# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 28 

### TITLE: FUEL - FUEL QUANTITY INDICATING SYSTEM - FQIC INTERCHANGEABILITY MODIFICATION No.: 04770H5229 This page transmits Revision No.01 of Service Bulletin No.A310-28-2039 ADDITIONAL WORK **CONF ALL Additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 issued to inform operators that this Service Bulletin is rendered MANDATORY. In order to demonstrate full compliance with SFAR 88 requirements, all Type 1 FQICs shall be replaced with Type 2 FQICs. Additional work has been added for aircraft that have accomplished this Service Bulletin at Revision No. 00; to inspect for Type 1 FQICs Part Number SIC5054, and to replace all Type 1 FQICs Part Number SIC5054 with Type 2 FQICs Part Number SIC5055, SIC5076, SIC5082 or SIC5083. The effectivity has been updated to include aircraft MSN 419 for operator JAB, MSN 427 for operator 83V and MSN 454 for operator FDX. The opportunity is taken to produce the Service Bulletin in the latest format. CHANGES SUMMARY MODIFICATIONS Minor editorial or document structure change N REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Minor editorial or document structure change N GENERAL EVALUATION Minor editorial or document structure change N MATERIAL PRICE INFORMATION Minor editorial or document structure change N EFFECTIVITY Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REFERENCES / REPERCUSSIONS Minor editorial or document structure change N DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 1 7

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
NATURE OF THE WORK Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N APPENDICES Minor editorial or document structure change N Fig. A-FSAAA Minor editorial or document structure change N Fig. A-FSAAA Sheet 01 Minor editorial or document structure change N PLANNING INFORMATION EFFECTIVITY Minor editorial or document structure change N Configuration definition Minor editorial or document structure change N CONF 001 Minor editorial or document structure change N Minor editorial or document structure change N Material Effectivity Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REASON Minor editorial or document structure change N History Minor editorial or document structure change N Objective/Action Minor editorial or document structure change N Advantages Minor editorial or document structure change N Operational/Maintenance Consequences Minor editorial or document structure change N DESCRIPTION Minor editorial or document structure change N COMPLIANCE Minor editorial or document structure change N Classification Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N Minor editorial or document structure change N APPROVAL Minor editorial or document structure change N Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N WEIGHT AND BALANCE Minor editorial or document structure change N ELECTRICAL LOAD DATA Minor editorial or document structure change N Minor editorial or document structure change N REFERENCES Minor editorial or document structure change N Minor editorial or document structure change N PUBLICATION AFFECTED Minor editorial or document structure change N Minor editorial or document structure change N INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N SPARES Minor editorial or document structure change N MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N Procurement Addresses Minor editorial or document structure change N Price and Availability Minor editorial or document structure change N INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N LIST OF COMPONENTS Minor editorial or document structure change N Kit 282039A01R01 Minor editorial or document structure change N DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 2 7

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
LIST OF MATERIALS - OPERATOR SUPPLIED Minor editorial or document structure change N Consumable Materials Minor editorial or document structure change N Components Minor editorial or document structure change N Component COMPA01 Minor editorial or document structure change N Component COMPB01 Minor editorial or document structure change N Component COMPB02 Minor editorial or document structure change N Component COMPB03 Minor editorial or document structure change N Component COMPB04 Minor editorial or document structure change N Component COMPB05 Minor editorial or document structure change N Component COMPB06 Minor editorial or document structure change N Component COMPB07 Minor editorial or document structure change N Component COMPB08 Minor editorial or document structure change N Component COMPB09 Minor editorial or document structure change N Equipment Minor editorial or document structure change N PARTS TO BE RE-IDENTIFIED BY OPERATOR Minor editorial or document structure change N TOOLING Minor editorial or document structure change N ACCOMPLISHMENT INSTRUCTIONS TASK 282039- 831-895-001- MODIFICATION Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Subtask 282039-910-001-001 Minor editorial or document structure change N Subtask 282039-839-403-001 Minor editorial or document structure change N Subtask 282039-941-001-001 Minor editorial or document structure change N Subtask 282039-941-403-001 Minor editorial or document structure change N Subtask 282039-020-001-001 Minor editorial or document structure change N Subtask 282039-831-001-001 Minor editorial or document structure change N Subtask 282039-831-403-001 Minor editorial or document structure change N Subtask 282039-710-403-001 Minor editorial or document structure change N Subtask 282039-720-403-001 Minor editorial or document structure change N Subtask 282039-942-001-001 Minor editorial or document structure change N TASK282039- 832-895-001-INSPECTION OF THE FQIC (15QT) - ADDITIONAL WORK Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N Subtask 282039-839-404-001 Minor editorial or document structure change N Subtask 282039-941-402-001 Minor editorial or document structure change N Subtask 282039-832-402-001 Minor editorial or document structure change N Subtask 282039-831-402-001 Minor editorial or document structure change N Subtask 282039-710-402-001 Minor editorial or document structure change N Subtask 282039-720-402-001 Minor editorial or document structure change N Subtask 282039-942-404-001 Minor editorial or document structure change N
DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 3 7

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-FCAAA Minor editorial or document structure change N Fig. A-FCAAA Sheet 01 Minor editorial or document structure change N Fig. A-FBAAA Minor editorial or document structure change N Fig. A-FBAAA Sheet 01 Minor editorial or document structure change N Fig. A-FBBAA Minor editorial or document structure change N Fig. A-FBBAA Sheet 01 Minor editorial or document structure change N FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS No previous revision REVISION SEQUENCE ORIGINAL: Jun 28/89 REVISION No. : 01 - Jan 19/11

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 4 7

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# @A310 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. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 28 

### TITLE: FUEL - FUEL QUANTITY INDICATING SYSTEM - FQIC INTERCHANGEABILITY **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 04770H5229 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 At the original issue this Service Bulletin enabled the installation of FQICs P/N SIC5055, SIC5076 or SIC5082 and ensured the correct operation of the automatic refuelling function for A310-200 aircraft. Type 1 FQIC P/N SIC5054 have been found not to meet the intrinsic safety requirements as per SFAR88 and are now required to be replaced by the later Type 2 FQICs. This Service Bulletin provides the details to modify the wiring in the RH electronics rack 90VU and replaces the Type 1 FQICs P/N SIC5054 with Type 2 FQICs P/N SIC5055, SIC5076, SIC5082 or SIC5083. Accomplishment of this Service Bulletin allows the Type 2 FQICs P/N SIC5055, SIC5076, SIC5082 or SIC5083 to be installed in A310-200 aircraft. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO
DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 1 7

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# @A310 SERVICE BULLETIN SUMMARY
EVALUATION TABLE KIT PRICE (USD) SEE SB NOTE (1): Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282039A01R01 1 107.00 BUNDLE Component COMPA01 1 See SB TIE Component COMPB01 See SB TYPE 2 FQIC P/N SIC5055-3 Component COMPB02 See SB TYPE 2 FQIC P/N SIC5055-4 Component COMPB03 See SB TYPE 2 FQIC P/N SIC5055-5 Component COMPB04 See SB TYPE 2 FQIC P/N SIC5076-2 Component COMPB05 See SB TYPE 2 FQIC P/N SIC5076-3 Component COMPB06 See SB TYPE 2 FQIC P/N SIC5082-1 Component COMPB07 See SB TYPE 2 FQIC P/N SIC5082-2 Component COMPB08 See SB TYPE 2 FQIC P/N SIC5083-1 Component COMPB09 See SB TYPE 2 FQIC P/N SIC5083-2 EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

83V BAF DAH F2I FDX IRA JAB JAV KYV CONCURRENT REQUIREMENTS If operators wish to install an FQIC Part Number SIC5083-2, 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. A310-28-2064 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No.A310-28-2166 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled). REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 2 7

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# @A310 SERVICE BULLETIN SUMMARY
LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD YES SOFT NO OBRM NO MANPOWER Task 282039-831-895-001: MODIFICATION TOTAL MANHOURS 4.00 ELAPSED TIME (HOURS) 4.00 Task 282039-832-895-001: INSPECTION OF THE FQIC (15QT) - ADDITIONAL WORK TOTAL MANHOURS 2.25 ELAPSED TIME (HOURS) 2.25 APPENDICES None

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 3 7

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

FR20

FR1 

### A

Z120



## B 90VU 

## A 15QT

92VU 

### B

B_SB_282039_5_SAAA_01_01 Figure A-FSAAA - Sheet 01

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 4 7

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# @A310 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 28 

### TITLE: FUEL - FUEL QUANTITY INDICATING SYSTEM - FQIC INTERCHANGEABILITY MODIFICATION No.: 04770H5229 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 (1) Models 310-203 310-204 310-221 310-222 (2) Effectivity by MSN 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360 0362 0364 0367 0369-0370 0372 0375 0379 0386 0389-0390 0394 0397 0400 0419 0427 0454 (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 83V 0427 DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 1 7

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# @A310 SERVICE BULLETIN

OPERATOR MSN BAF 0367 0372 DAH 0291 0293 F2I 0309 FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303 0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346 0353 0355 0356 0359 0360 0362 0364 0369 0394 0397 0400 0454 IRA 0338 0370 0375 0379 0389 0390 JAB 0320 0419 JAV 0357 KYV 0386 (4) Configuration by MSN MSN CONFIGURATION 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333 0335 0338 0339 0342 0343 0345 0346 0353 0355 0356 0357 0359 0360 0362 0364 0367 0369 0370 0372 0375 0379 0386 0389 0390 0394 0397 0400 0419 0427 0454 001

(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Kit 282039A01R01 1 Component COMPA01 1 Component COMPB01 As required (1) Component COMPB02 As required (2) Component COMPB03 As required (3) Component COMPB04 As required (4) Component COMPB05 As required (5) Component COMPB06 As required (6) Component COMPB07 As required (7) Component COMPB08 As required (8) Component COMPB09 As required (9) NOTE: Only one COMP BO(1,2,3,4,5,6,7,8 or 9) Kit is required per aircraft. Operators can install an FQIC P/N SIC5055-3 (COMPB01), or an FQIC P/N SIC5055-4 (COMPB02), or an FQIC P/N SIC5055-5 (COMPB03), or an FQIC P/N SIC5076-2 (COMPB04), or an FQIC P/N SIC5076-3 (COMPB05), or an FQIC P/N SIC5082-1 (COMPB06), or an FQIC P/N
DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 2 7

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# @A310 SERVICE BULLETIN
SIC5082-2 (COMPB07), or an FQIC P/N SIC5083-1 (COMPB08), or an FQIC P/N SIC5083-2 (COMPB09). NOTE(1): Component COMPB01 (TYPE 2 FQIC P/N SIC5055-3) NOTE (2): Component COMPB02 (TYPE 2 FQIC P/N SIC5055-4) NOTE (3): Component COMPB03 (TYPE 2 FQIC P/N SIC5055-5) NOTE (4): Component COMPB04 (TYPE 2 FQIC P/N SIC5076-2) NOTE (5): Component COMPB05 (TYPE 2 FQIC P/N SIC5076-3) NOTE (6): Component COMPB06 (TYPE 2 FQIC P/N SIC5082-1) NOTE (7): Component COMPB07 (TYPE 2 FQIC P/N SIC5082-2) NOTE (8): Component COMPB08 (TYPE 2 FQIC P/N SIC5083-1) NOTE (9): Component COMPB09 (TYPE 2 FQIC P/N SIC5083-2) B. CONCURRENT REQUIREMENTS If operators wish to install an FQIC Part Number SIC5083-2, 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. A310-28-2064 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No.A310-28-2166 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled). C. REASON (1) History At the original issue this Service Bulletin enabled the installation of FQICs P/N SIC5055, SIC5076 or SIC5082 and ensured the correct operation of the automatic refuelling function for A310-200 aircraft. Type 1 FQIC P/N SIC5054 have been found not to meet the intrinsic safety requirements as per SFAR88 and are now required to be replaced by the later Type 2 FQICs. (2) Objective/Action This Service Bulletin provides the details to modify the wiring in the RH electronics rack 90VU and replaces the Type 1 FQICs P/N SIC5054 with Type 2 FQICs P/N SIC5055, SIC5076, SIC5082 or SIC5083.

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 3 7

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# @A310 SERVICE BULLETIN
(3) Advantages Accomplishment of this Service Bulletin allows the Type 2 FQICs P/N SIC5055, SIC5076, SIC5082 or SIC5083 to be installed in A310-200 aircraft. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 282039-831-895-001: MODIFICATION (1) Remove the Fuel Quantity Computer 15QT (2) Modify the Wiring in the RH Electronics Rack 90VU (3) Modification - Install a Type 2 FQIC (15QT) Task 282039-832-895-001: INSPECTION OF THE FQIC (15QT) - ADDITIONAL WORK (1) Inspect the FQIC (15QT) (2) Modification - Replace the Type 1 FQIC (15QT) with a Type 2 FQIC (15QT) E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). It is anticipated that the AD will confirm the grace period of 30 months. F. APPROVAL Approved under EASA Design Organisation Approval No. EASA21J.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.

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 4 7

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# @A310 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. NOTE: This Service Bulletin assumes that the aircraft has been placed in a maintenance status. The manhours/elapsed time estimates do not include preparation for the modification, non-productive elapsed time or administrative functions. Task 282039-831-895-001: MODIFICATION Get Access 1.00 On Aircraft Remove the Fuel Quantity Computer 15QT 0.25 Modify the Wiring in the RH Electronics Rack 90VU 0.50 Modification - Install a Type 2 FQIC (15QT) 0.25 Tests 1.00 Close-Up 1.00 TOTAL MANHOURS 4.00 ELAPSED TIME (HOURS) 4.00

Task 282039-832-895-001: INSPECTION OF THE FQIC (15QT) - ADDITIONAL WORK Get Access 0.50 On Aircraft Inspect the FQIC (15QT) 0.25 Modification - Replace the Type 1 FQIC (15QT) with a Type 2 FQIC (15QT) 0.50 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.25 ELAPSED TIME (HOURS) 2.25 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 24-00-00 24-41-00 28-25-00 28-42-38 52-30-00 52-52-00

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 5 7

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# @A310 SERVICE BULLETIN
ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-55-00 24-52-21 Service Bulletin (SB) A310-28-2064 A310-28-2166 Standards Manual (SM) K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 28-04-89 Aircraft Schematic Manual (ASM) 28-42-00 28-42-01 Aircraft Wiring List (AWL) Aircraft Wiring Manual (AWM) 28-42-01 Illustrated Parts Catalog (IPC) 28-42-08 L. INTERCHANGEABILITY/MIXABILITY DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Computer-Fuel, Quantity SIC5054-1 SIC5055-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5055-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5055-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5055-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5055-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5055-4 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5055-4 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5055-4 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5055-4 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5055-4 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5055-5 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5055-5 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5055-5 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5055-5 01 Not Applicable

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 6 7

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# @A310 SERVICE BULLETIN

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Computer-Fuel, Quantity SIC5054-5 SIC5055-5 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5076-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5076-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5076-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5076-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5076-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5076-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5076-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5076-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5076-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5076-3 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5082-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5082-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5082-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5082-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5082-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5082-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5082-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5082-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5082-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5082-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5083-1 01 Not Applicable

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 7 7

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# @A310 SERVICE BULLETIN

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Computer-Fuel, Quantity SIC5054-2 SIC5083-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5083-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5083-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5083-1 01 Not Applicable Computer-Fuel, Quantity SIC5054-1 SIC5083-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-2 SIC5083-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-3 SIC5083-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-4 SIC5083-2 01 Not Applicable Computer-Fuel, Quantity SIC5054-5 SIC5083-2 01 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. M. SPARES None

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 8 7

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# @A310 SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 282039A01R01 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 modification kits by fax: +49 40 50 76 25 90 For ordering of single spares by fax: +49 40 50 76 40 13 Component COMPB01 Component COMPB02 Component COMPB03 Component COMPB04 Component COMPB05 Component COMPB06 Component COMPB07 Component COMPB08 Component COMPB09 Vendor parts are to be procured from: INTERTECHNIQUE 61 Rue Pierre Curie BP 1 78370 Plaisir France (2) Price and Availability

Kit 282039A01R01 Cost 107.00 USD Availability 60 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: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 9 7

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# @A310 SERVICE BULLETIN
Component COMPB01 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB02 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB03 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB04 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB05 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB06 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB07 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB08 Procurement to be negotiated directly with INTERTECHNIQUE. Component COMPB09 Procurement to be negotiated directly with INTERTECHNIQUE. B. INDUSTRY SUPPORT INFORMATION AIRBUS will provide a 10% reduction to the applicable sales prices given in the paragraph ’Price and Availability’ for orders placed before 31.12.2016. C. LIST OF COMPONENTS Kit 282039A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES A9000095085495 1 BUNDLE

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 10 7

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# @A310 SERVICE BULLETIN

D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES NSA935401-03 5 TIE NSA935401-05 5 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. Component COMPB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5055-3 FQIC SIC5054-1 01 SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5055-4 FQIC SIC5054-1 01 SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPB03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5055-5 FQIC SIC5054-1 01 SIC5054-2 01
DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 11 7

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPB04 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5076-2 FQIC SIC5054-1 01 SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPB05 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5076-3 FQIC SIC5054-1 01 SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPB06 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5082-1 FQIC SIC5054-1 01 SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 12 7

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# @A310 SERVICE BULLETIN
Component COMPB07 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5082-2 FQIC SIC5054-1 01 SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPB08 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5083-1 FQIC SIC5054-1 01 SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPB09 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5083-2 FQIC SIC5054-1 01 (1) SIC5054-2 01 SIC5054-3 01 SIC5054-4 01 SIC5054-5 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE(1): Operators who wish to install an FQIC Part Number SIC5083-2 must accomplish either: - Service Bulletin No. A310-28-2064 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No.A310-28-2166 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled).

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 13 7

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# @A310 SERVICE BULLETIN
(3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 14 7

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# @A310 SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 282039-831-895-001 - MODIFICATION WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. 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 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, CLEANING. Task Associated Data Zone 120 Modified FIN 15QT Access Door 132AZ Manpower TOTAL MANHOURS 4.00 ELAPSED TIME (HOURS) 4.00 A. GENERAL (1) Subtask 282039-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 24-52-21 (a) To install new wires, cut them to the necessary length, crimp the terminals and connect them.

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 15 7

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# @A310 SERVICE BULLETIN
(b) Route the new wires with the wires that are in the aircraft. (c) Do a continuity test of the new and modified wires (Refer to ESPM 24-52-21). (d) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM 20-25-51). (2) Subtask 282039-839-403-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 282039-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 52-30-00, Page Block 001 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put access platform(s) in position (c) Open the cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the FWD cargo compartment access door 132AZ (Refer to AMM 52-52-00, Page Block 001). (e) Open, safety and tag these circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 128VU FUEL/FQI/SUPPLY & IND 1QT 805/L83 128VU FUEL/FQI/CHAN SUPPLY 1 3QT 805/L84 128VU FUEL/FQI/CHAN SUPPLY 2 4QT 805/L85

(2) Subtask 282039-941-403-001 - Job Set-up Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 24-41-00, Page Block 301 DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 16 7

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# @A310 SERVICE BULLETIN
(a) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). C. PROCEDURE (1) Subtask 282039-020-001-001 - Remove the Fuel Quantity Computer 15QT Work Zones and Access Panels Zone Access/Work location 120 Access Door 132AZ Work location Electrical panel 90VU Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 Fig. A-FCAAA Location of the FQI Computer Sheet 01 (a) Remove the fuel quantity computer 15QT (Refer to AMM 28-42-38, Page Block 401). (2) Subtask 282039-831-001-001 - Modify the Wiring in the RH Electronics Rack 90VU Work Zones and Access Panels Zone Access/Work location 120 Access Door 132AZ Work location Electrical panel 90VU Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills ELECTRICAL Material necessary to do the job Kit 282039A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES A9000095085495 BUNDLE

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 17 7

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# @A310 SERVICE BULLETIN
Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES NSA935401-03 5 TIE NSA935401-05 5 TIE References Fig. A-FBAAA Modification of the Wiring in the Electronics Rack 90VU Sheet 01
Fig. A-FBBAA Hook-up Chart Sheet 01 (a) Install the wire as shown on the wiring diagram Fig. A-FBAAA Sheet 01 and as given on the Hook-up Chart line: - 1 (Refer to Fig. A-FBBAA Sheet 01) supplied in: Bundle A9000095085495 (b) Attach the wire with: 5 Tie-Cable NSA935401-03 5 Tie-Cable NSA935401-05

(3) Subtask 282039-831-403-001 - Modification - Install a Type 2 FQIC (15QT) Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills UTILITY Material necessary to do the job Component COMPB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5055-3 FQIC Component COMPB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5055-4 FQIC

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 18 7

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# @A310 SERVICE BULLETIN
Component COMPB03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5055-5 FQIC Component COMPB04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5076-2 FQIC Component COMPB05 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5076-3 FQIC Component COMPB06 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5082-1 FQIC Component COMPB07 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5082-2 FQIC Component COMPB08 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5083-1 FQIC Component COMPB09 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5083-2 FQIC (1) NOTE(1): Operators who wish to install an FQIC Part Number SIC5083-2 must accomplish either: - Service Bulletin No. A310-28-2064 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No.A310-28-2166 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled).

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 19 7

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 Service Bulletin (SB) A310-28-2064 A310-28-2166 Fig. A-FCAAA Location of the FQI Computer Sheet 01 (a) Do an inspection of the label on the front of the removed FQIC (15QT) (Refer to Fig. A-FCAAA Sheet 01). (b) If the part number of the FQIC (15QT) is SIC5055-2, SIC5055-3, SIC5055-4, SIC5055-5, SIC5076-3, SIC5082-1, SIC5082-2, SIC5083-1 or SIC 5083-2, re-install the Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 401). (c) If the part number of the FQIC (15QT) is SIC5054-1, SIC5054-2, SIC5054-3, SIC5054-4 or SIC 5054-5, do the step that follows: 1 Replace the Type 1 FQIC (15QT) as follows: Replace 1 Computer-Fuel, Quantity SIC5054-1 Discard or replace 1 Computer-Fuel, Quantity SIC5054-2 Discard or replace 1 Computer-Fuel, Quantity SIC5054-3 Discard or replace 1 Computer-Fuel, Quantity SIC5054-4 Discard or replace 1 Computer-Fuel, Quantity SIC5054-5 Discard with a Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 401): Install a 1 Computer-Fuel, Quantity SIC5055-3

or a

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 20 7

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# @A310 SERVICE BULLETIN
1 Computer-Fuel, Quantity SIC5055-4

or a 1 Computer-Fuel, Quantity SIC5055-5

or a 1 Computer-Fuel, Quantity SIC5076-2

or a 1 Computer-Fuel, Quantity SIC5076-3

or a 1 Computer-Fuel, Quantity SIC5082-1

or a 1 Computer-Fuel, Quantity SIC5082-2

or a 1 Computer-Fuel, Quantity SIC5083-1

or a 1 Computer-Fuel, Quantity SIC5083-2
NOTE: If operators wish to install a Type 2 FQIC (15QT) P/N SIC5083-2, Service Bulletin No. A310-28-2064 OR Service Bulletin No. A310-28-2166 must be accomplished. D. TEST (1) Subtask 282039-710-403-001 - Operational Test of the Type 2 FQIC (15QT) Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 501

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 21 7

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# @A310 SERVICE BULLETIN
(a) Remove the safety clip(s) and tag(s) and close this(these) circuit breaker(s): PANEL DESIGNATION FIN LOCATION SEE NOTES 128VU FUEL/FQI/SUPPLY & IND 1QT 805/L83 128VU FUEL/FQI/CHAN 1 SUPPLY 3QT 805/L84 128VU FUEL/FQI/CHAN 2 SUPPLY 4QT 805/L85 (b) Do an operational test of the Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 501). (2) Subtask 282039-720-403-001 - Functional Test Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 28-25-00, Page Block 501 (a) Do a functional test of the aircraft refuelling system (Referto AMM 28-25-00, Page Block 501). E. CLOSE-UP (1) Subtask 282039-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-30-00, Page Block 001 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 access door 132AZ (Refer to AMM 52-52-00, Page Block 001). (c) Close the cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Remove the access platform.

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 22 7

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# @A310 SERVICE BULLETIN

Task 282039-832-895-001 - INSPECTION OF THE FQIC (15QT) - ADDITIONAL WORK WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. 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 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, CLEANING. Task Associated Data Modified FIN 15QT Manpower TOTAL MANHOURS 2.25 ELAPSED TIME (HOURS) 2.25 A. GENERAL (1) Subtask 282039-839-404-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 282039-941-402-001 - Job Set-up Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 24-41-00, Page Block 301

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 23 7

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# @A310 SERVICE BULLETIN
(a) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). C. PROCEDURE (1) Subtask 282039-832-402-001 - Inspect the FQIC (15QT) Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills UTILITY References Fig. A-FCAAA Location of the FQI Computer Sheet 01 (a) Do an inspection of the FQIC (15QT) to check the part number on the label on the front of the FQIC (Refer to Fig. A-FCAAA Sheet 01): 1 If the part number of the FQIC (15QT) is SIC5055-2, SIC5055-3, SIC5055-4, SIC5055-5, SIC5076-3, SIC5082-1, SIC5082-2, SIC5083-1 or SIC 5083-2, no action is necessary. Go to SUBTASK 282039-942-404 001 Close-up . 2 If the part number of the FQIC (15QT) is SIC5054-1, SIC5054-2, SIC5054-3, SIC5054-4 or SIC 5054-5, do SUBTASK 282039-831-402 001 Modification - Replace the Type 1 FQIC (15QT) with a Type 2 FQIC (15QT) . (2) Subtask 282039-831-402-001 - Modification - Replace the Type 1 FQIC (15QT) with a Type 2 FQIC (15QT) Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills UTILITY Material necessary to do the job Component COMPB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5055-3 FQIC Component COMPB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5055-4 FQIC

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 24 7

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# @A310 SERVICE BULLETIN
Component COMPB03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5055-5 FQIC Component COMPB04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5076-2 FQIC Component COMPB05 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5076-3 FQIC Component COMPB06 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5082-1 FQIC Component COMPB07 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5082-2 FQIC Component COMPB08 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5083-1 FQIC Component COMPB09 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5083-2 FQIC (1) NOTE(1): Operators who wish to install an FQIC Part Number SIC5083-2 must accomplish either: - Service Bulletin No. A310-28-2064 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No.A310-28-2166 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled).

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 25 7

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 Service Bulletin (SB) A310-28-2064 A310-28-2166 (a) Make sure that this(these) circuit breaker(s) are open, safetied and tagged: PANEL DESIGNATION FIN LOCATION SEE NOTES 128VU FUEL/FQI/SUPPLY & IND 1QT 805/L83 128VU FUEL/FQI/CHAN 1 SUPPLY 3QT 805/L84 128VU FUEL/FQI/CHAN 2 SUPPLY 4QT 805/L85 (b) Remove the Type 1 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 401): Remove 1 Computer-Fuel, Quantity SIC5054-1 Discard

or remove 1 Computer-Fuel, Quantity SIC5054-2 Discard

or remove 1 Computer-Fuel, Quantity SIC5054-3 Discard

or remove 1 Computer-Fuel, Quantity SIC5054-4 Discard

or remove 1 Computer-Fuel, Quantity SIC5054-5 Discard (c) Install a Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 401): Install a 1 Computer-Fuel, Quantity SIC5055-3

or a 1 Computer-Fuel, Quantity SIC5055-4

or a

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 26 7

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# @A310 SERVICE BULLETIN
1 Computer-Fuel, Quantity SIC5055-5

or a 1 Computer-Fuel, Quantity SIC5076-2

or a 1 Computer-Fuel, Quantity SIC5076-3

or a 1 Computer-Fuel, Quantity SIC5082-1

or a 1 Computer-Fuel, Quantity SIC5082-2

or a 1 Computer-Fuel, Quantity SIC5083-1

or a 1 Computer-Fuel, Quantity SIC5083-2
NOTE: If operators wish to install a Type 2 FQIC (15QT) P/N SIC5083-2, Service Bulletin No. A310-28-2064 OR Service Bulletin No. A310-28-2166 must be accomplished. D. TEST (1) Subtask 282039-710-402-001 - Operational Test of the Type 2 FQIC (15QT) Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 501 (a) Remove the safety clip(s) and tag(s) and close this(these) circuit breaker(s): PANEL DESIGNATION FIN LOCATION SEE NOTES 128VU FUEL/FQI/SUPPLY & IND 1QT 805/L83 128VU FUEL/FQI/CHAN 1 SUPPLY 3QT 805/L84 128VU FUEL/FQI/CHAN 2 SUPPLY 4QT 805/L85
DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 27 7

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# @A310 SERVICE BULLETIN
(b) Do an operational test of the Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 501). (2) Subtask 282039-720-402-001 - Functional Test Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 28-25-00, Page Block 501 (a) Do a functional test of the aircraft refuelling system (Referto AMM 28-25-00, Page Block 501). E. CLOSE-UP (1) Subtask 282039-942-404-001 - Close-up Manpower Resources Skills UTILITY (a) Make sure that the work area is clean and clear of tools and other items. (b) Remove the access platform(s).

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 28 7

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# @A310 SERVICE BULLETIN

**CONF ALL

FR20

FR1 

### A

Z120



## B 90VU 

## A 15QT

B_SB_282039_5_CAAA_01_01 92VU 

### B

Figure A-FCAAA - Sheet 01 Location of the FQI Computer

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 29 7

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# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FBAAA - Sheet 01 Modification of the Wiring in the Electronics Rack 90VU

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 30 7

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# @A310 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 92VU 15QT−AB 6D ASNE0170FA2200 2842−0838 CF22 500 20 92VU 15QT−AB 10D ASNE0170FA2200 (a) A 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25

(a) = BUNDLE A9000095085495 A = ADDED WIRE
Figure A-FBBAA - Sheet 01 Hook-up Chart

DATE: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 31 7

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# @A310 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUEL - FUEL QUANTITY INDICATING SYSTEM - FQIC INTERCHANGEABILITY MODIFICATION No.: 04770H5229 Please complete the appropriate item (A or B): A - SB WILL BEembodied 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 BEENembodied 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: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 1 7

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

# @A310 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 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - Is this SB easy to understand ? Y / N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give 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: Jun 28/89 SERVICE BULLETIN No.: A310-28-2039 REVISION No.: 01 - Jan 19/11 Page: 1 7

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