AIRWORTHINESS LIMITATIONS – LINE NUMBER SPECIFIC …

LINE NUMBER SPECIFIC

ils Page 1.0-1

SPECIFIC

E991.Export ort license may be required before it is used for

sponsibility to abide by all export laws.

Boeing cla right in this document as a compilation and/or collective work. This the information it contains is governed by contract with Boeing. F 07, 717, 727, 737, 747, 757, 767, 777, 787, BBJ, DC-8,

DC-9, D trademark license is granted in connection with this

AUG 2

767-200/300/300F/400ER AIRWORTHINESS LIMITATIONS -

D622T001-9-02BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for deta

EXPORT CONTROLLED - EAR ECCN: 9E991

767-200/300/300F/400ERAIRWORTHINESS LIMITATIONS – LINE NUMBER

D622T001-9-02

AUGUST 2020This document has EAR data with an Export Control Classification Number (ECCN) of 9

of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An expdevelopment, production or use by foreign persons from specific countries. The controller of this data has the individual re

ims copyright in each page of this document on to the extent that the page contains copyrightable subject matter. Boeing also claims copy document includes proprietary information owned by the Boeing Company and/or one or more third parties. Treatment of the document andor more information, contact the Boeing Company, P.O. Box 3707, Seattle WA 98124. Boeing, the Boeing signature, the Boeing symbol, 7C-10, MD-10, MD-11, MD-80, MD-88, MD-90, and the red-white-blue Boeing livery are all trademarks owned by The Boeing Company; no

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COMPILED AND PUBLISHED BY:MAINTENANCE PROGRAMS ENGINEERINGBOEING COMMERCIAL AIRPLANE GROUP

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020

details Page 1.0-2

S - LINE NUMBER SPECIFIC

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D622T001-9-02
BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for EXPORT CONTROLLED - EAR ECCN: 9E991

767-200/300/300F/400ER AIRWORTHINESS LIMITATION

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REVIS .............................................................. 1.0-5

LIST O .............................................................. 1.0-8

A. IND .............................................................. 1.0-9

B. INS .............................................................. 1.1-1

SEP 20




TABLE OF CONTENTS

IONS ....................................................................................................................................................................

F EFFECTIVE PAGES ........................................................................................................................................

IVIDUAL AIRPLANE – LINE NUMBER SPECIFIC AIRWORTHINESS LIMITATIONS.........................................

PECTION AREA ILLUSTRATIONS ......................................................................................................................

19

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July 2014

Original R

This revi

Please s

Decembe

Revised ing Message Number shown in the Inspection Requirem

Added su

March 20

Added su

June 201

Added su

Added su

Septemb

Added su

Added su

August 2

Deleted t 9/AWL/CMR/SCI documents. Submittal signature

Added su

March 20

Added su

June 201

Added su

Added su

AUG 2




REVISIONS

REVISION DESCRIPTION

elease

sion contains no technical changes.

ee the 767 MPD Section 9, D622T001-9 for historical Revision Log information.

r 2014

Line Number 269 in the Supplemental Structural Fatigue Inspection Requirements Table in Section A by correcting the Boeents column. No technical changes were made.

pplemental inspection information for Line Number 1077 and corresponding Figure 1 as a result of NCR N1690269746.

15


5



er 2015



016

he FAA Approval signature column from the Revision Log to improve the layout and provide consistency across all Sections will no longer be included in the Revision Log.


17


7



020

details Page 1.0-6


Nov

Add 32.

May

Rev

Add

Aug

Add 62.

Sep

Add 76.

Nov

Add 18.

Add 81.

Dec

Add 14.

Febr

Add 21.

Apri

Rev in the DTR Check Form Title and Inspection Req

Add 62.

June

Add 38.

Sep

Add

Add 11.

AU
D622T001-9-02


ember 2017

ed supplemental inspection information for Line Number 1140 and corresponding Figure 11 as a result of NCR N16904721

2018

ised document header from 767 to 767-200/300/300F/400ER to list all derivatives.

ed supplemental inspection information for Line Number 1153 as a result of NCR N1690536736.

ust 2018


tember 2018


ember 2018



ember 2018


uary 2019


l 2019

ised the table entry for Line Number 1090 to correct 53-10-I07D/53-30-I04D/53-60-I05D from “Upper Row” to “Lower Row” uirements columns.


2019


tember 2019

a new Table of Contents entry, “Inspection Area Illustrations”.


REVISIONS


G 2020


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October

Added su 58151.

March 20

Revised y also be revised with approval of The Boeing Compan

Revised rmed due to repairs/modifications, alternative inspectio

Added su

Added su

Added su

August 2

Added su

AUG 2




2019

pplemental inspection information for Line Number 1197 and corresponding Figures 21 and 22 as a result of NCR N16906

20

Section A. Individual Airplane - Line Number Specific Airworthiness Limitations to specify that Airworthiness Limitations may ODA as delegated.

Section A. Individual Airplane - Line Number Specific Airworthiness Limitations to require that if inspections cannot be perfons must be approved by the FAA Oversight Office or The Boeing Company ODA as delegated.




020


REVISIONS


020

Section Page Date Section Page Date Section Page Date Section Page Date Section Page Date

D622T001-9-02BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for details Page 1.0-8


LIST OF EFFECTIVE PAGES767-200/300/300F/400ER AIRWORTHINESS LIMITATIONS - LINE NUMBER SPECIFIC

1.0 1 AUG 20201.0 2 BLANK1.0 3 SEP 20191.0 4 BLANK1.0 5 AUG 20201.0 6 AUG 20201.0 7 AUG 20201.0 8 AUG 20201.0 9 MAR 20201.0 10 DEC 20141.0 11 DEC 20141.0 12 MAR 20151.0 13 APR 20191.0 14 SEP 20181.0 15 JUN 20191.0 16 MAR 20201.0 17 AUG 20201.0 18 BLANK1.1 1 DEC 20141.1 2 MAR 20151.1 3 JUN 20151.1 4 JUN 20151.1 5 SEP 20151.1 6 SEP 20151.1 7 AUG 20161.1 8 MAR 20171.1 9 JUN 20171.1 10 JUN 20171.1 11 NOV 20171.1 12 AUG 20181.1 13 SEP 20181.1 14 NOV 20181.1 15 NOV 20181.1 16 DEC 20181.1 17 FEB 20191.1 18 APR 20191.1 19 JUN 20191.1 20 SEP 20191.1 21 OCT 2019

1.1 22 OCT 20191.1 23 MAR 20201.1 24 MAR 20201.1 25 MAR 20201.1 26 AUG 2020

AUG 2020


ils Page 1.0-9

A. INDIV

PUR

The ctural Fatigue Inspection requirements

uniq d AWLs. These additional or revised

AWL

The red under Title 14 Code of Federal

Reg

The e approval of the FAA Oversight Office

or Th epairs and/or modifications, an

alter any ODA as delegated.

The al line number airplanes. Each item is

listed n Requirements and Type/Threshold.

MAR 2




IDUAL AIRPLANE – LINE NUMBER SPECIFIC AIRWORTHINESS LIMITATIONS

POSE

purpose of this document is to identify additional or revised Airworthiness Limitation (AWL) Supplemental Stru

ue to a specific airplane. Only those individual airplanes listed in this document have these additional or revise

s are due to differences in configuration as a result of Material Review Board actions.

Airworthiness Limitations - Line Number Specific document is FAA-approved and specifies maintenance requi

ulations (CFR) § 43.16 and § 91.403, unless an alternative program has been FAA Oversight Office approved.

Airworthiness Limitations - Line Number Specific inspections or maintenance tasks may only be revised with th

e Boeing Company ODA as delegated. If an inspection or maintenance task cannot be accomplished due to r

native inspection or maintenance task must be approved by the FAA Oversight Office or by The Boeing Comp

following table lists the additional Supplemental Structural Fatigue Inspection requirements for certain individu

by Line Number, Structural Significant Item (SSI) Number, DTR Check Form Title, Inspection Zone, Inspectio

020

details Page 1.0-10


LiNum ion Requirements Type and

Threshold26 o: STA 654 + 22 to 654 + 110 must be

9-0008-01B (R1) 20 April 2009.Type 2

37,500 FC

87 icable to: STA 1197+82 and 1197+121, B 767-53-0103.

Type 230,000 FC

87 icable to: STA 1197+82 and 1197+121, B 767-53-0103.

Type 230,000 FC

94 icable to: STA 617 S-8R. Must Inspect Type 237,500 FC

94 icable to: STA 617 S-8R. Must Inspect Type 237,500 FC

94 icable to: STA 1175-1197, S-26R. Must 1.

Type 237,500 FC

94 icable to: STA 1175-1197, S-26R. Must 1.

Type 237,500 FC

96 icable to: STA 1465-1476, STR 8L. 53-0208

Type 237,500 FC

96 icable to: STA 1465-1476, STR 8L. 53-0208

Type 237,500 FC

96 icable to: STA 1564 - 1582, STR 26R. 3-0212.

Type 237,500 FC

96 icable to: STA 1564 - 1582, STR 26R. 3-0212.

Type 237,500 FC

DE
D622T001-9-02


ne ber SSI Number DTR Check Form Title Inspection

Zone Inspect

9 53-30-I04D BCF 1 – Skin Longitudinal Lap Splices – Lower Row – Bilge S-26L MDCD and L2 Panel

100 DTR Form not applicable tinspected per TBC-ANA-0

3 53-10-I07C53-30-I04C53-60-I05C

Skin Longitudinal Lap Splices – Upper Row – Bilge and Lower Lobe, Sections 41, 43 and 46.

100 DTR Check Form not applS-36R. Must inspect per S

3 53-10-I07D53-30-I04D53-60-I05D

Skin Longitudinal Lap Splices – Lower Row – Bilge and Lower Lobe, Sections 41, 43 and 46.

100 DTR Check Form not applS-36R. Must inspect per S

5 53-10-I07A53-30-I04A53-60-I05A

Skin Longitudinal Lap Splices – Upper Row – Crown and Upper Lobe, Sections 41, 43 and 46.

220230250

DTR Check Form not applper SB 767-53-0190

5 53-10-I07B53-30-I04B53-60-I05B

Skin Longitudinal Lap Splices – Lower Row – Crown and Upper Lobe, Sections 41, 43 and 46.

220230250

DTR Check Form not applper SB 767-53-0190

6 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applinspect per SB 767-53-019

6 53-10-I07D53-30-I04D53-60-I05D



3 53-10-I07A53-30-I04A53-60-I05A


220230250

DTR Check Form not applMust Inspect per SB 767-

3 53-10-I07B53-30-I04B53-60-I05B


220230250

DTR Check Form not applMust Inspect per SB 767-

7 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applMust inspect per SB 767-5

7 53-10-I07D53-30-I04D53-60-I05D



C 2014


ils Page 1.0-11

969 e to: from STA 1408 to 1417 7-53-0210.

Type 250,000 FC

969 e to: From STA 1408 to 1417 7-53-0210.

Type 250,000 FC

969 e to: S-4R from STA 758 to STA 767-53-0210.

Type 250,000 FC

971 to: Lap S-26L: BS 654 + 22 to BS ect per SB 767-53-0211.

Type 250,000 FC

971 to: Lap S-26L: BS 654 + 22 to BS ect per SB 767-53-0211.

Type 250,000 FC

973 e to: Lap S-8R, STA 1555. Must Type 250,000 FC

973 e to: Lap S-8R, STA 1555. Must Type 250,000 FC

994 e to: Lap S-26R: STA 1417. Must Type 250,000 FC

994 e to: Lap S-26R: STA 1417. Must Type 250,000 FC

1004 e to: BS 1464 to BS 1478, S-8R. 38.

Type 250,000 FC

1004 e to: BS 1464 to BS 1478, S-8R. 38.

Type 250,000 FC

Line Number Requirements Type and

Threshold

DEC 2




53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applicablS-26R: Must inspect per SB 76

53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applicablS-26R: Must inspect per SB 76

53-30-I0153-50-I0153-60-I01

Fuselage Crown Stringers – BS 654 to BS 1395, S-8L to S-8R

230240250

DTR Check Form not applicabl770. Must be inspected per SB

53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applicable654 + 44 and S-26L. Must insp

53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applicable654 + 44 and S-26L. Must insp

53-10-I07A53-30-I04A53-60-I05A


220230250

DTR Check Form not applicablInspect per SB 767-53-0231.

53-10-I07B53-30-I04B53-60-I05B


220230250

DTR Check Form not applicablInspect per SB 767-53-0231.

53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applicablinspect per SB 767-53-0230.

53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applicablinspect per SB 767-53-0230.

53-10-I07A53-30-I04A53-60-I05A


220230250

DTR Check Form not applicablMust Inspect per SB 767-53-02

53-10-I07B53-30-I04B53-60-I05B


220230250

DTR Check Form not applicablMust Inspect per SB 767-53-02

SSI Number DTR Check Form Title Inspection Zone Inspection

014

details Page 1.0-12


10 icable to: Lap S-26L: BS 303, 325, 347, SB 767-53-0240.

Type 240,000 FC

10 cable to: Lap S-26L: BS 292 to BS 314. 3-0244.

Type 250,000 FC

10 icable to: Lap S-26L: BS 292 to BS 314 3-0244.

Type 250,000 FC

10 icable to: Lap S-36L: STA 775-786. 3-0243.

Type 240,000 FC

10 icable to: Lap S-26R: STA 1562. Must 2.

Type 250,000 FC

10 icable to: Lap S-8L: STA 604. Must 6.

Type 250,000 FC

10 icable to: Lap S-8L: STA 604. Must 6.

Type 250,000 FC


Type 250,000 FC


Type 250,000 FC

10 icable to: Lap S-26R: STA 654 + 66. 53-30-I04D-N1690269746 - Lap Splice N1690269746.

Type 240,000 FC

10 icable to: Lap S-8L: STA 1533. 53-60-I05B-N1690285938 - Lap Splice N1690285938.

Type 240,000 FC


Threshold

MA
D622T001-9-02


08 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not appland 368. Must inspect per

19 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not appliMust inspect per SB 767-5

19 53-10-I07D53-30-I04D53-60-I05D



20 53-10-I07D53-30-I04D53-60-I05D



40 53-10-I07C53-30-I04C53-60-I05C



47 53-10-I07A53-30-I04A53-60-I05A


220230250

DTR Check Form not applinspect per SB 767-53-025

47 53-10-I07B53-30-I04B53-60-I05B


220230250

DTR Check Form not applinspect per SB 767-53-025

55 53-10-I07C53-30-I04C53-60-I05C



55 53-10-I07D53-30-I04D53-60-I05D



77 53-10-I07D53-30-I04D53-60-I05D

Skin Longitudinal Lap Splices – Lower Row – Bilge and Lower Lobe, Sections 41, 43, and 46.

100 DTR Check Form not applMust inspect per Figure 1: Lower Row Rework, NCR

82 53-10-I07B53-30-I04B53-60-I05B

Skin Longitudinal Lap Splices - Lower Row - Crown and Upper Lobe, Sections 41, 43, and 46.

220230250

DTR Check Form not applMust inspect per Figure 2: Lower Row Rework, NCR


Zone Inspect

R 2015


ils Page 1.0-13

1086 e to: Lap S-26L: STA 1197+79 and

0-I05C-N1690293868 - Lap Splice 0293868.

Type 240,000 FC

1087 e to: Lap S-26R: STA 1557.0-I05C/D-N1690296581 - Lap R N1690296581.

Type 240,000 FC

1087 e to: Lap S-26R: STA 1557. 0-I05C/D-N1690296581 - Lap R N1690296581.

Type 240,000 FC

1090 e to: Lap S-36R: STA 654+88. 0-I05C/D-N1690305281 - Lap R N1690305281.

Type 240,000 FC

1090 e to: Lap S-36R: STA 654+88. 0-I05C/D-N1690305281 - Lap R N1690305281.

Type 240,000 FC

1090 at WL 218, RBL 77. Must inspect - N1690304512- Pressure Dome

Type 240,000 FC

1110 e to: Lap S-26L: STA 720. 90368107 - S-26L Lap Splice

Type 240,000 FC

1110 e to: Lap S-26L: STA 720. 90368107 - S-26L Lap Splice

Type 240,000 FC

1123 e to: Lap S-8L, STA 698. 0-I04A - NCR N1690415876 ir at STA 698.

Type 240,000 FC

1123 e to: Lap S-8L, STA 698. 0-I04A - NCR N1690415876 ir at STA 698.

Type 240,000 FC

1130 e to: Lap S-26L, STA 1268. 0-I05C/D - NCR N1690436086 air at STA 1268.

Type 240,000 FC


Threshold

APR 20




53-10-I07C53-30-I04C53-60-I05C

Skin Longitudinal Lap Splices - Upper Row - Bilge and Lower Lobe, Sections 41, 43 and 46.

100 DTR Check Form not applicablSTA 1197+126.Must inspect per Figure 3: 53-6Upper Row Rework, NCR N169

53-10-I07C53-30-I04C53-60-I05C

Skin Longitudinal Lap Splices - Upper Row - Bilge and Lower Lobe, Sections 41, 43 and 46

100 DTR Check Form not applicablMust inspect per Figure 4: 53-6Splice Lower Row Rework, NC

53-10-I07D53-30-I04D53-60-I05D

Skin Longitudinal Lap Splices - Lower Row - Bilge and Lower Lobe, Sections 41, 43 and 46.

100 DTR Check Form not applicablMust inspect per Figure 4: 53-6Splice Lower Row Rework, NC

53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applicablMust inspect per Figure 5. 53-3Splice Upper Row Rework, NC

53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applicablMust inspect per Figure 5. 53-3Splice Lower Row Rework, NC

53-80-I01_MRB1 Pressure Dome Web, STA 1582 100 Repair to inner surface of web per Figure 6: 53-80-I01_MRB1Rework, NCR N1690304512.

53-10-I07C53-30-I04C53-60-I05C

Skin Longitudinal Lap Splices - Upper Row - Bilge and Lower Lobe, Section 41, 43, and 46

100 DTR Check Form not applicablMust inspect per Figure 7: N16Internal repair.

53-10-I07D53-30-I04D53-60-I05D

Skin Longitudinal Lap Splices - Lower Row - Bilge and Lower Lobe, Section 41, 43, and 46

100 DTR Check Form not applicablMust inspect per Figure 7: N16Internal repair.

53-10-I07A53-30-I04A53-60-I05A

Skin Longitudinal Lap Splices - Upper Row - Crown and Upper Lobe, Section 41, 43, and 46

200 DTR Check Form not applicablMust inspect per Figure 8: 53-3- S-8L Lap Splice Internal Repa

53-10-I07B53-30-I04B53-60-I05B

Skin Longitudinal Lap Splices - Lower Row - Crown and Upper Lobe, Section 41, 43, and 46

200 DTR Check Form not applicablMust inspect per Figure 8: 53-3- S-8L Lap Splice Internal Repa

53-10-I07C53-30-I04C53-60-I05C

Skin Longitudinal Lap Splices – Upper Row – Bilge and Lower Lobe, Sections 41, 43 and 46

100 DTR Check Form not applicablMust inspect per Figure 9: 53-6- S-26L Lap Splice Internal Rep


19

details Page 1.0-14


11 icable to: Lap S-26L, STA 1268. 53-60-I05C/D - NCR N1690436086 l Repair at STA 1268.

Type 240,000 FC

11 icable to: Lap S-36R, STA 1484. : 53-60-I05C/D - NCR N1690447322 - Repair at STA 1484.

Type 240,000 FC

11 icable to: Lap S-36R, STA 1484. : 53-60-I05C/D - NCR N1690447322 - Repair at STA 1484.

Type 240,000 FC

11 icable to: Lap S-26L, : 53-60-I05C/D - NCR N1690472132 – epair at STA 1369

Type 240,000 FC

11 icable to: Lap S-26L, : 53-60-I05C/D - NCR N1690472132 – epair at STA 1369

Type 240,000 FC

11 icable to: BS 1065.rocedure at all 53-50-I03A locations the inspection interval must be 12,000

Type 240,000 FC

11 icable to: Lap S-26L, between STA inspect per Figure 12: 53-60-I05C/D - L Lap Splice Internal Repair at

Type 240,000 FC

11 icable to: Lap S-26L, between STA inspect per Figure 12: 53-60-I05C/D - L Lap Splice Internal Repair at

Type 240,000 FC

11 icable to: Lap S-26L, between st inspect per Figure 13: 0552176 - S-26L Lap Splice Internal

Type 240,000 FC

11 icable to: Lap S-26L, between st inspect per Figure 13: 0552176 - S-26L Lap Splice Internal

Type 240,000 FC


Threshold

SE
D622T001-9-02


30 53-10-I07D53-30-I04D53-60-I05D

Skin Longitudinal Lap Splices – Lower Row – Bilge and Lower Lobe, Sections 41, 43 and 46

100 DTR Check Form not applMust inspect per Figure 9:- S-26L Lap Splice Interna

33 53-10-I07C53-30-I04C53-60-I05C

Skin Longitudinal Lap Splices - Upper Row - Bilge and Lower Lobe, Sections 41, 43 and 46

100 DTR Check Form not applMust inspect per Figure 10S-36R Lap Splice Internal

33 53-10-I07D53-30-I04D53-60-I05D

Skin Longitudinal Lap Splices - Lower Row - Bilge and Lower Lobe, Sections 41, 43 and 46

100 DTR Check Form not applMust inspect per Figure 10S-36R Lap Splice Internal

40 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not appl Must inspect per Figure 11S-26L Lap Splice Internal R

40 53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not appl Must inspect per Figure 11S-26L Lap Splice Internal R

53 53-50-I03A Fuselage Circumferential Splices in the Body Crown BS 1065 and BS 785.9, S-4L/R to S-5L/R.

240250

DTR Check Form not applInspect using 53-50-I03A pcommon to STA 1065, but flight cycles or less.

61 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not appl1175 and STA 1197. Must NCR N1690545562 - S-26STA 1187

61 53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not appl1175 and STA 1197. Must NCR N1690545562 - S-26STA 1187

65 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applSTA 390 and STA 412. Mu53-10-107C/D - NCR N169Repair at STA 407.

65 53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applSTA 390 and STA 412. Mu53-10-107C/D - NCR N169Repair at STA 407.


Zone Inspect

P 2018


ils Page 1.0-15

1169 e to: Lap S-8L, between STA 1329 r Figure 14: 53-60-I05A/B - NCR e Internal Repair at STA 1341

Type 240,000 FC

1169 e to: Lap S-8L, between STA 1329 r Figure 14: 53-60-I05A/B - NCR e Internal Repair at STA 1341

Type 240,000 FC

1169 e to: Lap S-26R, between STA spect per Figure 15: 53-30-I04C/D ap Splice External Repair at STA

Type 240,000 FC

1169 e to: Lap S-26R, between STA spect per Figure 15: 53-30-I04C/D ap Splice External Repair at STA

Type 240,000 FC

1171 etween STA 977 and STA 999, tions per Figure 16: 53-50- - Pressure Deck Web, STA 977 to ly.

Type 240,000 FC

1177 e to: Lap S-26R, between ust inspect per Figure 17: 321 - S-26R Lap Splice

1

Type 240,000 FC

1177 e to: Lap S-26R, between ust inspect per Figure 17: 321 - S-26R Lap Splice

1

Type 240,000 FC

1180 e for Left Hand Side. tion every 12,000 Flight Cycles. 3B - NCR N1690605962.

Type 125,000 FC

1186 e to: Lap S-26R, between STA 698 r Figure 19: 53-30-I04C/D

Type 240,000 FC

1186 e to: Lap S-26R, between STA 698 r Figure 19: 53-30-I04C/D

Type 240,000 FC


Threshold

JUN 20




53-10-I07A53-30-I04A53-60-I05A

Skin Longitudinal Lap Splices - Upper Row - Crown and Upper Lobe, Sections 41, 43 and 46.

100 DTR Check Form not applicabland STA 1351. Must inspect peN1690575718 - S-8L Lap Splic

53-10-I07B53-30-I04B53-60-I05B

Skin Longitudinal Lap Splices - Lower Row - Crown and Upper Lobe, Sections 41, 43 and 46.

100 DTR Check Form not applicabland STA 1351. Must inspect peN1690575718 - S-8L Lap Splic

53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applicabl654+110 and STA 676. Must in- NCR N1690567481 - S-26R L654+121

53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applicabl654+110 and STA 676. Must in- NCR N1690567481 - S-26R L654+121

53-50-51_MRB Wheel Well Pressure Deck Web

NOTE: No existing DTR Check Form with this title.100 Repair to pressure deck web b

RBL 30, approximately. Inspec51_MRB - NCR N1690580814STA 999, RBL 30, approximate

53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applicablSTA 1197 and STA 1197+22. M53-60-I05C/D - NCR N1690593External Repair at STA 1197+1

53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applicablSTA 1197 and STA 1197+22. M53-60-I05C/D - NCR N1690593External Repair at STA 1197+1

53-50-I13B Fuselage Rear Spar Bulkhead - Side Frame Fitting Inner Chord - BS 955, S-20 to S-21 at Seat Track Support Bracket.

100 DTR Check Form not applicablPerform Detailed Visual InspecInspect per Figure 18: 53-50-I1

53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not applicabland STA 720. Must inspect pe- NCR N1690619138.

53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not applicabland STA 720. Must inspect pe- NCR N1690619138.


19

details Page 1.0-16


11 icable to: Lap S-26R between STA 698 t per Figure 20: 53-30-I04C/D - NCR

Type 240,000 FC

11 icable to: Lap S-26R between STA 698 t per Figure 20: 53-30-I04C/D - NCR

Type 240,000 FC

11 icable to: Lap S-26L between STA st inspect per Figures 21 and 22:

0658151.

Type 240,000 FC

11 icable to: Lap S-26L between STA st inspect per Figures 21 and 22:

0658151.

Type 240,000 FC

12 icable to: Lap S-26L between STA 753 t per Figure 23: 53-30-I04C/D - NCR

Type 240,000 FC


Type 240,000 FC


Type 240,000 FC


Type 240,000 FC

12 icable to: Lap S-26L between STA 325 ect per Figure 25: 53-10-I07C/D - NCR Splice Internal Repair at STA 347.

Type 240,000 FC

12 icable to: Lap S-26L between STA 325 ect per Figure 25: 53-10-I07C/D - NCR Splice Internal Repair at STA 347.

Type 240,000 FC


Threshold

MA
D622T001-9-02


95 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not appland STA 742. Must inspecN1690650111.

95 53-10-I07D53-30-I04D53-60-I05D



97 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not appl654+110 and STA 676. Mu53-30-I04C/D - NCR N169

97 53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not appl654+110 and STA 676. Mu53-30-I04C/D - NCR N169

09 53-10-I07C53-30-I04C53-60-I05C



09 53-10-I07D53-30-I04D53-60-I05D



12 53-10-I07C53-30-I04C53-60-I05C



12 53-10-I07D53-30-I04D53-60-I05D



14 53-10-I07C53-30-I04C53-60-I05C


100 DTR Check Form not appland STA 347+2. Must inspN1610113314 - S-26L LAP

14 53-10-I07D53-30-I04D53-60-I05D


100 DTR Check Form not appland STA 347+2. Must inspN1610113314 - S-26L LAP


Zone Inspect

R 2020


ils Page 1.0-17

1217 C inspection of the upper wingad fitting, on the left wing, as0-I27-N1680112904, inmanual D634T301, Part 6, 51- 6, 51-00-14 for the fitting. inspection is 9,300 flightt hours (FH) <1>.

quirements for SSI 57-20-I27nt, D622T001-9-01 for the left

fore further flight, repair thepproved in accordance with paragraph (j) of AD 2012-08-oeing Service Bulletin 767-d to the left wing of this

e ACO Branch has approved the spection program for SSI Number thod of Compliance (AMOC) to the, as required by Paragraph (g) of12-08-14.

that are not specifically ent remain fully applicable and proval is applicable only to Boeing with Line Number 1217.This FAA irplane to other operators. Before propriate principal inspector, or

e manager of the local flight te holding district office. This able as long as the requirements ber 57-20-I27 for 767-300F Line

The Seattle ACO Branch will ACO Branch later determines that acceptable level of safety.

Type 114,500 FC

or 43,500 FH <1>

<1>


Threshold

AUG 2




57-20-I27 Skin Tab at Front Spar Pitch Load Fitting 511 1. Perform an open hole HFEskin and front spar pitch loshown per Figure 26. 57-2accordance with 767 NDT 00-16 for the skin and PartThe repeat interval for thiscycles (FC), or 27,900 fligh

2. This inspection fulfills the recontained in AWL Documewing only.

3. If any cracking is found, becracking using a method athe procedures specified in14. The repairs shown in B57A0117 cannot be applieairplane.

AMOC:

The Manager of the FAA Seattlaccomplishment of the above in57-20-I27, as an Alternative Meinspections on the left wing onlyAirworthiness Directive (AD) 20

All provisions of AD 2012-08-14referenced in the above statemmust be complied with. This apModel 767-300F series airplaneAMOC is transferable with the ausing this AMOC, notify your aplacking a principal inspector, thstandards district office/certificaAMOC remains valid and applicspecifically identified in SSI NumNumber 1217 are not changed.revoke this AMOC if the Seattlethis AMOC does not provide an

Whichever comes first


020

D622T001-9-02BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for details Page 1.0-18


767-200/300/300F/400ER AIRWORTHINESS LIMITATIONS - LINE NUMBER SPECIFIC


BLANK


ils Page 1.1-1

B. INSP

N1690269746

-30-I04D (Lower Fastener Row) guidelines. The use of a 0.25” minimum of 270° inspection at ° inspection must be terval remains the same as

n per 53-30-I04D is no longerrnal LFEC inspection option k area, including 2 fasteners

s not allowed at freeze plug

r SSI item 53-30-I04C (Upperted by the repair. Inspections still applicable and must be

st be inspected per SSI 53-30-I04D. ns remain valid.

DEC 2




ECTION AREA ILLUSTRATIONS

FIGURE 1. 53-30-I04D-N1690269746 – Lap Splice Lower Row Rework, NCR

Perform NDT inspections mandated by SSI 53using NDT manual D634T301 Part 6 53-00-06spot probe is recommended, this will allow a freeze plug repair location. A minimum of 270accomplished. The inspection threshold and instated in SSI 53-30-I04D DTR Check Form.

Note that the HFEC option inspectioapplicable at rework area. Only exteshould be used at freeze plug reworAFT and 4 fasteners FWD.Open-hole HFEC inspection option ilocation.Note that inspections mandated peFastener Row) have not been affecper DTR Check form 53-30-I04C areaccomplished.Areas outside the shaded region muAll DTR check form inspection optio

90° max. is shown

0.25” diameter Probe shown

014

details Page 1.1-2


CR N1690285938

I 53-60-I05B (Lower 1 Part 6 53-00-06

s recommended, this will eze plug repair location. A mplished. The spot probe outside the retaining

tion per 53-60-I05B is no Only external LFEC at freeze plug rework

n is not allowed at freeze

per SSI item 53-60-I05A een affected by the repair. 3-60-I05A are still

shed. outside the shaded

53-60-I05B. All DTR check alid.

ernal skin within 5 inches of cessary.

tive Flight Cycles

s

N1690285938

767Fuselage-15-003Attachment /2/

MA
D622T001-9-02


FIGURE 2. 53-60-I05B-N1690285938 - Lap Splice Lower Row Rework, N

Perform NDT inspections mandated by SSFastener Row) using NDT manual D634T30guidelines. The use of a 0.25” spot probe iallow a minimum of 270° inspection at freminimum of 270° inspection must be accomust contact the skin and inspect the areawasher.

Note that the HFEC option inspeclonger applicable at rework area.inspection option should be usedarea. Open-hole HFEC inspection optioplug location. Note that inspections mandated (Upper Fastener Row) have not bInspections per DTR Check form 5applicable and must be accompliAreas in the Lap Splice Lower Rowregion must be inspected per SSIform inspection options remain v

Perform Detailed Visual Inspection on extretaining washer. No removal of parts ne

Inspection Threshold: 40,000 Cumula

Inspection Interval: 3,000 Flight Cycle

Figure 2. 53-60-I05B-N1690285938 - Lap Splice Lower Row Rework, NCR

R 2015


ils Page 1.1-3

N1690293868

S-25L

S-26L

S-27L

I 53-60-I05C (Upper Fastener art 6, 51-00-01 or 51-00-19 ntact the skin and inspect the freeze plugs.

t allowed at freeze plug

ide the shaded region must check form inspection shaded region.

I item 53-60-I05D (Lower the repair. Inspections per cable and must be

external skin within 5 inches

lug in Shank Skin

inch pical

JUN 20




FIGURE 3. 53-60-I05C-N1690293868 - Lap Splice Upper Row Rework, NCR

Stringer

Lower Skin Edge

5 inch Typical

Upper Skin Edge

Countersunk Freeze Plug in Upper Skin and Straight Shank

Freeze Plug in Lower Skin(2 Places)

UP

FWD

Perform NDT inspections mandated by SSRow) using 767 NDT Manual D634T301 Pguidelines. The inspection probe must coarea outside the edge of the countersunk(Reference NCR N1690293868)

Open-hole HFEC inspection option is nolocations.

Areas in the Lap Splice Upper Row outsbe inspected per SSI 53-60-I05C. All DTR options remain valid for areas outside the

Note that inspections mandated per SSFastener Row) have not been affected byDTR Check form 53-60-I05D are still appliaccomplished.

Perform Detailed Visual Inspection of theof the freeze plugs.

Inspection Threshold: 40,000 Cumulative Flight Cycles

Inspection Interval: 6,000 Flight Cycles

Inspection ProbeCountersunk Freeze

Plug (2 Places)

Straight Shank Freeze Plug (2 Places)3/16 inch Fastener

Hole (2 Places)

Upper SkinLower Skin

0.4 inch

0.47 inch

A-ANot to Scale

Similar for Repair Between STA 1197+110 and 1197+132

Countersunk Freeze PUpper Skin and Straight

Freeze Plug in Lower(4 Places)

5TyA A

Retaining Washer (2 Places)

15

details Page 1.1-4


NCR N1690296581

with 767 NDT

still applicable

5D; refer to

, iller

JU
D622T001-9-02


FIGURE 4. 53-60-I05C/D-N1690296581 - Lap Splice Lower Row Rework,

2 inch Typical

Perform Detailed Visual Inspection of the upper and lower skin surfaces externally within 2 inches of all repair parts.

Perform High Frequency Eddy Current NDT inspection of the upper and lower skin surfaces externally in accordanceManual D634T301 Part 6, 51-00-01 or 51-00-19 guidelines.

All inspections mandated by SSI 53-60-I05C (Upper Fastener Row) and SSI 53-60-I05D (Lower Fastener Row) areand must be accomplished, with the exception of the area within the doubler profile.Note: Inspection Threshold and Inspection Interval shown above does not apply to SSI 53-60-I05C and SSI 53-60-I0D622T001-9-01 and D622T001-DTR for inspection requirements.

Structural Repair Filler

Repair Filler (Lower Skin)

Repair Filler (Upper Skin)

Repair Doubler

Repair Tear Strap Splice

Lower Tear Strap Trim Line

Inspection Threshold: 40,000 Cumulative Flight Cycles Inspection Interval: 12,000 Flight Cycles

Up

Forward

Drawing FastenerRepair Fastener

Note: All repair parts are internalexcept for the upper skin repair f

N 2015


ils Page 1.1-5

R N1690305281

SEP 20




FIGURE 5. 53-30-I05C/D-N1690305281 - Lap Splice Upper Row Rework, NC

15

details Page 1.1-6


CR N1690304512

SE
D622T001-9-02


FIGURE 6. 53-80-I01_MRB1 - N1690304512- Pressure Dome Rework, N

WL218

RBL77

5” Typ.

P 2015


ils Page 1.1-7

CR N1690368107

Add rows here

ncy Eddy Current Inspection of the surfaces externally in accordance with 4T301 Part 6, 51-00-01 or 51-00-19 of 12,000 FC.

urface inspection cannot be performed Low Frequency Eddy Current er and lower skin surfaces internally in NDT manual Part 6, 51-00-07 of 6,000 FC.

al Inspection of the upper and lower lly within 2 inches of the repair parts.

ed by SSI 53-30-104C (Upper I 53-30-104D (Lower Fastener Row) must be accomplished, with the ithin the doubler profile. Note: d inspection interval shown above do 104C and SSI 53-30-104D, refer to 22T001-DTR for inspection

40,000 FC

AUG 2




FIGURE 7. 53-60-I05C - N1690368107 - S-26L Lap Splice Repair at STA 720, N

Tear Strap Splice Repair

Internal Doubler

Internal Structural Filler

Edge of Upper Skin

Edge of Lower SkinPerform High Frequeupper and lower skin767 NDT Manual D63guidelines at intervals

OROption: If the HFEC son this area, performInspection of the uppaccordance with 767 guidelines at intervals

Perform Detailed Visuskin surfaces externa

All inspections mandatFastener Row) and SSare still applicable and exception of the area wInspection threshold annot apply to SSI 53-30-D622T001-9-01 and D6requirements

Inspection Threshold:

016

details Page 1.1-8


epair at STA 698

MA
D622T001-9-02


FIGURE 8. 53-30-I04A - NCR N1690415876 - S-8L Lap Splice Internal R

R 2017


ils Page 1.1-9

pair at STA 1268

JUN 20




FIGURE 9. 53-60-I05C/D - NCR N1690436086 - S-26L Lap Splice Internal Re

17

details Page 1.1-10


l Repair at STA 1484

JU
D622T001-9-02


FIGURE 10. 53-60-I05C/D - NCR N1690447322 - S-36R Lap Splice Interna

N 2017


ils Page 1.1-11

pair at STA 1369

NOV 2




FIGURE 11. 53-60-I05C/D - NCR N1690472132 – S-26L Lap Splice Internal Re

017

details Page 1.1-12


l Repair at STA 1187

AU
D622T001-9-02


FIGURE 12. 53-60-I05C/D - NCR N1690545562 - S-26L Lap Splice Interna

G 2018


ils Page 1.1-13

epair at STA 407

S-26L

ternaloubler

STA412

Tapered Fillers

SEP 20




FIGURE 13. 53-10-I07C/D - NCR N1690552176 - S-26L Lap Splice Internal R

InD

Internal Structural Filler

Upper Skin PanelTrim-Out and Filler

Lower Skin PanelTrimmed Edge

UP

FWD

Perform High Frequency Eddy Current Inspection of the upper and lowerskin surfaces externally in accordance with the 767 NDT Manual D634T301Part 6, 51-00-01 or 51-00-19 guidelines

All inspections mandated by SSI 53-10-07C (Upper Fastener Row) and SSI53-10-07D (Lower Fastener Row) are still applicable and must beaccomplished with exception of the area within the doubler profile.Note: Inspection threshold and inspection interval do not apply to SSI53-10-07C and SSI 53-10-07D. Refer to D622T001-9-01 and D622T001-DTRfor inspection requirements.

Perform Detail Visual Inspection of the upper and lower skin surfaceexternally within 2 inches of the repair parts.

Inspection Threshold: 40,000 FC Inspection Internal: 12,000 FC

STA390

Tapered Filler

18

details Page 1.1-14


Repair at STA 1341

NO
D622T001-9-02


FIGURE 14. 53-60-I05A/B - NCR N1690575718 - S-8L Lap Splice Internal

V 2018


ils Page 1.1-15

air at STA 654+121

NOV 2




FIGURE 15. 53-30-I04C/D - NCR N1690567481 - S-26R Lap Splice External Rep

018

details Page 1.1-16


TA 999, RBL 30, approximately

ht Cycles

e lower side of the pressure deck.

fillers within 2 inches of all repair

DE
D622T001-9-02


FIGURE 16. 53-50-51_MRB NCR N1690580814 - Pressure Deck Web, STA 977 to S

Inspection Threshold: 40,000 Cumulative Flight Cycles Inspection Interval: 6,000 Flig

AFT

OUTBD

Perform Low Frequency Eddy Current NDT Inspection of the pressure deck web from thRefer to 767 NDT Manual D634T301 Part 6, 51-00-06.

Perform Detailed Visual Inspection of the pressure deck web, repair doubler, and repairparts from the lower side of the pressure deck.

C 2018


ils Page 1.1-17

air at STA 1197+11

High Frequency Eddy Current on of the upper and lower skin s externally in accordance with the T Manual D634T301, Part 6, 51-00--00-19 guidelines.

ections mandated by SSI 53-60-I05C Fastener Row) and SSI 53-60-I05D Fastener Row) are still applicable st be accomplished with exception of within the doubler profile. Note: on threshold and inspection interval pply to SSI-53-60-I05C and SSI 53-. Refer to D622T001-0-01 and01-DTR for inspection requirements.

Detail Visual Inspection of the nd lower skin surfaces externally .0 inches of the repair parts.

on Threshold 40,000 FC on Interval 12,000 FC

FEB 20




FIGURE 17. 53-60-I05 C/D - NCR N1690593321 - S-26R Lap Splice External Rep

PerformInspectisurface767 ND01 or 51

All Insp(Upper (Lower and muthe areaInspectido not a60-I05DD622T0

Performupper awithin 2

InspectiInspecti

19

details Page 1.1-18


S0

00

06

81

10

0

FWD

DBNI

E

AP
D622T001-9-02


FIGURE 18. 53-50-I13B - NCR N1690605962

LEGEND:

DIRECTION OF DETAILED VISUAL INSPECTION.

NOTE:

INSPECTION THRESHOLD: 25,000 CUMULATIVE FLIGHT CYCLES.

INSPECTION INTERVAL: 12,000 FLIGHT CYCLES.

PERFORM DETAILED VISUAL INSPECTION TO STA 955.1 SIDE FRAME FITTING IN AREA COMMONTO SEAT TRACK SUPPORT BRACKET LOCATED BETWEEN STRINGER S-20 AND STRINGER S-21.INSPECT ALL EXPOSED SURFACES WITHOUT PERMANENT FASTENER REMOVAL.

SEAT TRACKSUPPORT FITTING

SIDE FRAMFITTING

SKIN

FAILSAFE STRAP

R 2019


ils Page 1.1-19

FWD

RAL FILLER

EDGE OFUPPER SKIN

EDGE OFLOWER SKIN

S-25R

S-27R

S-26R

ES EXTERNALLY AROUND THEIDELINES.LLY ALONG THE EDGE OF THE

DELINES.WITHIN 2 INCHES OF THE

FASTENER ROW) ARE STILLER PROFILE.SI 53-30-I04D, REFER TO

JUN 20




FIGURE 19. 53-30-I04C/D - NCR N1690619138

STA698

INTERNALSTRUCTURAL FILLER

INTERNALFILLER

INTERNALSTRUCTU

INTERNALDOUBLER

TEAR STRAPSPLICE REPAIR

EXTERNALFAIRING FITTING

STA720

NOTE:INSPECTION THRESHOLD: 40,000 CUMULATIVE FLIGHT CYCLES.INSPECTION INTERVAL: 12,000 FLIGHT CYCLES.

LEGEND:PERFORM HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE UPPER AND LOWER SKIN SURFACFASTENER HEADS IN ACCORDANCE WITH 767 NDT MANUAL D634T301 PART 6, 51-00-01 OR 51-00-19 GUPERFORM HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE LOWER SKIN SURFACES EXTERNAFAIRING FITTING IN ACCORDANCE WITH 767 NDT MANUAL D634T301 PART 6, 51-00-01 OR 51-00-19 GUIPERFORM DETAILED VISUAL INSPECTION OF THE UPPER AND LOWER SKIN SURFACES EXTERNALLYREPAIR PARTS.ALL INSPECTIONS MANDATED BY SSI 53-30-I04C (UPPER FASTENER ROW) AND SSI 53-30-104D (LOWERAPPLICABLE AND MUST BE ACCOMPLISHED, WITH THE EXCEPTION OF THE AREA WITHIN THE DOUBLNOTE: INSPECTION THRESHOLD AND INSPECTION INTERVAL DO NOT APPLY TO SSI 53-30-I04C AND S

D622T001-9-01 AND D622T001-DTR FOR INSPECTION REQUIREMENTS.

19

details Page 1.1-20


epair at STA 722

WD

-25R

-26R

S-27R

URFACES EXTERNALLY IN

(LOWER FASTENER ROW) ARE STILLDOUBLER PROFILE.

AND SSI 53-30-104D. REFER TO

NALLY WITHIN 2.0 INCHES OF THE

SE
D622T001-9-02


FIGURE 20. 53-30-I04C/D - NCR N1690650111 - Lap Splice External R

F

S

S

STA720

2 INCH(50.8 mm)

SHIM

EXTERNALDOUBLER

NOTE:INSPECTION THRESHOLD: 40,000 FLIGHT CYCLES.INSPECTION INTERVAL: 3,000 FLIGHT CYCLES.

LEGEND:PERFORM LOW FREQUENCY EDDY CURRENT INSPECTION OF THE UPPER AND LOWER SKIN SACCORDANCE WITH 767 NDT MANUAL D634T301 PART 6, 51-00-07 GUIDELINES.ALL INSPECTIONS MANDATED BY SSI 53-30-I04C (UPPER FASTENER ROW) AND SSI 53-30-I04DAPPLICABLE AND MUST BE ACCOMPLISHED WITH THE EXCEPTION OF THE AREA WITHIN THENOTE: INSPECTION THRESHOLD AND INSPECTION INTERVAL DO NOT APPLY TO SSI 53-30-I04C

D622T001-9-01 AND D622T001-DTR FOR INSPECTION REQUIREMENTS.PERFORM DETAILED VISUAL INSPECTION OF THE UPPER AND LOWER SKIN SURFACES EXTERREPAIR PARTS.

P 2019


ils Page 1.1-21

r at BS 654+110 - 676

OCT 2

FWD

LOWER FILLER SURFACES WHERES.OWER FASTENER ROW) ARE STILLOUBLER PROFILE.ND SSI 53-30-104D. REFER TO

CHES OF REPAIR PARTS.

S-25L

S-26L

STA676




FIGURE 21. 53-30-I04C/D - NCR N1690658151 - S-26L Lap Splice External Repai

019

A


LEGEND:PERFORM EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION OF UPPER DOUBLER ANDINDICATED IN ACCORDANCE WITH THE 767 NDT MANUAL D634T301, PART 6, 51-00-07 GUIDELINEALL INSPECTIONS MANDATED BY SSI 53-30-I04C (UPPER FASTENER ROW) AND SSI 53-30-I04D (LAPPLICABLE AND MUST BE ACCOMPLISHED, WITH THE EXCEPTION OF THE AREA WITHIN THE DNOTE: INSPECTION THRESHOLD AND INSPECTION INTERVAL DO NOT APPLY TO SSI 53-30-I04C A

D622T001-9-01 AND D622T001-DTR FOR INSPECTION REQUIREMENTS.PERFORM EXTERNAL DETAIL INSPECTION OF UPPER AND LOWER SKIN SURFACES WITHIN 2.0 IN

FILLER

DOUBLER

STA654

+110

STA654

+121

details Page 1.1-22


pair at BS 654+110 - 676

HIM

NINT RRENT INSPECTION.IT NT INSPECTION AROUND FASTENERS,ININ L HIGH FREQUENCY EDDY CURRENTIN

OC
D622T001-9-02


FIGURE 22. 53-30-I04C/D - NCR N1690658151 - S-26L Lap Splice External Re

A

S

OTE:THE REGION ABOVE AN EXTERNAL SHIM IS INSTALLED WITH BMS 5-95.

HE SHIM MUST BE REMOVED PRIOR TO PERFORMING AN EXTERNAL LOW FREQUENCY EDDY CUIS ACCEPTABLE IN THIS REGION TO SUBSTITUTE AN INTERNAL HIGH FREQUENCY EDDY CURRETERNAL DOUBLERS AND NUTPLATES.SPECTION INTERVALS ARE EXTENDED TO 12,000 FLIGHT CYCLES FOR THE OPTIONAL INTERNASPECTIONS FOR THIS REGION ONLY.

T 2019


ils Page 1.1-23

FWD

FASTENER LOCATIONS

OWER ROW) MUST BE

INCHES FROM EDGE OF

S-26L

S-27L

MAR 2




FIGURE 23. 53-30-I04C/D - NCR N1690696614


LEGEND:PERFORM LOW FREQUENCY EDDY CURRENT OF UPPER AND LOWER SKIN SURFACES AROUNDEXTERNALLY PER 767 NDT MANUAL, D634T301, PART 6 53-00-06 GUIDELINES.PERFORM ALL INSPECTIONS MANDATED BY SSI 53- 30-I04C (UPPER ROW) AND SSI 53-30-I04D (LPERFORMED EXCEPT IN AREA WITHIN DOUBLER PROFILE.NOTE: INSPECTION THRESHOLD AND INTERVAL DO NOT APPLY TO SSI 53-30-I04C/53-30-I04D.

REFER TO D622T001-9-01 AND D622T001-DTR.PERFORM DETAILED INSPECTION OF THE REPAIR AREA INCLUDING ALL STRUCTURE WITHIN 2 DOUBLER EXTERNALLY.

STA764

020

details Page 1.1-24


OUND 51- 00-19 GUIDELINES.4D (LOWER ROW) MUST BE

4D.

IN 2 INCHES FROM EDGE OF

S-25L

S-26L

M DOUBLER

N STRUCTURALFILLER

143T3362-8UPPER SKIN

143T3252-7LOWER SKIN

MA
D622T001-9-02


FIGURE 24. 53-30-I04C/D - NCR N1690706145

FWD


LEGEND:PERFORM HIGH FREQUENCY EDDY CURRENT OF UPPER AND LOWER SKIN SURFACES ARFASTENER LOCATIONS INTERNALLY PER 767 NDT MANUAL, D634T301, PART 6 51-00-01 ORPERFORM ALL INSPECTIONS MANDATED BY SSI 53- 30-I04C (UPPER ROW) AND SSI 53-30-I0PERFORMED EXCEPT IN AREA WITHIN DOUBLER PROFILE.NOTE: INSPECTION THRESHOLD AND INTERVAL DO NOT APPLY TO SSI 53-30-I04C/53-30-I0

REFER TO D622T001-9-01 AND D622T001-DTR.PERFORM DETAILED INSPECTION OF THE REPAIR AREA INCLUDING ALL STRUCTURE WITHDOUBLER EXTERNALLY OR INTERNALLY.

STA698

R 2020


ils Page 1.1-25

epair at STA 347

FACES EXTERNALLY IN

ER FASTENER ROW) AREUBLER PROFILE.

D SSI 53-10-07D. REFER TO

ITHIN 2 INCHES OF THE

L

L

L

ERNALRAPLICE

NALCTURALRS

MAR 2




FIGURE 25. 53-10-I07C/D - NCR N1610113314 - S-26L LAP Splice Internal R

FWD


LEGEND:PERFORM HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE UPPER AND LOWER SKIN SURACCORDANCE WITH THE 767 NDT MANUAL D634T301 PART 6, 51-00-01 OR 51-00-19 GUIDELINES.ALL INSPECTIONS MANDATED BY SSI 53-10-07C (UPPER FASTENER ROW) AND SSI 53-10-07D (LOWSTILL APPLICABLE AND MUST BE ACCOMPLISHED WITH EXCEPTION OF THE AREA WITHIN THE DONOTE: INSPECTION THRESHOLD AND INSPECTION INTERVAL DO NOT APPLY TO SSI 53-10-07C AN

D622T001-9-01 AND D622T001-DTR FOR INSPECTION REQUIREMENTS.PERFORM DETAIL VISUAL INSPECTION OF THE UPPER AND LOWER SKIN SURFACE EXTERNALLY WREPAIR PARTS.

INTERNALDOUBLER

STA347

S-25

S-26

S-27

TRIM OUTFILLER

LOWER SKINPANELTRIMMEDEDGE

INTSTSP

INTERSTRUFILLE

020

details Page 1.1-26


N HOLE HFEC INSPECTION ON ALLUPPER WING SKIN AND FRONT SPARGS, IN ACCORDANCE WITH 767 NDT, PART 6, 51-00-16 FOR THE SKIN-14 FOR THE FITTINGS

AU
D622T001-9-02


FIGURE 26. 57-20-I27 - NCR N1680112904

FWD

DBNI

FRONT SPAR PITCHLOAD FITTING(112T7007-11) FRONT SPAR WEB

FRONT SPAR PITCHLOAD FITTING(112T7007-15)

UPPER WINGSKIN

NOTE:PERFORM AN OPE24 HOLES ON THEPITCH LOAD FITTINMANUAL D634T301AND PART 6, 51-00

FASTENER SYMBOLS

BACB30YM14

G 2020

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