# @A330 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - ADAPT DUAL LOOP AFTER FIRST RETROFIT **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 58530D46962 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES The APU bleed leakdetection system detects any ambient overheat in the vicinity of the APU bleed air ducts. It is made of a single overheat detection loop which runs along the APU bleed air ducts in section 15/21 and section 16 thru 19.1. The SFAR88 requirements will induce MMEL restrictions on this system from 2009. This Service Bulletin details the installation of a second APU bleed leak detection loop (APU LOOP B) in parallel to the current APU loop (APU LOOP A) in section 15/21 and section 16 thru 19.1.The Service Bulletin No. A330-36-3032 ’Introduce Adapted Dual-Loop Overheat-Detection APU BleedAir-Duct ’was retrofitted on the first aircraft in May 2008. After a check of the overheat-detectionloop installation, some none compliances to ATA 36-22 installation requirements have been reported. This Service Bulletin provides design improvements to the Service Bulletin No. A330-36-3032 OHDS installation.The accomplishment of this Service Bulletin improves dual-loop overheat-detection of APU Bleed-AirDuct, in accordance to ATA 36-22 installation requirements. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO POTENTIAL AD NO A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 1 6

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# @A330 SERVICE BULLETIN SUMMARY EVALUATION TABLE STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational disruptions. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 363038A01R01 1 27,500.00 Sensing element Kit 363038A02R01 1 1,800.00 Bundle, Clamp, Hardware Kit 363038D01R01 1 280.00 Clamp, placards and tie-cables Kit 363038D10R01 1 55.00 Sleeves, screws, spacers and clamps Kit 363038D12R00 1 35.00 Sleeves, screw, spacer and clamps Kit 363038D14R00 1 2,870.00 Sleeves TOTAL 32,540.00 **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 363038A01R01 1 27,500.00 Sensing element Kit 363038A02R01 1 1,800.00 Bundle, Clamp, Hardware Kit 363038D01R01 1 280.00 Clamp, placards and tie-cables Kit 363038D11R01 1 65.00 Sleeves, screws, spacers and clamps Kit 363038D12R00 1 35.00 Sleeves, screw, spacer and clamps Kit 363038D14R00 1 2,870.00 Sleeves TOTAL 32,550.00 EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

AEA QAF QTR CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s):

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 2 6

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# @A330 SERVICE BULLETIN SUMMARY Service Bulletin No. A330-36-3032 Mod. No. 55198D46286 55961D46493 55962D46494 NOTE: The Service Bulletin No. A330-36-3032 introduces the adapted dual loop overheat leak detection of the APU bleed air duct. NOTE: The Mod. No. 55198D46286 introduces the adapted dual loop overheat leak detection of the APU bleed air duct. NOTE: The Mod. No. 55961D46493 introduces the modification of the dual loop overheat leak detection in section 19. NOTE: The Mod. No. 55962D46494 introduces the modification of the dual loop overheat detection (CFRP-bulkhead). REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER OIT SE999.0063/06 NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 363038-831-848-001: Modification TOTAL MANHOURS 166.00 ELAPSED TIME (HOURS) 88.25 **CONF 002 Task 363038-831-848-001: Modification TOTAL MANHOURS 166.50 ELAPSED TIME (HOURS) 88.25

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 3 6

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# @A330 SERVICE BULLETIN SUMMARY APPENDICES **CONF ALL Appendix 01: Elapsed Time Assumptions

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 4 6

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# @A330 SERVICE BULLETIN SUMMARY
**CONF ALL


### B
**A** Z310 Z170 Z160 Z150
Z140 Z130 Z120 FR56

FR39.2 FR39.1 FR37

FR19

FR56 FR65 FR72 FR80 FR95

/82

FR95

800VU 

## A

**B** ADAPTATION OF THE DUAL LOOP OVERHEAT LEAK DETECTION AFTER FIRST RETROFIT INSTALLATION

G_SB_363038_6_SAAA_01_00 ADAPTATION OF THE DUAL LOOP OVERHEAT LEAK DETECTION AFTER FIRST RETROFIT INSTALLATION

Figure A-GSAAA - Sheet 01
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 5 6

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# @A330 SERVICE BULLETIN SUMMARY

This Page Intentionally Left Blank

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# @A330 SERVICE BULLETIN AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - ADAPT DUAL LOOP AFTER FIRST RETROFIT MODIFICATION No.: 58530D46962 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY This modification is applicable by Service Bulletin only. (1) Models 330-202 330-243 (2) Effectivity by MSN 0473 0489 0551 0597 0605 (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN AEA 0551 0597 QAF 0605 QTR 0473 0489

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 1 6

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# @A330 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0473 0489 0551 0597 001 0605 002 (5) Configuration definition **CONF 001 Config. 001 is valid for all A330-200 aircraft given in the effectivity of this Service Bulletin on which the Modification No. 48980D42587 is not embodied and on which the Service Bulletin No. A330-36-3032 is accomplished. **CONF 002 Config. 002 is valid for all A330-200 aircraft given in the effectivity of this Service Bulletin on which the Modification No. 48980D42587 is embodied and the Service Bulletin No. A330-36-3032 is accomplished. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Kit 363038A01R01 1 Kit 363038A02R01 1 Reidentified part set REIDA01 1 Consumable CMLA01 1 Kit 363038D01R01 1 Kit 363038D10R01 1 Kit 363038D12R00 1 Kit 363038D14R00 1 Consumable CMLD01 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Kit 363038A01R01 1 Kit 363038A02R01 1 Reidentified part set REIDA01 1 Consumable CMLA01 1 Kit 363038D01R01 1 Kit 363038D11R01 1 Kit 363038D12R00 1 Kit 363038D14R00 1 Consumable CMLD01 1

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 2 6

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# @A330 SERVICE BULLETIN **CONF ALL B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A330-36-3032 Mod. No. 55198D46286 55961D46493 55962D46494 NOTE: The Service Bulletin No. A330-36-3032 introduces the adapted dual loop overheat leak detection of the APU bleed air duct. NOTE: The Mod. No. 55198D46286 introduces the adapted dual loop overheat leak detection of the APU bleed air duct. NOTE: The Mod. No. 55961D46493 introduces the modification of the dual loop overheat leak detection in section 19. NOTE: The Mod. No. 55962D46494 introduces the modification of the dual loop overheat detection (CFRP-bulkhead). C. REASON (1) History The APU bleed leakdetection system detects any ambient overheat in the vicinity of the APU bleed air ducts. It is made of a single overheat detection loop which runs along the APU bleed air ducts in section 15/21 and section 16 thru 19.1. The SFAR88 requirements will induce MMEL restrictions on this system from 2009. (2) Objective/Action This Service Bulletin details the installation of a second APU bleed leak detection loop (APU LOOP B) in parallel to the current APU loop (APU LOOP A) in section 15/21 and section 16 thru 19.1. The Service Bulletin No. A330-36-3032 ’Introduce Adapted Dual-Loop Overheat-Detection APU Bleed-Air-Duct ’was retrofitted on the first aircraft in May 2008. After a check of the overheat-detection-loop installation, some none compliances to ATA 36-22 installation requirements have been reported. This Service Bulletin provides design improvements to the Service Bulletin No. A330-36-3032 OHDS installation. (3) Advantages The accomplishment of this Service Bulletin improves dual-loop overheat-detection of APU Bleed-Air-Duct, in accordance to ATA 36-22 installation requirements. (4) Operational/Maintenance Consequences None

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 3 6

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# @A330 SERVICE BULLETIN D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 363038-831-848-001: Modification (1) Remove the sensing elements and the supports between FR39 and FR44 (2) Remove the sensing elements and the supports between FR44 and FR53.2 (3) Remove the sensing elements and the supports between FR53.2 and FR53.6 (4) Remove the sensing elements and the supports between FR53.6 and FR55 (5) If necessary, remove the ducts between FR35.5 and FR35.6 for access (6) Install a New Support for the Routing of the Sensing Elements between FR53.5 and FR53.6 (7) If removed, Install the Ducts between FR53.5 and FR53.6 (8) If necessary, Remove the Ducts between FR43 and FR45 for access (9) Install the new Brackets for the Routing of the Sensing Elements at FR44 (10) If removed, install the ducts between FR43 and FR45 (11) Install the Sensing Elements and the Supports between FR39 and FR44 (12) Install the sensing elements and the supports between FR44 and FR50 (13) Install the sensing elements and the supports between FR50 and FR53.6 (14) Install the sensing elements and the supports between FR53.6 and FR55 (15) If necessary, remove the ducts between FR39 and FR40 for access (16) Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. (17) Modify the existing Harness 2SG. (18) Modify the Wiring between the Avionics Compartment and the Cargo Compartment. (19) Modify the Wiring in the Main rack 800VU. (20) If removed, install the ducts between FR39 and FR40. (21) Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct (22) Remove the clamp and the attaching parts from the overheat sensing elements
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 4 6

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# @A330 SERVICE BULLETIN (23) Remove the clamp from the overheat-detection dual loops at Frame 80 (24) Reroute the sensing elements 32HF and 357HF (25) Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage (26) Install the clamp and the new attaching parts on the overheat sensing elements in the rear fuselage (27) Install the sleeves on the APU bleed-air-duct **CONF 002 Task 363038-831-848-001: Modification (1) Remove the sensing elements and the supports between FR39 and FR44 (2) Remove the sensing elements and the supports between FR44 and FR53.2 (3) Remove the sensing elements and the supports between FR53.2 and FR53.6 (4) Remove the sensing elements and the supports between FR53.6 and FR55 (5) If necessary, remove the ducts between FR35.5 and FR35.6 for access (6) Install a New Support for the Routing of the Sensing Elements between FR53.5 and FR53.6 (7) If removed, Install the Ducts between FR53.5 and FR53.6 (8) If necessary, Remove the Ducts between FR43 and FR45 for access (9) Install the new Brackets for the Routing of the Sensing Elements at FR44 (10) If removed, install the ducts between FR43 and FR45 (11) Install the Sensing Elements and the Supports between FR39 and FR44 (12) Install the sensing elements and the supports between FR44 and FR50 (13) Install the sensing elements and the supports between FR50 and FR53.6 (14) Install the sensing elements and the supports between FR53.6 and FR55 (15) If necessary, remove the ducts between FR39 and FR40 for access (16) Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. (17) Modify the existing Harness 2SG. (18) Modify the Wiring between the Avionics Compartment and the Cargo Compartment. (19) Modify the Wiring in the Main rack 800VU. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 5 6

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# @A330 SERVICE BULLETIN (20) If removed, install the ducts between FR39 and FR40. (21) Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct (22) Remove the clamps and the attaching parts from the overheat sensing elements (23) Remove the clamp from the overheat-detection dual loops at Frame 80 (24) Reroute the sensing elements 32HF and 357HF (25) Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage (26) Install the clamps and the new attaching parts on the overheat sensing elements in the rear fuselage (27) Install the sleeves on the APU bleed-air-duct **CONF ALL E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER 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.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 6 6

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# @A330 SERVICE BULLETIN **CONF 001 Task 363038-831-848-001: Modification Get Access 20.75 On Aircraft Remove the sensing elements and the supports between FR39 and FR44 4.00 Remove the sensing elements and the supports between FR44 and FR53.2 4.00 Remove the sensing elements and the supports between FR53.2 and FR53.6 4.00 Remove the sensing elements and the supports between FR53.6 and FR55 4.00 If necessary, remove the ducts between FR35.5 and FR35.6 for access 1.00 Install a New Support for the Routing of the Sensing Elements between FR53.5 and FR53.6 1.00 If removed, Install the Ducts between FR53.5 and FR53.6 2.00 If necessary, Remove the Ducts between FR43 and FR45 for access 1.00 Install the new Brackets for the Routing of the Sensing Elements at FR44 1.00 If removed, install the ducts between FR43 and FR45 2.00 Install the Sensing Elements and the Supports between FR39 and FR44 14.00 Install the sensing elements and the supports between FR44 and FR50 14.00 Install the sensing elements and the supports between FR50 and FR53.6 21.00 Install the sensing elements and the supports between FR53.6 and FR55 14.00 If necessary, remove the ducts between FR39 and FR40 for access 1.00 Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. 3.00 Modify the existing Harness 2SG. 10.00 Modify the Wiring between the Avionics Compartment and the Cargo Compartment. 1.00 Modify the Wiring in the Main rack 800VU. 2.00 If removed, install the ducts between FR39 and FR40. 2.00 Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct 1.25 Remove the clamp and the attaching parts from the overheat sensing elements 1.00 Remove the clamp from the overheat-detection dual loops at Frame 80 0.25 Reroute the sensing elements 32HF and 357HF 0.25 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 7 6

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# @A330 SERVICE BULLETIN
Task 363038-831-848-001: Modification Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage 1.50 Install the clamp and the new attaching parts on the overheat sensing elements in the rear fuselage 1.00 Install the sleeves on the APU bleed-air-duct 1.50 Tests 4.00 Close-Up 28.50 TOTAL MANHOURS 166.00 ELAPSED TIME (HOURS) 88.25 **CONF 002 Task 363038-831-848-001: Modification Get Access 20.75 On Aircraft Remove the sensing elements and the supports between FR39 and FR44 4.00 Remove the sensing elements and the supports between FR44 and FR53.2 4.00 Remove the sensing elements and the supports between FR53.2 and FR53.6 4.00 Remove the sensing elements and the supports between FR53.6 and FR55 4.00 If necessary, remove the ducts between FR35.5 and FR35.6 for access 1.00 Install a New Support for the Routing of the Sensing Elements between FR53.5 and FR53.6 1.00 If removed, Install the Ducts between FR53.5 and FR53.6 2.00 If necessary, Remove the Ducts between FR43 and FR45 for access 1.00 Install the new Brackets for the Routing of the Sensing Elements at FR44 1.00 If removed, install the ducts between FR43 and FR45 2.00 Install the Sensing Elements and the Supports between FR39 and FR44 14.00 Install the sensing elements and the supports between FR44 and FR50 14.00 Install the sensing elements and the supports between FR50 and FR53.6 21.00 Install the sensing elements and the supports between FR53.6 and FR55 14.00 If necessary, remove the ducts between FR39 and FR40 for access 1.00 Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. 3.00 Modify the existing Harness 2SG. 10.00 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 8 6

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# @A330 SERVICE BULLETIN
Task 363038-831-848-001: Modification Modify the Wiring between the Avionics Compartment and the Cargo Compartment. 1.00 Modify the Wiring in the Main rack 800VU. 2.00 If removed, install the ducts between FR39 and FR40. 2.00 Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct 1.25 Remove the clamps and the attaching parts from the overheat sensing elements 1.25 Remove the clamp from the overheat-detection dual loops at Frame 80 0.25 Reroute the sensing elements 32HF and 357HF 0.25 Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage 1.50 Install the clamps and the new attaching parts on the overheat sensing elements in the rear fuselage 1.25 Install the sleeves on the APU bleed-air-duct 1.50 Tests 4.00 Close-Up 28.50 TOTAL MANHOURS 166.50 ELAPSED TIME (HOURS) 88.25 **CONF ALL H. WEIGHT AND BALANCE **CONF 001 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +1.508 KG (+3.3245 LB) Effect on Balance +52.743 KGM (+381.490 LB.FT ) **CONF 002 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +1.510 KG (+3.3289 LB) Effect on Balance +52.850 KGM (+382.264 LB.FT ) **CONF ALL I. ELECTRICAL LOAD DATA Not Changed DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 9 6

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# @A330 SERVICE BULLETIN J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52 06-41-53 11-00-00 12-34-24 20-21-15 21-20-00 21-26-00 22-96-00 22-97-00 24-41-00 25-52-00 25-53-00 25-75-41 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 36-11-34 36-12-00 36-12-41 36-22-00 36-22-17 52-10-00 52-30-00 52-41-00 52-52-00 53-00-00 53-35-11 53-35-13 Consumable Material List (CML) ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44 20-43-10 20-48-00 20-52-10 20-55-00 Service Bulletin (SB) A330-36-3032 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52 06-41-53 11-00-00 12-34-24 20-21-15 21-20-00 21-26-00 22-96-00 22-97-00 24-41-00 25-52-00 25-53-00 25-75-41 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 36-11-34 36-12-00 36-12-41 36-22-00 36-22-17 52-10-00 52-30-00 52-41-00 52-52-00 53-00-00 53-35-11 53-35-13 Consumable Material List (CML) ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44 20-43-10 20-48-00 20-52-10 20-55-00 Service Bulletin (SB) A330-36-3032 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 10 6

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# @A330 SERVICE BULLETIN **CONF ALL K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 36-22-00 36-22-17 Aircraft Schematic Manual (ASM) 36-22-00 Aircraft Wiring List (AWL) Aircraft Wiring Manual (AWM) 36-12-04 36-22-05 91-03-06 91-03-07 Illustrated Parts Catalog (IPC) 24-92-02 24-92-04 25-14-01 25-71-01 25-92-31 36-22-03 36-22-04 53-36-03 Trouble Shooting Manual (TSM) 36-22-00 L. INTERCHANGEABILITY/MIXABILITY **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35610-2-255 35606-2-255 03 Not Applicable Sensing element 35631-2-255 35620-2-255 03 Not Applicable Sensing element 35627-2-255 35621-2-255 03 Not Applicable Sensing element 35616-2-255 35618-2-255 03 Not Applicable Sensing element 35610-2-255 35597-2-255 03 Not Applicable Sensing element 35611-2-255 35598-2-255 03 Not Applicable Sensing element 35601-2-255 35595-2-255 03 Not Applicable Sensing element 35600-2-255 35596-2-255 03 Not Applicable Sensing element 35569-2-255 35568-4-255 03 Not Applicable Sensing element 35569-2-255 35567-3-255 03 Not Applicable Sensing element 35593-3-255 35597-3-255 03 Not Applicable Sensing element 35579-2-255 35587-2-255 03 Not Applicable Sensing element 35632-2-255 35627-2-255 03 Not Applicable Sensing element 35627-2-255 35625-2-255 03 Not Applicable
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# @A330 SERVICE BULLETIN
DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Blanket-Insulation F2581677800000 F0041196500000 03 Not Applicable Blanket-Insulation F2581677900000 F0041196600000 03 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF 002 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35610-2-255 35606-2-255 03 Not Applicable Sensing element 35631-2-255 35620-2-255 03 Not Applicable Sensing element 35627-2-255 35621-2-255 03 Not Applicable Sensing element 35616-2-255 35618-2-255 03 Not Applicable Sensing element 35610-2-255 35597-2-255 03 Not Applicable Sensing element 35611-2-255 35598-2-255 03 Not Applicable Sensing element 35601-2-255 35595-2-255 03 Not Applicable Sensing element 35600-2-255 35596-2-255 03 Not Applicable Sensing element 35569-2-255 35568-4-255 03 Not Applicable Sensing element 35569-2-255 35567-3-255 03 Not Applicable Sensing element 35593-3-255 35597-3-255 03 Not Applicable Sensing element 35579-2-255 35587-2-255 03 Not Applicable Sensing element 35632-2-255 35627-2-255 03 Not Applicable Sensing element 35627-2-255 35625-2-255 03 Not Applicable Blanket-Insulation F2581677800000 F0041196500000 03 Not Applicable Blanket-Insulation F2581677900000 F0041196600000 03 Not Applicable

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 12 6

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# @A330 SERVICE BULLETIN NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF ALL M. SPARES None

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 13 6

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# @A330 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 14 6

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# @A330 SERVICE BULLETIN 2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 363038A01R01 Kit 363038A02R01 Kit 363038D01R01 Kit 363038D10R01 Kit 363038D11R01 Kit 363038D12R00 Kit 363038D14R00 Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 Hamburg Germany For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 2590 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability

Kit 363038A01R01 Cost 27,500.00 USD Availability 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with 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 at the issue date of the Service Bulletin. Kit 363038A02R01 Cost 1,800.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with 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 at the issue date of the Service Bulletin. Kit 363038D01R01 Cost 280.00 USD Availability 90 calendar days from receipt of order

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 15 6

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# @A330 SERVICE BULLETIN The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with 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 at the issue date of the Service Bulletin. Kit 363038D10R01 Cost 55.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with 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 at the issue date of the Service Bulletin. Kit 363038D11R01 Cost 65.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with 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 at the issue date of the Service Bulletin. Kit 363038D12R00 Cost 35.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with 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 at the issue date of the Service Bulletin. Kit 363038D14R00 Cost 2,870.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with 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 at the issue date of the Service Bulletin.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 16 6

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# @A330 SERVICE BULLETIN B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 10 NSA5543-00 123 CLAMP 11 ASNA0342T04-01 16 BOLT 13 NSA5539S 249 SLEEVE 14 ASNA2397-10L 152 WASHER 15 NSA5542-00 20 NUT 16 NSA5527-03-01 40 SPACER 17 NSA5527-03-10 3 SPACER 18 NSA5527-03-11 17 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 72 BOLT 21 NAS6603-9 33 BOLT 22 NSA5527-03-15 1 SPACER 23 NAS6603-16 3 BOLT 24 NAS6603-15 7 BOLT 25 NSA5545-00 1 ANGLE 26 NAS6603-32 3 BOLT 28 NAS6603-12 1 BOLT 29 NAS6603-2 22 BOLT 30 NSA5546-00 7 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 2 PLACARD 35 F1131031623800 2 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 2 PLACARD 41 F1131031624100 2 PLACARD 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 3 SUPPORT 71 F3611548800000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT 75 F3611548400000 1 SUPPORT DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 17 6

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 76 F3611548200000 1 SUPPORT 77 F3611548600000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 9 SUPPORT 80 F3611549500000 1 SUPPORT 81 F3611549600000 1 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200000 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 4 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT 100 35606-2-255 1 SNSGELEM (1) 35610-2-255 03 101 35621-2-255 1 SNSGELEM (11) 35627-2-255 03 102 35620-2-255 1 SNSGELEM (2) 35631-2-255 03 103 35618-2-255 2 SNSGELEM (12) 35616-2-255 03 104 35567-3-255 1 SNSGELEM (7) 35569-2-255 03 105 35598-2-255 1 SNSGELEM (13) 35611-2-255 03 106 35595-2-255 3 SNSGELEM (5) 35601-2-255 03 107 35596-2-255 1 SNSGELEM (15) 35600-2-255 03 108 35568-4-255 1 SNSGELEM (7) 35569-2-255 03 109 35597-3-255 1 SNSGELEM (8) 35593-3-255 03 110 35587-2-255 1 SNSGELEM (17) 35579-2-255 03 111 35627-2-255 1 SNSGELEM (9) 35632-2-255 03 112 35625-2-255 1 SNSGELEM (11) 35627-2-255 03 113 35610-2-255 1 SNSGELEM (1) 35610-2-255 114 35597-2-255 1 SNSGELEM (1) 35610-2-255 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 18 6

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# @A330 SERVICE BULLETIN NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 14 ASNA2397-10L 1 WASHER 16 NSA5527-03-01 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 20 WASHER 141 NSA5527-03-02 2 SPACER 150 NSA935807-04 4 CLAMP 151 NSA5159-17 1 STUD 152 NSA5527-03-08 1 SPACER 153 NSA935808-01 8 WASHER 157 NSA5159-10 1 STUD 158 NAS1801-3-9 3 SCREW 169 NSA935401-03 208 TIE 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 174 35301-74 2 CABLE 175 35301-75 2 CABLE 176 NSA5516-21ND 5 CLAMP 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP F9000095228595 1 BUNDLE NSA935401-06 200 TIE NSA935401-13 200 TIE NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363038D01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 169 NSA935401-03 30 TIE 210 MS21919WCH14 1 CLAMP 211 F9237000207200 8 PLCRDSET

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 19 6

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# @A330 SERVICE BULLETIN NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363038D10R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 13 NSA5539S 10 SLEEVE 16 NSA5527-03-01 4 SPACER 86 NSA5538-00 2 CLAMP 207 NAS1802-3-13 4 SCREW 208 NSA5527-03-04 2 SPACER 209 NAS1801-3-8 2 SCREW NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363038D11R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 13 NSA5539S 12 SLEEVE 16 NSA5527-03-01 4 SPACER 86 NSA5538-00 2 CLAMP 207 NAS1802-3-13 4 SCREW 208 NSA5527-03-04 3 SPACER 209 NAS1801-3-8 3 SCREW NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 363038D12R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 13 NSA5539S 2 SLEEVE 16 NSA5527-03-01 1 SPACER 86 NSA5538-00 2 CLAMP 207 NAS1802-3-13 1 SCREW NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 20 6

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# @A330 SERVICE BULLETIN Kit 363038D14R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 13 NSA5539S 6 SLEEVE 200 F3617062404000 1 SLEEVE 201 F3617062403800 1 SLEEVE 202 F3617062403600 1 SLEEVE 203 F3617062403400 1 SLEEVE 204 F3617062403200 1 SLEEVE NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (Insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005 As required Corrosion Inhibiting Fillet Consistency 09-016 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (Insulation Blanket Repair) 08-073 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required (2) Components None (3) Equipment None

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 21 6

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# @A330 SERVICE BULLETIN E. PARTS TO BE RE-IDENTIFIED BY OPERATOR Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 F. TOOLING None

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 22 6

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# @A330 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 363038-831-848-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: YOU MUST MAKE SURE THAT THE LANDING GEAR GROUND SAFETY LOCKS ARE INSTALLED AND THE WHEEL CHOCKS ARE IN POSITIONS. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON ELECTRICAL WIRING AND COMPONENTS - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone 120 150 190 210 310 Modified FIN 313AL 312AR 22HF 23HF 24HF 25HF 32HF 97HF 98HF 99HF 100HF 101HF 102HF 137HF 138HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF 310HF 311HF 312HF 357HF 3501VS 3503VS 3591VS 3593VS Access Door 312AR 313AL Manpower TOTAL MANHOURS 166.00 ELAPSED TIME (HOURS) 88.25 **CONF 002 Zone 120 150 190 210 310

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 23 6

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# @A330 SERVICE BULLETIN
Modified FIN 313AL 312AR 22HF 23HF 24HF 25HF 32HF 97HF 98HF 99HF 100HF 101HF 102HF 137HF 138HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF 310HF 311HF 312HF 357HF 3501VS 3503VS 3591VS 3593VS Access Door 312AR 313AL Manpower TOTAL MANHOURS 166.50 ELAPSED TIME (HOURS) 88.25 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 363038-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 11-00-00, Page Block 201 Task 20-21-15-912-801 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 20-43-10 20-48-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 (a) Use a non metallic spatula to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (b) For fasteners spacing and margin (Refer to SRM 51-47-00). DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 24 6

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# @A330 SERVICE BULLETIN (c) To torque tighten the electrical component fasteners (Refer to AMM Task 20-21-15-912-801). (d) Clean the areas where you will install the placards with : Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required

and (e) Apply the sealant (Refer to SRM 51-24-00). (f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (h) Tag all the parts you must remove and retain to make the subsequent installation easier. (i) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (j) If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the Standards Manual (SM). The SM will give you the correct part number to part number relationship. (k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201). (l) Apply a special protection on new parts (Refer to SRM 51-23-12). (m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00). (n) Obey the instructions of the splices installation (Refer to ESPM 20-43-10). (o) Make sure that the electrical connectors are serviceable before you connect them again. (p) To install new wires, cut them to the necessary length, crimp the terminals and connect them (Referto ESPM 20-48-00). (q) Put blanking plugs on the disconnected line ends. (2) Subtask 363038-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 25 6

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# @A330 SERVICE BULLETIN Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 Fig. A-GBHAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001). (c) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM 20-25-51). (d) For tolerances for waviness and bends in sensing element wires (Refer to Fig. AGBHAA). (e) Install the SB/MOD identification placards in a position where you can clearly see them. (f) If necessary, clean the work areas with: Solvent General Purpose 11-026 As required and Lint-Free Cotton Cloth 19-003 As required (3) Subtask 363038-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 26 6

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# @A330 SERVICE BULLETIN **CONF 002 (1) Subtask 363038-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 11-00-00, Page Block 201 Task 20-21-15-912-801 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 20-43-10 20-48-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 (a) Use a non metallic spatula to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (b) For fasteners spacing and margin (Refer to SRM 51-47-00). (c) To torque tighten the electrical component fasteners (Refer to AMM Task 20-21-15-912-801). (d) Clean the areas where you will install the placards with : Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required

and (e) Apply the sealant (Refer to SRM 51-24-00). DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 27 6

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# @A330 SERVICE BULLETIN (f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (h) Tag all the parts you must remove and retain to make the subsequent installation easier. (i) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (j) If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the Standards Manual (SM). The SM will give you the correct part number to part number relationship. (k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201). (l) Apply a special protection on new parts (Refer to SRM 51-23-12). (m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00). (n) Obey the instructions of the splices installation (Refer to ESPM 20-43-10). (o) Make sure that the electrical connectors are serviceable before you connect them again. (p) To install new wires, cut them to the necessary length, crimp the terminals and connect them (Referto ESPM 20-48-00). (q) Put blanking plugs on the disconnected line ends. (2) Subtask 363038-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 28 6

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# @A330 SERVICE BULLETIN
References Fig. A-GBHAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001). (c) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM 20-25-51). (d) For tolerances for waviness and bends in sensing element wires (Refer to Fig. AGBHAA). (e) Install the SB/MOD identification placards in a position where you can clearly see them. (f) If necessary, clean the work areas with: Solvent General Purpose 11-026 As required and Lint-Free Cotton Cloth 19-003 As required (3) Subtask 363038-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 363038-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 29 6

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# @A330 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 36-11-34-000-802 Task 36-22-17-000-801 Task 36-22-17-000-802 Task 52-10-00-010-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801). (d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801). (g) Do the Job Set-up procedure as specified in the removal of the sensing elements (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802). (h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring Computer (BMC) (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-000-802). (2) Subtask 363038-010-002-001 - Remove/Open for Access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-75-41-000-801 Task 53-00-00-000-802 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-000-802).
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 30 6

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# @A330 SERVICE BULLETIN(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (e) At Frame 20 in the FWD cargo-compartment, remove the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, remove (if necessary) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (h) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (i) On the LH side of the belly fairing, remove (if necessary) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). (j) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802). (k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-000-801). (3) Subtask 363038-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released : - BAT 1, BAT 2, APU BAT, - GEN 1, GEN 2, APU GEN, - EXT A (B). DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 31 6

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# @A330 SERVICE BULLETIN (b) Open, safety and tags the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel : - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (f) Make sure that there is a warning notice at the access door 121EL to tell persons not to connect the external power connector (s). (4) Subtask 363038-941-202-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Put access platform(s) in position at below the access doors 312AR and 313AL. (b) Open and secure the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (c) Open and secure the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). **CONF 002 (1) Subtask 363038-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 32 6

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# @A330 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 36-11-34-000-802 Task 36-22-17-000-801 Task 36-22-17-000-802 Task 52-10-00-010-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801). (d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801). (g) Do the Job Set-up procedure as specified in the removal of the sensing elements (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802). (h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring Computer (BMC) (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-000-802). (2) Subtask 363038-010-002-001 - Remove/Open for Access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-75-41-000-801 Task 53-00-00-000-802 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-000-802).
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 33 6

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# @A330 SERVICE BULLETIN(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (e) At Frame 20 in the FWD cargo-compartment, remove the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, remove (if necessary) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (h) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (i) On the LH side of the belly fairing, remove (if necessary) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). (j) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802). (k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-000-801). (3) Subtask 363038-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released : - BAT 1, BAT 2, APU BAT, - GEN 1, GEN 2, APU GEN, - EXT A (B). DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 34 6

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# @A330 SERVICE BULLETIN (b) Open, safety and tags the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel : - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (f) Make sure that there is a warning notice at the access door 121EL to tell persons not to connect the external power connector (s). (4) Subtask 363038-941-202-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR, Door 313AL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Put access platform(s) in position at below the access doors 312AR and 313AL. (b) Open and secure the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (c) Open and secure the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 35 6

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# @A330 SERVICE BULLETIN **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 363038-831-001-001 - Remove the sensing elements and the supports between FR39 and FR44 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 02, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 97HF 1 Sensing element 35610-2-255 Item (1) Discard FIN 98HF 1 Sensing element 35631-2-255 Item (2) Discard FIN 302HF 1 Sensing element 35610-2-255 Item (1) Discard FIN 303HF 1 Sensing element 35627-2-255 Item (11) Discard 2 Support Item (59) Discard 4 Rivet Item (45) Discard 2 Placard Item (23) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 36 6

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# @A330 SERVICE BULLETIN 1 Placard Item (24) Discard 2 Placard Item (29) Discard 1 Placard Item (30) Discard 4 Nut Item (57) Discard 14 Screw Item (76) Discard 32 Washer Item (46) Discard 64 Protective sleeve Item (56) Discard 23 Clamp Item (58) Discard 2 Screw Item (47) Discard 18 Clamp Item (82) Discard 9 Spacer Item (55) Discard 1 Screw Item (50) Discard 10 Spacer Item (53) Discard 5 Screw Item (52) Discard 4 Screw Item (52) Discard 6 Screw Item (48) Discard As required Wire-lock Item (100) Discard

(2) Subtask 363038-831-002-001 - Remove the sensing elements and the supports between FR44 and FR53.2 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 37 6

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# @A330 SERVICE BULLETIN
References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 99HF 1 Sensing element 35618-2-255 Item (3) Discard FIN 100HF 1 Sensing element 35610-2-255 Item (1) Discard FIN 304HF 1 Sensing element 35616-2-255 Item (12) Discard FIN 305HF 1 Sensing element 35611-2-255 Item (13) Discard 2 Support Item (59) Discard 4 Rivet Item (45) Discard 1 Placard Item (25) Discard 2 Placard Item (26) Discard 1 Placard Item (27) Discard 1 Placard Item (30) Discard 2 Placard Item (31) Discard 2 Placard Item (32) Discard 1 Placard Item (33) Discard 4 Nut Item (57) Discard 1 Plate assy Item (41) Discard 8 Screw Item (76) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 38 6

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# @A330 SERVICE BULLETIN 30 Washer Item (46) Discard 56 Protective sleeve Item (56) Discard 18 Clamp Item (58) Discard 1 Screw Item (47) Discard 20 Clamp Item (82) Discard 10 Spacer Item (55) Discard 5 Screw Item (50) Discard 17 Spacer Item (53) Discard 12 Screw Item (52) Discard 3 Screw Item (48) Discard 1 Screw Item (49) Discard 1 Spacer Item (54) Discard As required Wire-lock Item (100) Discard

(3) Subtask 363038-831-003-001 - Remove the sensing elements and the supports between FR53.2 and FR53.6 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 39 6

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# @A330 SERVICE BULLETIN (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 04, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 23HF 1 Sensing element 35569-2-255 Item (7) Discard FIN 101HF 1 Sensing element 35601-2-255 Item (5) Discard FIN 102HF 1 Sensing element 35601-2-255 Item (5) Discard FIN 306HF 1 Sensing element 35601-2-255 Item (5) Discard FIN 307HF 1 Sensing element 35600-2-255 Item (15) Discard FIN 308HF 1 Sensing element 35569-2-255 Item (7) Discard 3 Support Item (59) Discard 6 Rivet Item (45) Discard 2 Placard Item (20) Discard 1 Placard Item (27) Discard 2 Placard Item (28) Discard 1 Placard Item (33) Discard 2 Placard Item (34) Discard 2 Placard Item (35) Discard 6 Nut Item (57) Discard 1 Plate assy Item (40) Discard 11 Screw Item (76) Discard 38 Washer Item (46) Discard 74 Protective sleeve Item (56) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 40 6

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# @A330 SERVICE BULLETIN 29 Clamp Item (58) Discard 2 Screw Item (50) Discard 16 Clamp Item (82) Discard 8 Spacer Item (55) Discard 21 Spacer Item (53) Discard 19 Screw Item (52) Discard 6 Screw Item (48) Discard As required Wire-lock Item (100) Discard

(4) Subtask 363038-831-004-001 - Remove the sensing elements and the supports between FR53.6 and FR55 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 05, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 24HF 1 Sensing element 35593-3-255 Item (8) Discard FIN 25HF 1 Sensing element 35632-2-255 Item (9) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 41 6

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# @A330 SERVICE BULLETIN
FIN 311HF 1 Sensing element 35579-2-255 Item (17) Discard FIN 312HF 1 Sensing element 35627-2-255 Item (11) Discard 1 Support Item (59) Discard 2 Rivet Item (45) Discard 1 Placard Item (21) Discard 1 Placard Item (22) Discard 1 Placard Item (36) Discard 1 Placard Item (37) Discard 2 Nut Item (57) Discard 1 Connector Item (61) Discard 14 Screw Item (76) Discard 27 Washer Item (46) Discard 54 Protective sleeve Item (56) Discard 21 Clamp Item (58) Discard 4 Screw Item (52) Discard 14 Spacer Item (53) Discard 2 Screw Item (51) Discard 12 Clamp Item (82) Discard 6 Spacer Item (55) Discard 4 Screw Item (48) Discard 3 Screw Item (77) Discard As required Wire-lock Item (100) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 42 6

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# @A330 SERVICE BULLETIN (5) Subtask 363038-020-001-001 - If necessary, remove the ducts between FR35.5 and FR35.6 for access Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01
(a) Remove : Fig. A-FBBAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (112) Retain 1 Duct assy Item (113) Retain 1 Duct assy Item (114) Retain

(6) Subtask 363038-831-005-001 - Install a New Support for the Routing of the Sensing Elements between FR53.5 and FR53.6 Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 43 6

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 2 RIVET Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005 As required Corrosion Inhibiting Fillet Consistency 09-016 As required References Fig. A-FBCAA Installation of a New Bracket between FR53.5 and FR53.6 Sheet 01 Sheet 02 (a) Move the insulation blanket to get access to the modification area. (b) Put the bracket Item 96 in position as shown on Fig. A-FBCAA
. (c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the bracket Item 96. Refer to Fig. A-FBCAA (d) Cut the insulation blanket to permit the installation of the bracket Item 96. NOTE: For the repair of the insulation blanket use : Adhesive Tape (insulation Blanket Repair) 08-073 As required (e) Re-identify the insulation blanket : 1 Blanket-Insulation F2581677800000 becomes :
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 44 6

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# @A330 SERVICE BULLETIN
1 Blanket-Insulation F0041196500000 or, 1 Blanket-Insulation F2581677900000 becomes : 1 Blanket-Insulation F0041196600000 (f) Install : Refer to Fig. A-FBCAA 1 Support F5392059300000 Item 96 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016 As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005 As required (g) Install the insulation blanket. (7) Subtask 363038-420-001-001 - If removed, Install the Ducts between FR53.5 and FR53.6 Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 45 6

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# @A330 SERVICE BULLETIN (a) Install : Refer to Fig. A-FBBAA (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (113) Retained at removal 1 Duct assy Item (114) Retained at removal (8) Subtask 363038-020-002-001 - If necessary, Remove the Ducts between FR43 and FR45 for access Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01
(a) Remove : Refer to Fig. A-FBDAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (115) Retain 1 Duct assy Item (116) Retain

(9) Subtask 363038-831-006-001 - Install the new Brackets for the Routing of the Sensing Elements at FR44 Work Zones and Access Panels Zone Access/Work location 190 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 46 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 97 ASNA2050DCJ3215 2 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005 As required Corrosion Inhibiting Fillet Consistency 09-016 As required References Fig. A-FBKAA Installation of Two New Brackets at FR44 Sheet 01 Sheet 02 (a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBKAA

. (b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) as shown on Fig. A-FBKAA
. (c) Install : 1 Support F0041178800000 Item 98 1 Support F0041178800100 Item 99 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016 As required
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 47 6

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# @A330 SERVICE BULLETIN NOTE: Wet install the fasteners with : Interfay Sealant 09-005 As required (10) Subtask 363038-410-001-001 - If removed, install the ducts between FR43 and FR45 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01
(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (115) Retained at removal 1 Duct assy Item (116) Retained at removal (11) Subtask 363038-831-007-001 - Install the Sensing Elements and the Supports between FR39 and FR44 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 48 6

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 30 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 62 SLEEVE 14 ASNA2397-10L 34 WASHER 15 NSA5542-00 4 NUT 16 NSA5527-03-01 8 SPACER 18 NSA5527-03-11 6 SPACER 20 NAS6603-1 19 BOLT 21 NAS6603-9 8 BOLT 24 NAS6603-15 6 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 2 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 70 F3611548300000 1 SUPPORT 71 F3611548800000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 1 SUPPORT 100 35606-2-255 1 SNSGELEM 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM References Fig. A-FBEAA Installation of the New Sensing Elements between FR39 and FR44 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR39 and FR40.2. 1 Install the supports between FR39 and FR40 : 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 8 Clamp NSA5543-00 Item 10 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-11 Item 18 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 49 6

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# @A330 SERVICE BULLETIN
8 Washer ASNA2397-10L Item 14 6 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-15 Item 24 2 Install the supports between FR40 and FR40.2 : 1 Support F3611549100000 Item 79 1 Support F3611549700000 Item 78 5 Clamp NSA5543-00 Item 10 1 Spacer NSA5527-03-01 Item 16 8 Washer ASNA2397-10L Item 14 1 Bolt NAS6603-9 Item 21 6 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-2 Item 29 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 3 Install the placards between FR39 and FR40.2 : 2 Placard F1131031621700 Item 32 2 Placard F1131031623700 Item 33 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 4 Install the sensing elements between FR39 and FR40.2 : FIN 97HF 1 Sensing Element 35606-2-255 Item 100 FIN 302HF 1 Sensing Element 35610-2-255 Item 113 28 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 50 6

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# @A330 SERVICE BULLETIN (b) Install the sensing elements and the supports between FR40.2 and FR44. 1 Install the supports between FR40.2 and FR44 : 1 Support F3611548300000 Item 70 1 Support F3611548800000 Item 71 17 Clamp NSA5543-00 Item 10 4 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-01 Item 16 18 Washer ASNA2397-10L Item 14 13 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 4 Bolt NAS6603-15 Item 24 2 Install the sensing elements between FR40.2 and FR44 : FIN 98HF 1 Sensing Element 35620-2-255 Item 102 FIN 303HF 1 Sensing Element 35621-2-255 Item 101 34 Sleeve-Protective NSA5539S Item 13

(12) Subtask 363038-831-008-001 - Install the sensing elements and the supports between FR44 and FR50 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 50 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 51 6

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 29 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 58 SLEEVE 14 ASNA2397-10L 35 WASHER 15 NSA5542-00 8 NUT 16 NSA5527-03-01 10 SPACER 17 NSA5527-03-10 1 SPACER 18 NSA5527-03-11 5 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 13 BOLT 21 NAS6603-9 8 BOLT 23 NAS6603-16 3 BOLT 26 NAS6603-32 1 BOLT 29 NAS6603-2 8 BOLT 30 NSA5546-00 2 ANGLE 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 79 F3611549100000 4 SUPPORT 80 F3611549500000 1 SUPPORT 81 F3611549600000 1 SUPPORT 103 35618-2-255 2 SNSGELEM 105 35598-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM References Fig. A-FBFAA Installation of the New Sensing Elements between FR44 and FR50 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR44 and FR46 : 1 Install the supports between FR44 and FR46 : 1 Support F3611549600000 Item 81 17 Clamp NSA5543-00 Item 10
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 52 6

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# @A330 SERVICE BULLETIN 8 Spacer NSA5527-03-01 Item 16 5 Spacer NSA5527-03-11 Item 18 21 Washer ASNA2397-10L Item 14 2 Bolt NAS6603-24 Item 19 4 Bolt NAS6603-1 Item 20 6 Bolt NAS6603-9 Item 21 3 Bolt NAS6603-16 Item 23 2 Bolt NAS6603-2 Item 29 2 Install the placards at FR44 : 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 3 Install the sensing elements between FR44 and FR46 : FIN 99HF 1 Sensing Element 35618-2-255 Item 103 FIN 304HF 1 Sensing Element 35618-2-255 Item 103 34 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR46 and FR50. 1 Install the supports between FR46 and FR50 : 2 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 1 Support F3611549500000 Item 80 4 Support F3611549100000 Item 79 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 53 6

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# @A330 SERVICE BULLETIN 12 Clamp NSA5543-00 Item 10 2 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-10 Item 17 14 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-32 Item 26 6 Bolt NAS6603-2 Item 29 2 Install the placards between FR46 and FR50 : 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 2 Placard F1131031624000 Item 38 2 Placard F1131031622000 Item 39 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 3 Install the sensing elements between FR46 and FR50 : FIN 100HF 1 Sensing Element 35597-2-255 Item 114 FIN 305HF 1 Sensing Element 35598-2-255 Item 105 24 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (13) Subtask 363038-831-009-001 - Install the sensing elements and the supports between FR50 and FR53.6 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 50 to Frame 53.6
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 54 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 21.00 Minimum number of person 1 Subtask elapsed time 21.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 37 CLAMP 11 ASNA0342T04-01 6 BOLT 13 NSA5539S 74 SLEEVE 14 ASNA2397-10L 51 WASHER 15 NSA5542-00 6 NUT 16 NSA5527-03-01 16 SPACER 18 NSA5527-03-11 1 SPACER 20 NAS6603-1 23 BOLT 21 NAS6603-9 16 BOLT 22 NSA5527-03-15 1 SPACER 24 NAS6603-15 1 BOLT 25 NSA5545-00 1 ANGLE 28 NAS6603-12 1 BOLT 29 NAS6603-2 10 BOLT 30 NSA5546-00 2 ANGLE 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548600000 1 SUPPORT 79 F3611549100000 3 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 104 35567-3-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 55 6

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# @A330 SERVICE BULLETIN
References Fig. A-FBGAA Installation of the New Sensing Elements between FR50 and FR53.6 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR50 and FR53.2. 1 Install the supports between FR50 and FR53.2 : 1 Support F3611548700000 Item 72 1 Support F3611548400000 Item 75 1 Support F3611549400000 Item 82 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 13 Clamp NSA5543-00 Item 10 7 Spacer NSA5527-03-01 Item 16 16 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 2 Install the placards between FR50 and FR53.2 : 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 3 Install the sensing elements between FR50 and FR53.2 : FIN 101HF 1 Sensing Element 35595-2-255 Item 106 FIN 102HF 1 Sensing Element 35595-2-255 Item 106 26 Sleeve-Protective NSA5539S Item 13
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 56 6

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# @A330 SERVICE BULLETIN
2 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR53.2 and FR53.6. 1 Install the supports between FR53.2 and FR53.6 : 1 Support F3611548300000 Item 70 1 Support F3611548500000 Item 73 1 Support F3611548900000 Item 74 1 Support F3611548200000 Item 76 1 Support F3611548600000 Item 77 3 Support F3611549100000 Item 79 1 Support F3611549800000 Item 83 1 Support F3611549300000 Item 84 1 Angle NSA5545-00 Item 25 1 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 24 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-15 Item 22 35 Washer ASNA2397-10L Item 14 14 Bolt NAS6603-1 Item 20 9 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-15 Item 24 1 Bolt NAS6603-12 Item 28 10 Bolt NAS6603-2 Item 29 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 57 6

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# @A330 SERVICE BULLETIN
2 Install the placards between FR53.2 and FR53.6 : 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 2 Placard F1131031620400 Item 44 2 Placard F1131031624300 Item 45 3 Install the sensing elements between FR53.2 and FR53.6 : FIN 102HF 1 Sensing Element 35595-2-255 Item 106 FIN 307HF 1 Sensing Element 35596-2-255 Item 107 FIN 23HF 1 Sensing Element 35568-4-255 Item 108 FIN 308HF 1 Sensing Element 35567-3-255 Item 104 48 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (14) Subtask 363038-831-010-001 - Install the sensing elements and the supports between FR53.6 and FR55 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 27 CLAMP 11 ASNA0342T04-01 2 BOLT DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 58 6

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 55 SLEEVE 14 ASNA2397-10L 32 WASHER 15 NSA5542-00 2 NUT 16 NSA5527-03-01 6 SPACER 17 NSA5527-03-10 2 SPACER 18 NSA5527-03-11 5 SPACER 20 NAS6603-1 17 BOLT 21 NAS6603-9 1 BOLT 26 NAS6603-32 2 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 1 ANGLE 70 F3611548300000 1 SUPPORT 79 F3611549100000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200000 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 109 35597-3-255 1 SNSGELEM 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM 112 35625-2-255 1 SNSGELEM References Fig. A-FBHAA Installation of the New Sensing Elements between FR53.6 and FR55 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR53.6 and FR55. 1 Install the supports between FR53.6 and FR55 : 1 Support F3611548300000 Item 70 1 Support F3611549100000 Item 79 1 Support F3611549200000 Item 93 1 Support F3611549000000 Item 95 1 Angle NSA5546-00 Item 30 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 59 6

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# @A330 SERVICE BULLETIN
2 Rivet-Blind ASNA0342T04-01 Item 11 27 Clamp NSA5543-00 Item 10 3 Clamp NSA5538-00 Item 86 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-10 Item 17 5 Spacer NSA5527-03-11 Item 18 32 Washer ASNA2397-10L Item 14 17 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-32 Item 26 2 Bolt NAS6603-2 Item 29 5 Bolt NAS6603-17 Item 87 5 Bolt NAS6603-10 Item 94 2 Install the placards between FR53.6 and FR55 : 1 Placard F1131031620500 Item 88 1 Placard F1131031624400 Item 89 1 Placard F1131031620600 Item 90 1 Placard F1131031624500 Item 91 3 Install the sensing elements between FR53.6 and FR55 : FIN 24HF 1 Sensing Element 35597-3-255 Item 109 FIN 311HF 1 Sensing Element 35587-2-255 Item 110 FIN 25HF 1 Sensing Element 35627-2-255 Item 111 FIN 312HF 1 Sensing Element 35625-2-255 Item 112
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 60 6

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# @A330 SERVICE BULLETIN
2 Nut NSA5542-00 Item 15 2 Connector NSA5549-90 Item 85 55 Sleeve-Protective NSA5539S Item 13 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (15) Subtask 363038-010-001-001 - If necessary, remove the ducts between FR39 and FR40 for access Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01 (a) Remove : Fig. A-FBPAA (Refer to AMM Task 21-20-00-010-801) 1 Duct assy Item (125) Retain 1 Duct assy Item (126) Retain 1 Duct assy Item (127) Retain

(16) Subtask 363038-831-011-001 - Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. Work Zones and Access Panels Zone Access/Work location 150

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 61 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills ELECTRICAL Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 1 WASHER 169 NSA935401-03 8 TIE 174 35301-74 1 CABLE 175 35301-75 1 CABLE F9000095228595 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-10 Service Bulletin (SB) A330-36-3032 Fig. A-FBJAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Fig. A-FWCAA Installation of the Wiring of the New Sensing Elements Sheet 01 (a) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and Fig. A-FBJAA Sheet 02, remove without disconnection the FINs 137HF and 138HF and the FINs 309HF and 310HF attached with : 1 Screw Item (168) Retain 1 Washer Item (14) Discard 2 Clamp Item (155) Retain 1 Spacer Item (18) Retain (b) Modify the splice FIN 3503VS : 1 Before any disconnection, record the wires number associated to the FIN 137HF and the FIN 138HF.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 62 6

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# @A330 SERVICE BULLETIN
2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF : FIN 3503VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3503VS and of the wires associated to the FIN 137HF and the FIN 138HF. 3 Remove : FIN 137HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard 4 Maintain in position : FIN 138HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) 5 Put in position : FIN 137HF 1 Cable-Electrical Interconnecting 35301-75 Item 175 6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN 137HF and the FIN 138HF, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3503VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 137HF and 138HF with the retained identification sleeves. (c) Modify the splice FIN 3593VS : NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation. 1 Before any disconnection, record the wires number associated to the FIN 309HF and the FIN 310HF. 2 Remove the splice FIN 3593VS between the FIN 309HF and the FIN 310HF : FIN 3593VS 1 Splice Discard
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 63 6

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# @A330 SERVICE BULLETIN NOTE: Retain the identification sleeves and the identification label of the 3593VS and of the wires associated to the FIN 309HF and the FIN 310HF. 3 Remove : FIN 309HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) Discard 4 Maintain in position : FIN 310HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) 5 Put in position : FIN 309HF 1 Cable-Electrical Interconnecting 35301-74 Item 174 6 Install the new splice FIN 3593VS (PN E0360RK1816) between the FIN 309HF and the FIN 310HF, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3593VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 309HF and 310HF with the retained identification sleeves. (d) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and Fig. A-FBJAA Sheet 02, install the FINs 137HF and 138HF and the FINs 309HF and 310HF (spliced previously) with : 1 Spacer Item (18) Retained at removal 2 Clamp Item (155) Retained at removal 1 Washer ASNA2397-10L Item 14 1 Screw Item (168) Retained at removal and attach it with : 8 Tie-Cable NSA935401-03 Item 169
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 64 6

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# @A330 SERVICE BULLETIN NOTE: After connection, secure the FINs 137HF and 138HF and the FINs 309HF and 310HF with Wire-lock MS20995C32 Item 27, (Refer to Fig. A-FBJAA Sheet 03). (e) If necessary, secure the nuts (installed on the fuselage) and the FIN 138HF and the FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBJAA Sheet 03). (17) Subtask 363038-831-012-001 - Modify the existing Harness 2SG. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 10.00 Minimum number of person 1 Subtask elapsed time 5.00 Skills NON SPECIFIC Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 16 NSA5527-03-01 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 20 WASHER 141 NSA5527-03-02 2 SPACER 150 NSA935807-04 4 CLAMP 151 NSA5159-17 1 STUD 152 NSA5527-03-08 1 SPACER 153 NSA935808-01 8 WASHER 157 NSA5159-10 1 STUD 158 NAS1801-3-9 3 SCREW 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 174 35301-74 1 CABLE 175 35301-75 1 CABLE 176 NSA5516-21ND 5 CLAMP 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP F9000095228595 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-10
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 65 6

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# @A330 SERVICE BULLETIN
References Service Bulletin (SB) A330-36-3032 Fig. A-FBMAA Modification of the Existing Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Fig. A-FWCAA Installation of the Wiring of the New Sensing Elements Sheet 01 (a) Modify the supports of existing routing between 302HF located on the left hand side at stringer 36 and Frame 40 and the 3520VP located on the right hand side at Frame 39.1 : NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation. 1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, remove : a For Section A-A : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (152) Retain 1 Clamp Item (150) Retain 1 Stud Item (151) Retain DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 66 6

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# @A330 SERVICE BULLETIN b For Section B-B : 6 Nut Item (154) Retain 6 Washer Item (153) Discard 6 Clamp Item (150) Retain 6 Spacer Item (152) Retain 6 Clamp Item (150) Retain 6 Stud Item (151) Retain c For Section C-C : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (155) Discard 1 Spacer Item (152) Retain 1 Clamp Item (155) Discard 1 Stud Item (151) Retain 2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, install : a For Section D-D : 1 Stud Item (151) Retained at removal 1 Clamp Item (150) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 67 6

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# @A330 SERVICE BULLETIN b For Section E-E : 6 Stud Item (151) Retained at removal 6 Clamp Item (150) Retained at removal 6 Spacer Item (152) Retained at removal 6 Clamp Item (150) Retained at removal 6 Washer NSA935808-03 Item 131 6 Nut Item (154) Retained at removal c For Section F-F : 1 Stud Item (151) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Spacer Item (152) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, remove : a For Section G-G : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (155) Discard 1 Spacer Item (152) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 68 6

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# @A330 SERVICE BULLETIN 1 Clamp Item (150) Retain 1 Stud Item (151) Retain b For Section H-H : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (155) Discard 1 Spacer Item (152) Retain 1 Clamp Item (155) Retain 1 Stud Item (151) Retain 4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, install : a For Section J-J : 1 Stud Item (151) Retained at removal 1 Clamp Item (150) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal b For Section K-K : 1 Stud Item (151) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer Item (152) Retained at removal DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 69 6

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# @A330 SERVICE BULLETIN 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, remove for detail F : 2 Nut Item (154) Retain 2 Washer Item (153) Discard 2 Clamp Item (150) Retain 2 Spacer Item (152) Retain 2 Clamp Item (135) Retain 2 Clamp Item (134) Retain 2 Stud Item (151) Retain 6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, install for detail G : 2 Stud Item (151) Retained at removal 2 Clamp Item (134) Retained at removal 2 Clamp Item (135) Retained at removal 2 Spacer Item (152) Retained at removal 2 Clamp Item (150) Retained at removal 2 Washer NSA935808-03 Item 131 2 Nut Item (154) Retained at removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 70 6

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# @A330 SERVICE BULLETIN
7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section L-L : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Clamp Item (138) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain b For Section M-M : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain 8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section N-N : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 71 6

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# @A330 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal b For Section P-P : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 46 and 48, remove for section Q-Q : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (16) Discard
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 72 6

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# @A330 SERVICE BULLETIN 1 Clamp Item (139) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (157) Discard 10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 46 and 48, install for Section R-R : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 49 and 52, remove for detail K : 2 Nut Item (154) Retain 2 Washer Item (153) Discard 2 Clamp Item (150) Retain 2 Spacer Item (152) Retain 2 Clamp Item (138) Retain
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 73 6

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# @A330 SERVICE BULLETIN 2 Stud Item (151) Retain 12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 49 and 52, install for detail L : 2 Stud Item (151) Retained at removal 2 Clamp Item (138) Retained at removal 2 Spacer Item (152) Retained at removal 2 Clamp Item (150) Retained at removal 2 Washer NSA935808-03 Item 131 2 Nut Item (154) Retained at removal 13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 52 and 54, remove for Section S-S : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Clamp Item (138) Retain 1 Spacer Item (141) Retain 1 Clamp Item (138) Retain 1 Stud Item (140) Retain 14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 52 and 54, install for Section T-T : 1 Stud Item (140) Retained at removal 1 Clamp Item (138) Retained at removal
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 74 6

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# @A330 SERVICE BULLETIN 1 Spacer Item (141) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 15 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the Stringers 54, remove for detail N : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (152) Retain 1 Clamp Item (138) Retain 1 Stud Item (151) Retain 16 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the Stringers 54, install for detail P : 1 Stud Item (151) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 75 6

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# @A330 SERVICE BULLETIN
17 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 54 and 48, remove for detail Q : 3 Screw Item (167) Discard 3 Washer Item (153) Discard 3 Clamp Item (138) Retain 3 Clamp Item (150) Retain 18 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 54 and 48, install for detail R : 3 Clamp Item (150) Retained at removal 3 Clamp Item (138) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-9 Item 158 19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, remove : a For Section U-U : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Discard 1 Spacer Item (18) Discard 1 Clamp Item (134) Discard 1 Stud Item (151) Discard b For Section V-V : 1 Screw Item (183) Discard 1 Washer Item (153) Discard 1 Clamp Item (184) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 76 6

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# @A330 SERVICE BULLETIN 1 Spacer Item (141) Discard 1 Clamp Item (184) Discard 20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section W-W : 2 Spacer NSA5527-03-02 Item 141 2 Clamp NSA5516-07ND Item 179 or 2 Clamp NSA5516-08ND Item 180 or 2 Clamp NSA5516-10ND Item 181 and 2 Washer NAS1149F0332P Item 172 2 Screw NAS1801-3-17 Item 171 NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND or NSA5516-08ND or NSA5516-10ND. 21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail Y : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (165) Discard 1 Spacer Item (152) Retain 1 Clamp Item (155) Retain 1 Clamp Item (155) Retain 1 Stud Item (163) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 77 6

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# @A330 SERVICE BULLETIN
22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail Z : 1 Stud Item (163) Retained at removal 1 Clamp Item (155) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer Item (152) Retained at removal 1 Spacer NSA5527-03-15 Item 22 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, remove for detail W : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (18) Discard 1 Clamp Item (134) Discard 1 Stud Item (151) Discard 24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, install for detail X: 1 Stud NSA5159-10 Item 157 1 Clamp NSA5516-21ND Item 176 or DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 78 6

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# @A330 SERVICE BULLETIN 1 Clamp NSA5516-22ND Item 177 or 1 Clamp NSA5516-23ND Item 178 and 1 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-08 Item 152 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut Item (154) Retained at removal NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND. 25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, remove for detail AA : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (18) Retain 1 Clamp Item (134) Discard 1 Stud Item (151) Retain 26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, install for detail AB : 1 Stud Item (151) Retained at removal 1 Clamp NSA5516-21ND Item 176 or 1 Clamp NSA5516-22ND Item 177
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 79 6

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# @A330 SERVICE BULLETIN

or 1 Clamp NSA5516-23ND Item 178 and 1 Spacer Item (18) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut Item (154) Retained at removal NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND. 27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, remove for detail AC : 3 Screw Item (167) Retain 3 Washer Item (153) Discard 3 Clamp Item (135) Retain 3 Clamp Item (134) Discard 28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, install for detail AD : 3 Clamp NSA5516-21ND Item 176 or 3 Clamp NSA5516-22ND Item 177 or 3 Clamp NSA5516-23ND Item 178 and 3 Clamp Item (135) Retained at removal 3 Washer NSA935808-01 Item 153
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 80 6

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# @A330 SERVICE BULLETIN 3 Screw Item (167) Retained at removal NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND. (b) Modify the existing route 2SG between FIN 302HF located on the left hand side at stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment : NOTE: Apply the following modifications only if the Service Bulletin No. A330-36-3032 and the associated Technical Adaptation were applied. The following modification consists to restore the aircraft to the configuration before Service Bulletin No. A330-36-3032 and associated Technical Adaptation. 1 Modify the Interconnecting Electrical Wire FIN 301HF (Only if aircraft is equipped with FIN 301HF PN 35301-75) : Refer to ESPM 20-43-10 a Before any disconnection, record the wires number associated to the FIN 301HF. b Remove the splice FIN 3591VS between the FIN 301HF and the wire No. 3622-0540 : FIN 3591VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3591VS and of the wires associated to the FIN 301HF. c Remove : FIN 301HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) Discard d Install : 1 Cable-Electrical Interconnecting 35301-74 Item 174
e Install the new splice FIN 3591VS (PN NSA936809RG0002) between the FIN 301HF and the wire No. 3622-0540, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3591VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 81 6

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# @A330 SERVICE BULLETIN removal, identify the wires associated to the FINs 301HF with the retained identification sleeves. NOTE: After connection, Secure the FIN 301HF and FIN 302HF with Wire-lock MS20995C41 item 133. 2 Modify the Interconnecting Electrical Wire FIN 22HF (If aircraft is equipped with FIN 22HF PN 35301-74) : a Before any disconnection, record the wires number associated to the FIN 22HF. b Remove the splice FIN 3501VS between the FIN 22HF and the wire No. 3622-0082 : FIN 3501VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3501VS and of the wires associated to the FIN 22HF. c Remove : FIN 22HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard d Install : 1 Cable-Electrical Interconnecting 35301-75 Item 175
e Install the new splice FIN 3501VS (PN NSA936809RG0002) between the FIN 22HF and the wire No. 3622-0082, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3501VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 22HF with the retained identification sleeves. NOTE: After connection, Secure the FIN 22HF and FIN 97HF with Wire-lock MS20995C41 item 133.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 82 6

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# @A330 SERVICE BULLETIN (18) Subtask 363038-831-013-001 - Modify the Wiring between the Avionics Compartment and the Cargo Compartment. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES F9000095228595 BUNDLE References Service Bulletin (SB) A330-36-3032 Fig. A-FBMAA Modification of the Existing Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Fig. A-FWBAA Modification of the Wiring between the Cargo Compartment and the Avionics Compartment Sheet 01

NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation.
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 83 6

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# @A330 SERVICE BULLETIN (a) Modify the connection of the wire No. 3622-0542 as shown on the wiring diagram, Fig. A-FWBAA Sheet 01
. NOTE: If necessary use contact PN EN3155-003F2222 supplied in : Bundle F9000095228595 (19) Subtask 363038-831-014-001 - Modify the Wiring in the Main rack 800VU. Work Zones and Access Panels Zone Access/Work location 120 Work location Electrical panel 800VU Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 200 TIE F9000095228595 BUNDLE NSA935401-06 200 TIE NSA935401-13 200 TIE References Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802 Task 36-11-34-400-802 Service Bulletin (SB) A330-36-3032 Fig. A-FWAAA Modification of the Wiring in the Main Rack 800VU Sheet 01 Fig. A-FHAAA Hook-Up Chart of the Modification of the Wiring in the Main Rack 800VU Sheet 01
NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation. (a) Remove and retain the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-000-802).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 84 6

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# @A330 SERVICE BULLETIN (b) Remove the wire as shown on the wiring diagram Fig. A-FWAAA Sheet 01, and as given in the Hook-up Chart line : - 1 (Refer to Fig. A-FHAAA Sheet 01). (c) Install the wires as shown on the wiring diagram Fig. A-FWAAA Sheet 01 and as given in the Hook-up Chart lines : - 4 thru 5 (Refer to Fig. A-FHAAA Sheet 01) supplied in : Bundle F9000095228595 (d) Attach the wires with : 200 Tie-Cable NSA935401-03 Item 169 200 Tie-Cable NSA935401-06 200 Tie-Cable NSA935401-13 (e) Install the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802). (20) Subtask 363038-831-015-001 - If removed, install the ducts between FR39 and FR40. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01 (a) Install : Refer to Fig. A-FBPAA (Refer to AMM Task 21-20-00-410-801) 1 Duct assy Item (125) Retained at removal 1 Duct assy Item (126) Retained at removal DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 85 6

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# @A330 SERVICE BULLETIN 1 Duct assy Item (127) Retained at removal (21) Subtask 363038-831-201-001 - Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Work location from Frame 83 to Frame 93 Manpower Resources Manhours 1.25 Minimum number of person 2 Subtask elapsed time 0.75 Skills AIRFRAME References Fig. A-GBAAA Removal of the Sleeves from the APU Bleed-Air-Duct Sheet 01 (a) Remove the sleeves from the APU bleed-air-duct in the rear fuselage section. Refer to Fig. A-GBAAA Sheet 01
. 1 Between Frame 83 and Frame 93 remove the sleeves: 1 Sleeve Assy F3617062402000 Item (200) Discard 1 Sleeve Assy F3617062402400 Item (201) Discard 1 Sleeve Assy F3617062402600 Item (202) Discard 1 Sleeve Assy F3617062402800 Item (203) Discard 1 Sleeve Assy F3617062403000 Item (204) Discard

(22) Subtask 363038-831-202-001 - Remove the clamp and the attaching parts from the overheat sensing elements Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location from Frame 83 to Frame 88

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 86 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 1.00 Minimum number of person 2 Subtask elapsed time 0.50 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-GBBAA Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the clamp and the attaching parts in the rear fuselage. Refer to Fig. A-GBBAA Sheet 01 thru Fig. A-GBBAA Sheet 04
. Refer to AMM Task 36-22-17-000-801. 1 Between Frame 83 and Frame 84, remove: Refer to Fig. A-GBBAA Sheet 02, View B and Fig. A-GBBAA Sheet 04, View F. 2 Sleeve-Protective NSA5539S Item (13) Discard 1 Clamp NSA5543-00 Item (10) Retain with 1 Screw NAS1096-3-5 Item (205) Discard 2 Between Frame 84 and Frame 85, remove: Refer to Fig. A-GBBAA Sheet 02, View C and Fig. A-GBBAA Sheet 04, View F. 4 Sleeve-Protective NSA5539S Item (13) Discard 2 Clamp NSA5543-00 Item (10) Retain with 2 Screw NAS1096-3-5 Item (205) Discard 3 Between Frame 85 and Frame 86, remove: Refer to Fig. A-GBBAA Sheet 03, View D and Fig. A-GBBAA Sheet 04, View F. 2 Sleeve-Protective NSA5539S Item (13) Discard
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 87 6

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# @A330 SERVICE BULLETIN 1 Clamp NSA5543-00 Item (10) Discard with 1 Screw NAS1096-3-5 Item (205) Discard 4 Between Frame 86 and Frame 87, remove: Refer to Fig. A-GBBAA Sheet 03, View E and Fig. A-GBBAA Sheet 04, View F. 2 Sleeve-Protective NSA5539S Item (13) Discard 1 Clamp NSA5543-00 Item (10) Retain with 1 Screw NAS1096-3-5 Item (205) Discard 5 From the sensing elements clamp at Frame 88, remove: Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 04, View G. 1 Screw NAS1096-3-5 Item (205) Discard

(23) Subtask 363038-831-204-001 - Remove the clamp from the overheat-detection dual loops at Frame 80 Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location Frame 80 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-GBCAA Removal of the Clamps and theAttaching Parts from the OverheatDetection Dual Loops at Frame 80 Sheet 01 Sheet 02 (a) Remove the clamp from the sensing elements 32HF and 357HF. Refer to Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02
. Refer to AMM Task 36-22-17-000-801. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 88 6

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# @A330 SERVICE BULLETIN
1 From Frame 80, remove: 2 Sleeve-Protective NSA5539S Item (13) Discard 1 Clamp NSA5543-00 Item (10) Discard with 1 Screw NAS1096-3-5 Item (205) Discard

(24) Subtask 363038-831-205-001 - Reroute the sensing elements 32HF and 357HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location Frame 80 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Kit 363038D12R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 2 SLEEVE 16 NSA5527-03-01 1 SPACER 86 NSA5538-00 2 CLAMP 207 NAS1802-3-13 1 SCREW References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBDAA Rerouting of the Sensing Elements 32HF and 357HF and Installation of Clamps Sheet 01 Sheet 02 Fig. A-GBHAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) Reroute the sensing elements 32HF and 357HF and install the clamps. Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02
. Refer to AMM Task 36-22-17-400-801.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 89 6

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# @A330 SERVICE BULLETIN
1 Reroute the sensing elements 32HF and 357HF at Frame 80 from parallel installation to on-top-of-each-other installation and install: 2 Sleeve-Protective NSA5539S Item 13 1 Spacer NSA5527-03-01 Item 16 2 Clamp NSA5538-00 Item 86 with 1 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. (25) Subtask 363038-831-206-001 - Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location from Frame 90 to Frame 91 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Kit 363038D01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 30 TIE 210 MS21919WCH14 1 CLAMP 211 F9237000207200 8 PLCRDSET References Fig. A-GBEAA Replacement of the Clamp between Frame 90 and Frame 91 Sheet 01 Sheet 02 Sheet 03 (a) Replace the clamp between Frame 90 and Frame 91. Refer to Fig. A-GBEAA Sheet 01 thru Fig. A-GBEAA Sheet 03
. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 90 6

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# @A330 SERVICE BULLETIN
1 Between Frame 90 and Frame 91, STGR6RH, remove the clamp: Refer to Fig. A-GBEAA Sheet 03, View C. 1 Clamp-Loop, Crs ABS0805-09 Item (214) Discard 2 Install the new clamp between Frame 90 and Frame 91, STGR6RH: Refer to Fig. A-GBEAA Sheet 03, View D. 1 Clamp MS21919WCH14 Item 210 3 Install the Service Bulletin placards along the harness routing of 5866VB/2S: 8 Placard Set F9237000207200 Item 211 and 30 Tie-Cable NSA935401-03 Item 169

(26) Subtask 363038-831-207-001 - Install the clamp and the new attaching parts on the overheat sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location from Frame 83 to Frame 88 Manpower Resources Manhours 1.00 Minimum number of person 2 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 363038D10R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 10 SLEEVE 16 NSA5527-03-01 4 SPACER 86 NSA5538-00 2 CLAMP 207 NAS1802-3-13 4 SCREW 208 NSA5527-03-04 2 SPACER 209 NAS1801-3-8 2 SCREW References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 91 6

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# @A330 SERVICE BULLETIN
References Fig. A-GBFAA Installation of the Clamp and the Attaching Parts in the Rear Fuselage Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-GBHAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) Install the clamp and the new attaching parts in the rear fuselage. Refer to Fig. A-GBFAA Sheet 01 thru Fig. A-GBFAA Sheet 05
. Refer to AMM Task 36-22-17-400-801. 1 Between Frame 83 and Frame 84, install: Refer to Fig. A-GBFAA Sheet 02
. 1 Clamp NSA5543-00 Item (10) Retained at removal 2 Sleeve-Protective NSA5539S Item 13 with 1 Spacer NSA5527-03-04 Item 208 1 Screw NAS1801-3-8 Item 209 NOTE: The torque value of the screw, Item 209, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. 2 Between Frame 84 and Frame 85, install: Refer to Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA Sheet 04, View F. 2 Clamp NSA5543-00 Item (10) Retained at removal 4 Sleeve-Protective NSA5539S Item 13 with 2 Spacer NSA5527-03-01 Item 16 2 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 92 6

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# @A330 SERVICE BULLETIN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. 3 Between Frame 85 and Frame 86, install: Refer to Fig. A-GBFAA Sheet 05, Views G and H. 2 Sleeve-Protective NSA5539S Item 13 2 Clamp NSA5538-00 Item 86 with 1 Spacer NSA5527-03-01 Item 16 1 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. 4 Between Frame 86 and Frame 87, install: Refer to Fig. A-GBFAA Sheet 04
. 1 Clamp NSA5543-00 Item (10) Retained at removal 2 Sleeve-Protective NSA5539S Item 13 with 1 Spacer NSA5527-03-01 Item 16 1 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. 5 On the sensing elements clamp at Frame 88, install: Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 05, View J. 1 Spacer NSA5527-03-04 Item 208 1 Screw NAS1801-3-8 Item 209 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 93 6

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# @A330 SERVICE BULLETIN NOTE: The torque value of the screw, Item 209, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. (27) Subtask 363038-831-209-001 - Install the sleeves on the APU bleed-air-duct Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Work location from Frame 83 to Frame 94 Manpower Resources Manhours 1.50 Minimum number of person 2 Subtask elapsed time 0.75 Skills AIRFRAME Material necessary to do the job Kit 363038D14R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 6 SLEEVE 200 F3617062404000 1 SLEEVE 201 F3617062403800 1 SLEEVE 202 F3617062403600 1 SLEEVE 203 F3617062403400 1 SLEEVE 204 F3617062403200 1 SLEEVE Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (Insulation Blanket Repair) 08-073 As required References Fig. A-GBGAA Installation of the Sleeves on the APU Bleed-Air-Duct Sheet 01 (a) Install the sleeves on the APU bleed-air-duct in the rear fuselage section. Refer to Fig. A-GBGAA Sheet 01
. 1 Install new sleeves on the sensing elements at Frame 83, Frame 88 and Frame 91: Refer to Fig. A-GBGAA Sheet 01, View B. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 94 6

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# @A330 SERVICE BULLETIN
6 Sleeve-Protective NSA5539S Item 13 2 Between Frame 83 thru Frame 94, install the sleeves on the APU bleed-airduct and close them with adhesive strips: 1 Sleeve Assy F3617062404000 Item 200 1 Sleeve Assy F3617062403800 Item 201 1 Sleeve Assy F3617062403600 Item 202 1 Sleeve Assy F3617062403400 Item 203 1 Sleeve Assy F3617062403200 Item 204 with Adhesive Tape (Insulation Blanket Repair) 08-073 As required
NOTE: Make sure that the blowout apertures of the blankets are near (under) the sensing elements. NOTE: Make sure that there is no contact between the sensing elements and the sleeves between Frame 86 and Frame 87. **CONF 002 (1) Subtask 363038-831-001-001 - Remove the sensing elements and the supports between FR39 and FR44 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 95 6

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# @A330 SERVICE BULLETIN (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 02, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 97HF 1 Sensing element 35610-2-255 Item (1) Discard FIN 98HF 1 Sensing element 35631-2-255 Item (2) Discard FIN 302HF 1 Sensing element 35610-2-255 Item (1) Discard FIN 303HF 1 Sensing element 35627-2-255 Item (11) Discard 2 Support Item (59) Discard 4 Rivet Item (45) Discard 2 Placard Item (23) Discard 1 Placard Item (24) Discard 2 Placard Item (29) Discard 1 Placard Item (30) Discard 4 Nut Item (57) Discard 14 Screw Item (76) Discard 32 Washer Item (46) Discard 64 Protective sleeve Item (56) Discard 23 Clamp Item (58) Discard 2 Screw Item (47) Discard 18 Clamp Item (82) Discard 9 Spacer Item (55) Discard 1 Screw Item (50) Discard 10 Spacer Item (53) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 96 6

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# @A330 SERVICE BULLETIN 5 Screw Item (52) Discard 4 Screw Item (52) Discard 6 Screw Item (48) Discard As required Wire-lock Item (100) Discard

(2) Subtask 363038-831-002-001 - Remove the sensing elements and the supports between FR44 and FR53.2 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 99HF 1 Sensing element 35618-2-255 Item (3) Discard FIN 100HF 1 Sensing element 35610-2-255 Item (1) Discard FIN 304HF 1 Sensing element 35616-2-255 Item (12) Discard FIN 305HF 1 Sensing element 35611-2-255 Item (13) Discard 2 Support Item (59) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 97 6

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# @A330 SERVICE BULLETIN 4 Rivet Item (45) Discard 1 Placard Item (25) Discard 2 Placard Item (26) Discard 1 Placard Item (27) Discard 1 Placard Item (30) Discard 2 Placard Item (31) Discard 2 Placard Item (32) Discard 1 Placard Item (33) Discard 4 Nut Item (57) Discard 1 Plate assy Item (41) Discard 8 Screw Item (76) Discard 30 Washer Item (46) Discard 56 Protective sleeve Item (56) Discard 18 Clamp Item (58) Discard 1 Screw Item (47) Discard 20 Clamp Item (82) Discard 10 Spacer Item (55) Discard 5 Screw Item (50) Discard 17 Spacer Item (53) Discard 12 Screw Item (52) Discard 3 Screw Item (48) Discard 1 Screw Item (49) Discard 1 Spacer Item (54) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 98 6

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# @A330 SERVICE BULLETIN
As required Wire-lock Item (100) Discard

(3) Subtask 363038-831-003-001 - Remove the sensing elements and the supports between FR53.2 and FR53.6 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 04, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 23HF 1 Sensing element 35569-2-255 Item (7) Discard FIN 101HF 1 Sensing element 35601-2-255 Item (5) Discard FIN 102HF 1 Sensing element 35601-2-255 Item (5) Discard FIN 306HF 1 Sensing element 35601-2-255 Item (5) Discard FIN 307HF 1 Sensing element 35600-2-255 Item (15) Discard FIN 308HF 1 Sensing element 35569-2-255 Item (7) Discard 3 Support Item (59) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 99 6

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# @A330 SERVICE BULLETIN 6 Rivet Item (45) Discard 2 Placard Item (20) Discard 1 Placard Item (27) Discard 2 Placard Item (28) Discard 1 Placard Item (33) Discard 2 Placard Item (34) Discard 2 Placard Item (35) Discard 6 Nut Item (57) Discard 1 Plate assy Item (40) Discard 11 Screw Item (76) Discard 38 Washer Item (46) Discard 74 Protective sleeve Item (56) Discard 29 Clamp Item (58) Discard 2 Screw Item (50) Discard 16 Clamp Item (82) Discard 8 Spacer Item (55) Discard 21 Spacer Item (53) Discard 19 Screw Item (52) Discard 6 Screw Item (48) Discard As required Wire-lock Item (100) Discard

(4) Subtask 363038-831-004-001 - Remove the sensing elements and the supports between FR53.6 and FR55 Work Zones and Access Panels Zone Access/Work location 190
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 100 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills NON SPECIFIC References Fig. A-FBAAA Installation of the New Sensing Elements between FR39 and FR55, on the LH Side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 (a) Remove : Refer to Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 05, Fig. A-FBAAA Sheet 06 and Fig. A-FBAAA Sheet 07 FIN 24HF 1 Sensing element 35593-3-255 Item (8) Discard FIN 25HF 1 Sensing element 35632-2-255 Item (9) Discard FIN 311HF 1 Sensing element 35579-2-255 Item (17) Discard FIN 312HF 1 Sensing element 35627-2-255 Item (11) Discard 1 Support Item (59) Discard 2 Rivet Item (45) Discard 1 Placard Item (21) Discard 1 Placard Item (22) Discard 1 Placard Item (36) Discard 1 Placard Item (37) Discard 2 Nut Item (57) Discard 1 Connector Item (61) Discard
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 101 6

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# @A330 SERVICE BULLETIN 14 Screw Item (76) Discard 27 Washer Item (46) Discard 54 Protective sleeve Item (56) Discard 21 Clamp Item (58) Discard 4 Screw Item (52) Discard 14 Spacer Item (53) Discard 2 Screw Item (51) Discard 12 Clamp Item (82) Discard 6 Spacer Item (55) Discard 4 Screw Item (48) Discard 3 Screw Item (77) Discard As required Wire-lock Item (100) Discard

(5) Subtask 363038-020-001-001 - If necessary, remove the ducts between FR35.5 and FR35.6 for access Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01
(a) Remove : Fig. A-FBBAA DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 102 6

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# @A330 SERVICE BULLETIN (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (112) Retain 1 Duct assy Item (113) Retain 1 Duct assy Item (114) Retain

(6) Subtask 363038-831-005-001 - Install a New Support for the Routing of the Sensing Elements between FR53.5 and FR53.6 Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 2 RIVET Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005 As required Corrosion Inhibiting Fillet Consistency 09-016 As required References Fig. A-FBCAA Installation of a New Bracket between FR53.5 and FR53.6 Sheet 01 Sheet 02

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 103 6

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# @A330 SERVICE BULLETIN (a) Move the insulation blanket to get access to the modification area. (b) Put the bracket Item 96 in position as shown on Fig. A-FBCAA
. (c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the bracket Item 96. Refer to Fig. A-FBCAA (d) Cut the insulation blanket to permit the installation of the bracket Item 96. NOTE: For the repair of the insulation blanket use : Adhesive Tape (insulation Blanket Repair) 08-073 As required (e) Re-identify the insulation blanket : 1 Blanket-Insulation F2581677800000 becomes : 1 Blanket-Insulation F0041196500000 or, 1 Blanket-Insulation F2581677900000 becomes : 1 Blanket-Insulation F0041196600000 (f) Install : Refer to Fig. A-FBCAA 1 Support F5392059300000 Item 96 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016 As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005 As required (g) Install the insulation blanket. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 104 6

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# @A330 SERVICE BULLETIN (7) Subtask 363038-420-001-001 - If removed, Install the Ducts between FR53.5 and FR53.6 Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01
(a) Install : Refer to Fig. A-FBBAA (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (113) Retained at removal 1 Duct assy Item (114) Retained at removal (8) Subtask 363038-020-002-001 - If necessary, Remove the Ducts between FR43 and FR45 for access Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 105 6

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# @A330 SERVICE BULLETIN
References Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01
(a) Remove : Refer to Fig. A-FBDAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (115) Retain 1 Duct assy Item (116) Retain

(9) Subtask 363038-831-006-001 - Install the new Brackets for the Routing of the Sensing Elements at FR44 Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 97 ASNA2050DCJ3215 2 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005 As required Corrosion Inhibiting Fillet Consistency 09-016 As required References Fig. A-FBKAA Installation of Two New Brackets at FR44 Sheet 01 Sheet 02
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 106 6

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# @A330 SERVICE BULLETIN (a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBKAA

. (b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) as shown on Fig. A-FBKAA
. (c) Install : 1 Support F0041178800000 Item 98 1 Support F0041178800100 Item 99 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005 As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016 As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005 As required (10) Subtask 363038-410-001-001 - If removed, install the ducts between FR43 and FR45 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01
(a) Install : (Refer to AMM Task 36-12-41-400-801) DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 107 6

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# @A330 SERVICE BULLETIN 1 Duct assy Item (115) Retained at removal 1 Duct assy Item (116) Retained at removal (11) Subtask 363038-831-007-001 - Install the Sensing Elements and the Supports between FR39 and FR44 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 30 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 62 SLEEVE 14 ASNA2397-10L 34 WASHER 15 NSA5542-00 4 NUT 16 NSA5527-03-01 8 SPACER 18 NSA5527-03-11 6 SPACER 20 NAS6603-1 19 BOLT 21 NAS6603-9 8 BOLT 24 NAS6603-15 6 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 2 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 70 F3611548300000 1 SUPPORT 71 F3611548800000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 1 SUPPORT 100 35606-2-255 1 SNSGELEM 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 108 6

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# @A330 SERVICE BULLETIN
References Fig. A-FBEAA Installation of the New Sensing Elements between FR39 and FR44 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR39 and FR40.2. 1 Install the supports between FR39 and FR40 : 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 8 Clamp NSA5543-00 Item 10 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-11 Item 18 8 Washer ASNA2397-10L Item 14 6 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-15 Item 24 2 Install the supports between FR40 and FR40.2 : 1 Support F3611549100000 Item 79 1 Support F3611549700000 Item 78 5 Clamp NSA5543-00 Item 10 1 Spacer NSA5527-03-01 Item 16 8 Washer ASNA2397-10L Item 14 1 Bolt NAS6603-9 Item 21 6 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-2 Item 29 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 109 6

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# @A330 SERVICE BULLETIN 3 Install the placards between FR39 and FR40.2 : 2 Placard F1131031621700 Item 32 2 Placard F1131031623700 Item 33 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 4 Install the sensing elements between FR39 and FR40.2 : FIN 97HF 1 Sensing Element 35606-2-255 Item 100 FIN 302HF 1 Sensing Element 35610-2-255 Item 113 28 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR40.2 and FR44. 1 Install the supports between FR40.2 and FR44 : 1 Support F3611548300000 Item 70 1 Support F3611548800000 Item 71 17 Clamp NSA5543-00 Item 10 4 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-01 Item 16 18 Washer ASNA2397-10L Item 14 13 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 4 Bolt NAS6603-15 Item 24 2 Install the sensing elements between FR40.2 and FR44 : FIN 98HF 1 Sensing Element 35620-2-255 Item 102
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 110 6

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# @A330 SERVICE BULLETIN
FIN 303HF 1 Sensing Element 35621-2-255 Item 101 34 Sleeve-Protective NSA5539S Item 13

(12) Subtask 363038-831-008-001 - Install the sensing elements and the supports between FR44 and FR50 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 50 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 29 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 58 SLEEVE 14 ASNA2397-10L 35 WASHER 15 NSA5542-00 8 NUT 16 NSA5527-03-01 10 SPACER 17 NSA5527-03-10 1 SPACER 18 NSA5527-03-11 5 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 13 BOLT 21 NAS6603-9 8 BOLT 23 NAS6603-16 3 BOLT 26 NAS6603-32 1 BOLT 29 NAS6603-2 8 BOLT 30 NSA5546-00 2 ANGLE 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 79 F3611549100000 4 SUPPORT 80 F3611549500000 1 SUPPORT DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 111 6

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 81 F3611549600000 1 SUPPORT 103 35618-2-255 2 SNSGELEM 105 35598-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM References Fig. A-FBFAA Installation of the New Sensing Elements between FR44 and FR50 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR44 and FR46 : 1 Install the supports between FR44 and FR46 : 1 Support F3611549600000 Item 81 17 Clamp NSA5543-00 Item 10 8 Spacer NSA5527-03-01 Item 16 5 Spacer NSA5527-03-11 Item 18 21 Washer ASNA2397-10L Item 14 2 Bolt NAS6603-24 Item 19 4 Bolt NAS6603-1 Item 20 6 Bolt NAS6603-9 Item 21 3 Bolt NAS6603-16 Item 23 2 Bolt NAS6603-2 Item 29 2 Install the placards at FR44 : 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 3 Install the sensing elements between FR44 and FR46 : FIN 99HF 1 Sensing Element 35618-2-255 Item 103 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 112 6

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# @A330 SERVICE BULLETIN
FIN 304HF 1 Sensing Element 35618-2-255 Item 103 34 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR46 and FR50. 1 Install the supports between FR46 and FR50 : 2 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 1 Support F3611549500000 Item 80 4 Support F3611549100000 Item 79 12 Clamp NSA5543-00 Item 10 2 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-10 Item 17 14 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-32 Item 26 6 Bolt NAS6603-2 Item 29 2 Install the placards between FR46 and FR50 : 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 2 Placard F1131031624000 Item 38 2 Placard F1131031622000 Item 39 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 113 6

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# @A330 SERVICE BULLETIN 3 Install the sensing elements between FR46 and FR50 : FIN 100HF 1 Sensing Element 35597-2-255 Item 114 FIN 305HF 1 Sensing Element 35598-2-255 Item 105 24 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (13) Subtask 363038-831-009-001 - Install the sensing elements and the supports between FR50 and FR53.6 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 50 to Frame 53.6 Manpower Resources Manhours 21.00 Minimum number of person 1 Subtask elapsed time 21.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 37 CLAMP 11 ASNA0342T04-01 6 BOLT 13 NSA5539S 74 SLEEVE 14 ASNA2397-10L 51 WASHER 15 NSA5542-00 6 NUT 16 NSA5527-03-01 16 SPACER 18 NSA5527-03-11 1 SPACER 20 NAS6603-1 23 BOLT 21 NAS6603-9 16 BOLT 22 NSA5527-03-15 1 SPACER 24 NAS6603-15 1 BOLT 25 NSA5545-00 1 ANGLE 28 NAS6603-12 1 BOLT 29 NAS6603-2 10 BOLT 30 NSA5546-00 2 ANGLE 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 114 6

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548600000 1 SUPPORT 79 F3611549100000 3 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 104 35567-3-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM References Fig. A-FBGAA Installation of the New Sensing Elements between FR50 and FR53.6 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR50 and FR53.2. 1 Install the supports between FR50 and FR53.2 : 1 Support F3611548700000 Item 72 1 Support F3611548400000 Item 75 1 Support F3611549400000 Item 82 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 13 Clamp NSA5543-00 Item 10 7 Spacer NSA5527-03-01 Item 16 16 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 115 6

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# @A330 SERVICE BULLETIN
7 Bolt NAS6603-9 Item 21 2 Install the placards between FR50 and FR53.2 : 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 3 Install the sensing elements between FR50 and FR53.2 : FIN 101HF 1 Sensing Element 35595-2-255 Item 106 FIN 102HF 1 Sensing Element 35595-2-255 Item 106 26 Sleeve-Protective NSA5539S Item 13 2 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR53.2 and FR53.6. 1 Install the supports between FR53.2 and FR53.6 : 1 Support F3611548300000 Item 70 1 Support F3611548500000 Item 73 1 Support F3611548900000 Item 74 1 Support F3611548200000 Item 76 1 Support F3611548600000 Item 77 3 Support F3611549100000 Item 79 1 Support F3611549800000 Item 83 1 Support F3611549300000 Item 84 1 Angle NSA5545-00 Item 25 1 Angle NSA5546-00 Item 30
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 116 6

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# @A330 SERVICE BULLETIN
4 Rivet-Blind ASNA0342T04-01 Item 11 24 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-15 Item 22 35 Washer ASNA2397-10L Item 14 14 Bolt NAS6603-1 Item 20 9 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-15 Item 24 1 Bolt NAS6603-12 Item 28 10 Bolt NAS6603-2 Item 29 2 Install the placards between FR53.2 and FR53.6 : 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 2 Placard F1131031620400 Item 44 2 Placard F1131031624300 Item 45 3 Install the sensing elements between FR53.2 and FR53.6 : FIN 102HF 1 Sensing Element 35595-2-255 Item 106 FIN 307HF 1 Sensing Element 35596-2-255 Item 107 FIN 23HF 1 Sensing Element 35568-4-255 Item 108 FIN 308HF 1 Sensing Element 35567-3-255 Item 104 48 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 117 6

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# @A330 SERVICE BULLETIN NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (14) Subtask 363038-831-010-001 - Install the sensing elements and the supports between FR53.6 and FR55 Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 363038A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 27 CLAMP 11 ASNA0342T04-01 2 BOLT 13 NSA5539S 55 SLEEVE 14 ASNA2397-10L 32 WASHER 15 NSA5542-00 2 NUT 16 NSA5527-03-01 6 SPACER 17 NSA5527-03-10 2 SPACER 18 NSA5527-03-11 5 SPACER 20 NAS6603-1 17 BOLT 21 NAS6603-9 1 BOLT 26 NAS6603-32 2 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 1 ANGLE 70 F3611548300000 1 SUPPORT 79 F3611549100000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200000 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 109 35597-3-255 1 SNSGELEM 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 118 6

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 112 35625-2-255 1 SNSGELEM References Fig. A-FBHAA Installation of the New Sensing Elements between FR53.6 and FR55 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR53.6 and FR55. 1 Install the supports between FR53.6 and FR55 : 1 Support F3611548300000 Item 70 1 Support F3611549100000 Item 79 1 Support F3611549200000 Item 93 1 Support F3611549000000 Item 95 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 27 Clamp NSA5543-00 Item 10 3 Clamp NSA5538-00 Item 86 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-10 Item 17 5 Spacer NSA5527-03-11 Item 18 32 Washer ASNA2397-10L Item 14 17 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-32 Item 26 2 Bolt NAS6603-2 Item 29 5 Bolt NAS6603-17 Item 87 5 Bolt NAS6603-10 Item 94 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 119 6

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# @A330 SERVICE BULLETIN
2 Install the placards between FR53.6 and FR55 : 1 Placard F1131031620500 Item 88 1 Placard F1131031624400 Item 89 1 Placard F1131031620600 Item 90 1 Placard F1131031624500 Item 91 3 Install the sensing elements between FR53.6 and FR55 : FIN 24HF 1 Sensing Element 35597-3-255 Item 109 FIN 311HF 1 Sensing Element 35587-2-255 Item 110 FIN 25HF 1 Sensing Element 35627-2-255 Item 111 FIN 312HF 1 Sensing Element 35625-2-255 Item 112 2 Nut NSA5542-00 Item 15 2 Connector NSA5549-90 Item 85 55 Sleeve-Protective NSA5539S Item 13 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (15) Subtask 363038-010-001-001 - If necessary, remove the ducts between FR39 and FR40 for access Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 120 6

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# @A330 SERVICE BULLETIN (a) Remove : Fig. A-FBPAA (Refer to AMM Task 21-20-00-010-801) 1 Duct assy Item (125) Retain 1 Duct assy Item (126) Retain 1 Duct assy Item (127) Retain

(16) Subtask 363038-831-011-001 - Modify the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills ELECTRICAL Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 1 WASHER 169 NSA935401-03 8 TIE 174 35301-74 1 CABLE 175 35301-75 1 CABLE F9000095228595 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-10 Service Bulletin (SB) A330-36-3032 Fig. A-FBJAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Fig. A-FWCAA Installation of the Wiring of the New Sensing Elements Sheet 01

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 121 6

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# @A330 SERVICE BULLETIN (a) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and Fig. A-FBJAA Sheet 02, remove without disconnection the FINs 137HF and 138HF and the FINs 309HF and 310HF attached with : 1 Screw Item (168) Retain 1 Washer Item (14) Discard 2 Clamp Item (155) Retain 1 Spacer Item (18) Retain (b) Modify the splice FIN 3503VS : 1 Before any disconnection, record the wires number associated to the FIN 137HF and the FIN 138HF. 2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF : FIN 3503VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3503VS and of the wires associated to the FIN 137HF and the FIN 138HF. 3 Remove : FIN 137HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard 4 Maintain in position : FIN 138HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) 5 Put in position : FIN 137HF 1 Cable-Electrical Interconnecting 35301-75 Item 175 6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN 137HF and the FIN 138HF, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3503VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 122 6

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# @A330 SERVICE BULLETIN identify the wires associated to the FINs 137HF and 138HF with the retained identification sleeves. (c) Modify the splice FIN 3593VS : NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation. 1 Before any disconnection, record the wires number associated to the FIN 309HF and the FIN 310HF. 2 Remove the splice FIN 3593VS between the FIN 309HF and the FIN 310HF : FIN 3593VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3593VS and of the wires associated to the FIN 309HF and the FIN 310HF. 3 Remove : FIN 309HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) Discard 4 Maintain in position : FIN 310HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) 5 Put in position : FIN 309HF 1 Cable-Electrical Interconnecting 35301-74 Item 174 6 Install the new splice FIN 3593VS (PN E0360RK1816) between the FIN 309HF and the FIN 310HF, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3593VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 309HF and 310HF with the retained identification sleeves.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 123 6

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# @A330 SERVICE BULLETIN (d) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBJAA Sheet 01 and Fig. A-FBJAA Sheet 02, install the FINs 137HF and 138HF and the FINs 309HF and 310HF (spliced previously) with : 1 Spacer Item (18) Retained at removal 2 Clamp Item (155) Retained at removal 1 Washer ASNA2397-10L Item 14 1 Screw Item (168) Retained at removal and attach it with : 8 Tie-Cable NSA935401-03 Item 169 NOTE: After connection, secure the FINs 137HF and 138HF and the FINs 309HF and 310HF with Wire-lock MS20995C32 Item 27, (Refer to Fig. A-FBJAA Sheet 03). (e) If necessary, secure the nuts (installed on the fuselage) and the FIN 138HF and the FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBJAA Sheet 03). (17) Subtask 363038-831-012-001 - Modify the existing Harness 2SG. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 10.00 Minimum number of person 1 Subtask elapsed time 5.00 Skills NON SPECIFIC Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 16 NSA5527-03-01 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 20 WASHER 141 NSA5527-03-02 2 SPACER 150 NSA935807-04 4 CLAMP 151 NSA5159-17 1 STUD 152 NSA5527-03-08 1 SPACER 153 NSA935808-01 8 WASHER DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 124 6

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# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 157 NSA5159-10 1 STUD 158 NAS1801-3-9 3 SCREW 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 174 35301-74 1 CABLE 175 35301-75 1 CABLE 176 NSA5516-21ND 5 CLAMP 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP F9000095228595 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-10 Service Bulletin (SB) A330-36-3032 Fig. A-FBMAA Modification of the Existing Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Fig. A-FWCAA Installation of the Wiring of the New Sensing Elements Sheet 01 (a) Modify the supports of existing routing between 302HF located on the left hand side at stringer 36 and Frame 40 and the 3520VP located on the right hand side at Frame 39.1 : NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation.
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 125 6

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# @A330 SERVICE BULLETIN
1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, remove : a For Section A-A : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (152) Retain 1 Clamp Item (150) Retain 1 Stud Item (151) Retain b For Section B-B : 6 Nut Item (154) Retain 6 Washer Item (153) Discard 6 Clamp Item (150) Retain 6 Spacer Item (152) Retain 6 Clamp Item (150) Retain 6 Stud Item (151) Retain c For Section C-C : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (155) Discard 1 Spacer Item (152) Retain 1 Clamp Item (155) Discard 1 Stud Item (151) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 126 6

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# @A330 SERVICE BULLETIN
2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, install : a For Section D-D : 1 Stud Item (151) Retained at removal 1 Clamp Item (150) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal b For Section E-E : 6 Stud Item (151) Retained at removal 6 Clamp Item (150) Retained at removal 6 Spacer Item (152) Retained at removal 6 Clamp Item (150) Retained at removal 6 Washer NSA935808-03 Item 131 6 Nut Item (154) Retained at removal c For Section F-F : 1 Stud Item (151) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Spacer Item (152) Retained at removal DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 127 6

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# @A330 SERVICE BULLETIN 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, remove : a For Section G-G : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (155) Discard 1 Spacer Item (152) Retain 1 Clamp Item (150) Retain 1 Stud Item (151) Retain b For Section H-H : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (155) Discard 1 Spacer Item (152) Retain 1 Clamp Item (155) Retain 1 Stud Item (151) Retain 4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 07 , Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, install : a For Section J-J : 1 Stud Item (151) Retained at removal
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 128 6

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# @A330 SERVICE BULLETIN 1 Clamp Item (150) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal b For Section K-K : 1 Stud Item (151) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, remove for detail F : 2 Nut Item (154) Retain 2 Washer Item (153) Discard 2 Clamp Item (150) Retain 2 Spacer Item (152) Retain 2 Clamp Item (135) Retain 2 Clamp Item (134) Retain 2 Stud Item (151) Retain

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 129 6

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# @A330 SERVICE BULLETIN 6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, install for detail G : 2 Stud Item (151) Retained at removal 2 Clamp Item (134) Retained at removal 2 Clamp Item (135) Retained at removal 2 Spacer Item (152) Retained at removal 2 Clamp Item (150) Retained at removal 2 Washer NSA935808-03 Item 131 2 Nut Item (154) Retained at removal 7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section L-L : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Clamp Item (138) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain b For Section M-M : 1 Nut Item (154) Retain 1 Washer Item (153) Discard DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 130 6

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# @A330 SERVICE BULLETIN 1 Clamp Item (150) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain 8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section N-N : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal b For Section P-P : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 131 6

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# @A330 SERVICE BULLETIN 1 Spacer Item (152) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 46 and 48, remove for section Q-Q : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (16) Discard 1 Clamp Item (139) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (157) Discard 10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 12 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 46 and 48, install for Section R-R : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 132 6

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# @A330 SERVICE BULLETIN 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 49 and 52, remove for detail K : 2 Nut Item (154) Retain 2 Washer Item (153) Discard 2 Clamp Item (150) Retain 2 Spacer Item (152) Retain 2 Clamp Item (138) Retain 2 Stud Item (151) Retain 12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 13, along the Frame 39.1 and between Stringers 49 and 52, install for detail L : 2 Stud Item (151) Retained at removal 2 Clamp Item (138) Retained at removal 2 Spacer Item (152) Retained at removal 2 Clamp Item (150) Retained at removal 2 Washer NSA935808-03 Item 131 2 Nut Item (154) Retained at removal 13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 52 and 54, remove for Section S-S : 1 Nut Item (154) Retain
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 133 6

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# @A330 SERVICE BULLETIN 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Clamp Item (138) Retain 1 Spacer Item (141) Retain 1 Clamp Item (138) Retain 1 Stud Item (140) Retain 14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 52 and 54, install for Section T-T : 1 Stud Item (140) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (141) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 15 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the Stringers 54, remove for detail N : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (152) Retain 1 Clamp Item (138) Retain
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 134 6

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# @A330 SERVICE BULLETIN 1 Stud Item (151) Retain 16 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and near the Stringers 54, install for detail P : 1 Stud Item (151) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal 17 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 54 and 48, remove for detail Q : 3 Screw Item (167) Discard 3 Washer Item (153) Discard 3 Clamp Item (138) Retain 3 Clamp Item (150) Retain 18 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 54 and 48, install for detail R : 3 Clamp Item (150) Retained at removal 3 Clamp Item (138) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-9 Item 158

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 135 6

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# @A330 SERVICE BULLETIN 19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, remove : a For Section U-U : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Discard 1 Spacer Item (18) Discard 1 Clamp Item (134) Discard 1 Stud Item (151) Discard b For Section V-V : 1 Screw Item (183) Discard 1 Washer Item (153) Discard 1 Clamp Item (184) Discard 1 Spacer Item (141) Discard 1 Clamp Item (184) Discard 20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 16 and Fig. A-FBMAA Sheet 17, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section W-W : 2 Spacer NSA5527-03-02 Item 141 2 Clamp NSA5516-07ND Item 179 or 2 Clamp NSA5516-08ND Item 180 or 2 Clamp NSA5516-10ND Item 181 and 2 Washer NAS1149F0332P Item 172 2 Screw NAS1801-3-17 Item 171 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 136 6

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# @A330 SERVICE BULLETIN NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND or NSA5516-08ND or NSA5516-10ND. 21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail Y : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (150) Retain 1 Spacer Item (165) Discard 1 Spacer Item (152) Retain 1 Clamp Item (155) Retain 1 Clamp Item (155) Retain 1 Stud Item (163) Retain 22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail Z : 1 Stud Item (163) Retained at removal 1 Clamp Item (155) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer Item (152) Retained at removal 1 Spacer NSA5527-03-15 Item 22 1 Clamp Item (150) Retained at removal 1 Washer NSA935808-03 Item 131 1 Nut Item (154) Retained at removal

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 137 6

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# @A330 SERVICE BULLETIN 23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, remove for detail W : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (18) Discard 1 Clamp Item (134) Discard 1 Stud Item (151) Discard 24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, install for detail X: 1 Stud NSA5159-10 Item 157 1 Clamp NSA5516-21ND Item 176 or 1 Clamp NSA5516-22ND Item 177 or 1 Clamp NSA5516-23ND Item 178 and 1 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-08 Item 152 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut Item (154) Retained at removal NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 138 6

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# @A330 SERVICE BULLETIN 25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, remove for detail AA : 1 Nut Item (154) Retain 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (18) Retain 1 Clamp Item (134) Discard 1 Stud Item (151) Retain 26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, install for detail AB : 1 Stud Item (151) Retained at removal 1 Clamp NSA5516-21ND Item 176 or 1 Clamp NSA5516-22ND Item 177 or 1 Clamp NSA5516-23ND Item 178 and 1 Spacer Item (18) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut Item (154) Retained at removal NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 139 6

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# @A330 SERVICE BULLETIN
27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, remove for detail AC : 3 Screw Item (167) Retain 3 Washer Item (153) Discard 3 Clamp Item (135) Retain 3 Clamp Item (134) Discard 28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, install for detail AD : 3 Clamp NSA5516-21ND Item 176 or 3 Clamp NSA5516-22ND Item 177 or 3 Clamp NSA5516-23ND Item 178 and 3 Clamp Item (135) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw Item (167) Retained at removal NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND. (b) Modify the existing route 2SG between FIN 302HF located on the left hand side at stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment : NOTE: Apply the following modifications only if the Service Bulletin No. A330-36-3032 and the associated Technical Adaptation were applied. The following modification consists to restore the aircraft to the configuration before Service Bulletin No. A330-36-3032 and associated Technical Adaptation. 1 Modify the Interconnecting Electrical Wire FIN 301HF (Only if aircraft is equipped with FIN 301HF PN 35301-75) : Refer to ESPM 20-43-10 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 140 6

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# @A330 SERVICE BULLETIN

a Before any disconnection, record the wires number associated to the FIN 301HF. b Remove the splice FIN 3591VS between the FIN 301HF and the wire No. 3622-0540 : FIN 3591VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3591VS and of the wires associated to the FIN 301HF. c Remove : FIN 301HF 1 Cable-Electrical Interconnecting 35301-75 Item (175) Discard d Install : 1 Cable-Electrical Interconnecting 35301-74 Item 174
e Install the new splice FIN 3591VS (PN NSA936809RG0002) between the FIN 301HF and the wire No. 3622-0540, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3591VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 301HF with the retained identification sleeves. NOTE: After connection, Secure the FIN 301HF and FIN 302HF with Wire-lock MS20995C41 item 133. 2 Modify the Interconnecting Electrical Wire FIN 22HF (If aircraft is equipped with FIN 22HF PN 35301-74) : a Before any disconnection, record the wires number associated to the FIN 22HF. b Remove the splice FIN 3501VS between the FIN 22HF and the wire No. 3622-0082 : FIN 3501VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3501VS and of the wires associated to the FIN 22HF. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 141 6

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# @A330 SERVICE BULLETIN

c Remove : FIN 22HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard d Install : 1 Cable-Electrical Interconnecting 35301-75 Item 175
e Install the new splice FIN 3501VS (PN NSA936809RG0002) between the FIN 22HF and the wire No. 3622-0082, supplied in : Bundle F9000095228595 NOTE: Identify the splice FIN 3501VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 22HF with the retained identification sleeves. NOTE: After connection, Secure the FIN 22HF and FIN 97HF with Wire-lock MS20995C41 item 133. (18) Subtask 363038-831-013-001 - Modify the Wiring between the Avionics Compartment and the Cargo Compartment. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES F9000095228595 BUNDLE References Service Bulletin (SB) A330-36-3032

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 142 6

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# @A330 SERVICE BULLETIN
References Fig. A-FBMAA Modification of the Existing Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Fig. A-FWBAA Modification of the Wiring between the Cargo Compartment and the Avionics Compartment Sheet 01

NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation. (a) Modify the connection of the wire No. 3622-0542 as shown on the wiring diagram, Fig. A-FWBAA Sheet 01
. NOTE: If necessary use contact PN EN3155-003F2222 supplied in : Bundle F9000095228595 (19) Subtask 363038-831-014-001 - Modify the Wiring in the Main rack 800VU. Work Zones and Access Panels Zone Access/Work location 120 Work location Electrical panel 800VU Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills ELECTRICAL

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 143 6

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363038A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 200 TIE F9000095228595 BUNDLE NSA935401-06 200 TIE NSA935401-13 200 TIE References Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802 Task 36-11-34-400-802 Service Bulletin (SB) A330-36-3032 Fig. A-FWAAA Modification of the Wiring in the Main Rack 800VU Sheet 01 Fig. A-FHAAA Hook-Up Chart of the Modification of the Wiring in the Main Rack 800VU Sheet 01
NOTE: Apply the following modifications only if were not applied with the embodiment of the Service Bulletin No. A330-36-3032 or the associated Technical Adaptation. (a) Remove and retain the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-000-802). (b) Remove the wire as shown on the wiring diagram Fig. A-FWAAA Sheet 01, and as given in the Hook-up Chart line : - 1 (Refer to Fig. A-FHAAA Sheet 01). (c) Install the wires as shown on the wiring diagram Fig. A-FWAAA Sheet 01 and as given in the Hook-up Chart lines : - 4 thru 5 (Refer to Fig. A-FHAAA Sheet 01) supplied in : Bundle F9000095228595 (d) Attach the wires with : 200 Tie-Cable NSA935401-03 Item 169 200 Tie-Cable NSA935401-06 200 Tie-Cable NSA935401-13 (e) Install the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 144 6

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# @A330 SERVICE BULLETIN (20) Subtask 363038-831-015-001 - If removed, install the ducts between FR39 and FR40. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01 (a) Install : Refer to Fig. A-FBPAA (Refer to AMM Task 21-20-00-410-801) 1 Duct assy Item (125) Retained at removal 1 Duct assy Item (126) Retained at removal 1 Duct assy Item (127) Retained at removal (21) Subtask 363038-831-201-001 - Remove the sleeves from the Auxiliary Power Unit (APU) bleed-air-duct Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Work location from Frame 83 to Frame 93 Manpower Resources Manhours 1.25 Minimum number of person 2 Subtask elapsed time 0.75 Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 145 6

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# @A330 SERVICE BULLETIN
References Fig. A-GBAAA Removal of the Sleeves from the APU Bleed-Air-Duct Sheet 01 (a) Remove the sleeves from the APU bleed-air-duct in the rear fuselage section. Refer to Fig. A-GBAAA Sheet 01
. 1 Between Frame 83 and Frame 93 remove the sleeves: 1 Sleeve Assy F3617062402000 Item (200) Discard 1 Sleeve Assy F3617062402400 Item (201) Discard 1 Sleeve Assy F3617062402600 Item (202) Discard 1 Sleeve Assy F3617062402800 Item (203) Discard 1 Sleeve Assy F3617062403000 Item (204) Discard

(22) Subtask 363038-831-203-001 - Remove the clamps and the attaching parts from the overheat sensing elements Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location from Frame 83 to Frame 88 Manpower Resources Manhours 1.25 Minimum number of person 2 Subtask elapsed time 0.75 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-GBBAB Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the clamps and the attaching parts in the rear fuselage. Refer to Fig. A-GBBAB Sheet 01 thru Fig. A-GBBAB Sheet 04
. Refer to AMM Task 36-22-17-000-801.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 146 6

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# @A330 SERVICE BULLETIN
1 Between Frame 83 and Frame 84, remove: Refer to Fig. A-GBBAB Sheet 02, View B and Fig. A-GBBAB Sheet 04, View F. 4 Sleeve-Protective NSA5539S Item (13) Discard 2 Clamp NSA5543-00 Item (10) Retain with 2 Screw NAS1096-3-5 Item (205) Discard 2 Between Frame 84 and Frame 85, remove: Refer to Fig. A-GBBAB Sheet 02, View C and Fig. A-GBBAB Sheet 04, View F. 4 Sleeve-Protective NSA5539S Item (13) Discard 2 Clamp NSA5543-00 Item (10) Retain with 2 Screw NAS1096-3-5 Item (205) Discard 3 Between Frame 85 and Frame 86, remove: Refer to Fig. A-GBBAB Sheet 03, View D and Fig. A-GBBAB Sheet 04, View F. 2 Sleeve-Protective NSA5539S Item (13) Discard 1 Clamp NSA5543-00 Item (10) Discard with 1 Screw NAS1096-3-5 Item (205) Discard 4 Between Frame 86 and Frame 87, remove: Refer to Fig. A-GBBAB Sheet 03, View E and Fig. A-GBBAB Sheet 04, View F. 2 Sleeve-Protective NSA5539S Item (13) Discard 1 Clamp NSA5543-00 Item (10) Retain with 1 Screw NAS1096-3-5 Item (205) Discard

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 147 6

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# @A330 SERVICE BULLETIN 5 From the sensing elements clamp at Frame 88, remove: Refer to Fig. A-GBBAB Sheet 01 and Fig. A-GBBAB Sheet 04, View G. 1 Screw NAS1096-3-5 Item (205) Discard

(23) Subtask 363038-831-204-001 - Remove the clamp from the overheat-detection dual loops at Frame 80 Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location Frame 80 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-GBCAA Removal of the Clamps and theAttaching Parts from the OverheatDetection Dual Loops at Frame 80 Sheet 01 Sheet 02 (a) Remove the clamp from the sensing elements 32HF and 357HF. Refer to Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02
. Refer to AMM Task 36-22-17-000-801. 1 From Frame 80, remove: 2 Sleeve-Protective NSA5539S Item (13) Discard 1 Clamp NSA5543-00 Item (10) Discard with 1 Screw NAS1096-3-5 Item (205) Discard

(24) Subtask 363038-831-205-001 - Reroute the sensing elements 32HF and 357HF Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location Frame 80

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 148 6

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Kit 363038D12R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 2 SLEEVE 16 NSA5527-03-01 1 SPACER 86 NSA5538-00 2 CLAMP 207 NAS1802-3-13 1 SCREW References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBDAA Rerouting of the Sensing Elements 32HF and 357HF and Installation of Clamps Sheet 01 Sheet 02 Fig. A-GBHAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) Reroute the sensing elements 32HF and 357HF and install the clamps. Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02
. Refer to AMM Task 36-22-17-400-801. 1 Reroute the sensing elements 32HF and 357HF at Frame 80 from parallel installation to on-top-of-each-other installation and install: 2 Sleeve-Protective NSA5539S Item 13 1 Spacer NSA5527-03-01 Item 16 2 Clamp NSA5538-00 Item 86 with 1 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 149 6

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# @A330 SERVICE BULLETIN (25) Subtask 363038-831-206-001 - Replace the clamp of the electrical harness 5866VB/2S in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location from Frame 90 to Frame 91 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Kit 363038D01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 30 TIE 210 MS21919WCH14 1 CLAMP 211 F9237000207200 8 PLCRDSET References Fig. A-GBEAA Replacement of the Clamp between Frame 90 and Frame 91 Sheet 01 Sheet 02 Sheet 03 (a) Replace the clamp between Frame 90 and Frame 91. Refer to Fig. A-GBEAA Sheet 01 thru Fig. A-GBEAA Sheet 03
. 1 Between Frame 90 and Frame 91, STGR6RH, remove the clamp: Refer to Fig. A-GBEAA Sheet 03, View C. 1 Clamp-Loop, Crs ABS0805-09 Item (214) Discard 2 Install the new clamp between Frame 90 and Frame 91, STGR6RH: Refer to Fig. A-GBEAA Sheet 03, View D. 1 Clamp MS21919WCH14 Item 210 3 Install the Service Bulletin placards along the harness routing of 5866VB/2S: 8 Placard Set F9237000207200 Item 211 and 30 Tie-Cable NSA935401-03 Item 169 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 150 6

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# @A330 SERVICE BULLETIN (26) Subtask 363038-831-208-001 - Install the clamps and the new attaching parts on the overheat sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Access Door 312AR Work location from Frame 83 to Frame 88 Manpower Resources Manhours 1.25 Minimum number of person 2 Subtask elapsed time 0.75 Skills AIRFRAME Material necessary to do the job Kit 363038D11R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 12 SLEEVE 16 NSA5527-03-01 4 SPACER 86 NSA5538-00 2 CLAMP 207 NAS1802-3-13 4 SCREW 208 NSA5527-03-04 3 SPACER 209 NAS1801-3-8 3 SCREW References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBFAB Installation of the Clamp and the Attaching Parts in the Rear Fuselage Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-GBHAA Tolerances for Waviness and Bends in Sensing Elements Sheet 01 Sheet 02 (a) Install the clamps and the new attaching parts in the rear fuselage. Refer to Fig. A-GBFAB Sheet 01 and Fig. A-GBFAB Sheet 05
. Refer to AMM Task 36-22-17-400-801. 1 Between Frame 83 and Frame 84, install: Refer to Fig. A-GBFAB Sheet 02, Views B and C. 2 Clamp NSA5543-00 Item (10) Retained at removal
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 151 6

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# @A330 SERVICE BULLETIN
4 Sleeve-Protective NSA5539S Item 13 with 2 Spacer NSA5527-03-04 Item 208 2 Screw NAS1801-3-8 Item 209 NOTE: The torque value of the screw, Item 209, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. 2 Between Frame 84 and Frame 85, install: Refer to Fig. A-GBFAB Sheet 03 and Fig. A-GBFAB Sheet 04, View F. 2 Clamp NSA5543-00 Item (10) Retained at removal 4 Sleeve-Protective NSA5539S Item 13 with 2 Spacer NSA5527-03-01 Item 16 2 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. 3 Between Frame 85 and Frame 86, install: Refer to Fig. A-GBFAB Sheet 05, Views G and H. 2 Sleeve-Protective NSA5539S Item 13 2 Clamp NSA5538-00 Item 86 with 1 Spacer NSA5527-03-01 Item 16 1 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 152 6

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# @A330 SERVICE BULLETIN wires, refer to Fig. A-GBHAA
. 4 Between Frame 86 and Frame 87, install: Refer to Fig. A-GBFAB Sheet 04, View E and F. 1 Clamp NSA5543-00 Item (10) Retained at removal 2 Sleeve-Protective NSA5539S Item 13 with 1 Spacer NSA5527-03-01 Item 16 1 Screw NAS1802-3-13 Item 207 NOTE: The torque value of the screw, Item 207, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. 5 On the sensing elements clamp at Frame 88, install: Refer to Fig. A-GBFAB Sheet 01 and Fig. A-GBFAB Sheet 05, View J. 1 Spacer NSA5527-03-04 Item 208 1 Screw NAS1801-3-8 Item 209 NOTE: The torque value of the screw, Item 209, is 0.25m.daN (22.00lbf.in). NOTE: For tolerances for waviness and bends in sensing element wires, refer to Fig. A-GBHAA
. (27) Subtask 363038-831-209-001 - Install the sleeves on the APU bleed-air-duct Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Work location from Frame 83 to Frame 94 Manpower Resources Manhours 1.50 Minimum number of person 2 Subtask elapsed time 0.75 Skills AIRFRAME

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 153 6

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# @A330 SERVICE BULLETIN Material necessary to do the job Kit 363038D14R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 6 SLEEVE 200 F3617062404000 1 SLEEVE 201 F3617062403800 1 SLEEVE 202 F3617062403600 1 SLEEVE 203 F3617062403400 1 SLEEVE 204 F3617062403200 1 SLEEVE Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (Insulation Blanket Repair) 08-073 As required References Fig. A-GBGAA Installation of the Sleeves on the APU Bleed-Air-Duct Sheet 01 (a) Install the sleeves on the APU bleed-air-duct in the rear fuselage section. Refer to Fig. A-GBGAA Sheet 01
. 1 Install new sleeves on the sensing elements at Frame 83, Frame 88 and Frame 91: Refer to Fig. A-GBGAA Sheet 01, View B. 6 Sleeve-Protective NSA5539S Item 13 2 Between Frame 83 thru Frame 94, install the sleeves on the APU bleed-airduct and close them with adhesive strips: 1 Sleeve Assy F3617062404000 Item 200 1 Sleeve Assy F3617062403800 Item 201 1 Sleeve Assy F3617062403600 Item 202 1 Sleeve Assy F3617062403400 Item 203 1 Sleeve Assy F3617062403200 Item 204 with

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 154 6

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# @A330 SERVICE BULLETIN Adhesive Tape (Insulation Blanket Repair) 08-073 As required
NOTE: Make sure that the blowout apertures of the blankets are near (under) the sensing elements. NOTE: Make sure that there is no contact between the sensing elements and the sleeves between Frame 86 and Frame 87. **CONF ALL D. TEST **CONF 001 (1) Subtask 363038-861-001-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 (a) In the cockpit, on the panel 235VU, push these pushbutton switches : - BAT 1, BAT 2, APU BAT, - GEN 1, GEN 2, APU GEN, - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801). (d) Remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S

(2) Subtask 363038-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 155 6

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# @A330 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 25-75-41-400-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Task 36-11-34-400-802 Task 36-12-00-710-801 Task 36-12-41-400-801 Task 36-22-00-710-806 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Preliminary Tests : NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). 1 On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. NOTE: The Functional test and/or operational test requested by this ESPM procedure is given hereafter. 2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to AMM Task 33-13-00-710-801). 3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801). 4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer to AMM Task 21-26-00-710-803). 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803). 7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task 31-50-00-740-801). 8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to AMM Task 31-60-00-710-802).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 156 6

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# @A330 SERVICE BULLETIN (b) Test of the equipments : 1 If applicable, do the test procedure as specified after the installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). 2 If ducts removed, do the test procedure as specified after the installation of the APU bleed air ducts (Refer to AMM Task 36-12-41-400-801). 3 If ducts removed, do the test procedure as specified after the installation of the air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801). 4 Do the Operational Test of the APU bleed-air supply and crossbleed system (Refer to AMM Task 36-12-00-710-801). 5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802). (c) Test of the connectors : 1 Test of the connectors 3506VC and 3672VC : a Do the Operational Test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). 2 Test of the Terminal Block 2901VT : a None (Covered by the tests of the equipments) (3) Subtask 363038-710-201-001 - Operational Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806 (a) Do the operational test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). **CONF 002 (1) Subtask 363038-861-001-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 157 6

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# @A330 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 (a) In the cockpit, on the panel 235VU, push these pushbutton switches : - BAT 1, BAT 2, APU BAT, - GEN 1, GEN 2, APU GEN, - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801). (d) Remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S

(2) Subtask 363038-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 25-75-41-400-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Task 36-11-34-400-802 Task 36-12-00-710-801 Task 36-12-41-400-801 Task 36-22-00-710-806 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Preliminary Tests : NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). 1 On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 158 6

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# @A330 SERVICE BULLETIN NOTE: The Functional test and/or operational test requested by this ESPM procedure is given hereafter. 2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to AMM Task 33-13-00-710-801). 3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801). 4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer to AMM Task 21-26-00-710-803). 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803). 7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task 31-50-00-740-801). 8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to AMM Task 31-60-00-710-802). (b) Test of the equipments : 1 If applicable, do the test procedure as specified after the installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). 2 If ducts removed, do the test procedure as specified after the installation of the APU bleed air ducts (Refer to AMM Task 36-12-41-400-801). 3 If ducts removed, do the test procedure as specified after the installation of the air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801). 4 Do the Operational Test of the APU bleed-air supply and crossbleed system (Refer to AMM Task 36-12-00-710-801). 5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802). (c) Test of the connectors : 1 Test of the connectors 3506VC and 3672VC : a Do the Operational Test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). 2 Test of the Terminal Block 2901VT : a None (Covered by the tests of the equipments)

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 159 6

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# @A330 SERVICE BULLETIN (3) Subtask 363038-710-201-001 - Operational Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 36-22-00-710-806 (a) Do the operational test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 363038-410-002-001 - Install/Close Items Removed/Opened for access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-75-41-400-801 Task 53-00-00-400-802 Task 53-35-11-400-801 Task 53-35-13-400-801 Task 53-35-13-400-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-400-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).
DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 160 6

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# @A330 SERVICE BULLETIN (e) At Frame 20 in the FWD cargo-compartment, install the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (h) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (i) On the LH side of the belly fairing, install (if removed) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802) (j) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802). (k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). (2) Subtask 363038-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 36-11-34-400-802 Task 36-22-17-400-801 Task 36-22-17-400-802 Task 52-10-00-410-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 161 6

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# @A330 SERVICE BULLETIN (d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801). (e) Do the close-up procedure as specified in the installation of the sensing elements (Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802). (f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802). (g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). (i) Restore the systems and the aircraft to normal operating conditions. (3) Subtask 363038-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (b) Release and close the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). (c) Remove the access platform(s). **CONF 002 (1) Subtask 363038-410-002-001 - Install/Close Items Removed/Opened for access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-75-41-400-801 Task 53-00-00-400-802 Task 53-35-11-400-801 Task 53-35-13-400-801 Task 53-35-13-400-802

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 162 6

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# @A330 SERVICE BULLETIN (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-400-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (e) At Frame 20 in the FWD cargo-compartment, install the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (f) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).(g) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (h) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (i) On the LH side of the belly fairing, install (if removed) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802) (j) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802). (k) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). (2) Subtask 363038-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 163 6

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# @A330 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 36-11-34-400-802 Task 36-22-17-400-801 Task 36-22-17-400-802 Task 52-10-00-410-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801). (e) Do the close-up procedure as specified in the installation of the sensing elements (Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802). (f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1 and 1HA2) (Refer to AMM Task 36-11-34-400-802). (g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). (i) Restore the systems and the aircraft to normal operating conditions. (3) Subtask 363038-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 310 Access Door 313AL, Door 312AR Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001 (a) Release and close the maintenance door 312AR (Refer to AMM 52-41-00, Page Block 001). (b) Release and close the accessory-compartment access door 313AL (Refer to AMM 52-41-00, Page Block 001). DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 164 6

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# @A330 SERVICE BULLETIN (c) Remove the access platform(s).

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 165 6

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# @A330 SERVICE BULLETIN

**CONF ALL



### B **A**

FR39 FR45 FR53.5 FR56

(1) (2)

97HF 98HF (9) (8)
25HF 24HF (3) (1) 99HF 100HF (5) (5) 102HF
101HF

(7) 23HF Z190 

## AFTER

**A** (1) (7) (11) (11) (17) (12) (13) (5) (15)

G_SB_363038_5_BAAA_01_00 302HF 303HF 304HF 305HF 306HF 307HF 311HF
312HF

308HF 

### C **W B B** 

Figure A-FBAAA - Sheet 01 Installation of the New Sensing Elements between FR39 and FR55, on the LH Side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 166 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

BELLY FAIRING TRACE FUSELAGE TRACE

G_SB_363038_5_BAAA_02_00 (11)

(1) (1)

97HF 302HF (2) 98HF 303HF FR43

FR42
FR41

FR44 FR43
FR42
FR41
FR40.3 FR40.2

FR40 FR40.1 FR40.3
FR40.2

FR40.1
FR40 (45)

(45) (24) (30) (29)

(23)

(59) (23) (29)

(45) 

## B **E D** 



## D

**E J** 

**J F**  **G H** 

**J F**  **F**

**L**

**K F**  **F**

**K**

**K K** (59)



### K K

Figure A-FBAAA - Sheet 02 Installation of the New Sensing Elements between FR39 and FR55, on the LH Side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 167 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR51 FR50
FR49
FR48
FR47
FR46

FR45 FR48 FR47 FR46 FR45

BELLY FAIRING TRACE FUSELAGE TRACE

(46) (76) (46) (76) (46) (52) (56) (56) (53) (58) (30) (31) (32)

(26) (59)

(25) (31)

(45) (45)

(45) (32) (26) (27)

(33) (59)

G_SB_363038_5_BAAA_03_00 (12) (3) (13)

(1) 100HF 305HF

99HF

304HF 

## C **J N**  **R**
**G S** 

**U J**  **F**

**T**

**H F**  **M J** 

**V**

**V J**  **S**

**J J**  

## M

**N**

**P Q**  41



## R **K K**

**K K H** 

**Q P** 

Figure A-FBAAA - Sheet 03 Installation of the New Sensing Elements between FR39 and FR55, on the LH Side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 168 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

G_SB_363038_5_BAAA_04_00 (5) (5) (5) (15) (7) (7) 23HF 308HF
307HF

102HF

101HF 306HF FR53.6 FR53.5 FR53.4 FR53.3
FR53.2 FR53.1 FR53 FR52 FR51 FR53.5 FR53.4 FR53.3
FR53.2
FR53.1

FR53
FR52 FUSELAGE TRACE

BELLY FAIRING TRACE

(56) (58) (56) (46) (76) (56) (40)

(46) (50) (46) (76) (82) (20) (35) (45) (45) (59) (34)

(20) (35) (45)

(45) (59) (45) (27)
(33) (45) (34) (28) (59)

(28)



## W **X**

**Y**

**Z A A**  **X A A**  **Y**

**Z F**  **K J**  **J F**  **H**

**J F** 
**F J**  **J K K** 

**K K K**  **J**

(53)
Figure A-FBAAA - Sheet 04 Installation of the New Sensing Elements between FR39 and FR55, on the LH Side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 169 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

55° 55°
FR53.6 FR53.5
(17) (8) (9) (11)

(61) (100) (100) (22)

(37) (45)

(45) (36) (21) (59) FR55

FR54

FR53.9

FR53.8

FR53.7

FR53.6 311HF 24HF 25HF 312HF



### B **B A**  **A**

G_SB_363038_5_BAAA_05_00 

## B B **C C**

**D D A**  **A B**  **B C C**  **D D E E** 

**G G F** 
**F J J**  **G G J** 
**F J** 
**F F F** 

**K K H**  **H**

Figure A-FBAAA - Sheet 05 Installation of the New Sensing Elements between FR39 and FR55, on the LH Side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 170 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

G_SB_363038_5_BAAA_06_00 (56)
(56) (58) (46) (76) (56) (82) (55) (56) (82) (46) (47) (53)

(55) (56) (82)

(56) (82) (46) (50) (53) (56)
(56) (58) (46) (52) (55) (56) (82)

(46) (48) (56) (82)

(56) (82) (46) (48) (55)
(55) (46) (48) (56) (82) (56) (82)

(46) (50) (55) (53) (56) (82) (55)

(46) (48) (56) (82) (46) (50) (55) (53) (54) (55) (46) (49) (56) (82) 

## F **G H**  **J K** 

**L V**  **S T**  **U**

Figure A-FBAAA - Sheet 06 Installation of the New Sensing Elements between FR39 and FR55, on the LH Side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 171 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



## OR (53) (55) (46) (51) (56) (82) (55) (56) (82) (53)

(46) (51) (56) (82) (55) (46) (48)

(57)

(57) (100) (100) (100)

(57) (57) (56) (82)
(56) (82) (55) (46) (48)

(53) (56) (56) (58) (46) (77) (56) (46) (76)

(56) (58) (56) (58) (46) (76)



## H H **E E F F**  **G G**

**K K J J** 

G_SB_363038_5_BAAA_07_00 Figure A-FBAAA - Sheet 07 Installation of the New Sensing Elements between FR39 and FR55, on the LH Side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 172 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A



## B (113)

(112)

(114) FR53.5 FR53.6



## A Z150



### B

G_SB_363038_5_BBAA_01_00 Figure A-FBBAA - Sheet 01 Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 173 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A Z150 FR53.3 FR54

FR53.5 FR53.6 96 

### C **B**

**FWD**



## B **A**

STGR32

STGR33

STGR34

STGR35 STGR36

G_SB_363038_5_BCAA_01_00 Figure A-FBCAA - Sheet 01 Installation of a New Bracket between FR53.5 and FR53.6 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 174 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR53.5

197 mm (7.75 in)

96

FR53.6 

### D
**F W**  **D**



## D **C**

19.8 mm (0.78 in)

ASNA2050DCJ3215 3.25 mm (0.128 in) 3.35 mm (0.132 in) HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX RIVET VIEW LOOKING DOWN STGR23

STGR33

STGR34 APPLY MAT. No. 09−005A TO THE INTERFACE 01 SEALANT BEAD WITH MAT No. 09−016B. 02 WET INSTALL THE FASTENERS WITH MAT. No. 09−005A. 03 **NOTE:** OF THE NEW BRACKET AND THE STRUCTURE.

03 96 01 02

97 G_SB_363038_5_BCAA_02_00 Figure A-FBCAA - Sheet 02 Installation of a New Bracket between FR53.5 and FR53.6 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 175 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A Z190 FR47 FR44 FR40.2

(116)

(115) 

## A

**B B** 

G_SB_363038_5_BDAA_01_00 Figure A-FBDAA - Sheet 01 Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 176 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### B **A** FR56 FR53.5



## A FR45

FR39 101 102

113 100 303HF 98HF

302HF

97HF Z190

G_SB_363038_5_BEAA_01_00 Figure A-FBEAA - Sheet 01 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 177 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR44

FR43
FR42
FR41 FR40.3 FR40.2 FR40.1 FR40 FR40.2 FR40.3 FR41 FR42 FR43

FR40.1

FR40

BELLY FAIRING TRACE FUSELAGE TRACE

114 97HF 101 303HF

113 302HF

102 98HF 

### L

**J**

**C G** 

**E**

30

11
TYPICAL 

## P OR

15 27 15 27 27 15

15



## B **Q** G_SB_363038_5_BEAA_02_00 Figure A-FBEAA - Sheet 02 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 178 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### R **C C**  **C C**  **C C**  **H D**  **B B** 

**P Q** 

**P Q**  **FWD**

**FWD** VIEW LOOKING AFT 

### C **C**
**C C** 

**C C**  **B**

**B** FR39.2

FR40



## C **D** 113

114 302HF

97HF 

### F 

## E

13

14 20 10 10 13

14 20 14 20 13

14 16 21 10 14 20 13

14 20 10 78 

## F 33 32 35

34 30 33 32

30



## G **H** FR40.2 FR40.1 FR40

G_SB_363038_5_BEAA_03_00 Figure A-FBEAA - Sheet 03 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 179 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

13

10 14 20 18 10 13

14 24 16

13 10 14 21 FR41 FR40.3 FR40.2



### K 101 303HF

**FWD**


### D

**D A** 

**A A** 

**A A** 

**A B** 

**B** FR44 FR43 FR42



### N
**FWD** 10 13 14 20

13 14 20

10 13 14 20 14 20 14

13 10 14 16

13 10 70

10 13 14 18 24

18

13 14 24 18
13 10 10 14 24 79
14 29

1013 14 29

TYPICAL 

## R **S**

**N K**  **J**

**L**

**A A**  **B B**  **C C**  **D D**  10 

### S **A**

**A A** 

**A A** 

**A A** 

**A A** 

**A**
102 98HF 21 20

G_SB_363038_5_BEAA_04_00 Figure A-FBEAA - Sheet 04 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 180 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A

**B** Z190

FR56 FR53.5

FR39 

## AFTER

**A** 114 105 103 103 100HF 305HF 99HF 304HFFR45

G_SB_363038_5_BFAA_01_00 Figure A-FBFAA - Sheet 01 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 181 6

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

# @A330 SERVICE BULLETIN

**CONF ALL FR48 FR47 FR46 FR45

FR51
FR50
FR49

FR48
FR47
FR46 FR45 

### N

**L**

**F**

**C H**  **K** FUSELAGE TRACE

BELLY FAIRING TRACE 100 100HF 105 305HF

99HF 103

30

11
TYPICAL 

## S **B** OR

27

15 27 15

27

15

15



## T 103 304HF

G_SB_363038_5_BFAA_02_00 Figure A-FBFAA - Sheet 02 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 182 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

39 38 36

37 39

38 40

41 

### C

**C E**  **E**

**C C** 

**E E** 

**Q C**  **C**

**C C** 

FR45 FR44

VIEW LOOKING FORWARD FR46 VIEW LOOKING FORWARD VIEW LOOKING AFT

**FWD FWD** 

**FWD FWD**  **FWD** (2POS)

36

37 103

103 99HF

304HF 

### E

**J**

13 13 13 10 13 14 18 23 14 18 23 14 18 23 14 20 14 20 

## G **F** (2POS) 10 13 14 20 34
35 

## D **E**

**J H**  **D**



## C

**S T** 



## N **Q**

**Q**

30 30 

### C **C**

10 10 81

1010 13 14 20



### T



## K **S T**  **G**

**C C** 

G_SB_363038_5_BFAA_03_00 Figure A-FBFAA - Sheet 03 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 183 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

**FWD** 

## L **P**

**R R**  

## Q TYPICAL 13 10

14 20 14 20 14 20 13 10 13 10

14 20

79 14 29 80

14 29 13

10

13

14 20 10 16 10

13 14 21 17 10

13 14 26 16

18 10

13 14 19 

## A **A C**  **C E**  **E G**  **G Q**  105 305HP 100 100HP



### G **G**

**A A**  **A**

**A C**  **C**
**C C**  **A**

**A A** 

**A A** 

**A** FR50 FR49 FR48 FR47



### P

G_SB_363038_5_BFAA_04_00 Figure A-FBFAA - Sheet 04 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 184 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A

**B** Z190

FR56 FR53.5

FR45

FR39 

## AFTER 106 107 102HF 307HF 106 106 101HF 306HF

108 104 23HF 308HF



## A G_SB_363038_5_BGAA_01_00 Figure A-FBGAA - Sheet 01 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 185 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR52 FR53 FR53.1 FR53.2 FR53.4 FR53.5 307HF

306HF

101HF FUSELAGE TRACE

FR51 FR52 FR53 FR53.1 FR53.2 FR53.3 FR53.4 FR53.5 FR53.6

106 106 107 108 23HF 104 308HF 

### M

**C** 

## OR **G H** 

11 15 27 15 27 27 15

30 25 OR

TYPICAL 

## B **X Y**  FR53.3

BELLY FAIRING TRACE 102HF 106

15

G_SB_363038_5_BGAA_02_00 Figure A-FBGAA - Sheet 02 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 186 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### J **K** FR53.2 FR53.3 FR53.4 

### A

**A A**  **A D**  **A**

**A F**  FR51 FR52 FR53 FR53.1 

### C

**C C** 

**C C** 

**C**

14 20 14 20 14 20 70 10 10 10 13 13



## K 72 13 10

14 16 21

13 13 10 10 10

14 20 75 14 16 21 14 16 21 13 13 10 10



## E 82 

## F 14 20 14 16 21 14 20

13 10 13 10

14 20 14 16 21 74 

## J 14 16 21 14 20 13 10 13 10 83

73 14 20 

## L 13 

### A

**A A** 

**A A** 

**A** FR53.2

**FWD** 

## C **X Y** 

42

43 30 40

41 106 101HF

106 306HF 

## G 14 20 14 20



## D

**L** 

## H 13

14 29 14 20 

### E

G_SB_363038_5_BGAA_03_00 Figure A-FBGAA - Sheet 03 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 187 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

10 13

14 20 77 14 29

14 29 13 84 10
14 20

14 20 14 22 28

10 13 10 13 14 20

76 STGR36 STGR37 STGR38 STGR39 STGR40 STGR41 STGR42 STGR43 STGR44 STGR45 STGR46 STGR47 STGR48 STGR49 STGR50 FR53.5 FR53.6



### C

**C C**  **C C** 
**C T** 

**FWD** 

## N 43

42 45

44 30 

### X **Y**



## R **S T** 

**C C** 

**C C** 

**C C** 

**B B**  **N**
**P**
**Q R**  **C C** 
**T** 107

106 307HF

102HF104

108 308HF

23HF

VIEW LOOKING FORWARD 

## M 79 14 29

13
10 14 29


### U 

## T **U**
18

10 13

14 24 16

13 10 14 21 13

10 14 20 

## A **A B**  **B C**  **C P** 

**Q**

45 44 25 

### X


## S **Y**

G_SB_363038_5_BGAA_04_00 Figure A-FBGAA - Sheet 04 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 188 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### B **A**

FR56 FR53.5

FR45

FR39 

## AFTER

112 111 109 110 312HF 25HF 24HF 311HF



## A Z190

G_SB_363038_5_BHAA_01_00 Figure A-FBHAA - Sheet 01 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 189 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



## OR 27

15 27 15

27

15 30

11



## P **J**

**C** 109 24HF 312HF

TYPICAL 

## N FUSELAGE TRACE 112

FR53.6 FR53.7 FR53.8 FR53.9 FR54 FR55



## B 111 25HF

110 311HF 15

G_SB_363038_5_BHAA_02_00 Figure A-FBHAA - Sheet 02 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 190 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### N **F**

89
30 91

90 88

**FWD** 

## H 27 

### J **J**

10 14 20

13

14 20 93 10 14 20

13 

## F 14 29 79

13 10 14 29



## G **FWD** 

### D **D**

**H H**  13 14 20 86


## D VIEW LOOKING FORWARD 

### G



## E **C C** 

**G G** 

**D D** 

**B B**  **B B**  **D D**  **B B**  **D D**  **E** 112 312HF

111 25HF 108 24HF

110 311HF



## C **FWD**

**FWD** 92 27 85



## J **J H**  **H** 55° 27 

### D

**D D**  **F**

G_SB_363038_5_BHAA_03_00 

### E

**E D** 

**D B** 

**B D** 

**D H** 

**A A** 

Figure A-FBHAA - Sheet 03 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 191 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR53.9 FR55



### L **K** FR54 

### D

**D D** 

**D**

14 16 94
14 20 14 20 10 10 13

14 16 94 13

95 13

10

14 16 94 10

14 16 94 14 16 94 13 13

10 

## J

**K L**  13 10 14 87 17
13
10 14 26 17
13 10 14 26

10

14 20 13 13
14 21 10 16

14 87

13 86 18 13 1014 20

13 10

14 20 13



## G **G E**  **E D**  **D C**  **C B**  **B A**  **A** 18

70

G_SB_363038_5_BHAA_04_00 Figure A-FBHAA - Sheet 04 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 192 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A **B** Z150 FR53.3 FR54



## A FR53.5

FR53.6 

## AFTER

**B C** 

**D**

G_SB_363038_5_BJAA_01_02 Figure A-FBJAA - Sheet 01 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 193 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

169

169 (155)

2SG 1S REPLACED SENSING

**FWD** 14 169

(155) 169 (175) (175)

(175) (174) 175 310HF 138HF

137HF 309HF 174 (14)

(18) (168)



## C REPLACED SENSING

G_SB_363038_5_BJAA_02_02 27

3593VS 3503VS

27

Figure A-FBJAA - Sheet 02 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 194 6

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

# @A330 SERVICE BULLETIN

**CONF ALL EXAMPLE OF INSTALLATION OF WIRE−LOCK PN MS20995C32 (ITEM )



## D 27

G_SB_363038_5_BJAA_03_01 Figure A-FBJAA - Sheet 03 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 195 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A Z190 

### B FR44



## A

98 99



### C **A A** 

VIEW LOOKING FORWARD 

## C **B** 184.5 mm (7.26 in)

G_SB_363038_5_BKAA_01_00 Figure A-FBKAA - Sheet 01 Installation of Two New Brackets at FR44 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 196 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

99

98

**F W**  **D** 

## A **A**

ASNA2050DCJ3215 3.25 mm (0.128 in) 3.35 mm (0.132 in) HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX RIVET APPLY MAT. No. 09−005A TO THE INTERFACE 01 SEALANT BEAD WITH MAT No. 09−016B. 02 WET INSTALL THE FASTENERS WITH MAT. No. 09−005A. 03 **NOTE:** OF THE NEW BRACKET AND THE STRUCTURE.

03 01 02 01 02

109 mm (4.29 in)

97 G_SB_363038_5_BKAA_02_00 Figure A-FBKAA - Sheet 02 Installation of Two New Brackets at FR44 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 197 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A Z192 

### B FR39 FR40



## A
(125)

(126) (127) 

## B G_SB_363038_5_BPAA_01_00 Figure A-FBPAA - Sheet 01 Removal/Installation of the Ducts Between FR39 and FR40 for Access DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 198 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### A Z190

3520VP EXISTING HARNESS 2SG 

## A

301HF FR37 FR39.1 FR39.2 FR56FR57 FR58



### B **C**

G_SB_363038_5_BMAA_01_00 Figure A-FBMAA - Sheet 01 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 199 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

2HR 2M 2S 1M

2MK/2M1K 2SK/2S1K
2MK/2M1K 2S 2M 2SK/2S1K 1HR

1M

1M−2M 1M 2M

1SK/1S2K 1MK/1M2K

1M 1S 1S 1SK/1S2K 1M 1S 1MK/1M2K FR38 FR39 FR39.1 FR39.2 FR40 STGR36 STGR38 STGR40 STGR42 STGR44 STGR46 STGR48 STGR50 STGR52 STGR54 STGR54 STGR52 STGR50 STGR48 STGR46 STGR44 STGR42 STGR40 STGR38 STGR36 A/C C L 

## BEFORE

**FWD** 

## B 3501VS 

### D **H J**  **M N** 

**K**1M 

### Q **W Y**  **A A A C** 

**F**

G_SB_363038_5_BMAA_02_00 

### U

Figure A-FBMAA - Sheet 02 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 200 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

2HR 2M 2S 1M

2MK/2M1K 2SK/2S1K
2MK/2M1K 2S 2M 2SK/2S1K 1HR

1M1M 2SG

1M−2M 1M 2M

1SK/1S2K 1MK/1M2K

1M 1S 1S 2SG 1SK/1S2K 1M 1S 1MK/1M2K

NEW HARNESS NEW HARNESS NEW HARNESS FR38 FR39 FR39.1 FR39.2 FR40 STGR36 STGR38 STGR40 STGR42 STGR44 STGR46 STGR48 STGR50 STGR52 STGR54 STGR54 STGR52 STGR50 STGR48 STGR46 STGR44 STGR42 STGR40 STGR38 STGR36 A/C C L 

## AFTER

**FWD** 

## C 3501VS 3591VS 

### A B **A D**

**Z X**  **V**

**P A N** 

**A M**  **A L** 
**E R** 

**L**

**G**

G_SB_363038_5_BMAA_03_00 Figure A-FBMAA - Sheet 03 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 201 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

2SG 1SY2390

Z−2250

VIEW LOOKING FORWARD

2SG 1S FUSELAGE CONTOUR

BELLY−FAIRING AREA 

## BEFORE

**FWD** FR39.1 STGR38

STGR39

STGR40



### B

**B B** 

**B B**  **B**

**B B**  **B**

**B B** 

**B**

G_SB_363038_5_BMAA_04_00 

### A **E A**  **F**



## D **A A** 



## A **E** 3501VS 3591VS 

### C

**C**

Figure A-FBMAA - Sheet 04 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 202 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

2SG 1SY2390

Z−2250

VIEW LOOKING FORWARD

2SG 1S FUSELAGE CONTOUR

BELLY−FAIRING AREA 

## AFTER

**FWD** 3591VS 3501VS 

## E
FR39.1 STGR38

STGR39

STGR40

G_SB_363038_5_BMAA_05_00 

### A **G A H** 



## A **G D**  **D E** 

**E E** 

**E E**  **E**

**E E**  **E**

**E E** 

**E F** 

**F**

Figure A-FBMAA - Sheet 05 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 203 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

2SG

2SG 1S 

## BEFORE **AFTER**

(150) (152)

131 (154) (151) (151) 131 (154)

**FWD** (152) (150) (150)

G_SB_363038_5_BMAA_06_00 2SG
1S (151) (153) (154)

(152) (150) (150)

**FWD**

2SG 1S (150) (152)

131 (154) (151) VIEW LOOKING FORWARD

VIEW LOOKING FORWARD 2SG
1S (150) (152) (153) (154) (151)

2SG

1S (155) (152) (153) (154) (151) VIEW LOOKING FORWARD

VIEW LOOKING FORWARD 

## A **A D**  **D** 1S



## B **B E**  **E**

**C C**  **F F**  Figure A-FBMAA - Sheet 06 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 204 6

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# @A330 SERVICE BULLETIN

**CONF ALL 

## BEFORE

**FWD** G_SB_363038_5_BMAA_07_00 2SG



## A **F G** 

**G H**  **H**

Figure A-FBMAA - Sheet 07 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 205 6

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

# @A330 SERVICE BULLETIN

**CONF ALL 

## AFTER

**FWD** 2SG

G_SB_363038_5_BMAA_08_00 

## A H **K K**  **J**

**J**

Figure A-FBMAA - Sheet 08 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 206 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

1S

2SG 1S

2SG

1S 2SG 1M 

## BEFORE **AFTER**
(135) (134)

(152) (150) 131 (154) (151) 

## BEFORE

**AFTER**
(150) (152)

131 (154) 151 150 151

(155)
150 (152)

131 (154)



## F **G FWD** 

**FWD**

**FWD FWD**  **FWD** 1S

2SG 1S

2SG (150) (152) (153) (154) (151) (155) (151)

(155) (152)
(153) (154) **FWD** 

## G **G H**  **H**

**J J**  **K K** 

1S 2SG 1M (135) (134)

(152) (150) (153) (154) (151)
G_SB_363038_5_BMAA_09_01 Figure A-FBMAA - Sheet 09 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 207 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

STGR45

1M STGR45

1M FR39.1

FR39.1 

## BEFORE

**AFTER H** 

**A L**  **FWD**

**FWD** G_SB_363038_5_BMAA_10_00 

### L **L**

**M M** 

**N N** 

**P P** 

Figure A-FBMAA - Sheet 10 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 208 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

1S 1M 1M 2SG 

## BEFORE

**AFTER**

(151) (134) (152) (150) 131 (154) (135)

(138)

**FWD** 1S 1M 2SG (134) (152) (150) (151) (135)

131 (154)

G_SB_363038_5_BMAA_11_00 **FWD** 1S 1M 1M 2SG (151) (134) (152) (150) (153) (154) (135)

(138)

**FWD** 1S 1M 2SG (134) (152) (150) (151) (135)

(153) (154)

**FWD** 

## L **L M**  **M**

**N N**  **P P** 

Figure A-FBMAA - Sheet 11 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 209 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

STGR49

STGR48

STGR47 FR39.1 FR39.2

STGR49

STGR48

STGR47 FR39.1 FR39.2 

## BEFORE

**AFTER**

**J**

**A M**  **FWD**

**FWD** 

### R **R Q**  **Q**

G_SB_363038_5_BMAA_12_00 Figure A-FBMAA - Sheet 12 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 210 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

1M
2SG 

## AFTER

**FWD** FUSELAGE CONTOUR (138)
(150) (151) (152) 131 (154) **FWD** 

## BEFORE

G_SB_363038_5_BMAA_13_00 1M
2SG 

## BEFORE

**FWD** FUSELAGE CONTOUR (138)
(150) (151) (152) (153) (154) 2SG 1S 1M

1M (135) (139)

151 (134) (152) (150) 131 2SG 1S 1M

1M (135) (139) (157) (134) (152)

(150) (153) 

## AFTER

(154) (154)

**FWD** 

## Q **Q R**  **R**

**K L**  (16)

Figure A-FBMAA - Sheet 13 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 211 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

1M

1M 2SG STGR54 STGR54 

## BEFORE **AFTER**

**FWD FWD**  

## M

(140) (141) (150) (138)

131 (154) 

## BEFORE **AFTER**

**FWD FWD**  

## A N

G_SB_363038_5_BMAA_14_00 

### S **S T**  **T**



## S **S T**  **T** 1M

1M 2SG (140) (141) (150) (138)
(153) (154)

Figure A-FBMAA - Sheet 14 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 212 6

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# @A330 SERVICE BULLETIN

**CONF ALL

2SG 1M

1M 2SG 

## BEFORE **AFTER**

(138) (152) (150) (151)

131 (154)

(138) (150)

153 158 

## BEFORE **AFTER FWD**  **FWD**

**FWD FWD**  

## P

**R Q** 

G_SB_363038_5_BMAA_15_00 2SG 1M (138) (152) (150) (151)

(153) (154)

1M 2SG (138) (150)
(153) (167) 

## N

Figure A-FBMAA - Sheet 15 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 213 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



## AFTER

**NOTE:** ONLY ONE CONFIGURATION SHOWN. EQUIPMENT MAY DIFFER DEPENDING ON AIRCRAFT CONFIGURATION. 2S

2M


## V 2S

2SG 

## BEFORE STGR46


### U **U V**  **V V**  **V**

**FWD**

**FWD** 

## U

G_SB_363038_5_BMAA_16_02 

### W **W** 2SG 2SG

Figure A-FBMAA - Sheet 16 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 214 6

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

# @A330 SERVICE BULLETIN

**CONF ALL 

## BEFORE

1S 179 141 171 172 FUSELAGE CONTOUR

2S 179 171 172

141 180 180 181 181 2M FUSELAGE CONTOUR

2SG (134) (135) (151) (18) (153) (154)



## AFTER

G_SB_363038_5_BMAA_17_00 2S 1S FUSELAGE CONTOUR

(153) (183) (141)

(184) 

## U **U V**  **V**

**W W**  **FWD FWD**  2S

Figure A-FBMAA - Sheet 17 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 215 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

2SK/2S1K 2M FUSELAGE CONTOUR

2SG 2S

2SG FUSELAGE CONTOUR

2MK/2M1K 

## AFTER **BEFORE**

(155) (155) (152) 22 (163)

(150) 131 (154) 157 16 152 (135) 176
153 (154) 177 178

2SK/2S1K

2SG FUSELAGE CONTOUR

2MK/2M1K
(155) (155) (152) (165) (163)

(150) (153) (154) 2M FUSELAGE CONTOUR

2S (151)

(18) (135) (134) (153) (154)

**FWD FWD** 

**FWD FWD**  

## W **X**

**Y Z** 

G_SB_363038_5_BMAA_18_01 Figure A-FBMAA - Sheet 18 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 216 6

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# @A330 SERVICE BULLETIN

**CONF ALL

2M FUSELAGE CONTOUR
(151)

(135) 153 (154)

FUSELAGE CONTOUR FUSELAGE CONTOUR 

## AFTER **BEFORE**

2SG 2S
176 (18)

2SG 2S
176 2M (135) 153 (167) 

## A A **A B**

**A C A D**  **FWD FWD** 

**FWD FWD**  177

177 178

178

G_SB_363038_5_BMAA_19_00 2S 2M (135) (134) (153) (167) 2S

2M FUSELAGE CONTOUR
(151)

(135) (153) (154) (134) (18)

Figure A-FBMAA - Sheet 19 Modification of the Existing Harness 2SG DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 217 6

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# @A330 SERVICE BULLETIN

**CONF ALL

Figure A-FWCAA - Sheet 01 Installation of the Wiring of the New Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 218 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Figure A-FWBAA - Sheet 01 Modification of the Wiring between the Cargo Compartment and the Avionics Compartment DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 219 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 01 Modification of the Wiring in the Main Rack 800VU DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 220 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

END1 LEAD END2 Instructions Zone or

Panel Elec.Ident. Term Terminal P/N Wire Ident. Co Rte Gauge Lenght mm Inch Zone or Panel Elec.Ident. Term Terminal P/N L i n e 1 851VU 2901VT 65M 3612−0078 1M CF24 852VU 1HA2−AB 12A D 2 851VU 2901VT 54T EN3155−016M2222 3612−0078 1M CF24 3000 120 852VU 1HA2−AB 12A E0170FA2200 (a) A 3 851VU 2901VT 54X EN3155−016M2222 3612−0112 1M CF24 3000 120 852VU 1HA2−AA 11D E0170FA2200 (a) A 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25

(a) = BUNDLE F9000095228595 A = ADDED WIRE D = DELETED WIRE Figure A-FHAAA - Sheet 01 Hook-Up Chart of the Modification of the Wiring in the Main Rack 800VU DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 221 6

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# @A330 SERVICE BULLETIN

**CONF ALL

Z310

FR80 FR83 FR86 FR88 FR91 FR93 FR95



## A (200) (201) (202) (203) (204) 

### A

G_SB_363038_6_BAAA_01_01 Figure A-GBAAA - Sheet 01 Removal of the Sleeves from the APU Bleed-Air-Duct DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 222 6

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

# @A330 SERVICE BULLETIN

**CONF 001 

### A

Z310

FR80 FR83 FR85 FR86 FR88 FR91 FR93 FR95 34HF 361HF

140HF

139HF 33HF 358HF 359HF360HF



## A **B C**  **D**
**E G**  FR89

G_SB_363038_6_BBAA_01_01 Figure A-GBBAA - Sheet 01 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 223 6

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

# @A330 SERVICE BULLETIN

**CONF 001

G_SB_363038_6_BBAA_02_00 **FWD**



## B

**C** FR84 

### F

**F**

**F** FR80 FR83 FR84

Figure A-GBBAA - Sheet 02 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 224 6

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

# @A330 SERVICE BULLETIN

**CONF 001

FR86 **FWD** 

## D

**E**

**F F** 

G_SB_363038_6_BBAA_03_00 FR85

Figure A-GBBAA - Sheet 03 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 225 6

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# @A330 SERVICE BULLETIN

**CONF 001

TYPICAL (10)

(205) (13) 

## F

G_SB_363038_6_BBAA_04_00 

## G (205)

Figure A-GBBAA - Sheet 04 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 226 6

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

# @A330 SERVICE BULLETIN

**CONF 002 

### A

Z310

FR80 FR83 FR85 FR86 FR88 FR91 FR93 FR95 34HF 361HF

140HF

139HF 33HF 358HF 359HF360HF



## A **B C**  **D**
**E G**  FR89

G_SB_363038_6_BBAB_01_01 Figure A-GBBAB - Sheet 01 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 227 6

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# @A330 SERVICE BULLETIN

**CONF 002

**FWD** 

## B

**C** FR84 

### F

**F**

G_SB_363038_6_BBAB_02_00 

### F **F**

FR80 FR83 FR84

Figure A-GBBAB - Sheet 02 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 228 6

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# @A330 SERVICE BULLETIN

**CONF 002

G_SB_363038_6_BBAB_03_00 FR86 **FWD** 

## D

**E**

**F F**  FR85

Figure A-GBBAB - Sheet 03 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 229 6

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# @A330 SERVICE BULLETIN

**CONF 002

TYPICAL (10)

(205) (13) 

## F

**G** (205)

G_SB_363038_6_BBAB_04_00 Figure A-GBBAB - Sheet 04 Removal of the Clamp and the Attaching Parts from the Overheat Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 230 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

G_SB_363038_6_BCAA_01_00 

### A Z310 Z170

FR73 FR77
32HF
31HF
30HF FR83

355HF356HF 357HF



## A **B**

FR73

Figure A-GBCAA - Sheet 01 Removal of the Clamps and the Attaching Parts from the Overheat-Detection Dual Loops at Frame 80 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 231 6

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# @A330 SERVICE BULLETIN

**CONF ALL

**FWD**

G_SB_363038_6_BCAA_02_00 FR80



## B **C**

(205) (10)

(13) (13) 

## C

Figure A-GBCAA - Sheet 02 Removal of the Clamps and the Attaching Parts from the Overheat-Detection Dual Loops at Frame 80 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 232 6

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# @A330 SERVICE BULLETIN

**CONF ALL


### A Z310 Z170

FR73 FR77
32HF
31HF
30HF FR83

355HF356HF 357HF



## A

**NOTE:** THE SENSING ELEMENTS MUST BE INSTALLED IN FRONT OF THE VENTILATION HOLES. THE LENGTH COMPENSATION OF THE SENSING ELEMENTS MUST BE DONE AT THE COUPLINGS OR RETAINER RINGS 

### B

FR73

G_SB_363038_6_BDAA_01_00 Figure A-GBDAA - Sheet 01 Rerouting of the Sensing Elements 32HF and 357HF and Installation of Clamps DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 233 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

**FWD** FR80



## B

**C**

G_SB_363038_6_BDAA_02_00 

### C

01 TORQUE VALUE 0.25m.daN (22lbf.in) **NOTE:** 16 13

207 13 86
86 01

Figure A-GBDAA - Sheet 02 Rerouting of the Sensing Elements 32HF and 357HF and Installation of Clamps DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 234 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

G_SB_363038_6_BEAA_01_00 Z310 

### A

FR80 FR83 FR84 FR90 FR91 FR93 5866VB /2S



## A 5208VP 5151VS

5215VC 5410VS 5866VB /2S



### B

Figure A-GBEAA - Sheet 01 Replacement of the Clamp between Frame 90 and Frame 91 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 235 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

5866VB /2S

G_SB_363038_6_BEAA_02_00 VIEW LOOKING UP **FWD** FR91 FR90

STGR6LH STGR10LH

STGR6RH

STGR10RH AD



## B **E C**  **D E** 

**E**

Figure A-GBEAA - Sheet 02 Replacement of the Clamp between Frame 90 and Frame 91 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 236 6

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# @A330 SERVICE BULLETIN

**CONF ALL

TYPICAL PLACARD INSTALLATION 211 SB 36−3038

G_SB_363038_6_BEAA_03_00 5215VC

5410VC 5866VB /2S TO

TO 

## C (214) 

## BEFORE

TO

TO 210 

## AFTER



## D 169



## E 5215VC

5866VB /2S 5410VC

Figure A-GBEAA - Sheet 03 Replacement of the Clamp between Frame 90 and Frame 91 DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 237 6

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

# @A330 SERVICE BULLETIN

**CONF 001 

### A

Z310

FR80 FR83 FR85 FR86 FR88 FR91 FR93 FR95 34HF 361HF

140HF

139HF 33HF 358HF 359HF360HF



## A **B E**  **D G**  **J** FR89

G_SB_363038_6_BFAA_01_01 Figure A-GBFAA - Sheet 01 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 238 6

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

# @A330 SERVICE BULLETIN

**CONF 001

**FWD** 

## B

G_SB_363038_6_BFAA_02_00 

### C

13 (10)

13 208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in) **NOTE:** 

## C FR80 FR83 FR84

Figure A-GBFAA - Sheet 02 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 239 6

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

# @A330 SERVICE BULLETIN

**CONF 001

G_SB_363038_6_BFAA_03_00 FR84


## D

MIN 50.8 mm (2.00 in) MAX 80.0 mm (3.15 in)

12.7 mm (0.49 in) 16.5 mm (0.65 in)



## A **A** TYPICAL 

### A

**A A** 

**A**

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS 02 02

**NOTE:** 

### F

**F**

Figure A-GBFAA - Sheet 03 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 240 6

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

# @A330 SERVICE BULLETIN

**CONF 001 FR86



## E

MIN 50.8 mm (2.00 in) MAX 80.0 mm (3.15 in) 12.7 mm (0.49 in) 16.5 mm (0.65 in)

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS 02 G_SB_363038_6_BFAA_04_00 

### B
**B**



## B **B** TYPICAL 02

16

01 TORQUE VALUE 0.25m.daN (22lbf.in) **NOTE:** 

## F TYPICAL 

### F **B B** 

13 (10)

13 207 01

Figure A-GBFAA - Sheet 04 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 241 6

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# @A330 SERVICE BULLETIN

**CONF 001

**FWD** FR85

208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in) **NOTE:** G_SB_363038_6_BFAA_05_00 

## G **H**

13 86
86 207 13 16

01 

## H

**J**

Figure A-GBFAA - Sheet 05 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 242 6

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

# @A330 SERVICE BULLETIN

**CONF 002 

### A

Z310

FR80 FR83 FR85 FR86 FR88 FR91 FR93 FR95 34HF 361HF

140HF

139HF 33HF 358HF 359HF360HF



## A **B E**  **D G**  **J** FR89

G_SB_363038_6_BFAB_01_01 Figure A-GBFAB - Sheet 01 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 243 6

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

# @A330 SERVICE BULLETIN

**CONF 002

13 (10)

13 208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in) **NOTE:** 

## C

G_SB_363038_6_BFAB_02_00 **FWD**



## B **C C** 

TYPICAL FR80 FR83 FR84

Figure A-GBFAB - Sheet 02 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 244 6

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

# @A330 SERVICE BULLETIN

**CONF 002

FR84


## D

MIN 50.8 mm (2.00 in) MAX 80.0 mm (3.15 in)

12.7 mm (0.49 in) 16.5 mm (0.65 in)



## A **A** TYPICAL 

### A

**A A** 

**A**

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS 02 02

**NOTE:** 

### F

**F**

G_SB_363038_6_BFAB_03_00 Figure A-GBFAB - Sheet 03 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 245 6

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

# @A330 SERVICE BULLETIN

**CONF 002 FR86



## E

MIN 50.8 mm (2.00 in) MAX 80.0 mm (3.15 in) 12.7 mm (0.49 in) 16.5 mm (0.65 in)

MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS 02 

### B
**B**



## B **B** TYPICAL 02

01 TORQUE VALUE 0.25m.daN (22lbf.in) **NOTE:** 

### F **B B** 

G_SB_363038_6_BFAB_04_00 16



## F TYPICAL 13 (10)

13 207 01

Figure A-GBFAB - Sheet 04 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 246 6

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

# @A330 SERVICE BULLETIN

**CONF 002

**FWD** FR85

208

209 01

01 TORQUE VALUE 0.25m.daN (22lbf.in) **NOTE:** 

## G **H**

13 86
86 207 13 16

01 

## H

**J**

G_SB_363038_6_BFAB_05_00 Figure A-GBFAB - Sheet 05 Installation of the Clamp and the Attaching Parts in the Rear Fuselage DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 247 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

Z310

FR80 FR83 FR86 FR88 FR91 FR93 FR95

01 **NOTE:** HOOK AND LOOP TAPE USED FOR CLOSING INSULATION SLEEVE POSITION OF BLOWOUT APERTURE UNDER THE SENSING ELEMENT 02 01 02 01 02 01 02



## A 200 201 202 203 204 

### A

01 02 01 02

13

## B TYPICAL 

### B **B B** 

G_SB_363038_6_BGAA_01_02 Figure A-GBGAA - Sheet 01 Installation of the Sleeves on the APU Bleed-Air-Duct DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 248 6

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# @A330 SERVICE BULLETIN

**CONF ALL TOLERANCES FOR WAVINESS AND BEND IN WIRES
C

B A E C

A E

E A C

D E

E

E C

**NOTE:** FOR DIMENSIONS, REFER TO SHEET 2 G_SB_363038_6_BHAA_01_01 C E C

Figure A-GBHAA - Sheet 01 Tolerances for Waviness and Bends in Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 249 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

mm DIMENSIONS (in)

C D E B A 9.52 MAX 6.4
MIN 12.7 MIN 0.50 MIN 25.4 MIN 1.00 MIN R 25.4 MIN R 1.00 MAX 0.25

0.38 E

01 **NOTE:** USE OTHER HOLE OF BRACKET IF NECESSARY 02 01 02

ROTATE CLIP FOR SMOOTH ROUTING OF SENSING ELEMENT IF NECESSARY F

E

F MAX 203.0 MAX 7.99

G_SB_363038_6_BHAA_02_01 E E

01 02

Figure A-GBHAA - Sheet 02 Tolerances for Waviness and Bends in Sensing Elements DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 250 6

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

# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions **CONF ALL For details concerning the elapsed time assumptions, refer to the Gantt chart shown in the next page:

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 1 6

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

# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 001

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME STEPS

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01 02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 20.75 5.75 4 4.00 4.00 1

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS

MODIFY THE WIRING IN THE MAIN RACK 800VU 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 14.00 14.00 1 14.00 14.00 1 21.00 21.00 1 14.00 14.00 1 1.00 1.00 1 3.00 3.00 1 10.00 5.00 2 1.00 1.00 1 2.00 2.00 1 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR39 AND FR44

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR35.5 AND FR35.6 FOR ACCESS INSTALL A NEW SUPPORT FOR THE ROUTING OF THE SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6 IF REMOVED, INSTALL THE DUCTS BETWEEN FR53.5 AND FR53.6 IF NECESSARY, REMOVE THE DUCTS BETWEEN FR43 AND FR45 FOR ACCESS INSTALL THE NEW BRACKETS FOR THE ROUTING OF THE SENSING ELEMENTS AT FR44 IF REMOVED, INSTALL THE DUCTS BETWEEN FR43 AND FR45 BETWEEN FR39 AND FR44

MODIFY THE INTERCONNECTING ELECTRICAL WIRE FIN 309HF AND 310HF, BETWEEN THE SENSING ELEMENTS MODIFY THE EXISTING HARNESS 2SG MODIFY THE WIRING BETWEEN THE AVIONICS COMPARTMENT AND THE CARGO COMPARTMENT GET ACCESS **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038**

166.00

88.25 75 0 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR53.2 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.2 AND FR53.6 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR50 INSTALL THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR50 AND FR53.6 INSTALL THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 IF NECESSARY, REMOVE THE DUCTS BETWEEN FR39 AND FR40 FOR ACCESS

G_SB_363038_6_GAAA_01_00 Figure A-GGAAA - Sheet 01 Gantt Chart DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 2 6

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# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 001 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 166.00 88.25 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01 02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 2.00 2.00 1 1.25 0.75 2 1.00 0.50 2 0.25 0.25 1 1 1.50 1.50 1 1.00 0.50 2 1.50 0.75 2 4.00 4.00 1 28.50 7.50 4
70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 REMOVE THE SLEEVES FROM THE AUXILIARY POWER UNIT (APU) BLEED−AIR−DUCT

REPLACE THE CLAMP OF THE ELECTRICAL HARNESS 5866VB/2S IN THE REAR FUSELAGE INSTALL THE CLAMP AND THE NEW ATTACHING PARTS ON THE OVERHEAT SENSING ELEMENTS INSTALL THE SLEEVES ON THE APU BLEED−AIR−DUCT TEST CLOSE−UP REMOVE THE CLAMP AND THE ATTACHING PARTS FROM THE OVERHEAT SENSING ELEMENTS REMOVE THE CLAMP FROM THE OVERHEAT−DETECTION DUAL LOOPS AT FRAME 80 REROUTE THE SENSING ELEMENTS 32HF AND 357HF IF REMOVED, INSTALL THE DUCTS BETWEEN FR39 AND FR40

0.25 0.25

G_SB_363038_6_GAAA_02_00 Figure A-GGAAA - Sheet 02 Gantt Chart DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 3 6

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# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 002

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME STEPS

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01 02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 20.75 5.75 4 4.00 4.00 1

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS

MODIFY THE WIRING IN THE MAIN RACK 800VU 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 14.00 14.00 1 14.00 14.00 1 21.00 21.00 1 14.00 14.00 1 1.00 1.00 1 3.00 3.00 1 10.00 5.00 2 1.00 1.00 1 2.00 2.00 1 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR39 AND FR44

IF NECESSARY, REMOVE THE DUCTS BETWEEN FR35.5 AND FR35.6 FOR ACCESS INSTALL A NEW SUPPORT FOR THE ROUTING OF THE SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6 IF REMOVED, INSTALL THE DUCTS BETWEEN FR53.5 AND FR53.6 IF NECESSARY, REMOVE THE DUCTS BETWEEN FR43 AND FR45 FOR ACCESS INSTALL THE NEW BRACKETS FOR THE ROUTING OF THE SENSING ELEMENTS AT FR44 IF REMOVED, INSTALL THE DUCTS BETWEEN FR43 AND FR45 BETWEEN FR39 AND FR44

MODIFY THE INTERCONNECTING ELECTRICAL WIRE FIN 309HF AND 310HF, BETWEEN THE SENSING ELEMENTS MODIFY THE EXISTING HARNESS 2SG MODIFY THE WIRING BETWEEN THE AVIONICS COMPARTMENT AND THE CARGO COMPARTMENT GET ACCESS **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038**

166.50

88.25 75 0 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR53.2 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.2 AND FR53.6 REMOVE THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55

INSTALL THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR50 INSTALL THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR50 AND FR53.6 INSTALL THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 IF NECESSARY, REMOVE THE DUCTS BETWEEN FR39 AND FR40 FOR ACCESS

G_SB_363038_6_GAAB_01_00 Figure A-GGAAB - Sheet 01 Gantt Chart DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 4 6

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

# @A330 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 002 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−36−3038** MH ET/S STEPS

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01 02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 2.00 2.00 1 1.25 0.75 2 1.25 0.75 2 0.25 0.25 1 1 1.50 1.50 1 1.25 0.75 2 1.50 0.75 2 4.00 4.00 1 28.50 7.50 4 REMOVE THE SLEEVES FROM THE AUXILIARY POWER UNIT (APU) BLEED−AIR−DUCT

REPLACE THE CLAMP OF THE ELECTRICAL HARNESS 5866VB/2S IN THE REAR FUSELAGE INSTALL THE CLAMPS AND THE NEW ATTACHING PARTS ON THE OVERHEAT SENSING ELEMENTS INSTALL THE SLEEVES ON THE APU BLEED−AIR−DUCT TEST CLOSE−UP REMOVE THE CLAMPS AND THE ATTACHING PARTS FROM THE OVERHEAT SENSING ELEMENTS REMOVE THE CLAMP FROM THE OVERHEAT−DETECTION DUAL LOOPS AT FRAME 80 REROUTE THE SENSING ELEMENTS 32HF AND 357HF IF REMOVED, INSTALL THE DUCTS BETWEEN FR39 AND FR40

0.25 0.25

G_SB_363038_6_GAAB_02_00 SB ELAPSED TIME (HOURS) TOTAL MANHOURS SB ELAPSED TIME 166.00 88.25 75 0 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90

Figure A-GGAAB - Sheet 02 Gantt Chart DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 5 6

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: PNEUMATIC - LEAK DETECTION - ADAPT DUAL LOOP AFTER FIRST RETROFIT MODIFICATION No.: 58530D46962 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:
B - SB HAS BEEN embodied on aircraft: Operator comments: From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 1 6

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

# @A330 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve 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 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - 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 a short 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: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Jan 16/12 SERVICE BULLETIN No.: A330-36-3038 REVISION No.: 00 - Jan 16/12 Page: 1 6

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