM 052110/6AMT 052110-200-001MRB ZL-110-01-1

I 48 MO

2CCheck :

ALLZL-110-01-1 RADOME110 GVI Y

GENERAL VISUAL INSPECTION OF RADOME (EWIS)

Access panels :



Date ATA 05Date 22/01/2014Amendment NoIssue No Page ZNL - 05 [1 / 76] :

: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052120/6AMT 052120-200-001MRB ZL-121-01-1

I 24 MO

CCheck :

ALLZL-121-01-1 AVIONICS COMPARTMENT121 GVI122

Y

GENERAL VISUAL INSPECTION OF AVIONICCOMPARTMENT (EWIS)Access panels :



AMM 052120/6AMT 052120-200-007MRB ZL-121-02-1MRB 21.21.00/03MRB 27.21.00/08

I 6 YE ALLZL-121-02-1 AVIONICS COMPARTMENT121 GVI122

Y

GENERAL VISUAL INSPECTION OF AVIONICCOMPARTMENT (EWIS)PREP. : INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052120/6AMT 052120-200-012MRB ZL-123-02-1

I 4 MO ALLZL-123-02-1 NOSE LANDING GEAR WELL123 GVI Y

GENERAL VISUAL INSPECTION OF THE NOSE GEAR WELL (EWIS)

Access panels :



AMM 052120/6AMT 052120-200-003AMT 052120-200-008MRB ZL-125-01-2

I 24 MO ALLZL-125-01-2 LATERAL AVIONICS COMPARTMENT125 GVI126129

Y

GENERAL VISUAL INSPECTION OF LATERAL AVIONICCOMPARTMENT (EWIS)PREP: 813 IF INSTALLEDAccess panels :

125AL 812 8220.06Total access time : Hrs

Skills :AF1 0.40 MHrsB21 0.00 MHrsMEC1 0.20 MHrs


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052120/6AMT 052120-200-008MRB ZL-125-02-1MRB 212100/03MRB 253000/02MRB 351000/06

I 24 000 FHI 6 YE

ALLZL-125-02-1 LATERAL AVIONICS COMPARTMENT125 GVI126

Y

GENERAL VISUAL INSPECTION OF LATERAL AVIONICCOMPARTMENT (EWIS)PREP. : INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION 813 IF INSTALLEDAccess panels :



AMM 052120/6AMT 052120-200-005MRB ZL-127-01-1

I 24 MO

CCheck :

ALLZL-127-01-1 REAR AVIONICS COMPARTMENT127 GVI128

Y

GENERAL VISUAL INSPECTION OF REAR AVIONICCOMPARTMENT (EWIS)Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052120/6AMT 052120-200-010MRB ZL-127-02-2MRB 21.21.00/03MRB 21.27.00/04

I 6 YE ALLZL-127-02-2 REAR AVIONICS COMPARTMENT127 GVI128

Y

GENERAL VISUAL INSPECTION OF REAR AVIONICCOMPARTMENT (EWIS)PREP. : INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052130/6AMT 052130-200-001MRB ZL-131-01-2MRB 255000/04MRB 255000/05MRB 255000/06MRB 255000/07MRB 255000/08MRB 532137-02-1


ALLZL-131-01-2 FORWARD CARGO COMPARTMENT131 GVI132

Y

GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT(AS FAR AS VISIBLE IF ACT(S)INSTALLED) (EWIS)............Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052130/6AMT 052130-200-004MRB ZL-131-02-2MRB ZL-131-02-3MRB 212100/03MRB 383200/03

I 24 000 FHI 6 YE

ALLZL-131-02-2 FORWARD CARGO COMPARTMENT131 GVI132

Y

GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT (EWIS)

Access panels :

131FF 131GF 131JF 131KF 131QF 131VF 131WF131YF 131ZF 132FF 132GF 132JF 132MW 132QF132RF 132VF 132YF 825



AMM 052130/6AMT 052130-200-006MRB ZL-131-03-2MRB 532103-01-2

I 12 YE ALLZL-131-03-2 FORWARD CARGO COMPARTMENT131 GVI132

Y

GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT (EWIS)PREP. : - CEILING PANELS FROM FR 24 TO FR 35.7 - INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION - SIDEWALL PANELS FROM FR 24 TO FR 35.7Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052130/6AMT 052130-200-002MRB ZL-133-01-4MRB 383200/03

I 24 000 FHI 6 YE

ALLZL-133-01-4 BAY UNDER FWD CARGO COMPARTMENT FLOOR133 GVI134

Y

GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF FWDCARGO COMPARTMENT (EWIS)PREP. : FLOOR PANELS FROM FR 24 TO FR 35.7Access panels :

133AL 134AR 8250.07Total access time : Hrs


AMM 052130/6AMT 052130-200-003MRB ZL-137-01-1MRB 212100/03MRB 215000/08MRB 215000/09MRB 532103-01-1MRB 532103-01-2

I 24 000 FHI 6 YE

ALLZL-137-01-1 BAY BEHIND FWD CARGO COMPARTMENT137 GVI138

Y

GENERAL VISUAL INSPECTION OF BAY BEHIND FWD CARGOCOMPARTMENT (EWIS)PREP : ACT(S) NO.4 AND NO.6 REMOVED (IF INSTALLED) INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION

Access panels :

131NW 131PW 132PW 8250.11Total access time : Hrs



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052140/6AMT 052140-200-001MRB ZL-141-01-1MRB 28.11.00/05MRB 28.11.00/06MRB 28.21.00/07MRB 571150-01-1

I 12 YE ALLZL-141-01-1 WING CENTER BOX141 GVI142

Y

GENERAL VISUAL INSPECTION OF WING CENTER BOX (EWIS)

Access panels :



AMM 052140/6AMT 052140-200-002MRB ZL-145-01-1MRB 212100/03MRB 531900/04

I 6 YE ALLZL-145-01-1 ZONE UNDER CABIN FLOOR145 GVI146

Y

GENERAL VISUAL INSPECTION OF ZONE UNDER CABIN FLOOR (EWIS)PREP. : - FLOOR PANELS FROM FR 36 TO FR 46 - INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTIONAccess panels :




: : :

: :

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AMM 052140/6AMT 052140-200-004MRB ZL-145-02-1MRB 360000/08

I 4 MO ALLZL-147-02-1 MAIN GEAR WELL-HYDRAULICS COMPARTMENT147 GVI148

Y

GENERAL VISUAL INSPECTION OF MLG-WELL AND HYDRAULICCOMPARTMENT (EWIS)

Access panels :



AMM 052140/6AMT 052140-200-005MRB ZL-147-03-1MRB 282200/02MRB 291000/21MRB 291000/31MRB 571150-01-1

I 24 000 FHI 6 YE

ALLZL-147-03-1 MAIN GEAR WELL-HYDRAULICS COMPARTMENT147 GVI148

Y

GENERAL VISUAL INSPECTION OF MLG-WELL AND HYDRAULICCOMPARTMENT (EWIS)

Access panels :

147AB 147EB 734 7440.24Total access time : Hrs



: : :

: :

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AMM 052150/6AMT 052150-200-001MRB ZL-151-01-1MRB 25.50.00/05MRB 25.50.00/06MRB 25.50.00/07MRB 25.50.00/08MRB 25.50.00/09MRB 25.50.00/10MRB 25.50.00/19MRB 25.50.00/22MRB 534157-01-1MRB 534157-01-2MRB 534160-01-1MRB 534160-01-2


ALLZL-151-01-1 AFT CARGO COMPARTMENT151 GVI152

Y

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT(AS FAR AS VISIBLE, IF ACT IS INSTALLED) (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



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AMM 052150/6AMT 052150-200-003MRB ZL-151-02-4MRB 212100/03MRB 253000/02MRB 253000/03MRB 282200/02MRB 360000/09MRB 383200/03

I 24 000 FHI 6 YE

ALLZL-151-02-4 AFT CARGO COMPARTMENT151 GVI152

Y

GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT (EWIS)PREP. : ACT(S) REMOVED (IF INSTALLED);

Access panels :

151AC 151AW 151AY 151BC 151BW 151CW 151DC151DW 151EW 151HW 151JW 151KC 152BW 152CW152DW 152FW 152GW 152HW 152JW 826




: : :

: :

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AMM 052150/6AMT 052150-200-004MRB ZL-151-03-8MRB 534120-01-1

I 12 YE ALLZL-151-03-8 AFT CARGO COMPARTMENT151 GVI152

Y

GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT (EWIS)PREP. : CEILING PANELS FROM FR 46 TO FR 59; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SIDEWALL PANELS FROM FR 47.2 TO FR 59; ACT(S) REMOVED (IF INSTALLED);Access panels :



AMT 052150-200-002MRB ZL-153-01-10MRB 38.32.00/01MRB 38.32.00/03

I 24 000 FHI 6 YE

ALLZL-153-01-10 UNDERFLOOR BAY OF AFT CARGO COMPTMENT153 GVI154

Y

GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF AFTCARGO COMPARTMENT (EWIS)PREP. : FLOOR PANELS FROM FR 47.2 TO FR 59; ACT(S) REMOVED (IF INSTALLED);Access panels :




: : :

: :

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01



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AMM 052160/6AMT 052160-200-001MRB ZL-161-01-1MRB 25.50.00/05

I 750 FHI 4 MO

ALLZL-161-01-1 BULK CARGO COMPARTMENT161 GVI162

Y

GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT(AS FAR AS VISIBLE, IF ACT IS INSTALLED) (EWIS)

Access panels :



AMM 052160/6AMT 052160-200-003MRB ZL-161-02-1MRB 212100/03MRB 282200/02MRB 360000/09

I 24 000 FHI 6 YE


Y

GENERAL VISUAL INSPECTION OF BULK CARGOCOMPARTMENT (EWIS)PREP. : ACT(S) REMOVED (IF INSTALLED);

Access panels :

161AC 161AW 161BW 161CW 162BW 162CW 162EW826




: : :

: :

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01



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AMM 052160/6AMT 052160-200-004MRB ZL-161-03-2MRB 534120-01-1

T 12 YEI 12 YE


Y

GENERAL VISUAL INSPECTION OF BULK CARGOCOMPARTMENT (EWIS)PREP. : CEILING PANELS FROM FR 59 TO FR 65; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SIDEWALL PANELS FROM FR 59 TO FR 65;Access panels :



AMM 052160/6AMT 052160-200-002MRB ZL-163-01-1

I 6 YE ALLZL-163-01-1 UNDERFLOOR BAY OF BULK CARGO COMPT.163 GVI164

Y

GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF BULKCARGO COMPARTMENT (EWIS)PREP. : FLOOR PANELS FROM FR 59 TO FR 65Access panels :




: : :

: :

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I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-171-01-1 AFT CABIN UNDERFLOOR COMPARTMENT171 GVI172

Y

GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOORCOMPARTMENT (EWIS)

Access panels :



AMM 052170/6AMT 052170-200-002MRB ZL-171-01-2MRB 212100/03MRB 212300/01MRB 253000/02MRB 282200/02MRB 383101/04MRB 383200/01MRB 383200/03

I 24 000 FHI 72 MO

ALLZL-171-02-1 AFT CABIN UNDERFLOOR COMPARTMENT171 GVI172

Y

GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOORCOMPARTMENT (EWIS)PREP : ACT(S) REMOVED (IF INSTALLED); INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION

Access panels :




: : :

: :

1412/09/2013

01



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AMM 052190/6AMT 052190-200-001MRB ZL-191-01-1

I 24 MO

CCheck :

22552261

2267

23032480

2974

30053013

3022

31983315

3355

36003737

3862

39643966

4136

42134277

4311

4315

ZL-191-01-1 AIR CONDITIONING COMPT AND FAIRINGS191 GVI192

Y

GENERAL VISUAL INSPECTION OF AIR CONDITIONINGCOMPARTMENT AND FAIRINGS (EWIS)

Access panels :

191BB 191KB 192KB0.28Total access time : Hrs



: : :

: :

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AMT 052190-200-001I 24 MO 4669

4703

47374783

4826

48634945

4971

52515275

5306

53405385

5392

54185438

5456

54955555

5699

59165958

ZL-191-01-2 AIR CONDITIONING COMPT AND FAIRINGS191 GVI192

YR

AIR CONDITIONING COMPARTMENT ANDFAIRINGSGENERAL VISUAL INSPECTION OF AIR CONDITIONINGCOMPARTMENT AND FAIRINGS (EWIS)

Access panels :

191AB 191BB 191KB 192KB0.50Total access time : Hrs



: : :

: :

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I 24 000 FHI 6 YE

ALLZL-191-02-1 AIR CONDITIONING COMPT AND FAIRINGS191 GVI192

Y

GENERAL VISUAL INSPECTION OF AIR CONDITIONINGCOMPARTMENT AND FAIRINGS (EWIS)

Access panels :

191AB 191AT 191BT 191CT 191DT 191EB 191ET191GB 191HB 191JB 191KB 191LB 192AB 192AT192BT 192CT 192DT 192EB 192ET 192FB 192KB192LB 192MB



AMM 052190/6AMT 052190-200-003MRB ZL-193-01-1MRB ZL-193-01-2

I 6 YE ALLZL-193-01-2 OFFWING ESCAPE SLIDE STOWAGE AREA193 GVI194

Y

GENERAL VISUAL INSPECTION OF OFFWING ESCAPE SLIDESTOWAGE AREA (EWIS)

Access panels :




: : :

: :

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I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-195-01-1 HYDRAULICS COMPARTMENT AND FAIRINGS195 GVI196

Y

GENERAL VISUAL INSPECTION OF HYDRAULIC COMPARTMENTAND FAIRINGS (EWIS)

Access panels :

195BB 196BB0.04Total access time : Hrs


AMM 052190/6AMT 052190-200-007MRB ZL-197-01-2MRB 291000/21

I 6 YE ALLZL-197-01-2 REAR FAIRING197 GVI198

Y

GENERAL VISUAL INSPECTION OF REAR FAIRING (EWIS)

Access panels :

197AB 197GB 197KB 198GB 198KB1.16Total access time : Hrs



: : :

: :

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01



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AMM 052200/6AMT 052200-200-002MRB ZL-200-02-3MRB 531106-01-1MRB 531114-02-1MRB 531117-01-2MRB 531118-01-2MRB 531179-01-1MRB 532152-01-1MRB 532164-01-2MRB 533133-01-2MRB 534118-01-1MRB 534131-01-2MRB 534176-02-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-200-02-3 UPPER HALF OF FUSELAGE200 GVI Y

GENERAL VISUAL INSPECTION OF UPPER HALF OF FUSELAGE


AMM 052210/6AMT 052210-200-001MRB ZL-211-01-1

I 15 000 FHI 10 000 CYI 48 MO

2CCheck :

ALLZL-211-01-1 COCKPIT211 GVI212

Y

GENERAL VISUAL INSPECTION OF COCKPIT (EWIS)

Access panels :

211AW 211AZ 211BW 211EW 211LW 212AW 212AZ212BW 212EW 212JW 831




: : :

: :

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AMM 052210/6AMT 052210-200-002MRB ZL-211-02-1

I 12 YE ALLZL-211-02-1 COCKPIT211 GVI212

Y

GENERAL VISUAL INSPECTION OF COCKPIT (EWIS)PREP : INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;Access panels :

211BC 211FC 211HC 212BC 212FC 212KW 8310.14Total access time : Hrs


AMM 052220/6AMT 052220-200-006MRB ZL-221-02-1

I 12 YE ALLZL-221-02-1 FORWARD CABIN UTILITY AREA221 GVI222

Y

GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREASINCLUDING FLOOR STRUCTURE (EWIS)PREP. : DOOR FRAME LINING REMOVED; FLOOR PANELS FROM FR 12 TO FR 20; FURNISHINGS FROM FR 12 TO FR 20; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SEATS REMOVED; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 052220/6AMT 052220-200-003MRB ZL-223-01-1MRB 531185-01-1

I 12 YE ALLZL-223-01-1 FWD CABIN UTILITY AREA OVERHEAD COMPT.223 GVI224

Y

GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREAOVERHEAD COMPARTMENT (EWIS)PREP. : CEILING PANELS FROM FR 12 TO FR 20; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 052230/6AMT 052230-200-001MRB ZL-231-01-2MRB 532101-01-2

I 12 YE ALLZL-231-01-2 FORWARD PASSENGER COMPARTMENT231 GVI232

Y

GENERAL VISUAL INSPECTION OF FWD PASSENGERCOMPARTMENT (EWIS)(INCLUDING FLOOR STRUCTURE)PREP. : DOOR FRAME LINING REMOVED; FURNISHING REMOVED; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SEATS REMOVED; SIDEWALL PANELS FROM FR 20 TO FR 35.8; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 052230/6AMT 052230-200-003MRB ZL-233-01-2MRB 531185-01-1MRB 532101-01-2

I 12 YE ALLZL-233-01-2 FWD PASSENGER OVERHEAD COMPT233 GVI234

Y

GENERAL VISUAL INSPECTION OF FWD PASSENGER OVERHEADCOMPARTMENT (EWIS)PREP : CEILING PANELS FROM FR 20 TO FR 35.8 GALLEYS INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION OVERHEAD STOWAGE COMPARTMENTS REMOVED TOILET REMOVAL/INSTALLATIONAccess panels :




: : :

: :

1412/09/2013

01



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AMM 052240/6AMT 052240-200-001MRB ZL-241-01-2MRB 533134-01-2

I 12 YE ALLZL-241-01-2 MID PASSENGER COMPARTMENT241 GVI242

Y

GENERAL VISUAL INSPECTION OF CENTER PASSENGERCOMPARTMENT (EWIS)(INCLUDING FLOOR STRUCTURE)PREP. : FURNISHING, SIDEWALL AND FLOOR PANELS FROM FR 35.8 TO FR 47 REMOVED; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

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AMM 052240/6AMT 052240-200-003MRB ZL-243-01-3MRB 533134-01-2

I 12 YE ALLZL-243-01-3 MID PASSENGER OVERHEAD COMPT243 GVI244

Y

GENERAL VISUAL INSPECTION OF CENTER PASSENGEROVERHEAD COMPARTMENT (EWIS)PREP. : CEILING PANELS FROM FR 35.8 TO FR47; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



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Ctrl References Eff

AMM 052250/6AMT 052250-200-001MRB ZL-251-01-2MRB 534119-01-1

T 12 YEI 12 YE

ALLZL-251-01-2 AFT PASSENGER COMPARTMENT251 GVI252

Y

GENERAL VISUAL INSPECTION OF AFT PASSENGERCOMPARTMENT (EWIS)(INCLUDING FLOOR STRUCTURE)PREP. : DOOR FRAME LINING REMOVED; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SEATS REMOVED; FURNISHING, SIDEWALL AND FLOOR PANELS FROM FR 47 TO FR 64 REMOVED; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



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AMM 052250/6AMT 052250-200-003MRB ZL-253-01-1MRB 534119-01-1MRB 534119-01-2MRB 534119-01-3

T 12 YEI 12 YE

ALLZL-253-01-1 AFT PASSENGER OVERHEAD COMPT253 GVI254

Y

GENERAL VISUAL INSPECTION OF AFT PASSENGER OVERHEADCOMPARTMENT (EWIS)PREP : CEILING PANELS FROM FR 47 TO FR 64; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



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I 12 YE ALLZL-261-02-1 AFT CABIN UTILITY AREAS261 GVI262

Y

GENERAL VISUAL INSPECTION OF AFT CABIN UTILITY AREASINCLUDING FLOOR STRUCTURE (EWIS)PREP. : FLOOR PANELS BETWEEN FR 64 TO 70; FURNISHINGS BETWEEN FR 64 TO 70; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SEATS REMOVED; SIDEWALL/DOOR FRAME LINING REMOVED; TOILET REMOVAL/INSTALLATION;Access panels :




: : :

: :

1412/09/2013

01



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T 12 YEI 12 YE

ALLZL-263-01-1 AFT CABIN OVERHEAD COMPARTMENT263 GVI264

Y

GENERAL VISUAL INSPECTION OF AFT CABIN OVERHEADCOMPARTMENT (EWIS)PREP. : CEILING PANELS FROM FR 64 TO FR 70; GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET REMOVAL/INSTALLATION;Access panels :



AMM 052300/6AMT 052300-200-002MRB ZL-300-02-1MRB 236000/02MRB 491600/04-36MRB 535103-01-1MRB 535125-01-1MRB 551017-01-1MRB 551018-01-1MRB 552001-01-1MRB 553001-01-1MRB 554001-01-1

I 7 500 FHI 24 MO

ALLZL-300-02-1 STABILIZERS AND CONE/REAR FUSELAGE300 GVI Y

GENERAL VISUAL INSPECTION OF STABILIZERS ANDCONE/REAR FUSELAGENOTE: THE FIRST TIME OF TASK ACCOMPLISHMENT SINCE AMSISS14 AMD 00 EFFECTIVE DATE IS NEXT 2A CHECK



: : :

: :

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01



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AMM 052310/6AMT 052310-200-001MRB ZL-311-01-1MRB 27.21.00/08MRB 274000/19MRB 282200/02MRB 360000/08MRB 535124-01-1MRB 551005-01-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-311-01-1 AFT FUSELAGE TAIL SECTION311 GVI312

Y

GENERAL VISUAL INSPECTION OF AFT FUSELAGE TAILSECTION (EWIS)

Access panels :



AMM 052310/6AMT 052310-200-002MRB ZL-313-01-1MRB 360000/08MRB 491600/01-32MRB 491600/03-13MRB 491600/05-36

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-313-01-1 TAIL CONE APU AIR INTAKE AREA313 GVI314

Y

GENERAL VISUAL INSPECTION OF TAIL CONE APU AIR INTAKEAREA (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



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Ctrl References Eff

AMT 052310-200-003MRB ZL-315-01-1MRB 36.00.00/08MRB 49.12.00/01-13MRB 49.17.00/01-13MRB 49.30.00/01-13

I 24 MO ALLZL-315-01-1 TAIL CONE APU - ACCESSORY COMPARTMENT315 GVI316

Y

GENERAL VISUAL INSPECTION OF TAIL CONE APU ANDACCESSORY COMPARTMENT (EWIS)NOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH 131-9(A) APU

Access panels :



AMM 052310/6AMT 052310-200-003MRB ZL-315-01-2MRB 360000/08MRB 491200/01-32MRB 491700/01-32MRB 493100/01-32MRB 495100/01-32

I 24 MO ALLZL-315-01-2 TAIL CONE APU - ACCESSORY COMPARTMENT315 GVI316

Y

GENERAL VISUAL INSPECTION OF TAIL CONE APU ANDACCESSORY COMPARTMENT (EWIS)NOTE : TASK IS ONLY APPLICABLE TO AIRCRAFT FITTED WITH APIC 3200 APU

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052310/6AMT 052310-200-004MRB ZL-317-01-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-317-01-1 TAIL CONE/APU EXHAUST AREA317 GVI Y

GENERAL VISUAL INSPECTION OF TAIL CONE APU EXHAUSTAREA (EWIS)

Access panels :



AMM 052320/6AMT 052330-200-001MRB ZL-321-01-1

I 12 YE ALLZL-321-01-1 DORSAL FIN321 GVI Y

GENERAL VISUAL INSPECTION OF DORSAL FIN (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



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Ctrl References Eff

AMM 052320/6AMT 052320-200-002MRB ZL-322-01-1

I 12 YE ALLZL-322-01-1 VERTICAL STABILIZER LEADING EDGE322 GVI Y

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZERLEADING EDGE (EWIS)Access panels :

322AL 322BL 322CL1.06Total access time : Hrs


AMM 052320/6AMT 052320-200-003MRB ZL-323-01-1

I 12 YE ALLZL-323-01-1 VERTICAL STABILIZER SPAR BOX323 GVI Y

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SPARBOX (EWIS)PREP. : PEELABLE HOLE COVERS REMOVEDAccess panels :

321AL 322BL 323AL 323AR 325AL 325AR1.16Total access time : Hrs



: : :

: :

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01



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Ctrl References Eff

AMM 052320/6AMT 052320-200-004MRB ZL-324-01-1

I 12 YE ALLZL-324-01-1 VERTICAL STABILIZER TIP324 GVI YR

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZERTIP (EWIS)NOTE: RII TASKAccess panels :

324AT0.18Total access time : Hrs


AMM 052320/6AMT 052320-200-005MRB ZL-325-01-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-325-01-1 VERTICAL STABILIZER TRAILING EDGE325 GVI Y

GENERAL VISUAL INSPECTION OF VERTICALSTABILIZER TRAILING EDGE (EWIS)

Access panels :

325BL 325CL 325DL 325EL0.08Total access time : Hrs



: : :

: :

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01



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AMT 052320-200-007MRB ZL-325-02-1MRB 27.21.00/08MRB 553002-01-1MRB 553007-01-1MRB 554007-01-1MRB 554007-01-2

I 6 YE ALLZL-325-02-1 VERTICAL STABILIZER TRAILING EDGE325 GVI Y

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZERTRAILING EDGE (EWIS)

Access panels :

325AL 325AR 325BL 325BR 325CL 325CR 325DL325DR 325EL 325ER



AMT 052320-200-006MRB ZL-326-01-1MRB 554002-01-1MRB 554007-01-1

I 6 YE ALLZL-326-01-1 RUDDER326 GVI Y

GENERAL VISUAL INSPECTION OF RUDDER (EWIS)

Access panels :

325AL 325AR 325BL 325BR 325CL 325CR 325DL325DR 325EL 325ER 326AT




: : :

: :

1412/09/2013

01



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AMM 052320/6AMT 052320-200-008MRB ZL-326-02-1

I 12 YE ALLZL-326-02-1 RUDDER326 GVI Y

GENERAL VISUAL INSPECTION OF RUDDER (EWIS)PREP. : PEELABLE HOLE COVERS REMOVEDAccess panels :

325AL 325AR 325BL 325BR 325CL 325CR 325DL325DR 325EL 325ER 326AT



AMM 052330/6AMT 052330-200-001MRB ZL-331-01-1MRB 551015-01-1

I 6 YE ALLZL-331-01-1 THS LEADING EDGE331 GVI341

Y

GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTALSTABILIZER LEADING EDGE (EWIS)

Access panels :

331AB 331BB 331CB 341AB 341BB 341CB1.44Total access time : Hrs



: : :

: :

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01



Threshold Interval

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AMM 052330/6AMT 052330-200-002MRB ZL-332-01-1MRB 551015-01-1

I 12 YE ALLZL-332-01-1 THS TIP332 GVI342

YR

GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTALSTABILIZER TIP (EWIS)NOTE: RII TASKAccess panels :



AMM 052330/6AMT 052330-200-003MRB ZL-333-01-1

I 12 YE ALLZL-333-01-1 THS SPAR BOX333 GVI343

Y

GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTALSTABILIZER SPAR BOX (EWIS)PREP. : PEELABLE HOLE COVERS REMOVED;Access panels :

312AR 314AR 331AB 331BB 331CB 332AB 333AB333AT 334AB 334BB 334CB 334DB 334EB 334FB334GB 334HB 341AB 341BB 341CB 342AB 343AB343AT 344AB 344BB 344CB 344DB 344EB 344FB344GB 344HB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052330/6AMT 052330-200-004MRB ZL-334-01-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-334-01-1 THS TRAILING EDGE334 GVI344

Y

GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE (EWIS)

Access panels :





I 6 YE ALLZL-334-02-1 THS TRAILING EDGE334 GVI344

Y

GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE (EWIS)

Access panels :

334AB 334AT 334BB 334BT 334CB 334CT 334DB334DT 334EB 334FB 334GB 334HB 344AB 344AT344BB 344BT 344CB 344CT 344DB 344DT 344EB344FB 344GB 344HB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


I 6 YE ALLZL-335-01-1 ELEVATOR335 GVI345

Y

GENERAL VISUAL INSPECTION OF ELEVATOR (EWIS)

Access panels :

334BB 334DB 334FB 334HB 335AB 335BB 335CB335DB 344BB 344DB 344FB 344HB 345AB 345BB345CB 345DB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052400/6AMT 052400-200-002MRB ZL-400-02-2MRB 236000/02MRB 711100/01-I2MRB 711100/02-I2MRB 711300/01-I2MRB 723100/02-I2MRB 723100/02-I3MRB 723280/02-I2MRB 723280/03-I2MRB 723285/01-I2MRB 725000/02-I2MRB 781000/03-I2MRB 781000/05-I2MRB 7832BB/03-I2

I 750 CYI 4 MO

ALLZL-400-02-2 POWER PLANT, NACELLES AND PYLONS400 GVI Y

GENERAL VISUAL INSPECTION OF POWERPLANTS, NACELLESAND PYLONS



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052410/6AMT 052410-200-001MRB ZL-411-01-1MRB 360000/08MRB 572031-02-1

I 20 MO 22552261

2267

23032480

2974

30053013

3022

31983315

3355

ZL-411-01-1 UPPER FORWARD PYLON411 GVI413414421423424

Y

GENERAL VISUAL INSPECTION OF UPPER FWD PYLON (EWIS)

Access panels :

413AL 413BL 413CL 413DL 413EL 414AR 414AZ414BR 414CR 414FR 423AL 423AZ 423BL 423CL423DL 423FL 424AR 424BR 424CR 424ER




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052410/6AMT 052410-200-001MRB ZL-411-01-3MRB 36.00.00/08MRB 572031-02-1

I 20 MO 36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4863

49454971

5164

52415247

5251

52755297

5306

53405343

5385

5392

ZL-411-01-3 UPPER FORWARD PYLON411 GVI413414421423424

YR

GENERAL VISUAL INSPECTION OF UPPER FWD PYLON (EWIS)


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5418

5427

54385456

5469

54955555

5699

57095916

5958

5994

Access panels :

413AL 413AR 413BL 413BR 413CL 413CR 413DT414AZ 423AL 423AR 423AZ 423BL 423BR 423CL423CR 423DT 471AL 471AR 481AL 481AR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052410/6AMT 052410-200-002MRB ZL-415-01-2

I 20 MO ALLZL-415-01-2 LOWER PYLON415 GVI425

Y

GENERAL VISUAL INSPECTION OF LOWER PYLON (EWIS)

Access panels :




AMM 052430/6AMT 052430-200-001MRB ZL-433-01-2MRB 302100/04

I 24 000 FHI 6 YE

ALLZL-433-01-2 AIR INTAKE LIP433 GVI434443444

Y

GENERAL VISUAL INSPECTION OF AIR INTAKE LIP (EWIS)

Access panels :

434AR 434BR 437AL 438AR 444AR 444BR 447AL448AR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052430/6AMT 052430-200-002MRB ZL-435-01-2MRB 711100/03-I2MRB 717000/01-I2MRB 731000/02-I2MRB 7832AA/03-I2MRB 790000/04-I2MRB 800000/04-I2

I 16 MO ALLZL-435-01-2 FAN AND ACCESSORY GEARBOX435 GVI436445446

Y

GENERAL VISUAL INSPECTION OF FAN AND ACCESSORY GEARBOX (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052430/6AMT 052430-200-003MRB ZL-437-01-2MRB 711300/02MRB 711300/02-I2MRB 711300/03-I2MRB 711300/04-I2MRB 711300/05-I2MRB 783200-01-4

I 16 MO ALLZL-437-01-2 FAN COWLING437 GVI438447448

Y

GENERAL VISUAL INSPECTION OF FAN COWL (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052450/6AMT 052450-200-001MRB ZL-451-01-2MRB 752100/03-I2MRB 7832AA/03-I2MRB 7832BB/04-I2MRB 7832BB/06-I2MRB 783200-01-4MRB 783200BB/08-I2

I 16 MO ALLZL-451-01-2 THRUST REVERSER COWLING451 GVI452461462

Y

GENERAL VISUAL INSPECTION OF THRUST REVERSER (EWIS)PREP. : THRUST REVERSER DEPLOYED

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052450/6AMT 052450-200-002MRB ZL-453-01-2MRB 360000/08MRB 717000/01-I2MRB 724000/02-I2MRB 731000/02-I2MRB 75.23.00/01-I2MRB 752400/02-I2MRB 752400/03-I2MRB 753200/01-I2MRB 781000/04-I2MRB 781000/05-I2MRB 781000/06-I2MRB 7832BB/08-I2MRB 790000/04-I2

I 16 MO ALLZL-453-01-2 HOT SECTION453 GVI454463464

Y

GENERAL VISUAL INSPECTION OF HOT SECTION (EWIS)

Access panels :

451AL 452AR 452DR 452ER 461AL 462AR 462DR462ER




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052470/6AMT 052470-200-001MRB ZL-471-01-2MRB 572031-02-1MRB 572042-01-5MRB 572047-02-2MRB 572057-02-1SIL 54-023

I 20 MO 22552261

2267

23032480

2974

30053013

3022

31983315

3355

ZL-471-01-2 PYLON LEADING EDGE AND LOWER FAIRINGNT GVI Y

GENERAL VISUAL INSPECTION OF PYLON LEADING EDGE ANDLOWER FAIRING (EWIS)

Access panels :

471AL 471BL 471CL 472AR 472BR 473AL 475AL475BL 475CL 476AR 476BR 476CR 477AL 481AL481BL 482BR 482CR 483AL 485AL 485BL 485CL486AR 486BR 486CR 487AR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052470/6AMT 052470-200-001MRB ZL-471-01-5MRB 572031-02-1MRB 572042-01-5MRB 572047-02-2MRB 572057-02-1SIL 54-023

I 20 MO 36003737

3862

39643966

4136

42134277

4311

43154669

4703

47374783

4826

48634945

4971

51645241

5247

52515275

5297

53065340

5343

5385

ZL-471-01-5 PYLON LEADING EDGE AND LOWER FAIRINGNT GVI YR

GENERAL VISUAL INSPECTION OF PYLON LEADING EDGE ANDLOWER FAIRING (EWIS)


: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

5392

5418

54275438

5456

54695495

5555

56995709

5916

59585994

Access panels :

471BL 471BR 471CL 471CR 471DL 473AL 475AL475AR 475BL 475BR 477AL 481BL 481BR 481CL481CR 481DR 483AL 485AL 485AR 485BL 485BR487AR




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052500/6AMT 052500-200-002MRB ZL-500-02-1MRB 23.60.00/02MRB 36.00.00/07MRB 572031-02-1MRB 572059-01-1MRB 572166-01-1MRB 574207-01-1MRB 574307-01-1MRB 574407-01-1MRB 574507-01-1MRB 574607-01-1MRB 575158-01-3MRB 575158-01-4MRB 575161-01-4MRB 575162-01-3MRB 575201-01-1MRB 575221-01-2MRB 575251-02-1MRB 575301-01-1MRB 575321-01-1MRB 575351-02-1MRB 576104-02-1MRB 576106-02-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-500-02-1 WING LOWER SURFACE500 GVI600

Y

GENERAL VISUAL INSPECTION OF WING LOWER SURFACEINCLUDING UPPER AND LOWER SURFACES OF SLATS ANDFLAPS (EWIS)PREP. : FLAPS EXTENDED SLATS FULLY EXTENDED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052500/6AMT 052500-200-003MRB ZL-500-03-1MRB 572058-01-1MRB 572165-01-1MRB 574207-01-1MRB 574307-01-1MRB 574407-01-1MRB 574507-01-1MRB 574607-01-1MRB 575155-01-3MRB 575201-01-1MRB 575221-01-2MRB 575301-01-1MRB 575321-01-1MRB 576104-02-1MRB 576106-02-1MRB 577002-02-1MRB 577003-02-1MRB 577007-02-1MRB 577008-02-1MRB 577009-02-1

I 48 MO

2CCheck :

ALLZL-500-03-1 WING UPPER SURFACE500 GVI600

Y

GENERAL VISUAL INSPECTION OF WING UPPER SURFACEINCLUDING SLATS, FLAPS AND SPOILERSPREP. : FLAPS EXTENDED SPOILERS EXTENDED SLATS FULLY EXTENDED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052520/6AMT 052520-200-001MRB ZL-521-01-1MRB 30.11.00/01MRB 36.00.00/08MRB 572654-02-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-521-01-1 INBOARD FIXED LEADING EDGE STRUCTURE521 GVI621

Y

GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADINGEDGE STRUCTURE (EWIS)PREP. : SLATS FULLY EXTENDED

Access panels :

521AB 521AT 521BT 521CB 521EB 521GB 521HB621AB 621AT 621BT 621CB 621EB 621GB 621HB



AMM 052520/6AMT 052520-200-002MRB ZL-522-01-1MRB 30.11.00/01

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-522-01-1 OUTBOARD FIXED LEADING EDGE STRUCTURE522 GVI622

Y

GENERAL VISUAL INSPECTION OF OUTBOARD FIXED LEADINGEDGE STRUCTURE (EWIS)PREP. : SLATS FULLY EXTENDED

Access panels :

522AB 522AT 522BT 522CB 522EB 522FB 522HB522JB 522KB 522LB 522NB 522QB 522SB 522UB622AB 622AT 622BT 622CB 622EB 622FB 622HB622JB 622KB 622LB 622NB 622QB 622SB 622UB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-531-01-1 FLAP TRACK NO.2 FAIRING531 GVI631

Y

GENERAL VISUAL INSPECTION OF FLAP TRACK NO.2AND FAIRING (EWIS)PREP. : FLAPS EXTENDED

Access panels :




I 6 YE ALLZL-531-02-2 FLAP TRACK NO.2 FAIRING531 GVI631

Y


Access panels :

531AL 531AR 531AT 531CB 531DB 531EB 531FB631AL 631AR 631AT 631CB 631DB 631EB 631FB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


I 7 500 FHI 5 000 CYI 24 MO

CCheck :


Y


Access panels :





Y


Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


I 7 500 FHI 5 000 CYI 24 MO

CCheck :


Y


Access panels :





Y


Access panels :





: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052530/6AMT 052530-200-004MRB ZL-534-01-2MRB 573101-02-1

I 72 MO ALLZL-534-01-2 WING TIP534 GVI634

Y

GENERAL VISUAL INSPECTION OF WING TIP (EWIS)

Access panels :

534AB 534AL 534BL 634AB 634AL 634BL0.18Total access time : Hrs


AMM 052530/6AMT 052530-200-009MRB ZL-536-01-1MRB 275000/11

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-536-01-1 FLAP TAB HINGE FAIRING NO. 1B536 GVI636

Y

GENERAL VISUAL INSPECTION OF FLAP TAB HINGE ANDFAIRING NO. 1B (EWIS)PREP. : FLAPS EXTENDED

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


I 6 YE ALLZL-540-01-2 WING FUEL TANK540 GVI640

Y

GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)NOTE: INTERVAL MAY BE ADJUSTED BY INDIVIDUALOPERATORS IN CONSIDERATION OF THEIR OWNINSERVICE EXPERIENCE AND OPERATIONALENVIRONMENT.Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052540/6AMT 052540-200-004MRB ZL-540-02-2MRB 28.11.00/05MRB 28.11.00/06MRB 28.21.00/07MRB 572004-02-1MRB 572011-02-1MRB 572027-02-1MRB 572028-02-1MRB 572050-03-2MRB 572060-01-1MRB 572061-01-1MRB 572108-02-1MRB 572114-02-1MRB 572126-02-1MRB 572167-01-1MRB 572168-01-1

I 12 YE ALLZL-540-02-2 WING FUEL TANK540 GVI640

Y

GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)NOTE: ALTERNATIVE COMPLIANCE FOR THE DRY BAY AREA IS SHOWN BY PERFORMING TASKS 572050-02-1, 572050-02-2, 572050-02-4, 572050-02-5 AND 572050-02-6 AT THE SAME TIME. ACCESS PANELS 540/640CZ AND 540/640DZ NEED NOT TO BE REMOVED IN THIS CASE

Access panels :

521AZ 521BZ 540AB 540AZ 540BB 540BZ 540CB540CZ 540DB 540DZ 540EB 540FB 540GB 540HB540JB 540KB 540LB 540MB 540NB 540PB 540QB540RB 621AZ 621BZ 640AB 640AZ 640BB 640BZ640CB 640CZ 640DB 640DZ 640EB 640FB 640GB640HB 640JB 640KB 640LB 640MB 640NB 640PB640QB 640RB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052550/6AMT 052550-200-001MRB ZL-550-01-1MRB 572109-02-1MRB 572115-02-1MRB 572126-02-1MRB 572167-01-1MRB 572168-01-1

I 12 YE ALLZL-550-01-1 VENT SURGE TANK550 GVI650

Y

GENERAL VISUAL INSPECTION OF VENT SURGE TANK (EWIS)

Access panels :

550AB 550BB 550CB 550DB 650AB 650BB 650CB650DB



AMM 052560/6AMT 052560-200-001MRB ZL-560-01-1MRB 572109-02-1MRB 572115-02-1MRB 572126-02-2MRB 572167-01-1MRB 572168-01-1

I 12 YE ALLZL-560-01-1 DRY BAY560 GVI660

Y

GENERAL VISUAL INSPECTION OF DRY BAY(OUTBOARD) (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052570/6AMT 052570-200-006MRB ZL-571-02-1MRB 291000/21MRB 572652-01-1

I 15 000 FHI 10 000 CYI 48 MO

2CCheck :

ALLZL-571-02-1 MAIN LANDING GEAR571 GVI671

Y

GENERAL VISUAL INSPECTION OF MLG BAY (EWIS)


AMM 052570/6AMT 052570-200-002MRB ZL-572-01-2

I 15 000 FHI 10 000 CYI 48 MO

2CCheck :

ALLZL-572-01-2 SHROUD BOX572 GVI672

Y

GENERAL VISUAL INSPECTION OF SHROUD BOX (EWIS)PREP. : FLAPS EXTENDED

Access panels :



AMM 052570/6AMT 052570-200-003MRB ZL-573-01-1MRB 575151-02-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-573-01-1 INBOARD FIXED TRAILING EDGE STRUCTURE573 GVI673

Y

GENERAL VISUAL INSPECTION OF INBOARD FIXED TRAILINGEDGE STRUCTURE FROM SHROUD BOX TO RIB 9 (EWIS)PREP. : FLAPS EXTENDED SPOILERS EXTENDED



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052570/6AMT 052570-200-004MRB ZL-574-01-1MRB 291000/21MRB 575151-02-1MRB 575163-02-1

I 24 MO

CCheck :

ALLZL-574-01-1 FALSE SPAR BOX574 GVI674

Y

GENERAL VISUAL INSPECTION OF FALSE SPAR BOX (EWIS)PREP. : PYLON FAIRINGS REMOVED

Access panels :

573AB 573BB 573CB 573DB 573EB 574AB 574BB673AB 673BB 673CB 673DB 673EB 674AB 674BB



AMM 052570/6AMT 052570-200-005MRB ZL-575-01-1MRB 576102-01-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-575-01-1 OUTBOARD FIXED TRAILING EDGE STRUCTURE575 GVI675

Y

GENERAL VISUAL INSPECTION OF OUTBOARD FIXED TRAILINGEDGE STRUCTURE FROM RIB 9 TO RIB 27 (EWIS)PREP. : FLAPS EXTENDED; SPOILERS EXTENDED;Access panels :

575AT 575KB 575LB 575MB 675AT 675KB 675LB675MB




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052590/6AMT 052590-200-001MRB ZL-590-01-1

I 15 000 FHI 10 000 CYI 48 MO

2CCheck :

ALLZL-590-01-1 AILERON590 GVI690

Y

GENERAL VISUAL INSPECTION OF AILERON (EWIS)

Access panels :




I 4 MO ALLZL-711-01-1 NOSE GEARNT GVI Y

GENERAL VISUAL INSPECTION OF NOSE GEAR AND NOSE GEARDOORS (EWIS)NOTE: WORKING ZONES 711, 712, 713, 714, 715, 716

Access panels :


AMM 052730/6AMT 052730-200-001MRB ZL-731-01-1

I 4 MO ALLZL-731-01-1 MAIN LANDING GEAR731 GVI741

N

GENERAL VISUAL INSPECTION OF LH/RH MAIN LANDINGGEAR (EWIS)



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052730/6AMT 052730-200-002MRB ZL-732-01-1


N

GENERAL VISUAL INSPECTION OF MAIN LANDING GEARCYLINDER DOOR (EWIS)


AMM 052730/6AMT 052730-200-003MRB ZL-733-01-1


N

GENERAL VISUAL INSPECTION OF MAIN LANDING GEARSECONDARY DOOR (EWIS)


AMM 052730/6AMT 052730-200-004MRB ZL-734-01-1MRB 528105-01-1


N

GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR MAINDOORS (EWIS)

Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052810/6AMT 052810-200-001MRB ZL-811-01-1MRB 524112-01-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-811-01-1 FWD AVIONICS COMPARTMENT DOOR811 GVI Y

GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENTDOOR (EWIS)(INCLUDING EXTERNAL SURFACE)

Access panels :



AMM 052810/6AMT 052810-200-002MRB ZL-811-02-1

I 12 YE ALLZL-811-02-1 FWD AVIONICS COMPARTMENT DOOR811 GVI Y

GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENTDOOR (EWIS)PREP. : DOOR PANELS REMOVEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-812-01-1 LATERAL AVIONICS COMPARTMENT DOOR812 GVI822

Y

GENERAL VISUAL INSPECTION OF LATERAL AVIONICSCOMPARTMENT DOORS (EWIS)(INCLUDING EXTERNAL SURFACE)

Access panels :



AMM 052810/6AMT 052810-200-004MRB ZL-812-02-1

I 12 YE ALLZL-812-02-1 LATERAL AVIONICS COMPARTMENT DOOR812 GVI822

Y

GENERAL VISUAL INSPECTION OF LATERAL AVIONICSCOMPARTMENT DOORS (EWIS)Access panels :



: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052820/6AMT 052820-200-007MRB ZL-824-01-1MRB 524122-01-1

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-824-01-1 REAR AVIONICS COMPARTMENT DOOR824 GVI Y

GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENTDOOR (EWIS)(INCLUDING EXTERNAL SURFACE)

Access panels :



AMM 052820/6AMT 052820-200-008MRB ZL-824-02-1

I 12 YE ALLZL-824-02-1 REAR AVIONICS COMPARTMENT DOOR824 GVI Y

GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENTDOOR (EWIS)Access panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052820/6AMT 052820-200-001MRB ZL-825-01-1MRB 523101-01-2

I 4 MO ALLZL-825-01-1 FORWARD CARGO COMPARTMENT DOOR825 GVI N

GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENTDOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCKFITTINGS, EXTERNAL SURFACE (EWIS)Access panels :



AMM 052820/6AMT 052820-200-004MRB ZL-825-02-1

I 12 YE ALLZL-825-02-1 FORWARD CARGO COMPARTMENT DOOR825 GVI Y

GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENTDOOR (EWIS)PREP. : INSULATION REMOVEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052820/6AMT 052820-200-002MRB ZL-826-01-1MRB 523111-01-2

I 4 MO ALLZL-826-01-1 AFT CARGO COMPARTMENT DOOR826 GVI N

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENTDOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCKFITTINGS (EWIS)Access panels :



AMM 052820/6AMT 052820-200-005MRB ZL-826-02-1

I 12 YE ALLZL-826-02-1 AFT CARGO COMPARTMENT DOOR826 GVI Y

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENTDOOR (EWIS)PREP. : INSULATION REMOVEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff

AMM 052820/6AMT 052820-200-003MRB ZL-827-01-1MRB 523301-01-2

I 4 MO ALLZL-827-01-1 BULK CARGO COMPARTMENT DOOR827 GVI N

GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENTDOOR INCLUDING DOOR STOPS ON FUSELAGE DOORFRAME (EWIS)Access panels :



AMM 052820/6AMT 052820-200-006MRB ZL-827-02-1

I 12 YE ALLZL-827-02-1 BULK CARGO COMPARTMENT DOOR827 GVI Y

GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENTDOOR (EWIS)PREP. : INSULATION REMOVEDAccess panels :




: : :

: :

1412/09/2013

01



Threshold Interval

Ctrl References Eff


I 4 MO ALLZL-831-01-1 FWD AND AFT PASSENGER/CREW DOOR831 GVI832841842

Y

GENERAL VISUAL INSPECTION OF FWD AND AFTPASSENGER/CREW DOORS INCLUDING DOOR STOPS ON FUSELAGEDOOR FRAMES AND DOOR SEALS, EXTERNAL SURFACE (EWIS)

Access panels :



AMM 052830/6AMT 052830-200-005MRB ZL-831-02-1

I 12 YE ALLZL-831-02-1 FWD AND AFT PASSENGER/CREW DOOR831 GVI832841842

Y

GENERAL VISUAL INSPECTION OF FWD AND AFTPASSENGER/CREW DOORS (EWIS)PREP. : INSULATION REMOVEDAccess panels :

831 831AZ 831BZ 831CZ 831DZ 831EZ 831FZ831GZ 832 832AZ 832BZ 832CZ 832DZ 832EZ832FZ 832GZ 841 841AZ 841BZ 841CZ 841DZ841EZ 841FZ 841GZ 842 842AZ 842BZ 842CZ842DZ 842EZ 842FZ 842GZ




: : :

: :

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Ctrl References Eff

AMM 052830/6AMT 052830-200-007MRB ZL-833-02-2

I 6 YE ALLZL-833-02-2 FORWARD AND AFT EMERGENCY EXIT833 GVI834843844

Y

GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCYEXITS (EWIS)PREP. : INSULATION REMOVEDAccess panels :

833 833CZ 833DZ 833EZ 833FZ 833GZ 833HZ834 834CZ 834DZ 834EZ 834FZ 834GZ 834HZ843 843CZ 843DZ 843EZ 843FZ 843GZ 843HZ844 844CZ 844DZ 844EZ 844FZ 844GZ 844HZ




I 4 MO ALLZL-833-03-1 FORWARD AND AFT EMERGENCY EXIT833 GVI834843844

Y

GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCYEXITS - EXTERNAL SKIN (EWIS)



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Ctrl References Eff

AMM 052830/6AMT 052830-200-011MRB ZL-833-04-1MRB 522200/05

I 7 500 FHI 5 000 CYI 24 MO

CCheck :

ALLZL-833-04-1 FWD AND AFT EMERGENCY EXITS (INCLUDING833 GVI834843844

Y

DOOR STOPS ON FUSELAGE DOOR FRAMES)GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCYEXITS INCLUDING DOOR STOPS ON FUSELAGE DOORFRAMES (EWIS)Access panels :




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Date : SEP 2013 LIST OF EFFECTIVE PAGES - ECO Page : 1


LEP R 1 SEP 2013

A321 AIRCRAFT MAINTENANCE SCHEDULECHAPTER : 12 SERVICING (LUBRICATION)


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Ctrl References Eff

AMT 122111-615-072I 30 DYSee note

ALL12-ECO-00 EXTERNAL CLEANINGA/C CLN N

PERFORM WASHING AIRCRAFT

AMM 122111-615-002I 7 500 FHI 24 MO

CCheck :

ALL12-ECO-01 EXTERNAL CLEANINGA/C CLN N

C/O THE AIRCRAFT EXTERNAL CLEANING


Date ATA 12Date 22/01/2014Amendment NoIssue No Page ECO - 12 [1 / 1] :

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Ctrl References Eff

I 12 MO ALL31-ECO-01-1 DIGITAL FLIGHT DATA RECORDING SYSTEM210 OP NR

DOWNLOAD AND RECORD DFDR DATA.NOTE 1: TASK MAY BE COMBINED WITH TASK 31-ECO-01-2NOTE 2: INCASE OF TASK THRESHOLD IS OVERDUE WHEN AMS ISSUE 14 AMD 00 ISEFFECTIVE THE TASK THRESHOLD IS NEXT 2A CHECK.

I 12 MO ALL31-ECO-01-2 READ OUT DFDR DATA200 *** N

READ OUT OF DFDR DATA TO ENSURE RECORDEDPARAMETERS MEET THE RANGE AND ACCURACIES REQUIRED IN"BO QUY CHE AN TOAN HANG KHONG DAN DUNG LINH VUC TAU BAYVA KHAI THAC TAU BAY"NOTE 1: TASK MAY BE COMBINED WITH TASK 31-ECO-01-1NOTE 2: INCASE OF TASK THRESHOLD IS OVERDUE WHEN AMS ISSUE 14 AMD 00 ISEFFECTIVE THE TASK THRESHOLD IS NEXT 2A CHECK.


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AMT 720000-100-010I 1 500 FH ALL72-ECO-00 CLEAN THE ENGINE GAS PATH400 CLN N

CLEAN THE ENGINE GAS PATH FOR PERFORMANCEIMPROVEMENT (WATER ONLY)



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SECTION 5

SPECIAL PROCEDURES


SECTION MVT PAGE ISSUE 5 LEP R 1 SEP 2013 5 TOC R 1 SEP 2013 5.0 GENERAL INTRODUCTION N 1 SEP 2013 5.0 GENERAL INTRODUCTION N 2 SEP 2013 5.0 GENERAL INTRODUCTION N 3 SEP 2013 5.1 UNSCHEDULE MAINTENANCE CHECKS AND

INSPECTIONS N 1 SEP 2013

5.1 UNSCHEDULE MAINTENANCE CHECKS AND INSPECTIONS N 2 SEP 2013

5.2 PARKING / STORAGE PROCEDURES N 1 SEP 2013 5.2 PARKING / STORAGE PROCEDURES N 2 SEP 2013 5.3 COLD WEATHER MAINTENANCE PROCEDURE N 1 SEP 2013 5.4 A321 CRITICAL DESIGN CONFGURATION CONTROL

LIMITATION N 1 SEP 2013

ISSUE: SEP 2013 SECTION 5 - LEP PAGE 1


SECTION 5

SPECIAL PROCEDURES

TABLE OF CONTENTS

SUBJECT GENERAL SUB-SECTION 5.1: UNSCHEDULE MAINTENANCE CHECKS AND INSPECTIONS. SUB-SECTION 5.2: PARKING / STORAGE PROCEDURES. SUB-SECTION 5.3: COLD WEATHER MAINTENANCE PROCEDURE. SUB-SECTION 5.4: A321 CRITICAL DESIGN CONFGURATION CONTROL LIMITATION

ISSUE: SEP 2013 SECTION 5 - TOC PAGE 1


SECTION 5

SPECIAL PROCEDURES

ISSUE: SEP 2013 SECTION 5 – SPECIAL PROCEDURES PAGE 1

GENERAL This section of the Aircraft Maintenance Schedule is built in order to refer to the AMM tasks or procedure of the aircraft manufacturer which they are considered to be as the special maintenance procedures. This section covers: - Unscheduled maintenance checks and inspections. - Packing, storage and procedures. - Cold weather maintenance procedure. - Critical Design Configuration Control Limitations (CDCCL)

A. Sub-section 5.1- Unscheduled maintenance checks and inspections

Unscheduled maintenance checks includes procedures, instructions, and standards for maintenance that occurs on an unscheduled or unforeseen basis. A need for unscheduled maintenance may result from scheduled maintenance tasks, pilot reports, or unforeseen events such as hard or overweight landings, tail strikes, lightning strikes, or engine over temperature...ect This sub-section is built up as the cross-reference table, in which consists of the following causes abnormal may occurs during the operation or maintenance of aircraft and the corresponding procedures. Those inspections that are necessary after an incident, flight in abnormal conditions, abnormal operation or repair and will, in most cases, be called for as a result of flight crew report or maintenance report. Unless specified differently, the technical staff must do these inspections before the subsequent flight of the aircraft. If there is no inspection in this sub-section applicable to the incident or abnormal flight conditions that occurred, VNA or aircraft maintenance base’s VNA must tell Airbus and make a request for more instructions.

B. Sub-section 5.2 - Parking and storage procedures

These procedures need to be done for care and protection of aircraft in case of decommissions and stay on ground (AOG) for short or long terms, the instructions in those procedures necessary to park or store the aircraft in normal or abnormal conditions. Airbus give precise guidelines for handling parked aircraft in an aircraft maintenance manual (AMM), therefore, Parking and storage procedures are given in the form of AMM tasks in this sub-section. During storage or parking periods, do not stop or change the maintenance program without CAAV approval. The maintenance calendar clock continues during these periods. However, if the AMM storage or parking procedures are done correctly,


SECTION 5

SPECIAL PROCEDURES


and if you have the approval of CAAV, it is not necessary to do all the scheduled maintenance tasks (such as AMS tasks) immediately during storage/packing period. You can wait until the end of the period to do them all before the next flight. The Parking procedure can drawn up for the decommissioning of an aircraft for a period of up to twelve weeks, the Storage procedure can be taken when an aircraft is decommissioned for up to two years. Depending on the requirement or purpose in each particular case, normal or abnormal conditions, the length of time of the decommissioning or AOG, which procedure can be applied, or apply one after the other procedure in accordance with the respective period of each procedure. 1. Parking procedure:

This procedure is to keep the aircraft in flight-ready condition during the parking period, which means it can be returned to the operative fleet within a comparatively short time. Parking procedure would be start with an aircraft remain on the ground for more than two days. And it is divided into two sub-procedure corresponding to the two period is not more than 15 days and not more than 12 weeks. Each sub-procedure consists of three different work packages: A procedure for parking the aircraft in flight-ready condition, then the related tasks to do periodic ground check during parking, and finally there is a work package to return to operation or to do again the parking procedure. Note: - The parking procedure period of not more than 15 days can do again one

time only. - The procedure for the renewal of the 12-week parking period includes a non-

revenue flight procedure within the aircraft standard envelope.

2. Storage procedure: This procedure gives the preservation steps for a storage periods, and is often applied in the case of aircraft is not ready to fly condition or decommission for a long term. Just like parking procedures, this procedure is divided into two sub-procedures also, procedure for a period of not more than six months and more than two years. Each sub-procedure comprises: a storage procedure, various periodic ground checks, and return to operation after storage period or renewal for six months / two years Storage Period. Note: - The procedure to store the aircraft not more than six months can do again

one time only. - The procedure for the renewal of two years storage Period includes a non-

revenue flight procedure within the aircraft standard envelope.


SECTION 5

SPECIAL PROCEDURES


C. Sub-section 5.3 - Cold weather maintenance procedure.

This procedure supply a work package to keep aircraft operation safety in cold weather conditions, aircraft downtime and delays in flight schedules caused by cold weather problems can be minimized by a program of preventive cold weather servicing. The aircraft need to carry out this procedure if it is in cold soak configuration when:

1. It is parked in cold weather (Outside Air Temperature (OAT) lower than 0 deg.C (32.00 deg.F) ) and

2. There is no supply of power to the aircraft (no air conditioning).

This procedure also presents a form of reference AMM task. D. Sub-section 5.4 - Critical Design Configuration Control Limitations (CDCCL)

A CDCCL is a limitation requirement to preserve either a critical ignition source prevention feature of the fuel system design or a critical design feature of the flammability reduction system that is necessary to prevent the occurrence of an unsafe condition. The purpose of the CDCCL is to provide instructions to retain the critical ignition source prevention or critical flammability reduction feature during configuration change that may be caused by alterations, repairs, or maintenance actions. A critical ignition source prevention feature may exist in the fuel system and related Installation or in systems that, if a failure condition were to develop, could interact with the fuel system in such a way that an unsafe condition would develop in the fuel system without this limitation. A critical feature that contributes to the integrity of the flammability reduction system may exist in the fuel tank inerting system and related installation that, if not maintained, could compromise the design and lead to an unsafe condition in the fuel system. VAECO are responsible for ensuring that their internal documentation is amended to reflect the data contained within this sub-section and provides appropriate text to highlight the existence of each CDCCL. Such identification is necessary in the instructions used by the person who will be performing an installation, alteration, repair or modification so as to minimize the risk that the work performed compromises the original design criteria. This sub-section is quoted from ALS part 5 – section 2 and collated the reference with aircraft’s configuration. The mandatory requirements are based on the appropriate identification of the CDCCL in the accomplishment instructions associated with the installation, alteration, repair or modification (Reference and Applicability column).


SECTION 5

SPECIAL PROCEDURES

ISSUE: SEP 2013 SUB-SECTION 5.1 – UNSCHEDULE MAINT CHK&INSP PAGE 1

SUB-SECTION 5.1 UNSCHEDULE MAINTENANCE CHECKS AND INSPECTIONS

ITERM

INSPECTIONS AFTER

DESCRIPTION

REFERENCE

1 Airframe vibration / noise in flight

Identification of the Cause of In-Flight Airframe Vibrations and/or Noises.

TSM 05-50-00-810-801

2 Heavy landing Inspection After Hard/Overweight Landing.

AMM 05-51-11-200-004

3

the landing gear extends/retracts at more than the Geardown Limiting Speed

Inspection after Landing Gear Extension at more than the Geardown Limiting Speed

AMM 05-51-12-200-001

4 overspeed warning Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speed

AMM 05-51-13-200-001

5 Airframe Bird / Hail Strike Inspection of the Airframe after a Bird or Hail Strike.

AMM 05-51-14-200-001

6 Wheel / tyre failure Inspection after a Tire Burst or Tread Throw.

AMM 05-51-15-200-001

7 Brake Overheat Inspection After Brake Overheat

AMM 05-51-16-200-001

8 Excessive Load Factor in flight

Inspection after in Flight Excessive Load Factor due to Turbulence or Maneuver or in Excess of VMO/MMO

AMM 05-51-17-200-001

9 Lightning strike Inspection after Lightning Strike.

AMM 05-51-18-200-001

10 Engine bird strike Inspection of the Engine after a Bird Strike or Slush Ingestion.

AMM 05-51-19-200-001

11 Tail Runway Impact Inspection after a Tail Runway Impact.

AMM 05-51-21-200-001

12 NLG Towing Overload / Overrun

Inspection After a NLG Towing Overload or Overrun.

AMM 05-51-22-200-001

13 NLG Steering Angle exceedance

Inspection after NLG Steering Angle of more than 95 deg.

AMM 05-51-23-200-001

14 Aircraft spring out Runway / taxiway during taxi, takeoff or landing.

Inspection after Leaving Runway or Taxiway.

AMM 05-51-24-200-001

15 Flight through Dust Storm / Volcanic Ash / Severe Conditions on Ground

- Inspection after Flight through Dust Storm or Dust Contamination on Ground. - Inspection after Flight through Volcanic Ash or Volcanic Ash

AMM 05-51-25-200-002 AMM 05-51-25-200-003


SECTION 5

SPECIAL PROCEDURES

ISSUE: SEP 2013 SUB-SECTION 5.1 – UNSCHEDULE MAINT CHK&INSP PAGE 2

ITERM

INSPECTIONS

AFTER

DESCRIPTION

REFERENCE

Contamination on Ground.

16 Engine failure Inspection after engine failure AMM 05-51-26-200-001

17 Impact on Engine Cowls Inspection after Impact on Engine Cowls

AMM 05-51-27-200-001

18 Fluid spillage in cargo compartment Procedure after Fluid Spillage AMM

05-51-28-200-002

19 Pax / crew doors abnormal movement

Inspection after Abnormal Movement of the Pax/Crew or Emergency Exit

AMM 05-51-29-200-001

20 Significant MLG vibration at touch-down

Inspection after Significant MLG Vibration at Touch-Down

AMM 05-51-31-200-001

21 Engine Shut-Down in flight Inspection after Engine Windmilling (After Engine In-Flight Shut-Down)

AMM 05-51-34-200-001

22 Impact on Wing Tip/Fence Inspection after Impact on Wing Tip/Fence

AMM 05-51-35-200-001

23 Overweight Taxiing

Inspection after taxiing at a weight that is more than the Maximum design Taxi Weight (MTW)

AMM 05-51-41-200-001

24

The aircraft was in very high winds on the ground (wind speed of more than 80 knots (150 KM/H))

Inspection after Very High Winds on Ground

AMM 05-51-42-200-001

25 Work on System Electrical Installation

Inspection after Work on System Electrical Installation

AMM 05-51-43-700-001

26 Aircraft Operation with High Lateral Acceleration

Inspection after Aircraft Operation with High Lateral Acceleration

AMM 05-51-44-200-001

27 Fluid leak Leaks – Permitted values AMM 05-50-00-790-001

28 Abnormal sign during take-off Lateral Jerk at Take-off TSM

05-50-00-810-823

29 Smell of oil in cabin or Unsatisfactory Cabin Air Quality

Oil in the Air Conditioning System

TSM 21-00-00-810-801


SECTION 5 SPECIAL PROCEDURES

ISSUE: SEP 2013 SUB-SECTION 5.2 PAGE 1

PARKING/STORAGE PROCEDURE

SUB-SECTION 5.2

PARKING / STORAGE PROCEDURES.

1. Parking procedure: Ref. AMM task: 10-11-00-555-006 2. Storage procedure: Ref. AMM task: 10-12-00-553-005


SECTION 5

SPECIAL PROCEDURES

ISSUE: SEP 2013 SUB-SECTION 5.3 PAGE 1 COLD WEATHER MAINTENANCE PROCEDURE

SUB-SECTION 5.3 COLD WEATHER MAINTENANCE PROCEDURE.

Cold Weather Maintenance Procedures: Ref. A320 AMM task: 12-31-00-600-001.


SECTION 5

SPECIAL PROCEDURES


CRITICAL DESIGN CONFGURATION CONTROL LIMITATION

SUB-SECTION 5.4 A321 CRITICAL DESIGN CONFGURATION CONTROL LIMITATION

Itm CDCCL Requirement Reference Applicability

1

Air gap between a fuel quantity indicating probe and the aircraft structure.

Critical to prevent spark generation during lightning strike conditions and must not be compromised The gap stated in the relevant maintenance procedure in the AMM must be achieved during installation of a fuel quantity probe.

AMM 28-42-15-400

ALL

2

Separation of fuel quantity and level indicating system wiring from other wiring.

To prevent cross coupling of high voltage transients and thereby keep unsafe ignition energies from inside the tank it is required that operators obey the wire routing and separation standards given in the Electrical Standard Practices Manual (ESPM).

ESPM 20-10-00 20-33-20 20-33-21 20-33-22

ALL

3 Direct bonding on items of equipment inside a fuel tank.

Direct bonding is critical to prevent spark generation during component failure and lightning strike conditions and must not be compromised. Direct bonding in fuel tanks must be carried out during component installation to the appropriate bonding method and standard stated within the installation procedure in the AMM.

AMM 28-11-37-400 28-11-41-400 28-12-41-400 28-12-45-400 28-12-46-400 28-12-47-400 28-13-43-400 28-15-41-400 28-21-42-400 28-21-43-400 28-21-51-400 28-21-52-400 28-22-51-400 28-25-41-400 28-25-42-400 28-25-46-400 28-25-52-400 28-42-46-400 28-42-47-400 28-42-48-400 28-43-21-400 28-43-22-400 57-27-11-400

A321 Post 25453 ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL

4 Safety critical features of fuel pumps

These features must be maintained throughout the full life of the fuel pump to avoid the possibility of generation of an ignition source by overheating or sparks caused by arcing, friction etc.

CMM 28-20-40 28-21-51 28-22-19 28-24-11

A321 With ACT ALL ALL ALL


SECTION 5

SPECIAL PROCEDURES


CRITICAL DESIGN CONFGURATION CONTROL LIMITATION

Itm CDCCL Requirement Reference Applicability

Repair and overhaul of fuel pumps must be carried out in accordance with the equipment manufacturer’s maintenance instructions or other maintenance instructions acceptable to the certifying authority.

5 Centre fuel tank volume and ventilation flow rate

The volume of the centre fuel tank and the flow rate of the ventilation system must be maintained at values which, when used in the determination of the fuel tank flammability exposure, comply with the fuel tank inerting system requirements.

N/A A321 Post 38062

6

Protective coating on fuel tank at the connection of fuel tank inerting ystem

A protective coating (Finch paint) is necessary at the connection between the centre fuel tank and the dual flapper check valves’ housing of the Inert Gas Generating System (IGGS) to prevent fuel or fuel vapour leaks into an area containing ignition sources. After maintenance of the dual flapper check valves the protective coating must be restored to the appropriate standard using the method stated within the maintenance procedure in the AMM.

AMM 47-20-43-400 47-20-43-700

A321 Post 38062

7

Warning Placards for areas that may contain oxygen depleted atmospheres.

Warning placards installed to ensure maintenance personnel are aware of areas that may be hazardous because of possible oxygen depleted atmosphere, must be ensured to be present in the designated positions.

AMM 57-17-11-000 57-17-11-400 28-12-47-000 28-12-47-400

A321 Post 150837

Documents

AMS Issue 14 Amendment 01