South African Airways Technical W/O Barcode Registration ... · 2385403 ZS-SXY South African Airways Technical Private Bag X12, O R Tambo Airport Gauteng 1627 South Africa South Africa

WO2385403R5

2385403 ZS-SXYSouth African Airways TechnicalPrivate Bag X12, O R Tambo AirportGauteng 1627South AfricaSouth Africa

W/O Barcode Registration

A330 330 -243Working Copy

(Page 1 / 7)produced by AMOS www.swiss-as.comUNCONTROLLED PRINTOUT printed by CDW386W on Fri. 11.January 2019 at 09:49 out of database prod hosted on amos.flysaa.com

Area Code Description04 POWER PLANT, NACELLES AND PYLONSZone Description452 UPPER FORWARD PYLON

NOTE: MANPOWER ALL WORK TO BE DONE AS PER SERVICE BULLETIN NO.: A330-92-3130 REVISION 04. THE MANPOWER ESTIMATES GIVEN IN THIS SERVICE BULLETIN ARE BASED ON THE DIRECT LABOR COST TO DO THE WORK. THESE ESTIMATES ASSUME THAT THE WORK WILL BE DONE BY EXPERIENCED PERSONNEL, AND MAY NEED TO BE REVISED UPWARDS TO SUIT OPERATOR’S CIRCUMSTANCES. THE ESTIMATES DO NOT INCLUDE THE TIME TO PREPARE, PLAN OR INSPECT THE WORK. MANUFACTURE AND PROCUREMENT OF PARTS AND TOOLS, DRYING TIMES FOR PAINTS, SEALANTS, ETC., AND GENERAL ADMINISTRATION WORK ARE ALSO NOT INCLUDED. ACCOMPLISHMENT INSTRUCTIONS **CONF 003: PROVIDE ACCESS FOR AVIONICS. REFER TO TASK 923130-831-804-001: MODIFICATION OF THE CLAMP AND SLEEVE OF HARNESS 501VB IN THE LH PYLON - ADDITIONAL WORK








Action Step 1-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________

Description Step 1WSL.3083823

CIMECH-AC

SI *DI/RIIPROVIDE ACCESS

Phase:02

N/APosition

04Zone

28AreaATA

SType

EBOrigin

452,…UPPER FORWARD PYLON

POWER PLANT, NACELLES ANDPYLONSFUELSCHED

Due at TACDue Date

N/AN/ADue at TAH

30.Mar.2019

Classifications/Statistics/Requests

Defect Classification: I, Line/Heavy: LINE MAINTENANCE

Maintenance Provider

SXY/H-19Workpackage No. / Sequence No.

Flight-No.

Planning-Date Start - Planned-Date End

CKC-005 AMO1

Workpackage

SAA TECHNICAL SOC LTD01.Feb.19, 06:00 - 24.Feb.19, 03:00

Type Reference Description

DO 14-0048/OIT(RV.00)

DO A330-92-3130/SB(RV.04)

DO EO-330-92-0002-R00-SA-1/EB(RV.00)

DO EO-330-92-0002-R00-SA/EO(RV.00)

WO2385403R5





Component ChangesPN Off SN Off Label Position PN On SN On Description Certificate


NOTE: MANPOWER NOTE: 1. ALL WORK TO BE DONE AS PER SERVICE BULLETIN NO.: A330-92-3130 REVISION 04. 2. PROTECTIVE SLEEVE PART NUMBER EN6049-007-19-5 TO BE DRAWN FROM NORMAL STOCK. 3. CLAMP PN NSA5516C09BD TO BE DRAWN FROM NORMAL STOCK. THE MANPOWER ESTIMATES GIVEN IN THIS SERVICE BULLETIN ARE BASED ON THE DIRECT LABOR COST TO DO THE WORK. THESE ESTIMATES ASSUME THAT THE WORK WILL BE DONE BY EXPERIENCED PERSONNEL, AND MAY NEED TO BE REVISED UPWARDS TO SUIT OPERATOR’S CIRCUMSTANCES. THE ESTIMATES DO NOT INCLUDE THE TIME TO PREPARE, PLAN OR INSPECT THE WORK. MANUFACTURE AND PROCUREMENT OF PARTS AND TOOLS, DRYING TIMES FOR PAINTS, SEALANTS, ETC., AND GENERAL ADMINISTRATION WORK ARE ALSO NOT INCLUDED. ACCOMPLISHMENT INSTRUCTIONS **CONF 003: MODIFY THE CLAMP AND SLEEVE OF HARNESS 501VB IN THE LH PYLON TASK 923130-831-804-001: MODIFICATION OF THE CLAMP AND SLEEVE OF HARNESS 501VB IN THE LH PYLON - ADDITIONAL WORK (1) MODIFY THE CLAMP AND SLEEVE OF HARNESS 501VB IN THE LH PYLON












Action Step 2-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________

Part number Description QtyEN6049-007-19-5 PROTECTIVE SLEEVE 4

NSA5516C09BD CLAMP 2Component ChangesPN Off SN Off Label Position PN On SN On Description Certificate

Description Step 2WSL.3083824 INSPECT

CIAVION-AC

SI *DI/RIIMODIFY THE CLAMP AND SLEEVE OF HARNESS 501VB IN THE LH PYLON

Phase:03

Phase:06

WO2385403R5






NOTE: MANPOWER ALL WORK TO BE DONE AS PER SERVICE BULLETIN NO.: A330-92-3130 REVISION 04. THE MANPOWER ESTIMATES GIVEN IN THIS SERVICE BULLETIN ARE BASED ON THE DIRECT LABOR COST TO DO THE WORK. THESE ESTIMATES ASSUME THAT THE WORK WILL BE DONE BY EXPERIENCED PERSONNEL, AND MAY NEED TO BE REVISED UPWARDS TO SUIT OPERATOR’S CIRCUMSTANCES. THE ESTIMATES DO NOT INCLUDE THE TIME TO PREPARE, PLAN OR INSPECT THE WORK. MANUFACTURE AND PROCUREMENT OF PARTS AND TOOLS, DRYING TIMES FOR PAINTS, SEALANTS, ETC., AND GENERAL ADMINISTRATION WORK ARE ALSO NOT INCLUDED. ACCOMPLISHMENT INSTRUCTIONS **CONF 003: CLOSE-UP. REFER TO TASK 923130-831-804-001:







Action Step 3-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________



CIMECH-AC

SI *DI/RIICLOSE-UP

Area Code Description04 POWER PLANT, NACELLES AND PYLONSZone Description453 LOWER PYLON

NOTE: MANPOWER ALL WORK TO BE DONE AS PER SERVICE BULLETIN NO.: A330-92-3130 REVISION 04. THE MANPOWER ESTIMATES GIVEN IN THIS SERVICE BULLETIN ARE BASED ON THE DIRECT LABOR COST TO DO THE WORK. THESE ESTIMATES ASSUME THAT THE WORK WILL BE DONE BY EXPERIENCED PERSONNEL, AND MAY NEED TO BE REVISED UPWARDS TO SUIT OPERATOR’S CIRCUMSTANCES. THE ESTIMATES DO NOT INCLUDE THE TIME TO PREPARE, PLAN OR INSPECT THE WORK. MANUFACTURE AND PROCUREMENT OF PARTS AND TOOLS, DRYING TIMES FOR PAINTS, SEALANTS, ETC., AND GENERAL ADMINISTRATION WORK ARE ALSO NOT INCLUDED. ACCOMPLISHMENT INSTRUCTIONS **CONF 003: PROVIDE ACCESS FOR AVIONICS. REFER TO TASK 923130-831-803-001: MODIFICATION OF THE CLAMP AND SLEEVE OF HARNESS 500VB IN THE RH PYLON - ADDITIONAL WORK







CIMECH-AC


Phase:02

WO2385403R5







Action Step 4-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________



NOTE: MANPOWER NOTE: 1. ALL WORK TO BE DONE AS PER SERVICE BULLETIN NO.: A330-92-3130 REVISION 04. 2. PROTECTIVE SLEEVE PART NUMBER EN6049-007-19-5 TO BE DRAWN FROM NORMAL STOCK. 3. CLAMP PN NSA5516C09BD TO BE DRAWN FROM NORMAL STOCK. THE MANPOWER ESTIMATES GIVEN IN THIS SERVICE BULLETIN ARE BASED ON THE DIRECT LABOR COST TO DO THE WORK. THESE ESTIMATES ASSUME THAT THE WORK WILL BE DONE BY EXPERIENCED PERSONNEL, AND MAY NEED TO BE REVISED UPWARDS TO SUIT OPERATOR’S CIRCUMSTANCES. THE ESTIMATES DO NOT INCLUDE THE TIME TO PREPARE, PLAN OR INSPECT THE WORK. MANUFACTURE AND PROCUREMENT OF PARTS AND TOOLS, DRYING TIMES FOR PAINTS, SEALANTS, ETC., AND GENERAL ADMINISTRATION WORK ARE ALSO NOT INCLUDED. ACCOMPLISHMENT INSTRUCTIONS **CONF 003: MODIFY THE CLAMP AND SLEEVE OF HARNESS 501VB IN THE LH PYLON TASK 923130-831-803-001: MODIFICATION OF THE CLAMP AND SLEEVE OF HARNESS 500VB IN THE RH PYLON - ADDITIONAL WORK (1) MODIFY THE CLAMP AND SLEEVE OF HARNESS 500VB IN THE RH PYLON












Action Step 5-1

_____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________


CIAVION-AC

SI *DI/RIIMODIFY THE CLAMP AND SLEEVE OF HARNESS 500VB IN THE RH PYLON

Phase:03

WO2385403R5





_______________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________










Action Step 6-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________



CIMECH-AC

SI *DI/RIICLOSE-UP

Phase:06


Phase:03

WO2385403R5





462 UPPER FORWARD PYLON

PLEASE PROVIDE ACCESS ON PANEL 452CR, 452CL, 454BR, 454BL Action Step 7-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________

Panel Description452CL ACCESS

452CR ACCESS

454BR ACCESS

454BL ACCESS

462CL ACCESS

462CR ACCESS

464BL ACCESS

464BR ACCESSComponent ChangesPN Off SN Off Label Position PN On SN On Description Certificate


CIMECH-AC




MODIFY THE HANGING KNOT ON THE FEEDER ROUTING (LH AND RH PYLON) AS PER SB A330-92-3130 REV 04 CONF 003 TASK 923130-831-806-001 TASK 923130-831-805-001

MODIFY THE HANGING KNOT ON THE FEEDER ROUTING (LH AND RH PYLON) AS PER SB A330-92-3130 REV 04 CONF 003 TASK 923130-831-806-001 TASK 923130-831-805-001

Action Step 8-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________


CIAVION-AC

SI *DI/RIIMODIFICATION OF THE HANGING KNOT ON THE LH/RH PYLON

Phase:03

WO2385403R5





Panel Description452CR ACCESS

452CL ACCESS

454BR ACCESS

454BL ACCESS

462CR ACCESS

462CL ACCESS

464BL ACCESS

464BR ACCESSPart number Description QtyNSA8420-5 TAPE. SUPPLIED IN 100MTR ROLLS. 1Component ChangesPN Off SN Off Label Position PN On SN On Description Certificate



CLOSE ACCESS IN ACCORDANCE WITH SB A330-92-3130 REV 04 Action Step 9-1

____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________

Panel Description452CL ACCESS

452CR ACCESS

454BR ACCESS

454BL ACCESS

462CL ACCESS

462CR ACCESS

464BL ACCESS

464BR ACCESSComponent ChangesPN Off SN Off Label Position PN On SN On Description Certificate


CIMECH-AC

SI *DI/RIICLOSE UP

Phase:03

@A330SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUSCUSTOMER SERVICES DIRECTORATE1 Rond Point Maurice Bellonte31707 BLAGNAC CEDEXFRANCETel : (33) 5 61 93 33 33Telex : AIRBU 530526FFax : (33) 5 61 93 42 51

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - GENERAL -IMPROVE ROUTE G ROUTING IN PYLON FOR ROLLS ROYCE,GENERAL ELECTRIC AND PRATT & WHITNEY ENGINES

MODIFICATION No.: 203733S32670 203734S32434

This page transmits Revision No.04 of Service Bulletin No.A330-92-3130

ADDITIONAL WORK

**CONF ALL

Additional work is required by this revision for aircraft modified by revision No. 01, revision No. 02 andrevision No. 03.

The ADDITIONAL WORK consists in the modification of the hanging knot on the feeders routing ofeach pylon for aircraft on which the Technical Adaptations (TA) 80446801/012/2018 have not beenapplied.

AIRBUS recommends the additional work to be accomplished within one year after the issue of thisrevision.

REASON

Revision No. 04 issued to replace the Part Number (PN) NSA8420-7 (item 13) by PN NSA8420-5 (item56).

NOTE: This revision satisfies the requirements of the subsequent Technical Adaptation(s) (TA)issued for the related Manufacturer Serial Number (MSN)s:

TA MSN80473447/006/2018 All effectivity

CHANGES

The main changes of this revision are:

- Kits A01, A03, A05, A07, A09 and A11 revised

- Kits A01S02, A03S02, A05S02, A07S02, A09S02 and A11S02 added

- PN of the cord for the hanging knots modified

DATE: Sep 29/14 SERVICE BULLETIN No.: A330-92-3130

REVISION No.: 04 - Oct 30/18 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.



- Additional work procedure added

- Minor changes applied.

SUMMARYMATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATEDR

MATERIAL PRICE INFORMATION TABLEUPDATED

R

MATERIAL PRICE INFORMATION TABLEUPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED RMANPOWER MANPOWER UPDATED R

MANPOWER UPDATED RMANPOWER UPDATED R

PLANNING INFORMATIONEFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATEDR

Material Effectivity MATERIAL EFFECTIVITY UPDATEDMATERIAL SET UPDATEDMATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATEDMATERIAL SET UPDATEDMATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATEDMATERIAL SET UPDATEDMATERIAL SET QUANTITY UPDATED

R

MANPOWER MANPOWER UPDATED RMANPOWER UPDATED RMANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED RREFERENCED DOCUMENTATION UPDATED RREFERENCED DOCUMENTATION UPDATED R

MATERIAL INFORMATIONMATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATEDMATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATEDMATERIAL SET UPDATEDMATERIAL PRICE UPDATEDMATERIAL AVAILABILITY UPDATED

R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED RLIST OF COMPONENTS LIST OF COMPONENTS UPDATED R



5




Kit 923130A01R07 PART MATERIAL SET UPDATEDMATERIAL SET LABEL UPDATEDKEYWORD UPDATEDITEM NUMBER UPDATEDPART NUMBER UPDATEDQUANTITY UPDATEDNOTE UPDATED

R

Kit 923130A02R03 PART MATERIAL SET UPDATEDKEYWORD UPDATED

R


R


R


R


R


R


R


R


R



5





R


R

Supplementary Kit 923130A01S01 PART MATERIAL SET UPDATEDKEYWORD UPDATEDQUANTITY UPDATED

R

Supplementary Kit 923130A01S02 PART MATERIAL SET ADDED N


R


R



R


R



R


R



R


R



R


R




5





R

LIST OF MATERIALS - OPERATORSUPPLIED

Components

Component COMPA01 PART MATERIAL SET UPDATEDKEYWORD UPDATED

R

ACCOMPLISHMENT INSTRUCTIONSTASK 923130- 831-801-001-Modificationof the routing in the LH pylon

TASK SOLUTION UPDATEDCAUTION UPDATEDNOTE UPDATED

R

Subtask 923130-941-001-002 SUBTASK SOLUTION UPDATEDREFERENCED DOCUMENTATION UPDATEDREFERENCES UPDATED

R

Subtask 923130-831-001-001 SUBTASK SOLUTION UPDATEDKEYWORD UPDATEDITEM NUMBER UPDATEDPART NUMBER UPDATEDQUANTITY UPDATEDNOTE UPDATEDPART NUMBER DESCRIPTION UPDATEDMATERIAL LIST UPDATED

R

Subtask 923130-831-002-001 SUBTASK SOLUTION UPDATEDKEYWORD UPDATEDPART NUMBER DESCRIPTION UPDATEDMATERIAL LIST UPDATED

R


R


R


R



5





R

TASK 923130- 831-802-001-Modificationof the routing in the RH pylon

TASK SOLUTION UPDATEDCAUTION UPDATEDNOTE UPDATED

R


R


R


R


R


R


R


R

TASK 923130- 831-804-001-Modificationof the Clamp and Sleeve of Harness501VB in the LH Pylon - ADDITIONALWORK

TASK SOLUTION UPDATEDNOTE UPDATED

R



5





R


R


R


R


R


R

TASK 923130- 831-803-001-Modificationof the Clamp and Sleeve of Harness500VB in the RH Pylon - ADDITIONALWORK

TASK SOLUTION UPDATEDNOTE UPDATED

R


R


R


R


R

TASK 923130- 831-806-001-Modificationof the Hanging Knot on the LH Pylon -ADDITIONAL WORK

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED NTask associated data - 002 TASK ASSOCIATED DATA ADDED NTask associated data - 003 TASK ASSOCIATED DATA ADDED NSubtask 923130-910-012-001 SUBTASK SOLUTION ADDED NSubtask 923130-839-011-001 SUBTASK SOLUTION ADDED NSubtask 923130-910-012-001 SUBTASK SOLUTION ADDED N



5




Subtask 923130-839-011-001 SUBTASK SOLUTION ADDED NSubtask 923130-910-012-001 SUBTASK SOLUTION ADDED NSubtask 923130-839-011-001 SUBTASK SOLUTION ADDED NSubtask 923130-941-010-001 SUBTASK SOLUTION ADDED NSubtask 923130-941-010-001 SUBTASK SOLUTION ADDED NSubtask 923130-941-010-001 SUBTASK SOLUTION ADDED NSubtask 923130-831-011-001 SUBTASK SOLUTION ADDED NSubtask 923130-831-011-003 SUBTASK SOLUTION ADDED NSubtask 923130-831-011-002 SUBTASK SOLUTION ADDED NSubtask 923130-942-006-001 SUBTASK SOLUTION ADDED NSubtask 923130-942-006-001 SUBTASK SOLUTION ADDED NSubtask 923130-942-006-001 SUBTASK SOLUTION ADDED N

TASK 923130- 831-805-001-Modificationof the Hanging Knot on the RH Pylon -ADDITIONAL WORK

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED NTask associated data - 002 TASK ASSOCIATED DATA ADDED NTask associated data - 003 TASK ASSOCIATED DATA ADDED NSubtask 923130-910-011-001 SUBTASK SOLUTION ADDED NSubtask 923130-839-010-001 SUBTASK SOLUTION ADDED NSubtask 923130-910-011-001 SUBTASK SOLUTION ADDED NSubtask 923130-839-010-001 SUBTASK SOLUTION ADDED NSubtask 923130-910-011-001 SUBTASK SOLUTION ADDED NSubtask 923130-839-010-001 SUBTASK SOLUTION ADDED NSubtask 923130-941-007-001 SUBTASK SOLUTION ADDED NSubtask 923130-941-007-001 SUBTASK SOLUTION ADDED NSubtask 923130-941-007-001 SUBTASK SOLUTION ADDED NSubtask 923130-831-010-001 SUBTASK SOLUTION ADDED NSubtask 923130-831-010-003 SUBTASK SOLUTION ADDED NSubtask 923130-831-010-002 SUBTASK SOLUTION ADDED NSubtask 923130-942-007-001 SUBTASK SOLUTION ADDED NSubtask 923130-942-007-001 SUBTASK SOLUTION ADDED NSubtask 923130-942-007-001 SUBTASK SOLUTION ADDED N

Fig. A-FBAAA

Fig. A-FBAAA Sheet 04 SHEET UPDATED R

Fig. A-FBAAB

Fig. A-FBAAB Sheet 04 SHEET UPDATED R

Fig. A-FBAAC

Fig. A-FBAAC Sheet 04 SHEET UPDATED R

Fig. A-FBAAC Sheet 06 SHEET UPDATED R

Fig. A-FBCAA

Fig. A-FBCAA Sheet 05 SHEET UPDATED R

Fig. A-FBCAB

Fig. A-FBCAB Sheet 05 SHEET UPDATED R

Fig. A-FBCAC



5




Fig. A-FBCAC Sheet 03 SHEET UPDATED R



Fig. A-FBGAA FIGURE SOLUTION ADDED N

Fig. A-FBGAA Sheet 01 SHEET ADDED N

Fig. A-FBGAA Sheet 02 SHEET ADDED N

Fig. A-FBGAB FIGURE SOLUTION ADDED N

Fig. A-FBGAB Sheet 01 SHEET ADDED N

Fig. A-FBGAB Sheet 02 SHEET ADDED N

Fig. A-FBHAA FIGURE SOLUTION ADDED N

Fig. A-FBHAA Sheet 01 SHEET ADDED N

Fig. A-FBHAA Sheet 02 SHEET ADDED N

Fig. A-FBHAB FIGURE SOLUTION ADDED N

Fig. A-FBHAB Sheet 01 SHEET ADDED N

Fig. A-FBHAB Sheet 02 SHEET ADDED N

Fig. A-GBAAA FIGURE SOLUTION UPDATED R

Fig. A-GBAAA Sheet 02 SHEET UPDATED R

Fig. A-GBAAA Sheet 03 SHEET ADDED N

Fig. A-GBBAA

Fig. A-GBBAA Sheet 02 SHEET UPDATED R

Appendix 01 - Elapsed Time Assumption

APPENDIX CONTENT APPENDIX CONTENT UPDATED R

FILING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to:

Modify the ACCOMPLISHMENT INSTRUCTIONS paragraph

Update the effectivity.

Revision No. 02 issued to add Supplementary kit 923130A01S01 thru Supplementary kit923130A12S01 without additional work.

Revision No. 03 issued to:

Replace Protective Sleeve Part Number (PN) EN6049-007-08-5 (item 33) by PN EN6049-007-19-5

Replace a Clamp PN NSA5516C05BD (item 20) of harnesses 452VB and 453VB by PNNSA5516C09BD (item 55).



5




Revision No. 03 issued to incorporate changes found necessary and carried out during theaccomplishment of this Service Bulletin.

This revision satisfies the requirements of the subsequent Technical Adaptations (TA) issued to therelated MSNs:

TA

MSN

80406570/003/2018

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0065 0070-0072 0082 0083 0086 0087 00950096 0099 0102 0106 0109 0111-0113 0116 0118 0120 0121 0122 0127 0132 0138 0140 0143 01440148 0153 0155 0162 0165 0171 0172 0177 0181 0195 0200 0206 0209 0211 0219 0222-0224 02260229 0230-0232 0234 0238 0240 0241 0244 0247-0251 0253-0256 0258 0259 0261 0262 0265-02670269 0271 0272 0275-0277 0279 0281 0283-0288 0290 0291 0293 0295 0296 0300 0301 0303 03050306 0308 0309 0311-0317 0320 0322 0324 0328 0330 0333 0334 0337-0340 0342-0346 0348-03510353 0356-0358 0361 0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388 0389 03920393 0396-0398 0400 0401 0403-0405 0407-0409 0412 0418-0423 0425 0427 0428 0432 0437 04390441 0443 0444 0448 0451 0452 0454-0456 0458 0461-0463 0465 0466 0469 0472 0473 0476 04770479-0481 0484 0486 0487 0489 0490 0491 0493 0494 0496-0498 0500-0516 0518 0519 0521 05220524-0527 0529 0530 0532 0533 0535 0536 0539 0542 0548-0553 0555 0558 0564 0565 0567 05680570 0571 0573 0574 0576 0578 0579 0581 0584 0587 0588 0591 0593 0595 0597 0600 0602 06030605 0607 0609 0610 0612 0614 0616 0618 0620 0621 0623 0625 0627 0629 0631-0638 0640-06420644 0645 0647-0650 0652-0659 0661-0671 0673-0676 0678-0680 0682-0684 0686-0693 0695-06970699-0701 0703-0705 0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-07350737-0739 0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769 0770 0772-0774 0776-07780780-0782 0784-0786 0788 0789 0791 0792 0795-0797 0799-0803 0805-0807 0809-0811 0813-08150817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863 0865-0869 0871 0873-08770879 0881-0885 0887-0893 0895 0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922 09230925-0928 0930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-09860988-0992 0994-0998 1000-1004 1006-1016 1018-1023 1025 1026 1028 1029 1031-1039 1041-10491051-1055 1057-1063 1065-1067 1069-1078 1080-1082 1084-1090 1092-1101 1103-1108 1110 11121114-1116 1118 1120 1123 1124 1126 1127 1129-1133 1135-1138 1141 1143 1145-1151 11531155-1157 1159-1161 1163-1165 1167-1175 1177 1178 1180 1181 1183 1184 1186-1193 1195 11961198-1206 1208-1241 1243-1252 1254-1256 1258-1272 1274-1423 1425-1521 1523-1532

REVISION SEQUENCE

ORIGINAL: Sep 29/14

REVISION No. : 01 - Jun 15/16

REVISION No. : 02 - Dec 06/16

REVISION No. : 03 - Mar 22/18

REVISION No. : 04 - Oct 30/18



5



SUMMARY


This summary is for information only and is not approved for modification of the aircraft.

ATA SYSTEM: 92


**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATIONMAJOR NoneMINOR 203733S32670 203734S32434

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affecting theairworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Several events of wiring being damaged in pylon area have been reported to AIRBUS by A330operators as follows:

- Insulation damaged of feeder cables under bushing parts (PN F92430084200).

- Wires and convoluted conduit damaged to pressure transducers (FINs 8HA1, 9HA1, 8HA2 and9HA2).

The objective of this Service Bulletin is to prevent wiring from damage by:

- Replacing bushing and bobbin installation by a new assembly using standard parts.

- Replacing convoluted conduit by self-wrapping protective sleeve and suitable clamps.

Accomplishment of this Service Bulletin will improve the wiring installation in pylon area to prevent fromchafing and subsequent damages.

This will contribute to avoid unscheduled maintenance actions (wiring repair) and potential systemmisbehaviour of the pressure transducers (FINs 8HA1, 9HA1, 8HA2 and 9HA2).



5



SUMMARY

GENERAL EVALUATION

EVALUATION TABLECOMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD NO A/C OPERATION AFFECTED NORELIABILITY AFFECTED NO PAX COMFORT AFFECTED NOCOST SAVING NO ETOPS AFFECTED NOSTRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operationaldisruptions.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLEMATERIAL SET QTY PER

A/CPRICE PERA/C (USD)

MAIN PARTS

Kit 923130A01R07 1 770.00 PlateKit 923130A02R03 1 850.00 PlateKit 923130A03R07 1 910.00 PlateKit 923130A04R03 1 850.00 PlateKit 923130D01R01 2 190.00 Sleeve, Placard

Supplementary kit923130A01S01

1 260.00 Nut, Cord, Spacer, Stud


1 50.00 Cord


1 519.00 Clamp, Cord, Sleeve


1 70.00 Clamp, Sleeve




1 50.00 Cord


1 519.00 Clamp, Cord, Sleeve



TOTAL 5,430.00

Component COMPA01 2 See SB Cord

**CONF 002



MAIN PARTS

Kit 923130A05R06 1 770.00 Plate



5



SUMMARY



MAIN PARTS

Kit 923130A06R04 1 850.00 PlateKit 923130A07R06 1 910.00 PlateKit 923130A08R04 1 850.00 PlateKit 923130D01R01 2 190.00 Sleeve, Placard




1 50.00 Cord


1 602.00 Clamp, Cord, Sleeve, Screw, Spacer






1 50.00 Cord


1 602.00 Clamp, Cord, Sleeve, Screw, Spacer



TOTAL 5,596.00


**CONF 003



MAIN PARTS

Kit 923130A09R05 1 660.00 PlateKit 923130A10R03 1 770.00 PlateKit 923130A11R05 1 620.00 PlateKit 923130A12R03 1 770.00 PlateKit 923130D01R01 2 190.00 Sleeve, Placard


1 208.00 Nut, Cord


1 50.00 Cord


1 519.00 Screw, Clamp, Cord, Sleeve




1 208.00 Nut, Cord


1 50.00 Cord



5



SUMMARY



MAIN PARTS


1 519.00 Screw, Clamp, Cord, Sleeve



TOTAL 4,704.00


EFFECTIVITY

**CONF ALL

This Service Bulletin is applicable to this (these) operator(s) :

18P 36V 38W 39V 43P 46O 56O 57L 83V 87Z 98W AAF AALAAR AAW ABR ACA ACI AEA AFL AFR AIB ALD ALK ARG ASLASY AVA AZA AZU BEC BEL CAL CBJ CCA CEB CES CHH CPACRK CRL CSA CSC CSN D2F DAH DAL DGA DLH EDW EIN ETDEVA EVE F2I FIN FJI FWI G8E GFA GIA GRL HAL HDA HFMHFY HKC HVN I2L IAW IBE ISS JAI JAV KAL KLM LAA LMUMAS MAU MEA MLM MNB MSR NMB NWS OBS OHY OMA ONE P2CPAL PLM QAF QFA QTR RSF RSY RZO SAA SAI SAS SIA SVASWR SXD TAE TAM TAP TCX THA THY TOW TPA TSC U6A UAEUAF VIR VKG VOZ WOW WRC XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 36.11.00.071OEB NoneAOT NoneSIL NoneISI 00.00.00198LINE MAINTENANCE AFFECTED NoLIFE LIMIT NoneOTHER None

NATURE OF THE WORK

AIRCRAFT YESEQUIPMENT NO

HARD NOSOFT NOOBRM NO



5



SUMMARY

MANPOWER

**CONF 001

Task 923130-831-801-001: Modification of the routing in the LH pylon

TOTAL MANHOURS 13.50ELAPSED TIME (HOURS) 9.50

Task 923130-831-802-001: Modification of the routing in the RH pylon


Task 923130-831-804-001: Modification of the Clamp and Sleeve of Harness 501VB in the LHPylon - ADDITIONAL WORK


Task 923130-831-803-001: Modification of the Clamp and Sleeve of Harness 500VB in the RHPylon - ADDITIONAL WORK


Task 923130-831-806-001: Modification of the Hanging Knot on the LH Pylon - ADDITIONALWORK


Task 923130-831-805-001: Modification of the Hanging Knot on the RH Pylon - ADDITIONALWORK


**CONF 002









5



SUMMARY







**CONF 003















5



SUMMARY

APPENDICES

**CONF ALL


Appendix 02 - Retrofitted Modifications



5



SUMMARY

**CONF ALL

Z453

A

A

RIB11RIB8

Z463 A

ROUTING TO BE MODIFIED

G_SB_923130_5_SAAA_01_00

Figure A-FSAAA - Sheet 01



5



SUMMARY

**CONF ALL

Z462

A

RIB8A

RIB13A

RIB8A

RIB13A

Z452

B

A

B

NOTE:

AREA OF MODIFICATION

7701VB

7702VB

G_SB_923130_6_SAAA_01_00

Figure A-GSAAA - Sheet 01



5



SUMMARY

This Page Intentionally Left Blank



5




ATA SYSTEM: 92



This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain theproperty of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection withany information contained in it. It is delivered on the express condition that said document and theinformation contained in it shall be treated as confidential, shall not be used for any purpose other thanthat for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shallnot be duplicated in any manner (except for the purposes of performing the tasks described hereunderand provided that any recipient of such document shall comply with the conditions herein), withoutAIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

330-202 330-203 330-223 330-223F 330-243 330-243F 330-301 330-302330-303 330-321 330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0065 0070-0072 0082-00830086-0087 0095-0096 0099 0102 0106 0109 0111-0113 0116 0118 0120-0122 01270132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 01950200 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 02440247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-02770279 0281 0283-0288 0290-0291 0293 0295-0296 0300-0301 0303 0305-03060308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-03400342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 03750380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-04050407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 04480451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-04770479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-05160518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539 05420548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-05790581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610



5



0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638 0640-06420644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676 0678-06800682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-07090711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735 0737-07390741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769-0770 0772-07740776-0778 0780-0782 0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-08030805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 08470849-0855 0857-0863 0865-0869 0871 0873-0877 0879 0881-0885 0887-08930895-0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922-0923 0925-09280930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-09860988-0992 0994-0998 1000-1004 1006-1016 1018-1023 1025-1026 1028-10291031-1039 1041-1049 1051-1055 1057-1063 1065-1067 1069-1078 1080-10821084-1090 1092-1101 1103-1108 1110 1112 1114-1116 1118 1120 1123-11241126-1127 1129-1133 1135-1138 1141 1143 1145-1151 1153 1155-1157 1159-11611163-1165 1167-1175 1177-1178 1180-1181 1183-1184 1186-1193 1195-11961198-1206 1208-1241 1243-1252 1254-1256 1258-1272 1274-1423 1425-15211523-1532

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the timeof issue in accordance with the information available to AIRBUS. Any future changesresulting from transfer of an aircraft from one operator to another will not be reflected inthis list unless the Service Bulletin is revised for another reason.

OPERATOR MSN18P 132136V 116438W 040139V 025543P 105346O 065556O 023157L 073583V 017187Z 053598W 0054AAF 0444 0493AAL 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041

1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340

1435 1464 1518AAW 1043 1472ABR 0116 0127ACA 0277 0279 0284 0344 0400 0408 0412 0419ACI 0507 0510AEA 0461 0505 0526 0733 0745 0749 0814 0931 0950 0992 1097AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247

1264 1270 1284 1299 1301 1323 1328 1345 1356 1371



5



OPERATOR MSNAFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657AIB 0871ALD 0326 0328 0392ALK 0303 0306 0311 0313 0456 0627ARG 0290 0300 0358 0364 0587 0634ASL 0885ASY 0747 0892 0898 0951 0969 1036 1183AVA 1009 1016 1073 1224 1342 1357 1378 1400AZA 0272 0339 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313

1327 1354AZU 0365 0372 0462 0494 0527 0529 0532BEC 0863BEL 0030 0037 0045 0082 0095 0229 0249 0291 0324 0895 0915 0959

1010 1085CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450CBJ 0988 1020 1028 1052CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 11871199 1216 1237 1260 1282 1304 1330 1333 1353 1373 1383 13961413 1434 1444 1459 1471 1493 1509 1525

CEB 1420 1445 1495 1527CES 0773 0777 0781 0782 0791 0821 0830 0836 0851 0862 0866 0916

0928 0936 0942 1262 1267 1280 1291 1303 1324 1331 1372 13751402 1421 1429 1440 1461 1468 1479 1484 1500 1520

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255 1325 14381532

CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 05390548 0565 0679 0776 0850 0855 1163 1196 1222 1239 1285 13171343 1349 1362 1366 1387 1409 1436 1443

CRK 0396 0452 1031 1034 1039 1042 1054 1059 1099 1105 1107 11241146 1157 1277 1286 1322 1358 1369 1384 1398

CRL 0285 0320 1359 1376CSA 0425CSC 1082 1138 1241 1397 1432 1528CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 13351392 1425 1430 1494 1519

D2F 0209DAH 0644 0647 0650 0653 0667DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 07990806 0817 0827 0843 0857 0858 0859 0865

DGA 0240DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922 0989 1292 1305 1314 1497EDW 1193



5



OPERATOR MSNEIN 0269 0330 0397 0441 0841 0847 0985 1025 1106ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852

0854 0868 0975 0991 1032 1070 1071 1081 1167 1205 1226 12451414 1486 1521 1524

EVA 0678 0693 0755 1254 1268 1274EVE 0670 0802F2I 0055 0070 0072 0086 0087 0200FIN 0994 1007 1013 1023 1067 1078 1088 1173FJI 0751 0807 1394 1416 1465FWI 0253 0343 0758 0965 1021 1265G8E 0288 0463GFA 0276 0281 0286 0287 0334 0340GIA 0138 0140 0144 0148 0153 0165 1184 1214 1261 1288 1364 1410

1446 1474GRL 0230HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404

1422 1469 1488 1496 1511 1530HDA 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405

0479 0512 0581 0669 0673 1457 1503 1523HFM 0096HFY 0211 0262 1008HKC 1051 1062 1115 1175 1320HVN 0366 0943 0962 1019 1256 1266I2L 0275IAW 1339IBE 1377 1385 1405 1426 1437 1490 1507 1515ISS 0521 0571JAI 0888 0923 0947 0956 1351 1361 1370 1391JAV 0409KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0428 0484 0490 0550 1133 1155 1200 1203 1393KLM 0682 0686 0703 0738 0770 0801 0925 1161 1287 1294 1300 1381LAA 1412 1505LMU 0661MAS 0665 0822 0828 0911 0968 1112 1136 1148 1180 1209 1219 1229

1234 1243 1281 1318 1336 1337 1347 1388 1395 1431 1470 1489MAU 0883 1057MEA 0926 0984 0995 0998MLM 0451MNB 1332MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246NMB 1451 1466NWS 0979 1002OBS 0833OHY 0316 0345 0353 0362 0404 0437 0491 0509 0525 0625 0632OMA 1038 1044 1049 1063 1093 1120 1227



5



OPERATOR MSNONE 1208 1279 1492 1506 1508P2C 0891 0927PAL 1449 1456 1460 1463 1467 1475 1482 1504 1510 1531PLM 0261 0265 0454 0469 0551QAF 0487 0605QFA 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695

0705 0712 0842 0853 0887 0940 0945 0976 1061 1094 1169 11741198 1251 1258 1365

QTR 0473 0489 0511 0623 0637 0638 0659 0680 0711 0721 0734 07430746 0760 0789 0792 0813 0820 0826 0849 0893 0907 0918 13501386 1406

RSF 0980 0996 1235 1379 1478 1516RSY 0120 0283 0293 0295 0472 0700 0739 0946RZO 0970SAA 1191 1210 1223 1236 1249 1271SAI 0811 0819 0834 0900SAS 0496 0497 0515 0568SIA 0978 0983 0986 1132 1149 1156 1382 1401 1427 1447 1453 1477

1485 1517SVA 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290

1355 1403SXD 0504 0530 0555 0573 0612 0616 0684TAE 0348TAM 0232 0238 0247 0259 0361 0466TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486 0877 0899 0904

0914 0934 0997 1006 1012 1015TCX 0254 0266 0301 0398 0948 0967THA 0050 0060 0062 0112 0122 0346 0990 1003 1035 1037 1060 1074

1086 1090 1263 1269 1289 1338 1348 1374 1408THY 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901 0932 0939

0949 0961 0977 1004 1092 1118 1150 1160 1170 1172 1204 12121213 1221 1228 1240 1298 1307 1311 1344 1418 1442 1458 14761483 1487 1491 1499 1501 1514 1529

TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498TPA 1368 1380 1428 1448TSC 0111 0132 0177 0248 0250 0251 0271 0314 0369 0407 0427 0455

0480 0518 0536 0728 0732 0795 0966 0971U6A 0065 0143 0224UAE 0382 0384UAF 1080 1186 1250VIR 0322 0403 0432 0476 1195 1201 1206 1215 1231 1296 1315 1329

1341 1352VKG 0309 0349 0356 0357VOZ 1293 1306 1319 1407 1452WOW 1098WRC 0296



5



OPERATOR MSNXAX 0654 0662 0692 0713 0716 0720 0741 0786 0952 0974 1048 1066

1075 1126 1131 1165 1411 1423 1433 1481XLF 0501 0597 0635 1360



5



(4) Configuration by MSN

MSN CONFIGURATION0012 0017 0071 0083 0099 0102 0106 0109 0111 0113 01180121 0132 0138 0140 0144 0148 0153 0155 0165 0177 02340244 0248 0250 0251 0254 0261 0265 0266 0271 0276 02770279 0281 0283 0284 0285 0286 0287 0293 0295 0301 03030306 0309 0311 0313 0314 0316 0320 0326 0328 0334 03400344 0345 0348 0349 0356 0357 0365 0369 0372 0382 03840386 0389 0392 0393 0396 0398 0400 0401 0404 0405 04070408 0409 0412 0418 0419 0420 0421 0423 0427 0437 04390451 0452 0455 0456 0461 0462 0479 0480 0491 0494 04960497 0501 0505 0509 0512 0515 0518 0525 0526 0527 05290532 0536 0539 0548 0551 0565 0568 0570 0576 0579 05810597 0600 0610 0625 0627 0629 0632 0635 0636 0642 06450648 0649 0652 0654 0656 0658 0662 0664 0666 0669 06700673 0679 0683 0687 0688 0692 0696 0701 0709 0713 07160717 0720 0724 0726 0728 0729 0730 0732 0735 0737 07410750 0751 0756 0759 0773 0776 0777 0780 0781 0782 07850786 0788 0791 0795 0797 0807 0809 0810 0815 0818 08210824 0830 0832 0833 0836 0839 0840 0850 0851 0852 08540855 0860 0862 0863 0866 0867 0868 0873 0875 0879 08810884 0889 0890 0895 0896 0903 0905 0906 0908 0909 09130915 0916 0919 0922 0926 0928 0930 0935 0936 0937 09410942 0944 0948 0952 0954 0957 0958 0959 0963 0964 09660967 0971 0973 0974 0975 0978 0982 0983 0984 0986 09880989 0990 0991 0992 0995 0997 0998 1000 1003 1004 10061008 1009 1010 1011 1012 1014 1015 1016 1018 1020 10221026 1028 1029 1032 1033 1035 1037 1038 1041 1044 10451046 1047 1048 1049 1051 1052 1053 1058 1060 1062 10631065 1066 1069 1070 1071 1072 1073 1074 1075 1076 10771080 1081 1082 1084 1085 1086 1087 1089 1090 1092 10931095 1097 1098 1099 1100 1101 1103 1104 1105 1107 11081110 1114 1115 1120 1124 1126 1127 1130 1131 1132 11371138 1141 1143 1145 1146 1147 1149 1150 1153 1156 11571159 1160 1163 1165 1167 1168 1170 1171 1172 1175 11781181 1184 1186 1187 1188 1189 1190 1191 1192 1193 11951196 1199 1201 1204 1205 1206 1208 1210 1212 1214 12151216 1217 1222 1223 1224 1226 1227 1228 1230 1231 12321236 1237 1238 1239 1240 1241 1245 1246 1247 1248 12491250 1255 1259 1260 1261 1262 1263 1264 1267 1269 12701271 1275 1276 1277 1279 1280 1282 1284 1285 1286 12881289 1290 1291 1292 1293 1295 1296 1298 1299 1301 13021303 1304 1305 1306 1307 1310 1311 1312 1314 1315 13161317 1319 1320 1322 1323 1324 1325 1328 1329 1330 13311332 1333 1334 1338 1341 1342 1343 1344 1345 1348 13491350 1352 1353 1355 1356 1357 1358 1359 1362 1363 13641366 1368 1369 1371 1372 1373 1374 1375 1376 1378 13801382 1383 1384 1386 1387 1389 1390 1394 1396 1397 13981399 1400 1401 1402 1403 1404 1406 1407 1408 1409 14101411 1413 1414 1415 1416 1417 1418 1419 1420 1421 14221423 1427 1428 1429 1432 1433 1434 1436 1438 1439 1440

003



5



MSN CONFIGURATION1441 1442 1443 1444 1445 1446 1447 1448 1449 1451 14521453 1454 1455 1456 1457 1459 1460 1461 1462 1463 14651466 1467 1468 1469 1471 1473 1474 1475 1477 1479 14801481 1482 1483 1484 1485 1486 1488 1491 1492 1493 14951496 1497 1498 1500 1502 1503 1504 1506 1508 1509 15101511 1512 1513 1517 1520 1521 1523 1524 1525 1526 15271528 1530 1531 1532

003

0030 0037 0045 0054 0055 0070 0086 0200 0211 0269 02720330 0339 0397 0422 0441 0443 0448 0458 0463 0465 04660472 0473 0477 0481 0486 0487 0489 0498 0500 0502 05030504 0506 0507 0508 0510 0511 0513 0516 0519 0521 05220530 0535 0553 0555 0558 0564 0567 0571 0573 0574 05840587 0593 0595 0602 0603 0605 0607 0612 0616 0623 06340637 0638 0641 0644 0647 0650 0653 0655 0657 0659 06610667 0671 0675 0678 0680 0682 0684 0686 0691 0693 06950697 0699 0700 0703 0704 0705 0707 0711 0712 0714 07210725 0733 0734 0738 0742 0743 0745 0746 0747 0749 07520754 0755 0760 0769 0770 0774 0789 0792 0801 0805 08110813 0814 0819 0820 0823 0825 0826 0831 0834 0838 08410842 0847 0849 0853 0861 0871 0877 0882 0883 0885 08870888 0892 0893 0898 0899 0900 0901 0904 0907 0914 09180920 0923 0925 0931 0932 0934 0940 0945 0947 0950 09510956 0969 0976 0980 0985 0994 0996 1007 1013 1023 10251036 1043 1057 1061 1067 1078 1088 1094 1106 1123 11351161 1169 1173 1174 1177 1183 1198 1218 1225 1235 12511252 1254 1258 1268 1272 1274 1278 1283 1287 1294 13001308 1313 1321 1327 1339 1346 1351 1354 1360 1361 13651367 1370 1377 1379 1381 1385 1391 1405 1412 1426 14371450 1458 1472 1476 1478 1487 1490 1499 1501 1505 15071514 1515 1516 1529

001

0050 0060 0062 0065 0072 0082 0087 0095 0096 0112 01160120 0122 0127 0143 0162 0171 0172 0181 0195 0206 02090219 0222 0223 0224 0226 0229 0230 0231 0232 0238 02400241 0247 0249 0253 0255 0256 0258 0259 0262 0267 02750288 0290 0291 0296 0300 0305 0308 0312 0315 0317 03220323 0324 0333 0337 0338 0342 0343 0346 0350 0351 03530358 0361 0362 0364 0366 0368 0370 0375 0380 0388 04030425 0428 0432 0444 0454 0469 0476 0484 0490 0493 05240533 0542 0549 0550 0552 0578 0588 0591 0609 0614 06180620 0621 0631 0633 0640 0663 0665 0674 0676 0690 07080718 0722 0739 0758 0772 0778 0784 0796 0799 0802 08030806 0817 0822 0827 0828 0843 0845 0857 0858 0859 08650869 0874 0876 0891 0911 0927 0939 0943 0946 0949 09610962 0965 0968 0970 0977 0979 1001 1002 1019 1021 10311034 1039 1042 1054 1055 1059 1096 1112 1116 1118 11291133 1136 1148 1151 1155 1164 1180 1200 1202 1203 12091211 1213 1219 1220 1221 1229 1233 1234 1243 1244 12561265 1266 1281 1297 1309 1318 1326 1335 1336 1337 13401347 1388 1392 1393 1395 1425 1430 1431 1435 1464 14701489 1494 1518 1519

002



5



(5) Configuration definition

**CONF 001Config. 001 is valid for aircraft equipped with GE engines.

**CONF 002Config. 002 is valid for aircraft equipped with P&W engines.

**CONF 003Config. 003 is valid for aircraft equipped with RR engines.

For the retrofitted modifications after accomplishment of this Service Bulletin, refer toAppendix 02.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTESKit 923130A01R07 1Kit 923130A02R03 1Kit 923130A03R07 1Kit 923130A04R03 1Kit 923130D01R01 2Supplementary kit 923130A01S01 1

Supplementary kit 923130A01S02 1







Component COMPA01 2 (1)

Consumable CMLA01 1Consumable CMLD01 1

NOTE (1): Component COMPA01 is only valid for aircraft on which additional workis required.

**CONF 002





5



MATERIAL QTY PER A/C SEE NOTESSupplementary kit 923130A06S01 1









**CONF 003












**CONF ALL

B. CONCURRENT REQUIREMENTS

None



5



C. REASON

(1) History

Several events of wiring being damaged in pylon area have been reported to AIRBUS byA330 operators as follows:

- Insulation damaged of feeder cables under bushing parts (PN F92430084200).

- Wires and convoluted conduit damaged to pressure transducers (FINs 8HA1, 9HA1,8HA2 and 9HA2).

(2) Objective/Action

The objective of this Service Bulletin is to prevent wiring from damage by:

- Replacing bushing and bobbin installation by a new assembly using standard parts.

- Replacing convoluted conduit by self-wrapping protective sleeve and suitableclamps.

(3) Advantages

Accomplishment of this Service Bulletin will improve the wiring installation in pylon areato prevent from chafing and subsequent damages.

This will contribute to avoid unscheduled maintenance actions (wiring repair) andpotential system misbehaviour of the pressure transducers (FINs 8HA1, 9HA1, 8HA2and 9HA2).

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001


(1) Modify the feeder’s routing LH pylon

(2) Modify the harness 501VB LH pylon

(3) Modify the Wire Insulation in the Left Wing Pylon


(1) Modify the feeder’s routing RH pylon

(2) Modify the harness 500VB RH pylon



5



(3) Modify the Wire Insulation in the Right Wing Pylon

Task 923130-831-804-001: Modification of the Clamp and Sleeve of Harness 501VB in theLH Pylon - ADDITIONAL WORK

(1) Modify the Clamp and Sleeve of Harness 501VB in the LH Pylon

Task 923130-831-803-001: Modification of the Clamp and Sleeve of Harness 500VB in theRH Pylon - ADDITIONAL WORK

(1) Modify the Clamp and Sleeve of Harness 500VB in the RH Pylon


(1) Modify the Hanging Knot on LH Pylon


(1) Modify Hanging Knot on RH Pylon

**CONF 002

















5





**CONF 003

















**CONF ALL

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to preventsignificant operational disruptions.



5



(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunitywhere manpower and facilities are available.

F. APPROVAL

The technical content of this document is approved under the authority of DesignOrganisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not ofAIRBUS origin, and which affects the content of this Service Bulletin, the operator isresponsible for obtaining approval by its airworthiness authority for any adaptation necessarybefore incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost todo the work. These estimates assume that the work will be done by experienced personnel,and may need to be revised upwards to suit operator’s circumstances. The estimates do notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are also notincluded.

**CONF 001


Get Access 2.00On Aircraft

Modify the feeder’s routing LH pylon 4.00

Modify the harness 501VB LH pylon 4.00

Modify the Wire Insulation in the Left Wing Pylon 0.50

Tests 1.00Close-Up 2.00


NOTE: For an explanation of the man-hours and elapsed time, refer to the GanttChart, Fig. A-FAAAA given in Appendix 01.



Modify the feeder’s routing RH pylon 4.00

Modify the harness 500VB RH pylon 4.00

Modify the Wire Insulation in the Right Wing Pylon 0.50


TOTAL MANHOURS 13.50



5




ELAPSED TIME (HOURS) 9.50

NOTE: For an explanation of the man-hours and elapsed time, refer to the GanttChart, Fig. A-FABAA given in Appendix 01.



Modify the Clamp and Sleeve of Harness 501VB in theLH Pylon

1.00

Close-Up 2.00




Modify the Clamp and Sleeve of Harness 500VB in theRH Pylon

1.00

Close-Up 2.00




Modify the Hanging Knot on LH Pylon 1.00

Close-Up 2.00




Modify Hanging Knot on RH Pylon 1.00

Close-Up 2.00




5



**CONF 002




















1.00

Close-Up 2.00





1.00

Close-Up 2.00



5








Close-Up 2.00





Close-Up 2.00


**CONF 003














Tests 1.00



5




Close-Up 2.00






1.00

Close-Up 2.00





1.00

Close-Up 2.00





Close-Up 2.00





Close-Up 2.00




5



**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 05-24-50 06-20-00 06-31-5306-31-54 06-41-53 12-34-2420-11-11 20-16-00 20-21-1122-97-00 24-41-00 36-11-1536-11-16 36-11-42

Aircraft Wiring List (AWL)Aircraft Wiring Manual (AWM) 24-22-03 24-42-02Consumable Material List (CML)Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-30 20-33-33

20-33-35 20-33-40 20-33-4220-33-44 20-44-16 20-48-2420-51-12 20-52-20 20-52-2120-55-00 20-56-51

Standards Manual (SM)Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00

51-43-00 51-43-12 51-44-0051-44-11 51-46-11 51-75-12

**CONF 002



20-33-35 20-33-40 20-33-4220-33-44 20-44-16 20-48-2420-51-12 20-52-20 20-52-2120-55-00 20-56-51


51-43-00 51-43-12 51-44-0051-44-11 51-46-11 51-75-12



5



**CONF 003



20-33-35 20-33-40 20-33-4220-33-44 20-44-16 20-48-2420-51-12 20-52-20 20-52-2120-55-00 20-56-51


51-43-00 51-43-12 51-44-0051-44-11 51-46-11 51-75-12

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)Illustrated Parts Catalog (IPC) 24-92-06

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None



5



2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send apurchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Kit 923130A01R07Kit 923130A02R03Kit 923130A03R07Kit 923130A04R03Kit 923130A05R06Kit 923130A06R04Kit 923130A07R06Kit 923130A08R04Kit 923130A09R05Kit 923130A10R03Kit 923130A11R05Kit 923130A12R03Supplementary kit 923130A01S01Supplementary kit 923130A01S02Supplementary kit 923130A02S01Supplementary kit 923130A03S01Supplementary kit 923130A03S02Supplementary kit 923130A04S01Supplementary kit 923130A05S01Supplementary kit 923130A05S02Supplementary kit 923130A06S01Supplementary kit 923130A07S01Supplementary kit 923130A07S02Supplementary kit 923130A08S01Supplementary kit 923130A09S01Supplementary kit 923130A09S02Supplementary kit 923130A10S01Supplementary kit 923130A11S01Supplementary kit 923130A11S02Supplementary kit 923130A12S01Supplementary kit 923130A02S02Supplementary kit 923130A04S02Supplementary kit 923130A06S02Supplementary kit 923130A08S02Supplementary kit 923130A10S02Supplementary kit 923130A12S02Kit 923130D01R01

AIRBUS Material, Logistics and SuppliersATP II B,Hein-Sass-Weg 2421129 HAMBURGGERMANYFor ordering by internet:http://spares.airbus.comFor ordering by E-mail: [email protected] Hotline: +49 40 743 51616

For standard hardware the purchase order shall be addressed to AIRBUS. Quote thenumber of this Service Bulletin, the MSN and, if applicable the Retrofit Information Letter(RIL) reference. Please send your request to:



5



Component COMPA01 AIRBUS Material, Logistics and SuppliersStandard PartsFor ordering by internet:http://spares.airbus.com or via SPEC2000For ordering by E-mail:[email protected]: +49 (0) 40 50 76 40 03

(2) Price and Availability

Kit 923130A01R07Cost 770.00 USDAvailability 250 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchaseorder. If items are required before this time, please include a retrofit planning schedulewith your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.The latest valid price and lead time for ordering purposes shall be obtained through theAIRBUS Spares portal or through a request for quotation to [email protected].










5


















5


















5



Supplementary kit 923130A01S01

Cost 260.00 USDAvailability 150 calendar days from receipt of order

















5





















5





















5





















5











Kit 923130D01R01Cost 95.00 USDAvailability 120 calendar days from receipt of order









5





















5







Component COMPA01

Operator supplied standard hardware parts, required to accomplish this Service Bulletin,are to be supplied from the operator’s stock.

B. INDUSTRY SUPPORT INFORMATION

For aircraft under warranty at Jun 01/13, AIRBUS will share the costs of accomplishment ofthis Service Bulletin by providing the kits at no charge for orders placed before Jun 30/17.

For aircraft under warranty at Jun 01/13, AIRBUS will credit the man hours indicated in thisService Bulletin at the agreed in-house warranty labor rate for claims received no later than90 days after completion of the last affected aircraft of your fleet, for the accomplishment ofthis Service Bulletin before Apr 01/19.

As a special policy, AIRBUS will share the costs by providing the supplementary kits at nocharge for orders placed before Apr 01/19 and AIRBUS will credit the COMPA01 parts fororders placed before Apr 01/19.

Claims for this allowance should be received no later than 90 days after completion of the lastaffected aircraft of your fleet.

C. LIST OF COMPONENTS

This table shows the supplemental kits (S kits) needed to update the kits already held in yourstock to the latest status.

Kit held by Operator Supplementary Kit required Latest status of Kit

923130A01R03 923130A01S01 and923130A01S02

923130A01R07

923130A01R06 923130A01S02 923130A01R07923130A01R07 None 923130A01R07923130A02R00 923130A02S01 and

923130A02S02923130A02R03


923130A03S02923130A03R07

923130A03R06 923130A03S02 923130A03R07



5




923130A03R07 None 923130A03R07923130A04R00 923130A04S01 and

923130A04S02923130A04R03

923130A04R02 923130A04S02 923130A04R03923130A04R03 None 923130A04R03



923130A05R02 923130A05S01 and923130A05S02

923130A05R06


923130A06S02923130A06R04


923130A07S02923130A07R06


923130A08S02923130A08R04

923130A08R03 923130A08S02 923130A08R04923130A08R04 None 923130A08R04



923130A09R02 923130A09S01 and923130A09S02

923130A09R05


923130A10S02923130A10R03


923130A11S02923130A11R05


923130A12S02923130A12R03

923130A12R02 923130A12S02 923130A12R03923130A12R03 None 923130A12R03



5



Kit 923130A01R07

ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEENOTES

1 ABS0678B01 2 SUPPORT4 F5493013720095 1 PLATE5 NSA5516C08BD 2 CLAMP6 NSA5050-3 5 NUT7 ASNA2397-10L 4 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER36 NSA5415N32-15 3 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)

NOTE: If you find part numbers of hardware components in the related kit(s) whichyou cannot identify in the LIST OF COMPONENTS of this Service Bulletin,refer to Standards Manual (SM). The SM will give you the correct part numberto part number relationship.

NOTE (1): Part number reference 4244 (COUSIN TRESTEC) and L0H103(HELLERMANNTYTON SA) is an alternative to PN reference NSA8420-5.

Kit 923130A02R03


13 NSA8420-7 5 (M) TAPE

17 NAS1801-3-8 3 SCREW18 NSA5067-3-1 6 NUT19 NAS1149C0332R 6 WASHER20 NSA5516C05BD 2 CLAMP25 D7171000621200 1 SPACER26 NSA5516C16BD 1 CLAMP27 NSA935808C01 2 WASHER28 NAS1801-3-20 1 SCREW29 NAS1801-3-9 1 SCREW30 NAS1801-3-10 1 SCREW31 F9241063620000 1 PLATE32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-19-5 2 (M) SLEEVE

55 NSA5516C09BD 1 CLAMP



5




Kit 923130A03R07


1 ABS0678B01 2 SUPPORT5 NSA5516C08BD 2 CLAMP6 NSA5050-3 6 NUT7 ASNA2397-10L 2 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER34 F5493015420095 1 PLATE35 F5493015520095 1 PLATE36 NSA5415N32-15 7 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)



Kit 923130A04R03


13 NSA8420-7 5 (M) TAPE

17 NAS1801-3-8 3 SCREW18 NSA5067-3-1 6 NUT19 NAS1149C0332R 6 WASHER20 NSA5516C05BD 2 CLAMP25 D7171000621200 1 SPACER26 NSA5516C16BD 1 CLAMP27 NSA935808C01 2 WASHER28 NAS1801-3-20 1 SCREW29 NAS1801-3-9 1 SCREW



5




30 NAS1801-3-10 1 SCREW31 F9241063620000 1 PLATE32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-19-5 2 (M) SLEEVE



Kit 923130A05R06


1 ABS0678B01 2 SUPPORT4 F5493013720095 1 PLATE5 NSA5516C08BD 2 CLAMP6 NSA5050-3 5 NUT7 ASNA2397-10L 4 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER36 NSA5415N32-15 3 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)



Kit 923130A06R04


13 NSA8420-7 5 (M) TAPE

17 NAS1801-3-8 2 SCREW18 NSA5067-3-1 4 NUT



5




19 NAS1149C0332R 4 WASHER20 NSA5516C05BD 2 CLAMP26 NSA5516C16BD 1 CLAMP29 NAS1801-3-9 1 SCREW31 F9241063620000 1 PLATE32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-19-5 2 (M) SLEEVE

39 D7171000620800 1 SPACER46 NAS1801-3-17 1 SCREW55 NSA5516C09BD 1 CLAMP


Kit 923130A07R06


1 ABS0678B01 2 SUPPORT5 NSA5516C08BD 2 CLAMP6 NSA5050-3 6 NUT7 ASNA2397-10L 2 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER34 F5493015420095 1 PLATE35 F5493015520095 1 PLATE36 NSA5415N32-15 7 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)





5



Kit 923130A08R04


13 NSA8420-7 5 (M) TAPE

17 NAS1801-3-8 2 SCREW18 NSA5067-3-1 4 NUT19 NAS1149C0332R 4 WASHER20 NSA5516C05BD 2 CLAMP26 NSA5516C16BD 1 CLAMP29 NAS1801-3-9 1 SCREW31 F9241063620000 1 PLATE32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-19-5 2 (M) SLEEVE



Kit 923130A09R05


1 ABS0678B01 2 SUPPORT5 NSA5516C08BD 1 CLAMP6 NSA5050-3 3 NUT10 ABS0679-01 1 BRACKET12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER17 NAS1801-3-8 3 SCREW19 NAS1149C0332R 3 WASHER36 NSA5415N32-15 4 RIVET40 F5493072020095 1 PLATE43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)





5



Kit 923130A10R03


13 NSA8420-7 5 (M) TAPE


33 EN6049-007-19-5 2 (M) SLEEVE

45 NAS1801-3-7 1 SCREW55 NSA5516C09BD 1 CLAMP


Kit 923130A11R05


1 ABS0678B01 2 SUPPORT6 NSA5050-3 2 NUT10 ABS0679-01 1 BRACKET12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER17 NAS1801-3-8 2 SCREW36 NSA5415N32-15 3 RIVET41 F5493072120095 1 PLATE42 NAS1149F0332P 2 WASHER43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)





5



Kit 923130A12R03


13 NSA8420-7 5 (M) TAPE


33 EN6049-007-19-5 2 (M) SLEEVE





13 NSA8420-7 TAPE14 NSA5050-4C 6 NUT37 D7171000621400 1 SPACER38 NSA5159-17 1 STUD




56 NSA8420-5 2 (M) TAPE (1)




13 NSA8420-7 TAPE26 NSA5516C16BD 1 CLAMP



5




32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-08-5 2 (M) SLEEVE




33 EN6049-007-19-5 2 (M) SLEEVE





6 NSA5050-3 2 NUT13 NSA8420-7 TAPE14 NSA5050-4C 6 NUT37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD




56 NSA8420-5 2 (M) TAPE (1)




13 NSA8420-7 TAPE



5




26 NSA5516C16BD 1 CLAMP32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-08-5 2 (M) SLEEVE




33 EN6049-007-19-5 2 (M) SLEEVE





13 NSA8420-7 TAPE14 NSA5050-4C 6 NUT37 D7171000621400 1 SPACER38 NSA5159-17 1 STUD




56 NSA8420-5 2 (M) TAPE (1)




13 NSA8420-7 TAPE



5




26 NSA5516C16BD 1 CLAMP32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-08-5 2 (M) SLEEVE

39 D7171000620800 1 SPACER46 NAS1801-3-17 1 SCREW




33 EN6049-007-19-5 2 (M) SLEEVE





6 NSA5050-3 2 NUT13 NSA8420-7 TAPE14 NSA5050-4C 6 NUT37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD




56 NSA8420-5 2 (M) TAPE (1)




5





13 NSA8420-7 TAPE26 NSA5516C16BD 1 CLAMP32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-08-5 2 (M) SLEEVE

39 D7171000620800 1 SPACER46 NAS1801-3-17 1 SCREW




33 EN6049-007-19-5 2 (M) SLEEVE





13 NSA8420-7 TAPE14 NSA5050-4C 6 NUT




56 NSA8420-5 2 (M) TAPE (1)




5






33 EN6049-007-08-5 2 (M) SLEEVE

45 NAS1801-3-7 1 SCREW




33 EN6049-007-19-5 2 (M) SLEEVE





13 NSA8420-7 TAPE14 NSA5050-4C 6 NUT17 NAS1801-3-8 1 SCREW




56 NSA8420-5 2 (M) TAPE (1)




5






33 EN6049-007-08-5 2 (M) SLEEVE

45 NAS1801-3-7 1 SCREW




33 EN6049-007-19-5 2 (M) SLEEVE



Kit 923130D01R01


51 EN6049-007-08-5 2 (M) SLEEVE

54 F9239026700100 1 PLCRDSET


D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CMLMAT. No.

QTY PER A/C SEENOTES

Primer Paint - Composite Structure 04FMA5 As required

Polysulfide Sealant-GeneralPurpose Interfay -

06AAC1 As required



5





Silicone Adhesive Sealant-GeneralPurpose One Par

06CMD9 As required

Non Aqueous Cleaner-General 08BAA9 As required

Consumable CMLD01



Adhesive Tape-Electrical Insulation 05TKC1 As required

Wirelocking Dia: 0.5 mm CresNickel Alloy

14QDB1 As required

Cord-Ligature 14RBA1 As required

(2) Components

NOTE: To accomplish this Service Bulletin it is necessary to use the expendableparts listed in the subsequent referenced tasks:

- AMM Task 36-11-15-400-802

- AMM Task 36-11-16-400-802

- AMM Task 36-11-42-400-802

Component COMPA01


13 NSA8420-7 5 (M) TAPE

NOTE: Component COMPA01 is only valid for aircraft on which additional workis required.

NOTE: The above list of components is not an AIRBUS Kit, the required partsshall be ordered as necessary through the given channel.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None



5



3. ACCOMPLISHMENT INSTRUCTIONS

Task 923130-831-801-001 - Modification of the routing in the LH pylon

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEPELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLYAND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCEWORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DOTHIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., ASNECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL ANDOTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATIONAND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures givenin other documents or in other sections of the Service Bulletin. When the words’refer to’ are used and the operator has a procedure accepted by the local authorityhe belongs to, the accepted alternative procedure can be used. When the words ’inaccordance with’ are used then the given procedure must be followed.

NOTE: The access and close-up instructions, not comprising return to service tests, in thisService Bulletin do not constitute or affect the technical intent of the ServiceBulletin. Operators can therefore, as deemed necessary, omit or add access and/orclose-up steps to add flexibility to their maintenance operations as long as thetechnical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenancenecessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions, including Required for Compliance (RC)paragraph contained herein, contact AIRBUS for further instructions and approval.

NOTE: Discarded parts must be managed at the operator’s discretion.



5



Task Associated Data

**CONF 001

Zone210 452 453

Modified FIN8HA1A 8HA1A1 9HA1A 9HA1A1 7701VB 3855VC 3855VCA 3855VT

AccessDoor 831

Panel 452CL 452CR 453BL 453BR 454BL 454BRManpower


**CONF 002

Zone210 452 453


AccessDoor 831



**CONF 003

Zone210 452 453


AccessDoor 831





5



**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 923130-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01ITEM DESCRIPTION REFERENCE TO

CML MAT. No.QTY PER A/C SEE

NOTESPrimer Paint - CompositeStructure

04FMA5 As required

Non Aqueous Cleaner-General

08BAA9 As required

ReferencesAircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-54, Page Block 00106-41-53, Page Block 001Task 20-11-11-911-803Task 20-16-00-912-801Task 20-21-11-911-801

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-0020-33-3020-33-3320-33-3520-33-4220-44-1620-48-2420-51-1220-52-21

Structural Repair Manual (SRM) 51-24-0051-40-0051-42-0051-43-0051-44-1151-46-1151-75-12

(a) For the wirelocking safety procedures and warnings, refer to AMM Task20-11-11-911-803.

(b) For the installation of lockwire, refer to ESPM 20-51-12.

(c) For the lacing tape application and tooling, refer to ESPM 20-33-35.



5



(d) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(e) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(f) For the identification of pylon stations and ribs, refer to AMM 06-31-54, Page Block001.

(g) For the installation of backshells and plugs, refer to ESPM 20-44-16.

(h) For the installation of connectors, refer to ESPM 20-48-24.

(i) For continuity testing of electrical harnesses, refer to ESPM 20-52-21.

(j) For the installation of conduits, refer to ESPM 20-33-33.

(k) For the installation of conduit protection, refer to ESPM 20-33-30.

(l) For the specification of materials (Mat. No.) given in this Service Bulletin, refer tothe Consumable Materials List (CML).

(m) Clean the work areas with:

Non AqueousCleaner-General

08BAA9 As required

(n) To torque tighten the standard threaded fasteners, refer to AMM Task20-21-11-911-801.

(o) Remove and install fasteners in accordance with SRM 51-42-00.

(p) Drill and deburr the holes in accordance with SRM 51-44-11.

(q) To countersink the holes in accordance with SRM 51-46-11.

(r) Cut the rivets to the necessary length.

(s) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00.

(t) If alternative and substitute fasteners have to be used, you must make sure that theassociated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’column.

(u) If the length of any fastener specified in this Service Bulletin does not meetinstallation standards given in SRM Chapter 51, then a fastener of the samespecification, or an approved substitute, with a length which meets the installationstandards given in SRM Chapter 51 may be used. In addition, washers may beinstalled for fastener grip length in accordance with SRM Chapter 51.

(v) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(w) Apply sealant in accordance with SRM 51-24-00.



5



(x) Renew the protective finish with:

Primer Paint -CompositeStructure

04FMA5 As required

(y) Renew the protective finish in accordance with SRM 51-75-12.

(z) For circuit breaker safety precautions, refer to AMM Task 20-16-00-912-801.

(aa) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(ab) Put all the retained hardware in identified plastic bags and attach the bags to therelated unit.

(ac) Tag all the parts you must remove and retain to make the subsequent installationeasier.

(2) Subtask 923130-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in thisService Bulletin.

**CONF 002


Manpower Resources

Skills NON SPECIFIC





04FMA5 As required


08BAA9 As required






5



ReferencesElec. Std. Practices Manual (ESPM) 20-33-00

20-33-3020-33-3320-33-3520-33-4220-44-1620-48-2420-51-1220-52-21
















08BAA9 As required





5













04FMA5 As required







Manpower Resources

Skills NON SPECIFIC


**CONF 003


Manpower Resources

Skills NON SPECIFIC



5







04FMA5 As required


08BAA9 As required




Elec. Std. Practices Manual (ESPM) 20-33-0020-33-3020-33-3320-33-3520-33-4220-44-1620-48-2420-51-1220-52-21












5









08BAA9 As required













04FMA5 As required






5






Manpower Resources

Skills NON SPECIFIC


**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 923130-941-001-001 - Job Set-up

Work Zones and Access PanelsZone Access/Work location

452453

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802Task 36-11-15-000-802Task 36-11-16-000-802Task 36-11-42-000-802

NOTE: The items given in this note shall be considered as the basic Aircraftconfiguration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safetylocks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers are closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized



5



- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position.

(a) Make sure that the aircraft is electrically grounded, refer to AMM Task12-34-24-860-802.

(b) Do the Job Set-up procedure as specified in the removal of the Bleed RegulatedPressure Transducer (FIN 8HA1), refer to AMM Task 36-11-16-000-802.

(c) Do the Job Set-up procedure as specified in the removal of the Bleed TransferredPressure Transducer (FIN 9HA1), refer to AMM Task 36-11-15-000-802.

(d) Do the Job Set-up procedure as specified in the removal of the Bleed Air PrecoolerExchanger (FIN 7150HA1), refer to AMM Task 36-11-42-000-802.

(e) Remove the access panels 454BL, 452CL, 454BR, 452CR, 453BL, 453BR, refer toAMM 05-24-50, Page Block 601.

(f) Open, safety/lock and tag this (these) circuit breaker(s):

PANEL DESIGNATION FIN LOCATION SEENOTES

721VU GCU 1 4XU1 10 Q721VU GCU 2 4XU2 11 Q721 VU GCU 2 4XU2 06 N

NOTE: Depending on the aircraft configuration, circuit breaker(s) can havedifferent locations.

**CONF 002



452453

Manpower Resources

Skills NON SPECIFIC






5



















721VU GCU 1 4XU1 10 Q721VU GCU 2 4XU2 11 Q721VU GCU 2 4XU2 06 N


**CONF 003



452453



5



Manpower Resources

Skills NON SPECIFIC




















721VU GCU 1 4XU1 10 Q721VU GCU 2 4XU2 11 Q



5




721VU GCU 2 4XU2 06 N


**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 923130-831-001-001 - Modify the feeder’s routing LH pylon


452 Access Panel 452CR, Panel 452CL, Panel 454BR,Panel 454BL

Manpower Resources

Manhours 4.00Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL


Kit 923130A01R07ITEM NEW PART N˚ QTY (UM) KEYWORD SEE

NOTES1 ABS0678B01 2 SUPPORT4 F5493013720095 1 PLATE5 NSA5516C08BD 2 CLAMP6 NSA5050-3 5 NUT7 ASNA2397-10L 4 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER36 NSA5415N32-15 3 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)



5



NOTE (1): Part number reference 4244 (COUSIN TRESTEC) and L0H103(HELLERMANNTYTON SA) is an alternative to PN referenceNSA8420-5.




04FMA5 As required


06AAC1 As required

Silicone Adhesive Sealant-General Purpose One Par

06CMD9 As required


08BAA9 As required

ReferencesAircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-33-42

Structural Repair Manual (SRM) 51-44-0051-75-12

Fig. A-FBAAAModification of the feeder’s routing of theLH pylon

Sheet 01Sheet 02Sheet 03Sheet 04Sheet 05

Fig. A-FBEAARemoval/Installation of the duct

Sheet 01

NOTE: During the modification of the feeders routing at LH pylon, you mayencounter some resistance to connect back the feeders to terminal block.In that case, you can easily proceed to connection, retrieving some over-length in the wing itself.

(a) For better access, refer to Fig. A-FBEAA Sheet 01, remove:

1 Duct Item (50) Retain

and

2 Clamps Item (51) Retain

Put blanking plugs on the disconnected line ends.

(b) Modify the feeder routing, refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 02,Fig. A-FBAAA Sheet 03, Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05

(c) On 3855VT, remove the lockwire and the cover protective.

(d) On 3855VT, disconnect wires as per Aircraft Wiring List (AWL).

Discard hardware.



5



(e) Disconnect 3855VCA from 3855VC.

(f) Put a blanking cap on the disconnected electrical connector.

(g) Remove:

1 Clamp Item (12) Discard

1 Spacer Cable Item (1) Discard

and associated bushings:

7 Bushing Item (44) Discard

(h) Remove:


1 Support fairlead Item (3) Discard

1 Plate Item (4) Discard

Discard hardware.

(i) Temporarily, at the same position than the old plate item (4), put in position thenew plate item 4 in accordance with the positioning hole.

NOTE: Be careful at the edge marging with the holes which must becounterdrilled from the pylon structure to the plate item 4.

(j) Drill the two other holes on the plate item 4 to match the holes of the pylonstructure in accordance with SRM 51-44-00.

(k) Remove and deburr the plate item 4.

(l) Clean the area with:


08BAA9 As required

(m) Renew the protective finish in accordance with SRM 51-75-12:


04FMA5 As required

(n) Install:

1 Plate F5493013720095 Item 4

with

3 Rivet NSA5415N32-15 Item 36



5



Do the installation of the parts with:

Polysulfide Sealant-General PurposeInterfay -

06AAC1 As required

(o) On plate item 4, install:

1 Bracket,Cable Support ABS0679-01 Item 10

with

2 Nut NSA5050-3 Item 6

2 Washer ASNA2397-10L Item 7

2 Screw NAS1096-3-8 Item 11

(p) On Bracket, Cable Support item 10, put in position:

2 Support-Cable ABS0678B01 Item 1

(q) Thru Support-Cable item 1, install feeders and excitation wires as shown on Fig. A-FBAAA Sheet 02, Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04.

(r) On Bracket,Cable Support item 10, affix Support-Cable item 1 with:

1 Clamp ASNA0032H067 Item 12

(s) Fix the tail of the clamp item 12 with:

1 (M) Wire-Lock MS20995C20 Item 43

(t) On 3855VT, re-connect wires as per Aircraft Wiring List (AWL) with:

6 Nut NSA5050-4C Item 14

6 Washer-Locking ASNA2553-0601 Item 15

6 Washer NSA5307-4C Item 16

(u) On 3855VT, affix cover protective then secure with:


(v) On plate item 4, install:

1 Clamp NSA5516C08BD Item 5

NOTE: It is permitted to use a clamp two sizes larger or two sizes smallerthan the given one, refer to ESPM 20-33-42.

with



5





1 Stud NSA5159-17 Item 38

1 Spacer D7171000621400 Item 37

(w) On structure, remove 1 screw and 1 washer in order to install new routing asshown on picture of figure Fig. A-FBAAA Sheet 05.

(x) On structure, install as shown on picture of figure Fig. A-FBAAA Sheet 05:



with



1 Spacer D7171000621400 Item 37


(y) Do the new routing thru the 2 news clamps item 5 and re-connect 3855VC.

(z) As shown on Fig. A-FBAAA Sheet 04, do an hanging knot as shown on view Lwith:

2 (M) Lacing Tape NSA8420-5 Item 56

Safety the knot with:

Silicone AdhesiveSealant-GeneralPurpose One Par

06CMD9 As required

(aa) Remove blanking plugs on the disconnected line ends.

Install (refer to Fig. A-FBEAA Sheet 01):

1 Duct Item (50) Retained atremoval

and

2 Clamps Item (51) Retained atremoval



5



(2) Subtask 923130-831-002-001 - Modify the harness 501VB LH pylon


453 Access Panel 453BR, Panel 453BL

Manpower Resources



Skills ELECTRICAL



NOTES13 NSA8420-7 5 (M) TAPE


33 EN6049-007-19-5 2 (M) SLEEVE




NOTESSilicone Adhesive Sealant-General Purpose One Par

06CMD9 As required


Elec. Std. Practices Manual (ESPM) 20-33-3320-33-4020-33-42

Fig. A-FBBAAModification of the harness 501VB of theLH pylon

Sheet 01Sheet 02Sheet 03



5



ReferencesFig. A-FBFAAOrientation of the backshells 8HA1A1,9HA1A1, 8HA2A1, 9HA2A1

Sheet 01

(a) Modify harness 501VB, refer to Fig. A-FBBAA Sheet 01, Fig. A-FBBAA Sheet 02and Fig. A-FBBAA Sheet 03

(b) Disconnect:

FIN 8HA1A1 Connector Retain


Remove:

FIN 8HA1A11 Backshell Retain


(c) On connectors 8HA1A and 9HA1A disconnect wires.

(d) On view C, remove:


1 Screw Item (17) Discard

1 Washer Item (19) Discard

1 Nut Item (18) Discard

(e) On view D, remove:





then





5



1 Spacer Item (25) Discard

1 Stud Item (23) Discard


(f) On view E, remove and discard:






(g) On view F, remove:


and associated hardware.

(h) On view G, have a look to see if you are not in view J AFTER conditions. If Yes goto next step.

If No, keep in place 2 clamps, then remove:






Move the clamps along the sleeves, turn the plate with an angle of 180 degrees,then fix the plate as seen on view J with:



2 Nut NSA5067-3-1 Item 18

2 Washer NAS1149C0332R Item 19



5



2 Washer NSA935808C01 Item 27

(i) On view B, remove:

Sleeves Item (32) Discard

between clamps view E and connectors 8HA1A and 9HA1A.

(j) On view B detail F, uncross the wires in order to keep routes M and S separatedas shown on view H.

(k) On view H, install between clamps view K and connectors 8HA1A and 9HA1A:

2 (M) Sleeve-Protective EN6049-007-05-5 Item 32

On the separated branches.


On the entire branch.

NOTE: For the installation of sleeve, refer to ESPM 20-33-33.

(l) Attach sleeves item 32 and 33 with:




06CMD9 As required

(m) On connectors 8HA1A and 9HA1A, connect wires as per Aircraft Wiring List (AWL).

(n) Install with orientation angle of 45 degrees:

Refer to Fig. A-FBFAA Sheet 01

Refer to ESPM 20-33-40

FIN 8HA1A11 backshell Retained at

removal


removal

Connect:



5



FIN 8HA1A1 connector Retained at

removal


removal

(o) On view M, install:



with




(p) On view L, install:

1 Plate F9241063620000 Item 31

with




(q) On Plate item 31, install:



with

1 Spacer D7171000621200 Item 25




NOTE: Routes have to be gathered on the same sleeve, making their path



5



thru one clamp.

(r) On view K, install:



with




NOTE: Routes have to be separated, making their path thru two differentclamps.

(3) Subtask 923130-831-201-004 - Modify the Wire Insulation in the Left Wing Pylon


452 Access Panel 452CL

Manpower Resources



Skills ELECTRICAL


Kit 923130D01R01ITEM NEW PART N˚ QTY (UM) KEYWORD SEE

NOTES51 EN6049-007-08-5 2 (M) SLEEVE

54 F9239026700100 1 PLCRDSET

Consumable CMLD01ITEM DESCRIPTION REFERENCE TO


NOTESAdhesive Tape-ElectricalInsulation

05TKC1 As required

Wirelocking Dia: 0.5 mmCres Nickel Alloy

14QDB1 As required




5




Aircraft Wiring Manual (AWM) 24-42-02

Elec. Std. Practices Manual (ESPM) 20-33-3020-33-3320-33-3520-44-16

Fig. A-GBAABModification to the Wire Insulation in theLeft Wing Pylon

Sheet 01Sheet 02

Fig. A-GHAAAHook-up Chart

Sheet 01

Fig. A-GWAAAWiring Diagram

Sheet 01

(a) Modify the wire insulation in the left wing pylon.

1 As shown in Fig. A-GBAAB Sheet 01, View B, remove the lockwire from theelectrical connector at FIN 3855VCA.

2 As shown in Fig. A-GBAAB Sheet 01, View B, remove from the electricalconnector at FIN 3855VCA, refer to ESPM 20-44-16:

1 Backshell E0455-03-16N Item (52) Retain

1 Connector E0454RS16-10PN Item (53) Retain

3 As shown in Fig. A-GBAAB Sheet 01, View B, remove from the wire at FIN7701VB:

1 Electrical Conduit NSA935806-09 Item (51) Discard

4 As shown in Fig. A-GBAAB Sheet 02, View C, the wiring diagram Fig. A-GWAAA Sheet 01 and the hook-up chart Fig. A-GHAAA Sheet 01, lines 1 thruto 6, connect the wires and install:

1 Connector E0454RS16-10PN Item (53) Retained atremoval

1 Backshell E0455-03-16N Item (52) Retained atremoval

5 As shown in Fig. A-GBAAB Sheet 02, View C, cut to the necessary lengthand install on the wire at FIN 7701VB, refer to ESPM 20-33-30 and ESPM20-33-33:

2 (M) Textile Sleeve EN6049-007-08-5 Item 51

with




5



NOTE: The Textile Sleeve, Item 51, must exceed 20 mm (0.787 in.)over the last wing fixing point.

6 As shown in Fig. A-GBAAB Sheet 02, View C, attach the Textile Sleeve, Item51, to the Open Backshell, Item (52), with:

Adhesive Tape-Electrical Insulation

05TKC1 As required

7 Secure the Connector, Item (53) and the Backshell, Item (52), use:

Wirelocking Dia: 0.5mm Cres NickelAlloy

14QDB1 As required

8 As shown in Fig. A-GBAAB Sheet 02, View C, attach to the wire, refer toESPM 20-33-35:

1 Placard F9239026700100 Item 54

with:


**CONF 002



452 Access Panel 452CR, Panel 452CL, Panel 454BL, Panel454BR

Manpower Resources



Skills ELECTRICAL



NOTES1 ABS0678B01 2 SUPPORT4 F5493013720095 1 PLATE5 NSA5516C08BD 2 CLAMP6 NSA5050-3 5 NUT7 ASNA2397-10L 4 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW



5



ITEM NEW PART N˚ QTY (UM) KEYWORD SEENOTES

12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER36 NSA5415N32-15 3 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)





04FMA5 As required


06AAC1 As required


06CMD9 As required


08BAA9 As required




Fig. A-FBAABModification of the feeder’s routing of theLH pylon



Sheet 01

NOTE: During the modification of the feeders routing at LH pylon, you mayencounter some resistance to connect back the feeders to terminal block.In that case, you can easily proceed to connection, retrieving some over-length in the wing itself.





5



and



(b) Modify the feeder routing, refer to Fig. A-FBAAB Sheet 01, Fig. A-FBAAB Sheet 02,Fig. A-FBAAB Sheet 03, Fig. A-FBAAB Sheet 04 and Fig. A-FBAAB Sheet 05



Discard hardware.



(g) Remove:





(h) Remove:




Discard hardware.

(i) Temporarily, at the same position than the old plate item (4), put in position thenew plate item 4 in accordance with the positioning hole.

NOTE: Be careful at the edge marging with the holes which must to becounterdrilled from the pylon structure to the plate item 4.





5





08BAA9 As required



04FMA5 As required

(n) Install:

1 Plate F5493013720095 Item 4

with




06AAC1 As required


1 Bracket, Cable Support ABS0679-01 Item 10

with




(p) On Bracket,Cable Support item 10, put in position:


(q) Thru Support-Cable item 1, install feeders and excitation wires as shown on Fig. A-FBAAB Sheet 02, Fig. A-FBAAB Sheet 03 and Fig. A-FBAAB Sheet 04.

(r) On Bracket,Cable Support item 10, affix Support-Cable item 1 with:






5









(v) On plate item 4, install:



with




1 Spacer D7171000621400 Item 37

(w) On structure, remove 1 screw and 1 washer in order to install new routing asshown on picture of figure Fig. A-FBAAB Sheet 05.

(x) On structure, install as shown on picture of figure Fig. A-FBAAB Sheet 05:



with



1 Spacer D7171000621400 Item 37


(y) Do the new routing thru the 2 news clamps item 5 and re-connect 3855VC.



5



(z) As shown on Fig. A-FBAAB Sheet 04, do an hanging knot as shown on view Lwith:




06CMD9 As required




and




453 Access Panel 453BL, Panel 453BR

Manpower Resources



Skills ELECTRICAL





33 EN6049-007-19-5 2 (M) SLEEVE



5








06CMD9 As required



Fig. A-FBBABModification of the harness 501VB of theLH pylon


Fig. A-FBFAAOrientation of the backshells 8HA1A1,9HA1A1, 8HA2A1, 9HA2A1

Sheet 01

(a) Modify harness 501VB, refer to Fig. A-FBBAB Sheet 01, Fig. A-FBBAB Sheet 02and Fig. A-FBBAB Sheet 03

(b) Disconnect:



Remove:









5










then















(h) On view B, remove:





5



(i) On view B detail F, uncross the wires in order to keep routes M and S separatedas shown on view G.

(j) On view G, install between clamps view H and connectors 8HA1A and 9HA1A:






(k) Attach sleeves item 32 and 33 with:




06CMD9 As required

(l) Install with orientation angle of 45 degrees:




removal


removal

Connect:


removal


removal

(m) On view K, install:




5




with




(n) On view J, install:

1 Plate F9241063620000 Item 31

with




(o) On Plate item 31, install:



with

1 Spacer D7171000620800 Item 39




NOTE: Routes have to be gathered on the same sleeve, making their paththru one clamp.

(p) On view H, install:



with




5









Manpower Resources



Skills ELECTRICAL



NOTES51 EN6049-007-08-5 2 (M) SLEEVE

54 F9239026700100 1 PLCRDSET




05TKC1 As required


14QDB1 As required





Fig. A-GBAABModification to the Wire Insulation in theLeft Wing Pylon

Sheet 01Sheet 02


Sheet 01



5



ReferencesFig. A-GWAAAWiring Diagram

Sheet 01


1 As shown in Fig. A-GBAAB Sheet 01, View B, remove the lockwire from theelectrical connector at FIN 3855VCA.

2 As shown in Fig. A-GBAAB Sheet 01, View B, remove from the electricalconnector at FIN 3855VCA, refer to ESPM 20-44-16:



3 As shown in Fig. A-GBAAB Sheet 01, View B, remove from the wire at FIN7701VB:


4 As shown in Fig. A-GBAAB Sheet 02, View C, the wiring diagram Fig. A-GWAAA Sheet 01 and the hook-up chart Fig. A-GHAAA Sheet 01, lines 1 thruto 6, connect the wires and install:



5 As shown in Fig. A-GBAAB Sheet 02, View C, cut to the necessary lengthand install on the wire at FIN 7701VB, refer to ESPM 20-33-30 and ESPM20-33-33:


with


NOTE: The Textile Sleeve, Item 51, must exceed 20 mm (0.787 in.)over the last wing fixing point.

6 As shown in Fig. A-GBAAB Sheet 02, View C, attach the Textile Sleeve, Item51, to the Open Backshell, Item (52), with:


05TKC1 As required



5





14QDB1 As required

8 As shown in Fig. A-GBAAB Sheet 02, View C, attach to the wire, refer toESPM 20-33-35:

1 Placard F9239026700100 Item 54

with:


**CONF 003




Manpower Resources



Skills ELECTRICAL



NOTES1 ABS0678B01 2 SUPPORT5 NSA5516C08BD 1 CLAMP6 NSA5050-3 3 NUT10 ABS0679-01 1 BRACKET12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER17 NAS1801-3-8 3 SCREW19 NAS1149C0332R 3 WASHER36 NSA5415N32-15 4 RIVET40 F5493072020095 1 PLATE43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)



5







04FMA5 As required


06AAC1 As required


06CMD9 As required


08BAA9 As required




Fig. A-FBAACModification of the feeder’s routing of theLH pylon

Sheet 01Sheet 02Sheet 03Sheet 04Sheet 05Sheet 06


Sheet 01



and



(b) Modify the feeder routing, refer to Fig. A-FBAAC Sheet 01, Fig. A-FBAAC Sheet02, Fig. A-FBAAC Sheet 03, Fig. A-FBAAC Sheet 04, Fig. A-FBAAC Sheet 05 andFig. A-FBAAC Sheet 06



Discard hardware.




5




(g) Remove:





(h) Remove:


Discard hardware.

(i) Remove:


Discard hardware.

(j) Temporarily, at the same position than the old plate item (40), put in position thenew plate item 40 in accordance with the positioning hole.


(k) Drill the three other holes on the plate item 40 to match the holes of the pylonstructure in accordance with SRM 51-44-00.

(l) Remove and deburr the plate item 40.

(m) Clean the area with:


08BAA9 As required

(n) Renew the protective finish in accordance with SRM 51-75-12:


04FMA5 As required

(o) Install:

1 Plate F5493072020095 Item 40

with





5




06AAC1 As required

(p) On plate item 40, install:


with




(q) On Bracket, Cable Support item 10, put in position:


(r) Thru Support-Cable item 1, install feeders and excitation wires as shown on Fig. A-FBAAC Sheet 03, Fig. A-FBAAC Sheet 04 and Fig. A-FBAAC Sheet 05

(s) On Bracket, Cable Support item 10, affix Support-Cable item 1 with:


(t) Fix the tail of the clamp item 12 with:


(u) On 3855VT, re-connect wires as per Aircraft Wiring List (AWL) with:




(v) On 3855VT, affix cover protective then secure with:


(w) On structure, remove:


Discard hardware.

(x) On structure, install as shown on picture of figure Fig. A-FBAAC Sheet 05:




5




with




(y) Do the new routing thru clamp item 5 and re-connect 3855VC.

(z) As shown on figure Fig. A-FBAAC Sheet 06, do an hanging knot as shown on viewP with:




06CMD9 As required




and





Manpower Resources



Skills ELECTRICAL



5







33 EN6049-007-19-5 2 (M) SLEEVE





06CMD9 As required



Fig. A-FBBACModification of the harness 501VB of theLH pylon



Sheet 01

(a) Modify harness 501VB, refer to Fig. A-FBBAC Sheet 01, Fig. A-FBBAC Sheet 02and Fig. A-FBBAC Sheet 03

(b) Disconnect:



Remove:



5
















then













5






(h) On view F, remove:






(j) On view B detail F, uncross the wires in order to keep routes M and S separatedas shown on view G.

(k) On view G, install between clamps view H and connectors 8HA1A and 9HA1A:










06CMD9 As required

(m) Install with orientation angle of 45 degrees:




removal



5




removal

Connect:


removal


removal

(n) On view K, install:



with




(o) On view J, install:

1 Plate F9241063620000 Item 31

with




(p) On Plate item 31, install:



with





5





(q) On view H, install:



with








Manpower Resources



Skills ELECTRICAL



NOTES51 EN6049-007-08-5 2 (M) SLEEVE

54 F9239026700100 1 PLCRDSET




05TKC1 As required


14QDB1 As required



5



ITEM DESCRIPTION REFERENCE TOCML MAT. No.






Fig. A-GBAAAModification to the Wire Insulation in theLeft Wing Pylon



Sheet 01

Fig. A-GWAAAWiring Diagram

Sheet 01


1 As shown in Fig. A-GBAAA Sheet 01, View B, remove the lockwire from theelectrical connector at FIN 3855VCA.

2 As shown in Fig. A-GBAAA Sheet 01, View B, remove the electrical connectorat FIN 3855VCA, refer to ESPM 20-44-16:



3 As shown in Fig. A-GBAAA Sheet 01, View B, remove from the wire at FIN7701VB:


4 As shown in Fig. A-GBAAA Sheet 02, View C, the wiring diagram Fig. A-GWAAA Sheet 01 and the hook-up chart Fig. A-GHAAA Sheet 01, lines 1 thruto 6, connect the wires and install:



5 As shown in Fig. A-GBAAA Sheet 02, View C, cut to the necessary lengthand install on the wire at FIN 7701VB, refer to ESPM 20-33-30 and ESPM20-33-33:




5



with


6 As shown in Fig. A-GBAAA Sheet 02, View C, attach the Textile Sleeve, Item51, to the Open Backshell, Item (52), with:


05TKC1 As required



14QDB1 As required

8 As shown in Fig. A-GBAAA Sheet 02, View C, attach to the wire, refer toESPM 20-33-35:

1 Placard F9239026700100 Item 54

with:


**CONF ALL

D. TEST

**CONF 001

(1) Subtask 923130-730-002-001 - System


210 Access Door 831

Manpower Resources

Skills NON SPECIFIC

ReferencesAircraft Maintenance Manual (AMM) Task 22-97-00-740-801


Elec. Std. Practices Manual (ESPM) 20-48-2420-52-20

(a) Job Set-Up

NOTE: If the aircraft is operated in actual CAT III conditions, you mustalso do the LAND CAT III capability test, refer to AMM Task



5



22-97-00-740-801.

1 Remove the safety clip(s) and/or tag(s) and close/unlock this (these) circuitbreaker(s):



2 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakersas specified after the Installation of the Bleed Transferred Pressure-Transducer (FIN 9HA1), refer to AMM Task 36-11-15-400-802.

3 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakersas specified after the Installation of the Bleed Regulated Pressure-Transducer(FIN 8HA1), refer to AMM Task 36-11-16-400-802.

4 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakersas specified after the Installation of the Bleed Air Precooler Exchanger (FIN7150HA1), refer to AMM Task 36-11-42-400-802.

(b) Procedure

1 Test of the equipment (FINs 9HA1 and 8HA1)

a Do the test procedure as specified after the Installation of the BleedTransferred Pressure-Transducer (FIN 9HA1), refer to AMM Task36-11-15-400-802.

b Do the test procedure as specified after the Installation of theBleed Regulated Pressure-Transducer (FIN 8HA1), refer to AMM Task36-11-16-400-802.

c Do the test procedure as specified after the Installation of theBleed Air Precooler Exchanger (FIN 7150HA1), refer to AMM Task36-11-42-400-802.

2 Test of the connector (FIN 3855VC)

a Do a continuity test on the wire at FIN 7701VB and connector at FIN3855VCA, refer to ESPM 20-48-24.

b Do the BITE Test of the Electrical Power Generation System (EPGS)(GCU and GPCU), refer to AMM Task 24-41-00-740-801.



5



**CONF 002

(1) Subtask 923130-730-002-002 - System


210 Access Door 831

Manpower Resources

Skills NON SPECIFIC




(a) Job Set-Up

NOTE: If the aircraft is operated in actual CAT III conditions, you mustalso do the LAND CAT III capability test, refer to AMM Task22-97-00-740-801.









5



(b) Procedure








**CONF 003

(1) Subtask 923130-730-002-003 - System


210 Access Door 831

Manpower Resources

Skills NON SPECIFIC




(a) Job Set-Up




5






2 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakersas specified after the Installation of the Bleed Transferred Pressure-Transducer (FIn 9HA1), refer to AMM Task 36-11-15-400-804.



(b) Procedure










5



**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 923130-942-002-001 - Close-up


453452

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-802Task 36-11-16-400-802Task 36-11-42-400-802

(a) Close the access panels 454BL, 452CL, 454BR, 452CR, 453BL, 453BR, refer toAMM 05-24-50, Page Block 601.

(b) Do the Close-up procedure as specified in the Installation of the Bleed RegulatedPressure-Transducer (FIN 8HA1), refer to AMM Task 36-11-16-400-802.

(c) Do the Close-up procedure as specified in the Installation of the Bleed TransferredPressure-Transducer (FIN 9HA1), refer to AMM Task 36-11-15-400-802.

(d) Do the Close-up procedure as specified in the Installation of the Bleed AirPrecooler Exchanger (FIN 7150HA1), refer to AMM Task 36-11-42-400-802.

(e) Put the aircraft back to its initial configuration.

**CONF 002

(1) Subtask 923130-942-002-002 - Close-up


453452

Manpower Resources

Skills NON SPECIFIC



5




Task 36-11-15-400-803Task 36-11-16-400-803Task 36-11-42-400-803






**CONF 003

(1) Subtask 923130-942-002-003 - Close-up


453452

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-804Task 36-11-16-400-804Task 36-11-42-400-804








5






5



Task 923130-831-802-001 - Modification of the routing in the RH pylon

**CONF ALL



- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., ASNECESSARY ON WIRING AND COMPONENTS



IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.









5




**CONF 001

Zone210 462 463

Modified FIN8HA2A 8HA2A1 9HA2A 9HA2A1 8HA2A 9HA2A 7702VB 3854VC 3854VCA 3854VT

AccessDoor 831



**CONF 002

Zone210 462 463


AccessDoor 831



**CONF 003

Zone210 462 463


AccessDoor 831





5



**CONF ALL

A. GENERAL

**CONF 001


Manpower Resources

Skills NON SPECIFIC





04FMA5 As required


08BAA9 As required




Elec. Std. Practices Manual (ESPM) 20-33-0020-33-3020-33-3320-33-3520-44-1620-48-2420-51-1220-52-21

Structural Repair Manual (SRM) 51-40-0051-42-0051-43-1251-44-1151-46-1151-75-12







5













08BAA9 As required




(q) If alternative and substitute fasteners have to be used, you must make sure that theassociated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’column.

(r) If the length of any fastener specified in this Service Bulletin does not meetinstallation standards given in SRM Chapter 51, then a fastener of the samespecification, or an approved substitute, with a length which meets the installationstandards given in SRM Chapter 51 may be used. In addition, washers may beinstalled for fastener grip length in accordance with SRM Chapter 51.

(s) To countersink the holes in accordance with SRM 51-46-11.

(t) Cut the rivets to the necessary length.

(u) For alternative and substitute fasteners in accordance with SRM 51-43-12.

(v) Renew the protective finish with:


04FMA5 As required

(w) Renew the protective finish in accordance with SRM 51-75-12.



5



(x) For circuit breaker safety precautions, refer to AMM Task 20-16-00-912-801.

(y) Obey the instructions for the general wiring installation, refer to ESPM 20-33-00.

(z) Put all the retained hardware in identified plastic bags and attach the bags to therelated unit.

(aa) Tag all the parts you must remove and retain to make the subsequent installationeasier.


Manpower Resources

Skills NON SPECIFIC


**CONF 002


Manpower Resources

Skills NON SPECIFIC





04FMA5 As required


08BAA9 As required







5



ReferencesStructural Repair Manual (SRM) 51-40-00

51-42-0051-43-1251-44-1151-46-1151-75-12















08BAA9 As required







5









04FMA5 As required







Manpower Resources

Skills NON SPECIFIC


**CONF 003


Manpower Resources

Skills NON SPECIFIC





04FMA5 As required



5






08BAA9 As required





Structural Repair Manual (SRM) 51-40-0051-42-0051-43-1251-44-1151-46-1151-75-12














5






08BAA9 As required











04FMA5 As required







Manpower Resources

Skills NON SPECIFIC



5




**CONF ALL

B. PREPARATION

**CONF 001



463462

Manpower Resources

Skills NON SPECIFIC

















5





(e) Open the access panels 464BL, 462CL, 464BR, 462CR, 463BL, 463BR, refer toAMM 05-24-50, Page Block 601.





**CONF 002



462463

Manpower Resources

Skills NON SPECIFIC











5
















**CONF 003



462463

Manpower Resources

Skills NON SPECIFIC





5
























5



**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 923130-831-003-001 - Modify the feeder’s routing RH pylon



Manpower Resources



Skills ELECTRICAL



NOTES1 ABS0678B01 2 SUPPORT5 NSA5516C08BD 2 CLAMP6 NSA5050-3 6 NUT7 ASNA2397-10L 2 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER34 F5493015420095 1 PLATE35 F5493015520095 1 PLATE36 NSA5415N32-15 7 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)




5






04FMA5 As required


06AAC1 As required


06CMD9 As required


08BAA9 As required




Fig. A-FBCAAModification of the feeder’s routing of theRH pylon



Sheet 01



and



(b) Modify the feeder routing, refer to Fig. A-FBCAA Sheet 01, Fig. A-FBCAA Sheet02, Fig. A-FBCAA Sheet 03, Fig. A-FBCAA Sheet 04 and Fig. A-FBCAA Sheet 05



Discard hardware.

(e) Disconnect 3854VCA.


(g) Remove:




5






(h) Remove:





Discard hardware.

(i) Temporarily, put in position the plate item 34 in accordance with the positioninghole.


(j) Drill the three other holes on the plate item 34 to match the holes of the pylonstructure in accordance with SRM 51-44-00.




08BAA9 As required



04FMA5 As required

(n) Install:

1 Plate F5493015420095 Item 34

with




06AAC1 As required



5



(o) Temporarily, put in position the plate item 35 in accordance with the positioninghole. You have to remove one more rivet to do it.


(p) Drill the two other holes on the plate item 35 to match the holes of the pylonstructure in accordance with SRM 51-44-00.

(q) Remove and deburr the plate item 35.

(r) Clean the area with:


08BAA9 As required

(s) Renew the protective finish in accordance with SRM 51-75-12:


04FMA5 As required

(t) Install:

1 Plate F5493015520095 Item 35

with




06AAC1 As required

(u) On plate item 34, install:


with




(v) On Bracket, Cable Support item 10, put in position:


(w) Thru Support-Cable item 1, install feeders and excitation wires as shown on Fig. A-FBCAA Sheet 02, Fig. A-FBCAA Sheet 03, Fig. A-FBCAA Sheet 04 and Fig. A-FBCAA Sheet 05



5



(x) On Bracket, Cable Support item 10, affix Support-Cable item 1 with:


(y) Fix the tail of the clamp item 12 with:


(z) On 3854VT, re-connect wires as per Aircraft Wiring List (AWL) with:




(aa) On 3854VT, affix cover protective then secure with:


(ab) On plate item 35, install:



with



2 Spacer D7171000621400 Item 37

(ac) Do the new routing thru the 2 news clamps item 5 and re-connect 3854VC.

(ad) As shown on Fig. A-FBCAA Sheet 05, do an hanging knot as shown on view Nwith:




06CMD9 As required

(ae) Remove blanking plugs on the disconnected line ends.




5




and


(2) Subtask 923130-831-004-001 - Modify the harness 500VB RH pylon


463 Access Panel 463BR, Panel 463BL

Manpower Resources



Skills ELECTRICAL





33 EN6049-007-19-5 2 (M) SLEEVE





06CMD9 As required



5





Fig. A-FBDAAModification of the harness 500VB of theRH pylon



Sheet 01

(a) Modify harness 500VB, refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02and Fig. A-FBDAA Sheet 03

(b) Disconnect:



Remove:



(c) On connectors FINs 8HA2A and 9HA2A disconnect wires.












5




then















(h) On view G, have a look to see if you are not in view J AFTER conditions. If Yes goto next step.

If No, keep in place 2 clamps, then remove:






Move the clamps along the sleeves, turn the plate with an angle of 180 degrees,then fix the plate as seen on view J with:



5







2 Washer NSA935808C01 Item 27




(j) On view B detail F, uncross the wires in order to keep routes M and S separatedas shown on view H.

(k) On view H, install between clamps view K and connectors 8HA2A and 9HA2A:










06CMD9 As required

(m) On connectors FINs 8HA2A and 9HA2A, connect wires as per Aircraft Wiring List(AWL).

Install with orientation angle of 45 degrees:




removal



5




removal

Connect:


removal


removal

(n) On view M, install:



with




(o) On view L, install:

1 Plate F9241063620000 Item 31

with




(p) On Plate item 31, install:



with

1 Spacer D7171000621200 Item 25




5






(q) On view K, install:



with





(3) Subtask 923130-831-202-002 - Modify the Wire Insulation in the Right Wing Pylon



Manpower Resources



Skills ELECTRICAL



NOTES51 EN6049-007-08-5 2 (M) SLEEVE

54 F9239026700100 1 PLCRDSET




05TKC1 As required



5






14QDB1 As required





Fig. A-GBBABModification to the Wire Insulation in theRight Wing Pylon

Sheet 01Sheet 02

Fig. A-GHBAAHook-up Chart

Sheet 01

Fig. A-GWBAAWiring Diagram

Sheet 01

(a) Modify the wire insulation in the right wing pylon.

1 As shown in Fig. A-GBBAB Sheet 01, View B, remove the lockwire from theElectrical Connector at FIN 3854VCA.

2 As shown in Fig. A-GBBAB Sheet 01, View B, remove from the electricalconnector at FIN 3854VCA, refer to ESPM 20-44-16:




3 As shown in Fig. A-GBBAB Sheet 02, View C, the wiring diagram Fig. A-GWBAA Sheet 01 and the hook-up chart Fig. A-GHBAA Sheet 01, lines 1 thruto 6, connect the wires and install:



4 As shown in Fig. A-GBBAB Sheet 02, View C, cut to the necessary lengthand install on the wire at FIN 7702VB, refer to ESPM 20-33-30 and ESPM20-33-33:




5



with


5 As shown in Fig. A-GBBAB Sheet 02, View C, attach the Textile Sleeve, Item51, to the Open Backshell, Item (52), with:


05TKC1 As required

6 Secure the Connector, Item (53) and the Backshell, Item (52), with lockwire,use:


14QDB1 As required

7 As shown in Fig. A-GBBAB Sheet 02, View C, attach to the wire, refer toESPM 20-33-35:

1 Placard F9239026700100 Item 54

with:


**CONF 002



462 Access Panel 462CR, Panel 464BR, Panel 462CL,Panel 464BL

Manpower Resources



Skills ELECTRICAL



NOTES1 ABS0678B01 2 SUPPORT5 NSA5516C08BD 2 CLAMP6 NSA5050-3 6 NUT7 ASNA2397-10L 2 WASHER10 ABS0679-01 1 BRACKET11 NAS1096-3-8 2 SCREW



5




12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER34 F5493015420095 1 PLATE35 F5493015520095 1 PLATE36 NSA5415N32-15 7 RIVET37 D7171000621400 2 SPACER38 NSA5159-17 2 STUD43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)





04FMA5 As required


06AAC1 As required


06CMD9 As required


08BAA9 As required




Fig. A-FBCABModification of the feeder’s routing of theRH pylon



Sheet 01



and



5





(b) Modify the feeder routing, refer to Fig. A-FBCAB Sheet 01, Fig. A-FBCAB Sheet02, Fig. A-FBCAB Sheet 03, Fig. A-FBCAB Sheet 04 and Fig. A-FBCAB Sheet 05



Discard hardware.



(g) Remove:





(h) Remove:





Discard hardware.



(j) Drill the three other holes on the plate item 34 to match the holes of the pylonstructure in accordance with SRM 51-44-00.




5





08BAA9 As required



04FMA5 As required

(n) Install:

1 Plate F5493015420095 Item 34

with




06AAC1 As required

(o) Temporarily, put in position the plate item 35 in accordance with the positioninghole. You have to remove one more rivet to do it.


(p) Drill the two other holes on the plate item 35 to match the holes of the pylonstructure in accordance with SRM 51-44-00.

(q) Remove and deburr the plate item 35.

(r) Clean the area with:


08BAA9 As required

(s) Renew the protective finish in accordance with SRM 51-75-12:


04FMA5 As required

(t) Install:

1 Plate F5493015520095 Item 35

with




5





06AAC1 As required

(u) On plate item 34, install:


with




(v) On Bracket, Cable Support item 10, put in position:


(w) Thru Support-Cable item 1, install feeders and excitation wires as shown on Fig. A-FBCAB Sheet 02, Fig. A-FBCAB Sheet 03, Fig. A-FBCAB Sheet 04 and Fig. A-FBCAB Sheet 05

(x) On Bracket, Cable Support item 10, affix Support-Cable item 1 with:


(y) Fix the tail of the clamp item 12 with:


(z) On 3854VT, re-connect wires as per Aircraft Wiring List (AWL) with:




(aa) On 3854VT, affix cover protective then secure with:


(ab) On plate item 35, install:





5



with



2 Spacer D7171000621400 Item 37

(ac) Do the new routing thru the 2 news clamps item 5 and re-connect 3854VC.

(ad) As shown on Fig. A-FBCAB Sheet 05, do an hanging knot as shown on view Nwith:




06CMD9 As required

(ae) Remove blanking plugs on the disconnected line ends.



and





Manpower Resources



Skills ELECTRICAL




17 NAS1801-3-8 2 SCREW



5




18 NSA5067-3-1 4 NUT19 NAS1149C0332R 4 WASHER20 NSA5516C05BD 2 CLAMP26 NSA5516C16BD 1 CLAMP29 NAS1801-3-9 1 SCREW31 F9241063620000 1 PLATE32 EN6049-007-05-5 2 (M) SLEEVE

33 EN6049-007-19-5 2 (M) SLEEVE





06CMD9 As required



Fig. A-FBDABModification of the harness 500VB of theRH pylon



Sheet 01

(a) Modify harness 500VB, refer to Fig. A-FBDAB Sheet 01, Fig. A-FBDAB Sheet 02and Fig. A-FBDAB Sheet 03

(b) Disconnect:



Remove:





5














then
















5


















06CMD9 As required





removal


removal

Connect:


removal



5




removal




with





1 Plate F9241063620000 Item 31

with







with

1 Spacer D7171000620800 Item 39







5






with








Manpower Resources



Skills ELECTRICAL



NOTES51 EN6049-007-08-5 2 (M) SLEEVE

54 F9239026700100 1 PLCRDSET




05TKC1 As required


14QDB1 As required






5




20-33-3320-33-3520-44-16

Fig. A-GBBABModification to the Wire Insulation in theRight Wing Pylon

Sheet 01Sheet 02


Sheet 01


Sheet 01


1 As shown in Fig. A-GBBAB Sheet 01, View B, remove the lockwire from theElectrical Connector at FIN 3854VCA.

2 As shown in Fig. A-GBBAB Sheet 01, View B, remove from the electricalconnector at FIN 3854VCA, refer to ESPM 20-44-16:




3 As shown in Fig. A-GBBAB Sheet 02, View C, the wiring diagram Fig. A-GWBAA Sheet 01 and the hook-up chart Fig. A-GHBAA Sheet 01, lines 1 thruto 6, connect the wires and install:



4 As shown in Fig. A-GBBAB Sheet 02, View C, cut to the necessary lengthand install on the wire at FIN 7702VB, refer to ESPM 20-33-30 and ESPM20-33-33:


with


5 As shown in Fig. A-GBBAB Sheet 02, View C, attach the Textile Sleeve, Item51, to the Open Backshell, Item (52), with:


05TKC1 As required



5



6 Secure the Connector, Item (53) and the Backshell, Item (52), with lockwire,use:


14QDB1 As required

7 As shown in Fig. A-GBBAB Sheet 02, View C, attach to the wire, refer toESPM 20-33-35:

1 Placard F9239026700100 Item 54

with:


**CONF 003



462 Access Panel 462CR, Panel 464BR, Panel 462CL,Panel 464BL

Manpower Resources



Skills ELECTRICAL



NOTES1 ABS0678B01 2 SUPPORT6 NSA5050-3 2 NUT10 ABS0679-01 1 BRACKET12 ASNA0032H067 1 CLAMP14 NSA5050-4C 6 NUT15 ASNA2553-0601 6 WASHER16 NSA5307-4C 6 WASHER17 NAS1801-3-8 2 SCREW36 NSA5415N32-15 3 RIVET41 F5493072120095 1 PLATE42 NAS1149F0332P 2 WASHER43 MS20995C20 1 (M) LOCK WIR

47 MS20995C32 1 (M) LOCK WIR

56 NSA8420-5 2 (M) TAPE (1)



5







04FMA5 As required


06AAC1 As required


06CMD9 As required


08BAA9 As required




Fig. A-FBCACModification of the feeder’s routing of theRH pylon

Sheet 01Sheet 02Sheet 03Sheet 04Sheet 05Sheet 06


Sheet 01



and



(b) Modify the feeder routing, refer to Fig. A-FBCAC Sheet 01, Fig. A-FBCAC Sheet02, Fig. A-FBCAC Sheet 03, Fig. A-FBCAC Sheet 04, Fig. A-FBCAC Sheet 05, Fig.A-FBCAC Sheet 06



Discard hardware.




5




(g) Remove:





(h) Remove:



Discard hardware.







08BAA9 As required



04FMA5 As required

(n) Install:

1 Plate F5493072120095 Item 41

with





5




06AAC1 As required


1 Bracket,Cable Support ABS0679-01 Item 10

with



2 Washer NAS1149F0332P Item 42

(p) On Bracket, Cable Support item 10, put in position:


(q) Thru Support-Cable item 1, install feeders and excitation wires as shown on figureFig. A-FBCAC Sheet 02, Fig. A-FBCAC Sheet 03, Fig. A-FBCAC Sheet 04, Fig. A-FBCAC Sheet 05 and Fig. A-FBCAC Sheet 06

(r) On Bracket, Cable Support item 10, affix Support-Cable item 1 with:










(v) Re-connect 3854VC.

(w) As shown on Fig. A-FBCAC Sheet 06, do an hanging knot as shown on view Pwith:





5




06CMD9 As required

(x) Remove blanking plugs on the disconnected line ends.



and





Manpower Resources



Skills ELECTRICAL





33 EN6049-007-19-5 2 (M) SLEEVE




5






06CMD9 As required



Fig. A-FBDACModification of the harness 500VB of theRH pylon



Sheet 01

(a) Modify harness 500VB, refer to Fig. A-FBDAC Sheet 01, Fig. A-FBDAC Sheet 02and Fig. A-FBDAC Sheet 03

(b) Disconnect:



Remove:











5








then






















5











06CMD9 As required





removal


removal

Connect:


removal


removal




with




5






1 Plate F9241063620000 Item 31

with







with








with







5






Manpower Resources



Skills ELECTRICAL



NOTES51 EN6049-007-08-5 2 (M) SLEEVE

54 F9239026700100 1 PLCRDSET




05TKC1 As required


14QDB1 As required





Fig. A-GBBAAModification to the Wire Insulation in theRight Wing Pylon

Sheet 01Sheet 02


Sheet 01


Sheet 01


1 As shown in Fig. A-GBBAA Sheet 01, View B, remove the lockwire from theElectrical Connector at FIN 3854VCA.



5



2 As shown in Fig. A-GBBAA Sheet 01, View B, remove from the electricalconnector at FIN 3854VCA, refer to ESPM 20-44-16:



3 As shown in Fig. A-GBBAA Sheet 01, View B, remove from the wire at FIN7702VB:


4 As shown in Fig. A-GBBAA Sheet 02, View C, the wiring diagram Fig. A-GWBAA Sheet 01 and the hook-up chart Fig. A-GHBAA Sheet 01 lines 1 thruto 6, connect the wires and install:



5 As shown in Fig. A-GBBAA Sheet 02, View C, cut to the necessary lengthand install on the wire at FIN 7702VB, refer to ESPM 20-33-30 and ESPM20-33-33:


6 As shown in Fig. A-GBBAA Sheet 02, View C, attach the Textile Sleeve, Item51, to the Open Backshell, Item (52), with:


05TKC1 As required



14QDB1 As required

8 As shown in Fig. A-GBBAA Sheet 02, View C, attach to the wire, refer toESPM 20-33-35:

1 Placard F9239026700100 Item 54

with:




5



**CONF ALL

D. TEST

**CONF 001

(1) Subtask 923130-730-001-001 - System


210 Access Door 831

Manpower Resources

Skills ELECTRICAL




(a) Job Set-Up










5



(b) Procedure

1 Test of the equipment (FINS 9HA2 and 8HA2)







**CONF 002

(1) Subtask 923130-730-001-002 - System


210 Access Door 831

Manpower Resources

Skills ELECTRICAL




(a) Job Set-Up




5









(b) Procedure








**CONF 003

(1) Subtask 923130-730-001-003 - System


210 Access Door 831



5



Manpower Resources

Skills ELECTRICAL




(a) Job Set-Up








(b) Procedure






5







**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 923130-942-001-001 - Close-up


463462

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-802Task 36-11-16-400-802Task 36-11-42-400-802








5



**CONF 002

(1) Subtask 923130-942-001-002 - Close-up


463462

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-803Task 36-11-16-400-803Task 36-11-42-400-803






**CONF 003

(1) Subtask 923130-942-001-003 - Close-up


463462

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-804Task 36-11-16-400-804Task 36-11-42-400-804




5









5






5



Task 923130-831-804-001 - Modification of the Clamp and Sleeve of Harness 501VB in theLH Pylon - ADDITIONAL WORK

**CONF ALL



- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., ASNECESSARY ON WIRING AND COMPONENTS.



IF THERE CONTAMINATION, REFER TO ESPM 20-55-00.









5




**CONF 001

Zone453

Modified FIN8HA1A 9HA1A

Manpower


**CONF 002

Zone453


Manpower


**CONF 003

Zone453


Manpower


**CONF ALL

A. GENERAL

**CONF 001


Manpower Resources

Skills NON SPECIFIC


06-31-54, Page Block 00106-41-53, Page Block 001Task 20-21-11-911-801




5




20-33-3020-33-3320-33-4220-33-4420-56-51

Structural Repair Manual (SRM) 51-42-00

(a) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(b) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(c) For the identification of pylon stations and ribs, refer to AMM 06-31-54, Page Block001.

(d) For the installation of conduits, refer to ESPM 20-33-33.

(e) For the installation of conduit protection, refer to ESPM 20-33-30.

(f) For the specification of materials (Mat. No.) given in this Service Bulletin, refer tothe Consumable Materials List (CML).

(g) To torque tighten the standard threaded fasteners, refer to AMM Task20-21-11-911-801.

(h) Remove and install fasteners in accordance with SRM 51-42-00.

(i) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM20-56-51.

(j) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(k) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(l) Put all the retained hardware in identified plastic bags and attach the bags to therelated unit.


Manpower Resources

Skills NON SPECIFIC


**CONF 002


Manpower Resources

Skills NON SPECIFIC



5






Elec. Std. Practices Manual (ESPM) 20-33-0020-33-3020-33-3320-33-4220-33-4420-56-51















Manpower Resources

Skills NON SPECIFIC




5



**CONF 003


Manpower Resources

Skills NON SPECIFIC




















5




Manpower Resources

Skills NON SPECIFIC


**CONF ALL

B. PREPARATION

**CONF 001



453

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802Task 36-11-15-000-802Task 36-11-16-000-802Task 36-11-16-400-802Task 36-11-42-400-802



- Engine shut down, thrust reversers closed and locked










5




(b) Do the job set-up procedure as specified in the Removal of the Bleed RegulatedPressure Transducer (FIN 8HA1), refer to AMM Task 36-11-16-000-802.

(c) Do the job set-up procedure as specified in the Removal of the Bleed TransferredPressure-Transducer (FIN 9HA1), refer to AMM Task 36-11-15-000-802.

(d) If necessary, remove the access panels 454BL, 452CL, 454BR, 452CR, 453BL,453BR, refer to AMM 05-24-50, Page Block 601.

**CONF 002



453

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802Task 36-11-15-000-802Task 36-11-16-000-802











(a) Make sure that the aircraft is electrically grounded, refer to .



5






**CONF 003



453

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802Task 36-11-15-000-802Task 36-11-16-000-802















5





**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 923130-831-007-001 - Modify the Clamp and Sleeve of Harness 501VB inthe LH Pylon


453

Manpower Resources



Skills ELECTRICAL




33 EN6049-007-19-5 2 (M) SLEEVE


Component COMPA01


13 NSA8420-7 5 (M) TAPE






06CMD9 As required



5




20-33-42Fig. A-FCAAAModification of the clamp and sleeve ofharness 501VB in the LH pylon -ADDITIONAL WORK

Sheet 01

NOTE: Check the installation done.

If the installation is not compliant with this SB revision, re-install inaccordance with the instructions belows:

(a) Modify the clamp and the sleeve of the harness 501VB in the LH Pylon, refer toFig. A-FCAAA Sheet 01.

(b) On view C, remove:


1 Screw Item (17) Retain

1 Washer Item (19) Retain

(c) On view D, remove:

1 Clamp Item (26) Retain



(d) On view B, remove:

Cord-Fiber Glass Item (13) Discard

Textile Sleeve Item (33) Discard

(e) On view B, install between clamps and connectors 8HA1A and 9HA1A:




(f) Attach sleeves item 33 with:





5




06CMD9 As required

(g) On view C, install:



with

1 Washer Item (19) Retained atremoval

1 Screw Item (17) Retained atremoval


(h) On view D, install:

1 Clamp Item (26) Retained atremoval



**CONF 002



453

Manpower Resources



Skills ELECTRICAL



5






33 EN6049-007-19-5 2 (M) SLEEVE


Component COMPA01


13 NSA8420-7 5 (M) TAPE






06CMD9 As required



Sheet 01










5


















06CMD9 As required




with






5







**CONF 003



453

Manpower Resources



Skills ELECTRICAL




33 EN6049-007-19-5 2 (M) SLEEVE


Component COMPA01


13 NSA8420-7 5 (M) TAPE






06CMD9 As required



5





Sheet 01
























5




06CMD9 As required




with








**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None



5



**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 923130-942-004-001 - Close-up


453

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-802Task 36-11-16-400-802

(a) If removed, close the access panels 454BL, 452CL, 454BR, 452CR, 453BL,453BR, refer to AMM 05-24-50, Page Block 601.

(b) Do the Close-up procedure as specified in the Installation of the Bleed RegulatedPressure Transducer (FIN 8HA1), refer to AMM Task 36-11-16-400-802.

(c) Do the Close-up procedure as specified in the Installation of the Bleed TransferredPressure Transducer (FIN 9HA1), refer to AMM Task 36-11-15-400-802.

(d) Put the aircraft back to its initial configuration.

**CONF 002

(1) Subtask 923130-942-004-002 - Close-up


453

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-803Task 36-11-16-400-803





5





**CONF 003

(1) Subtask 923130-942-004-003 - Close-up


453

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-804Task 36-11-16-400-804







5



Task 923130-831-803-001 - Modification of the Clamp and Sleeve of Harness 500VB in theRH Pylon - ADDITIONAL WORK

**CONF ALL


CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEPELECTRICAL WIRING IN A SATIFACTORY CONDITION (ELECTRICALLYAND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCEWORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DOTHIS:




IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.









5




**CONF 001

Zone463


Manpower


**CONF 002

Zone463


Manpower


**CONF 003

Zone463


Manpower


**CONF ALL

A. GENERAL

**CONF 001


Manpower Resources

Skills NON SPECIFIC






5




20-33-3020-33-3320-33-4220-33-4420-56-51















Manpower Resources

Skills NON SPECIFIC


**CONF 002


Manpower Resources

Skills NON SPECIFIC



5





















Manpower Resources

Skills NON SPECIFIC




5



**CONF 003


Manpower Resources

Skills NON SPECIFIC




















5




Manpower Resources

Skills NON SPECIFIC


**CONF ALL

B. PREPARATION

**CONF 001



463

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802Task 36-11-15-000-802Task 36-11-16-000-802














5



(b) Do the Job Set-up procedure as specified in the removal of Bleed RegulatedPressure Transducer (FIN 8HA2), refer to AMM Task 36-11-16-000-802.

(c) Do the Job Set-up procedure as specified in the removal of Bleed TransferredPressure Transducer (FIN 9HA2), refer to AMM Task 36-11-15-000-802.


**CONF 002



463

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802Task 36-11-15-000-804Task 36-11-16-000-804















5





**CONF 003



463

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802Task 36-11-15-000-804Task 36-11-16-000-804
















5




**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 923130-831-006-001 - Modify the Clamp and Sleeve of Harness 500VB inthe RH Pylon


463

Manpower Resources



Skills ELECTRICAL




33 EN6049-007-19-5 2 (M) SLEEVE


Component COMPA01


13 NSA8420-7 5 (M) TAPE






06CMD9 As required


20-33-42



5



ReferencesFig. A-FCCAAModification of the clamp and sleeve ofharness 500VB in the RH pylon -ADDITIONAL WORK

Sheet 01



(a) Modify the clamp and the sleeve of the harness 500VB in the RH Pylon, refer to,Fig. A-FCCAA Sheet 01.





















5




06CMD9 As required




with








**CONF 002



463

Manpower Resources



Skills NON SPECIFIC



5






33 EN6049-007-19-5 2 (M) SLEEVE


Component COMPA01


13 NSA8420-7 5 (M) TAPE






06CMD9 As required


20-33-42Fig. A-FCCAAModification of the clamp and sleeve ofharness 500VB in the RH pylon -ADDITIONAL WORK

Sheet 01










5


















06CMD9 As required




with






5







**CONF 003



463

Manpower Resources



Skills NON SPECIFIC




33 EN6049-007-19-5 2 (M) SLEEVE


Component COMPA01


13 NSA8420-7 5 (M) TAPE






06CMD9 As required



5




20-33-42Fig. A-FCCAAModification of the clamp and sleeve ofharness 500VB in the RH pylon -ADDITIONAL WORK

Sheet 01
























5




06CMD9 As required




with








**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None



5



**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 923130-942-005-001 - Close-up


463

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-802Task 36-11-16-400-802





**CONF 002

(1) Subtask 923130-942-005-002 - Close-up


463

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-803Task 36-11-16-400-803





5





**CONF 003

(1) Subtask 923130-942-005-003 - Close-up


463

Manpower Resources

Skills NON SPECIFIC


Task 36-11-15-400-804Task 36-11-16-400-804







5



Task 923130-831-806-001 - Modification of the Hanging Knot on the LH Pylon - ADDITIONALWORK

**CONF ALL






IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.









5




**CONF 001

Zone452

Modified FIN454BL 454BR 452CL 452CR

AccessPanel 452CL 452CR 454BL 454BR

Manpower


**CONF 002

Zone452



Manpower


**CONF 003

Zone452



Manpower


**CONF ALL

A. GENERAL

**CONF 001


Manpower Resources

Skills NON SPECIFIC



5




06-31-53, Page Block 00106-31-54, Page Block 001




(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.


(d) For the specification of materials (Mat. No.) given in this Service Bulletin, refer toConsumable Material List (CML).

(e) For hanging knots installation, refer to ESPM 20-33-44.


Manpower Resources

Skills NON SPECIFIC


**CONF 002


Manpower Resources

Skills NON SPECIFIC












5




Manpower Resources

Skills NON SPECIFIC


**CONF 003


Manpower Resources

Skills NON SPECIFIC











Manpower Resources

Skills NON SPECIFIC




5



**CONF ALL

B. PREPARATION

**CONF 001



452

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802

NOTE: For the basic Aircraft configuration, refer to AMM Chapter "Introduction -Aircraft status for maintenance" in Manual Front Matter section.


(b) If necessary, remove the access panels 454BL, 452CL, 454BR, 452CR, refer toAMM 05-24-50, Page Block 601.

**CONF 002



452

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802






5



**CONF 003



452

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802




**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 923130-831-011-001 - Modify the Hanging Knot on LH Pylon



Manpower Resources



Skills NON SPECIFIC




56 NSA8420-5 2 (M) TAPE (1)



5







06CMD9 As required


Fig. A-FBGAAModification of the Hanging Knot-ADDITIONAL WORK

Sheet 01Sheet 02

(a) Modify Hanging knot on the feeder routing:

Refer to Fig. A-FBGAA

1 Remove:

2 (M) Lacing Tape NSA8420-7 Item (13) Discard

2 Install:



3 Safety the knot with:


06CMD9 As required

**CONF 002




Manpower Resources



Skills NON SPECIFIC



5






56 NSA8420-5 2 (M) TAPE (1)





06CMD9 As required


Fig. A-FBGAAModification of the Hanging Knot-ADDITIONAL WORK

Sheet 01Sheet 02


Refer to Fig. A-FBGAA

1 Remove:


2 Install:





06CMD9 As required

**CONF 003



452 Access Panel 452CR, Panel 452CL, Panel 454BR,Panel 454BL



5



Manpower Resources



Skills NON SPECIFIC




56 NSA8420-5 2 (M) TAPE (1)





06CMD9 As required


Fig. A-FBGABModification of the Hanging Knot-ADDITIONAL WORK

Sheet 01Sheet 02


Refer to Fig. A-FBGAB

1 Remove:


2 Install:





06CMD9 As required



5



**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 923130-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC


(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.

(b) If removed, close the access panels 454BL, 452CL, 454BR, 452CR, refer to AMM05-24-50, Page Block 601.

(c) Put the aircraft back to its initial configuration.

**CONF 002

(1) Subtask 923130-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC






5




**CONF 003

(1) Subtask 923130-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC







5






5



Task 923130-831-805-001 - Modification of the Hanging Knot on the RH Pylon - ADDITIONALWORK

**CONF ALL






IF THERE IS CONTAMINATION, REFER TOESPM 20-55-00.









5




**CONF 001

Zone462



Manpower


**CONF 002

Zone462



Manpower


**CONF 003

Zone462



Manpower


**CONF ALL

A. GENERAL

**CONF 001


Manpower Resources

Skills NON SPECIFIC



5




06-31-54, Page Block 001









Manpower Resources

Skills NON SPECIFIC


**CONF 002


Manpower Resources

Skills NON SPECIFIC


06-31-54, Page Block 001










5




Manpower Resources

Skills NON SPECIFIC


**CONF 003


Manpower Resources

Skills NON SPECIFIC


06-31-54, Page Block 001









Manpower Resources

Skills NON SPECIFIC


**CONF ALL

B. PREPARATION

**CONF 001



462



5



Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802




**CONF 002



462

Manpower Resources

Skills NON SPECIFIC


Task 12-34-24-860-802




**CONF 003



462

Manpower Resources

Skills NON SPECIFIC



5




Task 12-34-24-860-802




**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 923130-831-010-001 - Modify Hanging Knot on RH Pylon



Manpower Resources



Skills NON SPECIFIC




56 NSA8420-5 2 (M) TAPE (1)





06CMD9 As required



5




Fig. A-FBHAAModification of the Hanging Knot-ADDITIONAL WORK

Sheet 01Sheet 02


Refer to Fig. A-FBHAA

1 Remove:


2 Install:





06CMD9 As required

**CONF 002




Manpower Resources



Skills NON SPECIFIC




56 NSA8420-5 2 (M) TAPE (1)




5






06CMD9 As required


Fig. A-FBHAAModification of the Hanging Knot-ADDITIONAL WORK

Sheet 01Sheet 02


Refer to Fig. A-FBHAA

1 Remove:


2 Install:





06CMD9 As required

**CONF 003




Manpower Resources



Skills NON SPECIFIC



5






56 NSA8420-5 2 (M) TAPE (1)





06CMD9 As required


Fig. A-FBHABModification of the Hanging Knot-ADDITIONAL WORK

Sheet 01Sheet 02


Refer to Fig. A-FBHAB

1 Remove:


2 Install:





06CMD9 As required

**CONF ALL

D. TEST

**CONF 001

None



5



**CONF 002

None

**CONF 003

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 923130-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC





**CONF 002

(1) Subtask 923130-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC







5



**CONF 003

(1) Subtask 923130-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC







5



**CONF ALL

Z453

A

RIB11RIB8

Z463

BFWD

A

B

(50) (51)(51)

G_SB_923130_5_BEAA_01_00

Figure A-FBEAA - Sheet 01Removal/Installation of the duct



5



**CONF 001

B

A

A

Z453RIB8A

RIB13A

D

C

BEFORE

B

E

F

G_SB_923130_5_BAAA_01_01

Figure A-FBAAA - Sheet 01Modification of the feeder’s routing of the LH pylon



5



**CONF 001

(12)

(1)

(4)

VIEW LOOKING FWD

PYLON CL

(2)

(44) x7

(4)

C D

AFTER

A

A

A

A

A

A

A

A

A

A

A

A

J

G

M

KN

P

E

F

(3)

G_SB_923130_5_BAAA_02_05




5



**CONF 001

H

NOTE:UNLESS OTHERWISE SPECIFIED ENSURE 25 mm (0.984 in) MIN BETWEEN FEEDERS AND STRUCTURE.

3855VT

10

141516

A A

4

6

1 x211

7

PYLON CL

VIEW LOOKING FWD

412

43

36

G

H J

3855VC

F

G_SB_923130_5_BAAA_03_04




5



**CONF 001

d = 25.00 mm~(0.984 in)

G ROUTE

E ROUTE

G ROUTE

d

01

02

L

56

FEEDER CABLES IN THE SAME ROUTE THAT GO IN DIFFERENT (NON PARALLEL) DIRECTIONS MUSTNOT DIRECTLY TOUCH. A MINIMUN DISTANCE OF 5.00 mm (0.197 in) IS NECESSARY. THE MINIMUMDISTANCE "d" THAT YOU CAN GET WITH LACING TAPE IS 10.00 mm (0.394 in).

NOTE:01

THIS DETAIL IS PROVIDED FOR CLARIFICATION PURPOSE OF THE SEPERATOR KNOT. IN THE REALCONFIGURATION OF THE AIRCRAFT, THE EXCITATION ROUTE IS PROTECTED BY A SLEEVE.

02

THE EXCITER CABLE DOES NOT GO THRU THE ROUNDED SUPPORT.03

K 03

5025

5026

502450295027

EXCITER CABLE

5028

L

G_SB_923130_5_BAAA_04_07




5



**CONF 001

6

37

38

6

7

5

75

6

38

37

NEW ROUTING

VIEW LOOKING FWD

M

N P

N

P

G_SB_923130_5_BAAA_05_00




5



**CONF 002

B

A

A

Z453RIB8A

RIB13A

D

C

BEFORE

B

E

F

G_SB_923130_5_BAAB_01_01

Figure A-FBAAB - Sheet 01Modification of the feeder’s routing of the LH pylon



5



**CONF 002

(12)

(1)

(4)

VIEW LOOKING FWD

PYLON CL

(2)

(44) x7

(4)

C D

AFTER

A

A

A

A

A

A

A

A

A

A

A

AP

NK

M

G

J

E

F

(3)

G_SB_923130_5_BAAB_02_05




5



**CONF 002

H

NOTE:UNLESS OTHERWISE SPECIFIED ENSURE 25 mm (0.984 in) MIN BETWEEN FEEDERS AND STRUCTURE.

3855VT

10

141516

A A

4

6

1 x211

7

PYLON CL

VIEW LOOKING FWD

412

43

36

G

H J

3855VC

F

G_SB_923130_5_BAAB_03_04




5



**CONF 002


NOTE:01


02

d = 25.00 mm~(0.984 in)

G ROUTE

E ROUTE

G ROUTE

d

01

02

L

56


5025

5026

502450295027

EXCITER CABLE

5028

K 03

L

G_SB_923130_5_BAAB_04_08




5



**CONF 002

6

37

38

6

7

5

75

6

38

37

NEW ROUTING

VIEW LOOKING FWD

M

N P

N

P

G_SB_923130_5_BAAB_05_00




5



**CONF 003

E

BEFORE

B

C

D

Z453

A

A

RIB8A

RIB13A

B

G

F

G_SB_923130_5_BAAC_01_01

Figure A-FBAAC - Sheet 01Modification of the feeder’s routing of the LH pylon



5



**CONF 003

(40)

(2)

PYLON CL

45°

3855VC

(12)

(1)

(44) x7

PYLON CL(40)

VIEW LOOKING FWD

VIEW LOOKING FWD

(3)

C

D

E

G_SB_923130_5_BAAC_02_04




5



**CONF 003

N

H

G

J

L

F

4036

VIEW LOOKING FWD

PYLON CL

AFTER

H

3855VC

G

M

G_SB_923130_5_BAAC_03_02




5



**CONF 003

K

10

40

17

6

19

J

1x2

K

43

12

56

A

A

A

A

A

A

A

A

AA

AA

54

52

50

55

53

51

L

FWD

G_SB_923130_5_BAAC_04_06




5



**CONF 003

FWD

M

61719

5

PYLON CL

45°

VIEW LOOKING FWD

3855VC

N

5025

5026

5024

5029

5027

5028

EXCITER CABLE

P

G_SB_923130_5_BAAC_05_04




5



**CONF 003


NOTE:01


02

14

1516

3855VT

A A

d = 25.00 mm~(0.984 in)

G ROUTE

E ROUTE

G ROUTE

d

01

02

P

56

G_SB_923130_5_BAAC_06_02




5



**CONF 001

B

Z463

A

A

RIB13ARIB8A

(5)

(35)

C

F

E

D

BEFORE

B

C

G

G_SB_923130_5_BCAA_01_02

Figure A-FBCAA - Sheet 01Modification of the feeder’s routing of the RH pylon



5



**CONF 001

(1)(3)

(34)

(34)

PYLON CL

VIEW LOOKING FWD

(12)(44) x7

(35)D EAFTER

F

J

G

K

H

A

A

A

A

A

A

A

A

A

A

A

A

M

G_SB_923130_5_BCAA_02_05




5



**CONF 001

34

10

6

35

x2

36

PYLON CL

VIEW LOOKING FWD

11

7

1

6

538

37

6 34

35 36

H

J

K

L

3854VC

G

G_SB_923130_5_BCAA_03_04




5



**CONF 001

14

1516

A A

3854VT

12

43

L

G_SB_923130_5_BCAA_04_03




5



**CONF 001

G ROUTE

E ROUTE

G ROUTE

d = 25.00 mm~(0.984 in)

01

02

56

M

N


NOTE:01


02

5044

EXCITER CABLE

5045

50425047

5043

5046

N

d

FWD

G_SB_923130_5_BCAA_05_03




5



**CONF 002

E

D

B

Z463

A

A

RIB13ARIB8A

BEFORE

B

C

(5)

(35)

C

G

F

G_SB_923130_5_BCAB_01_02

Figure A-FBCAB - Sheet 01Modification of the feeder’s routing of the RH pylon



5



**CONF 002

(1)

(34)

(34)

PYLON CL

VIEW LOOKING FWD

(12)(44) x7

(35)

(3)

D E

J

G

K

AFTER

H

F

A

A

A

A

A

A

A

A

A

A

A

A

M

G_SB_923130_5_BCAB_02_05




5



**CONF 002

L

34

10

6

35

x2

36

PYLON CL

VIEW LOOKING FWD

11

7

1

6

538

37

6 34

35 36

H

J

K

3854VC

G

G_SB_923130_5_BCAB_03_04




5



**CONF 002

14

1516

A A

3854VT

12

43

L

G_SB_923130_5_BCAB_04_02




5



**CONF 002

G ROUTE

E ROUTE

G ROUTE

d = 25.00 mm~(0.984 in)

d

01

02

56

N

M


NOTE:01


02

FWD

5044

EXCITER CABLE

5045

50425047

5043

5046

N

G_SB_923130_5_BCAB_05_03




5



**CONF 003

C

F

D

B E

Z463

A

A

RIB13ARIB8A

BEFORE

B

G_SB_923130_5_BCAC_01_02

Figure A-FBCAC - Sheet 01Modification of the feeder’s routing of the RH pylon



5



**CONF 003

H

G

(1)

(41)

VIEW LOOKING FWD

(41)

PYLON CL(12)

(44) x7

(3)

C D

AFTER

F

E

G_SB_923130_5_BCAC_02_04




5



**CONF 003

A

AA

AA

AAAA

AAA

56

56

G

83

81

79

84

82

80

VIEW LOOKING FWD

FWD

PYLON CL

3854VC 41

36

F

H

J

K

N

G_SB_923130_5_BCAC_03_04




5



**CONF 003

PYLON CL

45°

UNLESS OTHERWISE SPECIFIED ENSURE 25 mm (0.984 in) MIN BETWEEN FEEDERS AND STRUCTURE.NOTE:

3854VC

4110

x217

42

1

6

J

KL

G_SB_923130_5_BCAC_04_06




5



**CONF 003

3854VC

56

43 12

L

M

M

G_SB_923130_5_BCAC_05_06




5



**CONF 003

3854VT

14

1516

A A


NOTE:01


02

d = 25.00 mm~(0.984 in)

G ROUTE

E ROUTE

G ROUTE

d

01

02

56N

P

EXCITER CABLE

50425047

5043

5046

5044

5045

P

FWD

G_SB_923130_5_BCAC_06_05




5



**CONF 001

(17)

(18)

(19)(20)

A

A

Z453

F

(32)

(32)

B

C

RIB11RIB8

BEFORE

ROUTE S

ROUTE M

G

E

D C

B H

9HA1

8HA1

G_SB_923130_5_BBAA_01_04

Figure A-FBBAA - Sheet 01Modification of the harness 501VB of the LH pylon



5



**CONF 001

(17)

(18)

(19)

(18)

(26)

(26)

(19)

(29)

(27)

(27)

(18)

(23)(25)

(22)

(22)

(26)

(26)

(19)

(19)

(28)

(31)

D

E

G

(18)

(19)

(30)

(27)

(20)

F

(18)

(17)

(19)

G_SB_923130_5_BBAA_02_02




5



**CONF 001

L A

A

AFTER

H

MJ L

ROUTE S

ROUTE M 13

32

32

13

K

32 32

M S M S

B BA A

18

20

18

55

19

17

33

19

20

29

1818

27

19

30

17

1925

18

26

17

19

31

19

28

18

13

13

33

B

B

B

B

NOTE:ROUTES HAVE TO BE SEPARATED, MAKING THEIR PATH THRU TWO DIFFERENT CLAMPS.01

02

01

02

01 02

J

K

M

ROUTES HAVE TO BE GATHERED ON THE SAME SLEEVE, MAKING THEIR PATH THRU ONE CLAMP ONLY.

9HA1

8HA1

G_SB_923130_5_BBAA_03_07




5



**CONF 002

(17)

(18)

(19)(20)

A

Z453

F

(32)

(32)

B

C

BEFORE

ROUTE S

ROUTE M

A

RIB11RIB8

E

DC

9HA1

8HA1

B G

G_SB_923130_5_BBAB_01_04

Figure A-FBBAB - Sheet 01Modification of the harness 501VB of the LH pylon



5



**CONF 002

(18)

(26)

(26)

(19)

(29)

(27)

(27)

(18)

(23)(25)

(22)

(22)

(26)

(26)

(19)

(19)

(28)

(31)

D

E

(20)

F

(18)

(17)

(19)

G_SB_923130_5_BBAB_02_01




5



**CONF 002

A

A

AFTER

ROUTE S

ROUTE M 13

32

32

13

32 32

M S M S

B BA A

18

20

18

55

19

17

33

19

20

29

39

18

26

17

19

31

19

46

18

13

13

33

B

B

B

B01

02

01 02


02 ROUTES HAVE TO BE GATHERED ON THE SAME SLEEVE, MAKING THEIR PATH THRU ONE CLAMP ONLY.

G

H J K

H

J K

9HA1

8HA1

G_SB_923130_5_BBAB_03_07




5



**CONF 003

(17)

(18)

(19)(20)

A

Z453

F

(32)

(32)

B

C

BEFORE

ROUTE S

ROUTE M

E

DC

A

RIB11RIB8

9HA1

8HA1

B G

G_SB_923130_5_BBAC_01_04

Figure A-FBBAC - Sheet 01Modification of the harness 501VB of the LH pylon



5



**CONF 003

(18)

(26)

(26)

(19)

(29)

(27)

(27)

(22)

(26)

(26)

(19)

(19)

(28)

(31)

D

E

(19)

(28)

(18)

(20)

F

(18)

(17)

(19)

G_SB_923130_5_BBAC_02_01




5



**CONF 003

A

A

AFTER

ROUTE S

ROUTE M 13

32

32

13

32 32

M S M S

B BA A

18

20

18

55

19

17

33

19

20

29

18

2617

19

31

19

45

18

13

13

33

B

B

B

B01

02

01 02



G

H J K

H

J K

9HA1

8HA1

G_SB_923130_5_BBAC_03_07




5



**CONF 001

(17)

(18)

(19)(20)

F

(32)

(32)

B

C

BEFORE

Z463

A

RIB11 RIB8

ROUTE S

ROUTE M

A

B H

G

E

D C

8HA2

9HA2

G_SB_923130_5_BDAA_01_04

Figure A-FBDAA - Sheet 01Modification of the harness 500VB of the RH pylon



5



**CONF 001

(17)

(18)

(19)

(18)

(26)

(26)

(19)

(29)

(27)

(27)

(18)

(23)(25)

(22)

(22)

(26)

(26)

(19)

(19)

(28)

(31)

D

E

G

(18)

(19)

(30)

(27)

(20)

F

(18)

(17)

(19)

G_SB_923130_5_BDAA_02_02




5



**CONF 001

A

A

AFTER

H

MJ L

ROUTE S

ROUTE M 13

32

32

13

K

32 32

M S M S

B BA A

18

20

18

55

19

17

33

19

20

29

1818

27

19

30

17

1925

18

26

17

19

31

19

28

18

13

13

33

B

B

B

BK

M

J

L

01 02

01

02



8HA2

9HA2

G_SB_923130_5_BDAA_03_07




5



**CONF 002

(17)

(18)

(19)(20)

F

(32)

(32)

B

C

BEFORE

ROUTE S

ROUTE M

Z463

A

RIB11 RIB8

A

8HA2

9HA2

CE

D

B G

G_SB_923130_5_BDAB_01_04

Figure A-FBDAB - Sheet 01Modification of the harness 500VB of the RH pylon



5



**CONF 002

(18)

(26)

(26)

(19)

(29)

(27)

(27)

(18)

(23)(25)

(22)

(22)

(26)

(26)

(19)

(19)

(28)

(31)

D

E

(20)

F

(18)

(17)

(19)

G_SB_923130_5_BDAB_02_01




5



**CONF 002

A

A

AFTER

ROUTE S

ROUTE M 13

32

32

13

32 32

M S M S

B BA A

18

20

18

55

19

17

33

19

20

29

39

18

26

17

19

31

19

46

18

13

13

33

B

B

B

B01

02

01 02



G

H J K

8HA2

9HA2

H

J K

G_SB_923130_5_BDAB_03_07




5



**CONF 003

(17)

(18)

(19)(20)

F

(32)

(32)

B

C

BEFORE

ROUTE S

ROUTE M

Z463

A

RIB11 RIB8

A

8HA2

9HA2

E

D C

B G

G_SB_923130_5_BDAC_01_04

Figure A-FBDAC - Sheet 01Modification of the harness 500VB of the RH pylon



5



**CONF 003

(20)

(18)

(26)

(26)

(19)

(29)

(27)

(27)

E

F

(22)

(26)

(26)

(19)

(19)

(28)

(31)

D

(19)

(28)

(18)

(18)

(17)

(19)

G_SB_923130_5_BDAC_02_01




5



**CONF 003

A

A

AFTER

ROUTE S

ROUTE M 13

32

32

13

32 32

M S M S

B BA A

18

20

18

55

19

17

33

19

20

29

18

2617

19

31

19

45

18

13

13

33

B

B

B

B01

02

01 02



8HA2

9HA2

G

H J K

H

J K

G_SB_923130_5_BDAC_03_07




5



**CONF ALL

0° ANGLE REFERENCEAND CONNECTOR AXIS

CONNECTOR MASTER KEYWAY

ANGULAR = IN CLOCKWISE DIRECTION

BACKSHELL ANGLE

BACKSHELL

FROM 0° TO 360°

45°

A A

A A

G_SB_923130_5_BFAA_01_01

Figure A-FBFAA - Sheet 01Orientation of the backshells 8HA1A1, 9HA1A1, 8HA2A1, 9HA2A1



5



**CONF ALL

C

ROUTE S

ROUTE M

55

(19)

(17)

(26)

(19)

(28)

(13)

339HA1

8HA1

A

Z453RIB11RIB8

B

(20)

C D

D

(33)

B

A

13

G_SB_923130_5_CAAA_01_01

Figure A-FCAAA - Sheet 01Modification of the clamp and sleeve of harness 501VB in the LH pylon - ADDITIONAL WORK



5



**CONF ALL

CD

ROUTE S

ROUTE M (13)

33

8HA2

9HA2

(26)

(19)

(28)

D

55

(19)

(17)

(20)

C

(33)

Z463

A

RIB11 RIB8

A

B

B

13

G_SB_923130_5_CCAA_01_01

Figure A-FCCAA - Sheet 01Modification of the clamp and sleeve of harness 500VB in the RH pylon - ADDITIONAL WORK



5



**CONF 001 thru 002

C

B

B

Z453

A

A

RIB8A

RIB13A

G_SB_923130_5_BGAA_01_00

Figure A-FBGAA - Sheet 01Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 001 thru 002

FEEDER CABLES IN THE SAME ROUTE THAT GO IN DIFFERENT (NON PARALLEL) DIRECTIONS MUSTNOT DIRECTLY TOUCH. A MINIMUN DISTANCE OF 5 mm (0.197 in) IS NECESSARY. THE MINIMUMDISTANCE "d" THAT YOU CAN GET WITH LACING TAPE IS 10 mm (0.394 in).

NOTE:01


02

d = 25 mm~(0.984 in)

G ROUTE

E ROUTE

G ROUTE

d

01

02

(13)


5025

5026

502450295027

EXCITER 5028

03

D

C

56

FWD

VIEW LOOKING DOWN

TYPICAL VIEW

D

CABLE

G_SB_923130_5_BGAA_02_00

Figure A-FBGAA - Sheet 02Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 003

C

Z453

A

RIB8A

RIB13A

B

B

A

G_SB_923130_5_BGAB_01_00

Figure A-FBGAB - Sheet 01Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 003

FWD

5025

5026

5024

5029

5027

5028

EXCITER CABLE


NOTE:01


02

C

d = 25 mm~(0.984 in)

G ROUTE

E ROUTE

G ROUTE

d

01

02

(13)56

D

D

VIEW LOOKING DOWN

TYPICAL VIEW

G_SB_923130_5_BGAB_02_00

Figure A-FBGAB - Sheet 02Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 001 thru 002

C

B

A

RIB13ARIB8A

BZ463 A

G_SB_923130_5_BHAA_01_00

Figure A-FBHAA - Sheet 01Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 001 thru 002

G ROUTE

E ROUTE

G ROUTE

d = 25 mm~(0.984 in)

d

01

02

(13)


NOTE:01


02

FWD

5044

EXCITER CABLE

5045

50425047

5043

5046

56

D

C

D

VIEW LOOKING DOWN

TYPICAL VIEW

G_SB_923130_5_BHAA_02_00

Figure A-FBHAA - Sheet 02Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 003

C

Z463 A

B

A

RIB13ARIB8A

B

G_SB_923130_5_BHAB_01_00

Figure A-FBHAB - Sheet 01Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 003

D

83

81

79

84

82

80

FWD

EXCITER CABLE

50425047

5043

5046

5044

5045

FWD


NOTE:01


02

d = 25 mm~(0.984 in)

G ROUTE

E ROUTE

G ROUTE

d

01

02

(13)56

E

D

C

E

VIEW LOOKING DOWN

TYPICAL VIEW

G_SB_923130_5_BHAB_02_00

Figure A-FBHAB - Sheet 02Modification of the Hanging Knot- ADDITIONAL WORK



5



**CONF 003

BEFORE

RIB8A

RIB13A

A

B

A

Z452

B C

REMOVE THE LOCKWIRE.NOTE:01

(52)

01

(53) −A3855VC

7701VB (51)

G_SB_923130_6_BAAA_01_04

Figure A-GBAAA - Sheet 01Modification to the Wire Insulation in the Left Wing Pylon



5



**CONF 003

AFTER

54

C

SB 92−3130

03

04

(52)

REPLACE THE CONDUIT BY TEXTILE SLEEVE, REFER TO ESPM 20−33−33.NOTE:02

SAFETY WITH LOCKWIRE.03

ATTACH TEXTILE SLEEVE AND LABELS WITH LACING TAPE AS REQUIRED,04REFER TO ESPM 20−33−35.

(53) −A3855VC

5102 7701VB

D

G_SB_923130_6_BAAA_02_08




5



**CONF 003

INSTALL THE TEXTILE SLEEVE STARTING FROM 160 mm (6.2 in) FROMNOTE:05

160 mm(6.2 in)

AREA WITHOUT SLEEVE

LAST WING FIXINGPOINT05

THE LAST WING FIXING POINT.

D

G_SB_923130_6_BAAA_03_00




5



**CONF 001 thru 002

BEFORE

RIB8A

RIB13A

A

B

A

Z452

B C

(52)


01

(53)−A3855VC

7701VB(51)

G_SB_923130_6_BAAB_01_04

Figure A-GBAAB - Sheet 01Modification to the Wire Insulation in the Left Wing Pylon



5



**CONF 001 thru 002

AFTER

54

C

SB 92−3130

03



(52)

ATTACH TEXTILE SLEEVE AND LABELS WITH LACING TAPE AS REQUIRED,04REFER TO ESPM 20−33−35.

REFER TO ESPM 20−33−30.TEXTILE SLEEVE MUST EXCEED 20 mm (0.787 in) OVER LAST WING FIXING POINT, 05

LAST WINGFIXING POINT

05

04

(53) −A3855VC

51 027701VB

20 mm(0.787 in)

G_SB_923130_6_BAAB_02_06

Figure A-GBAAB - Sheet 02Modification to the Wire Insulation in the Left Wing Pylon



5



**CONF 003

BEFORE

(51)

Z462

AB C

RIB8A

RIB13A

A

B

(52)


01(53)3854VC−A

7702VB

G_SB_923130_6_BBAA_01_04

Figure A-GBBAA - Sheet 01Modification to the Wire Insulation in the Right Wing Pylon



5



**CONF 003

CSB 92−3130 54

04

05


INSTALL THE TEXTILE SLEEVE STARTING FROM 160 mm (6.2 in) FROM THE LAST WING FIXING POINT.03


ATTACH LABELS WITH LACING TAPE AS REQUIRED, REFER TO ESPM 20−33−35.05

AFTER


03

(52)

AREA WITHOUTSLEEVE

(53)3854VC−A

51 027702VB

160 mm(6.2 in)

G_SB_923130_6_BBAA_02_09

Figure A-GBBAA - Sheet 02Modification to the Wire Insulation in the Right Wing Pylon



5



**CONF 001 thru 002

BEFORE

(51)

Z462

AB C

RIB8A

RIB13A

A

B


(52)

01

−A3854VC(53)

7702VB

G_SB_923130_6_BBAB_01_04

Figure A-GBBAB - Sheet 01Modification to the Wire Insulation in the Right Wing Pylon



5



**CONF 001 thru 002

AFTER

54

C

SB 92−3130


03

160 mm(6.2 in)


INSTALL THE TEXTILE SLEEVE STARTING FROM 160 mm (6.2 in) FROM THE LAST WING FIXING POINT.03


ATTACH LABELS WITH LACING TAPE AS REQUIRED, REFER TO ESPM 20−33−35.05

WITHOUTSLEEVE

AREA

(52)04

−A3854VC(53)51 027702VB

05

G_SB_923130_6_BBAB_02_07

Figure A-GBBAB - Sheet 02Modification to the Wire Insulation in the Right Wing Pylon



5



**CONF ALL

1 452 3855VC−A 1 EN2997R61610BN 2422−6010

LINEZONE OR

PANELELEC.IDENT

TERM. TERMINAL P/N WIREIDENT

INSTRUCTIONS

TERMINAL P/NELEC.IDENT

TERM.ZONE OR

PANEL

LENGTH

MM INCHGAUGEROUTECOL

2 2

3 3

4 4

5 5

6 6 2422−5035

7

8

9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

END 1 LEAD END 2

R

B

R

Y

B

452

452

452

452

452

3855VC−A

3855VC−A

3855VC−A

3855VC−A

3855VC−A

EN2997R61610BN

EN2997R61610BN

EN2997R61610BN

EN2997R61610BN

EN2997R61610BN

2422−6010

2422−6011

2422−6011

2422−6011

G_SB_923130_6_HAAA_01_00

Figure A-GHAAA - Sheet 01Hook-up Chart



5



**CONF ALL

1 462 3854VC−A 1 EN2997R61610BN 2422−6016

LINEZONE OR

PANELELEC.IDENT

TERM. TERMINAL P/N WIREIDENT

INSTRUCTIONS

TERMINAL P/NELEC.IDENT

TERM.ZONE OR

PANEL

LENGTH

MM INCHGAUGEROUTECOL

2 2

3 3

4 4

5 5

6 6 2422−5053

7

8

9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

END 1 LEAD END 2

R

B

R

Y

B

EN2997R61610BN

EN2997R61610BN

EN2997R61610BN

EN2997R61610BN

EN2997R61610BN

2422−6016

2422−6017

2422−6017

2422−6017

462

462

462

462

462

3854VC−A

3854VC−A

3854VC−A

3854VC−A

3854VC−A

G_SB_923130_6_HBAA_01_00

Figure A-GHBAA - Sheet 01Hook-up Chart



5



**CONF ALL

1

2

A

3

4

5

2422−6010

2422−6010

2422−6011

2422−6011

2422−6011

2422

−50

35

6

4523855VC

R

B

R

Y

BF.R.

W/P

F.R. − FOR REFERENCE

G_SB_923130_6_WAAA_01_00

Figure A-GWAAA - Sheet 01Wiring Diagram



5



**CONF ALL

1

2

A

3

4

5

2422−6016

2422−6016

2422−6017

2422−6017

2422−6017

2422

−50

53

6

4623854VC

R

B

R

Y

BF.R.

W/P

F.R. − FOR REFERENCE

G_SB_923130_6_WBAA_01_00

Figure A-GWBAA - Sheet 01Wiring Diagram



5




**CONF ALL

For an explanation of the man-hours and elapsed time, refer to the following Gantt Chart.



5




**CONF ALL

MH ET/S

TOTAL MANHOURSELAPSED TIME (ET)

13.509.50

STEPS

0

PER

SB ELAPSED TIME(HOURS)

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A330−92−3130

MH

ET/S:PER

MANHOURS

ELAPSED TIME PER STEPNUMBER OF PERSONS

THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.

NOTE:

::

1 2 3 4 5

01

02

01

02 IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.

6 7 8 9

GET ACCESS 2.00 2.00

MODIFY THE FEEDERS ROUTING 4.00 4.00

TEST 1.00 1.00

CLOSE−UP 2.00 2.00

1

1

1

1

LH PYLON

MODIFY THE HARNESS 501VB 4.00 4.001LH PYLON

MODIFY THE WIRE INSULATION IN 0.50 0.501THE LEFT WING PYLON

G_SB_923130_5_AAAA_01_04

Figure A-FAAAA - Sheet 01Gantt Chart for LH Pylon



5




**CONF ALL

MH ET/S

TOTAL MANHOURSELAPSED TIME (ET)

13.509.50

STEPS

0

PER

SB ELAPSED TIME(HOURS)

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A330−92−3130

MH

ET/S:PER

MANHOURS

ELAPSED TIME PER STEPNUMBER OF PERSONS

THIS CHART IS ONLY A PROPOSAL.OPERATORS MAY DETERMINE THAT ANOTHER WAYTO DO THE WORK IS MORE SUITABLE FOR THEM.

NOTE:

::

1 2 3 4 5

01

02

01

02 IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURSARE NOT REFLECTED IN THIS GANTT CHART.

6 7 8 9

GET ACCESS 2.00 2.00

MODIFY THE FEEDERS ROUTING 4.00 4.00

TEST 1.00 1.00

CLOSE−UP 2.00 2.00

1

1

1

1

RH PYLON

MODIFY THE HARNESS 500VB 4.00 4.001RH PYLON

MODIFY THE WIRE INSULATION IN 0.50 0.501THE RIGHT WING PYLON

G_SB_923130_5_ABAA_01_02

Figure A-FABAA - Sheet 01Gantt Chart for RH Pylon



5







5




**CONF ALL

For the retrofitted modifications after accomplishment of this Service Bulletin, refer to the next page.



5




**CONF ALL

"X" IS USED FOR THE RETROFITTED MODIFICATIONS AFTER ACCOMPLISHMENTNOTE:

OF THIS SERVICE BULLETIN.

203733S32670

MOD001

CONFIG002 003

203734S32434 X X

X

CONFIG CONFIG

G_SB_923130_5_ACAA_01_00

Figure A-FACAA - Sheet 01Retrofitted Modifications



5



Service Bulletin REPORTING



SB Reporting status

This Service Bulletin will only be incorporated into affected customized Maintenance and FlightOperations Products if it is duly reported to Airbus.

General information

The SB Reporting policy is published in ISI 00.00.00135. This document provides information regarding:the SB Reporting means and benefits, the update of customized Maintenance Products and customizedFlight Operations Products.

If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations Products" forfurther information on the update of affected Flight Operations Products.

SB Reporting procedure

Standard practice to report SB is to use the online reporting application on AirbusWorld.

Refer to ISI 00.00.00179:- For complete information on reporting means to Airbus. Question 2 "What are the standard

practices for SB reporting?"- If this SB requires previous or simultaneous accomplishment of other SBs, Question 3 "What about

the reporting of prerequisite Service Bulletin?"

NOTE: ISI 00.00.00179 covers all the frequently asked questions about SB Reporting. It is revised on aregular basis.



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QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported datathat you provide us will be used to analyse areas of difficulties and to take corrective action to furtherimprove the quality of our Service Bulletins.We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- Is this SB easy to understand ? Y / N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give ashort description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUSCUSTOMER SERVICES DIRECTORATE1 Rond Point Maurice Bellonte31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins ManagementFAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.



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