# @A300-600 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.: 08121H5245 This page transmits Revision No.02 of Service Bulletin No.A300-28-6024 ADDITIONAL WORK **CONF ALL Additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 02 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 or 01; to inspect for Type 1 FQICs Part Number SIC5051, and to replace the Type 1 FQICs Part Number SIC5051 with Type 2 FQICs Part Number SIC5077. 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 NATURE OF THE WORK Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N
DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 1 7

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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 286024A01R01 Minor editorial or document structure change N LIST OF MATERIALS - OPERATOR SUPPLIED Minor editorial or document structure change N

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 2 7

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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 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 286024- 831-895-001- MODIFICATION Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Subtask 286024-910-001-001 Minor editorial or document structure change N Subtask 286024-839-401-001 Minor editorial or document structure change N Subtask 286024-941-401-001 Minor editorial or document structure change N Subtask 286024-020-401-001 Minor editorial or document structure change N Subtask 286024-831-001-001 Minor editorial or document structure change N Subtask 286024-420-401-001 Minor editorial or document structure change N Subtask 286024-710-401-001 Minor editorial or document structure change N Subtask 286024-720-401-001 Minor editorial or document structure change N Subtask 286024-942-401-001 Minor editorial or document structure change N TASK286024- 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 286024-839-402-001 Minor editorial or document structure change N Subtask 286024-941-402-001 Minor editorial or document structure change N Subtask 286024-832-401-001 Minor editorial or document structure change N Subtask 286024-831-401-001 Minor editorial or document structure change N Subtask 286024-710-402-001 Minor editorial or document structure change N Subtask 286024-720-402-001 Minor editorial or document structure change N Subtask 286024-942-402-001 Minor editorial or document structure change N 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

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 3 7

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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 REVISION SEQUENCE ORIGINAL: Feb 27/91 REVISION No. : 02 - Jan 19/11

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 4 7

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# @A300-600 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 08121H5245 MINOR None 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 In order to demonstrate full compliance with SFAR 88 requirements, all Type 1 FQICs P/N SIC5051 shall be replaced with Type 2 FQICs P/N SIC5077. In order to install the Type 2 FQICs P/N SIC5077, a wiring change to the aircraft is required. This Service Bulletin provides the details to modify the wiring in the RH electronics rack 90VU and replaces the Type 1 FQICs P/N SIC5051 with the Type 2 FQICs P/N SIC5077. Accomplishment of this Service Bulletin allows the Type 2 FQICs P/N SIC5077 (approved for the A300-600R aircraft) to be installed on A300-600 aircraft without a trim tank. 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 KIT PRICE (USD) SEE SB
DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 1 7

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# @A300-600 SERVICE BULLETIN SUMMARY 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 286024A01R01 1 198.00 BUNDLE Component COMPB01 See SB TYPE 2 FQIC P/N SIC5077-2 Component COMPB02 See SB TYPE 2 FQIC P/N SIC5077-3 Component COMPB03 See SB TYPE 2 FQIC P/N SIC5077-4 Component COMPA01 1 See SB TIE EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

F2I FDX IRM KAC THA CONCURRENT REQUIREMENTS If operators wish to install an FQIC Part Number SIC5077-4, 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. A300-28-6038 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No. A300-28-6093 (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 LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD YES SOFT NO OBRM NO

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 2 7

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# @A300-600 SERVICE BULLETIN SUMMARY MANPOWER Task 286024-831-895-001: MODIFICATION TOTAL MANHOURS 4.00 ELAPSED TIME (HOURS) 4.00 Task 286024-832-895-001: INSPECTION OF THE FQIC (15QT) - ADDITIONAL WORK TOTAL MANHOURS 2.25 ELAPSED TIME (HOURS) 2.25 APPENDICES None

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 3 7

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# @A300-600 SERVICE BULLETIN SUMMARY

**CONF ALL

FR20

FR1 

### A

Z120



## B 90VU 

## A 15QT

92VU 

### B

D_SB_286024_5_SAAA_01_01 Figure A-FSAAA - Sheet 01

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 4 7

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# @A300-600 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.: 08121H5245 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 B4-601 B4-603 B4-620 B4-622 C4-620 (2) Effectivity by MSN 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0358 0361 0365 0368 0380 0388 0398 0401 0405 0408 0411 0414 0417 (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 F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 FDX 0358 0361 0365 0388 0417 IRM 0380 0401 0405 0408 0411 0414
DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 1 7

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# @A300-600 SERVICE BULLETIN

OPERATOR MSN KAC 0344 THA 0368 0398 (4) Configuration by MSN MSN CONFIGURATION 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0358 0361 0365 0368 0380 0388 0398 0401 0405 0408 0411 0414 0417 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 Component COMPB01 As required (1) Component COMPB02 As required (2) Component COMPB03 As required (3) Kit 286024A01R01 1 Component COMPA01 1 NOTE (1): Component COMPB01 (TYPE 2 FQIC P/N SIC5077-2) NOTE (2): Component COMPB02 (TYPE 2 FQIC P/N SIC5077-3) NOTE (3): Component COMPB03 (TYPE 2 FQIC P/N SIC5077-4) B. CONCURRENT REQUIREMENTS If operators wish to install an FQIC Part Number SIC5077-4, 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. A300-28-6038 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No. A300-28-6093 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled). C. REASON (1) History In order to demonstrate full compliance with SFAR 88 requirements, all Type 1 FQICs P/N SIC5051 shall be replaced with Type 2 FQICs P/N SIC5077. DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 2 7

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# @A300-600 SERVICE BULLETIN In order to install the Type 2 FQICs P/N SIC5077, a wiring change to the aircraft is required. (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 SIC5051 with the Type 2 FQICs P/N SIC5077. (3) Advantages Accomplishment of this Service Bulletin allows the Type 2 FQICs P/N SIC5077 (approved for the A300-600R aircraft) to be installed on A300-600 aircraft without a trim tank. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 286024-831-895-001: MODIFICATION (1) Remove the Type 1 FQIC P/N SIC5051 (15QT) (2) Modify the wiring in the RH electronics rack 90VU (3) Install a Type 2 FQIC P/N SIC5077 (15QT) Task 286024-832-895-001: 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.

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 3 7

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# @A300-600 SERVICE BULLETIN 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. 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 286024-831-895-001: MODIFICATION Get Access 1.00 On Aircraft Remove the Type 1 FQIC P/N SIC5051 (15QT) 0.25 Modify the wiring in the RH electronics rack 90VU 0.50 Install a Type 2 FQIC P/N SIC5077 (15QT) 0.25 Tests 1.00 Close-Up 1.00 TOTAL MANHOURS 4.00 ELAPSED TIME (HOURS) 4.00

Task 286024-832-895-001: 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

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 4 7

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# @A300-600 SERVICE BULLETIN
J. REFERENCES

Aircraft Maintenance Manual (AMM) 24-00-00 28-42-38 52-30-00 52-52-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-52-21 20-55-00 Service Bulletin (SB) A300-28-6038 A300-28-6093 Service Information Letter (SIL) 28-024 Standards Manual (SM) K. PUBLICATION AFFECTED

Aircraft Schematic Manual (ASM) 28-42-00 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 SIC5051-1 SIC5077-2 01 Not Applicable Computer-Fuel Quantity SIC5051-2 SIC5077-2 01 Not Applicable Computer-Fuel Quantity SIC5051-3 SIC5077-2 01 Not Applicable Computer-Fuel Quantity SIC5051-4 SIC5077-2 01 Not Applicable Computer-Fuel Quantity SIC5051-5 SIC5077-2 01 Not Applicable Computer-Fuel Quantity SIC5051-6 SIC5077-2 01 Not Applicable Computer-Fuel Quantity SIC5051-1 SIC5077-3 01 Not Applicable Computer-Fuel Quantity SIC5051-2 SIC5077-3 01 Not Applicable Computer-Fuel Quantity SIC5051-3 SIC5077-3 01 Not Applicable Computer-Fuel Quantity SIC5051-4 SIC5077-3 01 Not Applicable Computer-Fuel Quantity SIC5051-5 SIC5077-3 01 Not Applicable Computer-Fuel Quantity SIC5051-6 SIC5077-3 01 Not Applicable

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 5 7

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# @A300-600 SERVICE BULLETIN

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Computer-Fuel Quantity SIC5051-1 SIC5077-4 01 Not Applicable Computer-Fuel Quantity SIC5051-2 SIC5077-4 01 Not Applicable Computer-Fuel Quantity SIC5051-3 SIC5077-4 01 Not Applicable Computer-Fuel Quantity SIC5051-4 SIC5077-4 01 Not Applicable Computer-Fuel Quantity SIC5051-5 SIC5077-4 01 Not Applicable Computer-Fuel Quantity SIC5051-6 SIC5077-4 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: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 6 7

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# @A300-600 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 286024A01R01 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 Vendor parts are to be procured from: INTERTECHNIQUE 61 Rue Pierre Curie BP 1 78370 Plaisir France

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 7 7

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# @A300-600 SERVICE BULLETIN
Component COMPB03 Vendor parts can alternatively be procured from: GE AVIATION SYSTEMS LTD Bishops Cleeve Cheltenham Gloucestershire GL52 8SF Great Britain (2) Price and Availability

Kit 286024A01R01 Cost 198.00 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. 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 or GE AVIATION SYSTEMS LTD. 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 286024A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES A9000095094995 1 BUNDLE
DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 8 7

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# @A300-600 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 SIC5077-2 FQIC SIC5051-1 01 SIC5051-2 01 SIC5051-3 01 SIC5051-4 01 SIC5051-5 01 SIC5051-6 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 SIC5077-3 FQIC SIC5051-1 01 SIC5051-2 01 SIC5051-3 01 SIC5051-4 01 SIC5051-5 01 SIC5051-6 01 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 9 7

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# @A300-600 SERVICE BULLETIN Component COMPB03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES SIC5077-4 FQIC SIC5051-1 01 (1) SIC5051-2 01 SIC5051-3 01 SIC5051-4 01 SIC5051-5 01 SIC5051-6 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 SIC5077-4 must accomplish either: - Service Bulletin No. A300-28-6038 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No. A300-28-6093 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled). (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 10 7

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# @A300-600 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 286024-831-895-001 - 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 286024-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-52-21 (a) To install new wires, cut them to the necessary length, crimp the terminals and connect them.

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 11 7

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# @A300-600 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 20-52-21). (d) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM 20-25-51). (2) Subtask 286024-839-401-001 - 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 286024-941-401-001 - Job Set-up Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 52-30-00, Page Block 001 52-52-00, Page Block 001 (a) Open the access door 121BL. (b) Open the cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (c) Open the FWD cargo compartment access door 132AZ (Refer to AMM 52-52-00, Page Block 001). (d) Put the access platform in position. (e) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (f) Open, safety and tag this (these) circuit breaker(s): PANEL DESIGNATION FIN LOCATION SEE NOTES 132VU FUEL/FQI/SUPPLY & IND 1QT 321/P59 132VU FUEL/FQI/CHAN SUPPLY 1 3QT 321/P60 132VU FUEL/FQI/CHAN SUPPLY 2 4QT 321/P61

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 12 7

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# @A300-600 SERVICE BULLETIN
C. PROCEDURE (1) Subtask 286024-020-401-001 - Remove the Type 1 FQIC P/N SIC5051 (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 ELECTRICAL References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 (a) Remove the Type 1 FQIC (15QT) as follows (Refer to AMM 28-42-38, Page Block 401): Remove 1 Computer-Fuel Quantity SIC5051-1 Discard

or remove 1 Computer-Fuel Quantity SIC5051-2 Discard

or remove 1 Computer-Fuel Quantity SIC5051-3 Discard

or remove 1 Computer-Fuel Quantity SIC5051-4 Discard

or remove 1 Computer-Fuel Quantity SIC5051-5 Discard

or remove 1 Computer-Fuel Quantity SIC5051-6 Discard

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 13 7

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# @A300-600 SERVICE BULLETIN (2) Subtask 286024-831-001-001 - 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 92VU Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills ELECTRICAL Material necessary to do the job Kit 286024A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES A9000095094995 BUNDLE 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 wires 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 A9000095094995 (b) Attach the wire with: 5 Tie-Cable NSA935401-03 5 Tie-Cable NSA935401-05

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 14 7

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# @A300-600 SERVICE BULLETIN (3) Subtask 286024-420-401-001 - Install a Type 2 FQIC P/N SIC5077 (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 ELECTRICAL Material necessary to do the job Component COMPB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5077-2 FQIC Component COMPB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5077-3 FQIC Component COMPB03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5077-4 FQIC (1) NOTE (1): Operators who wish to install an FQIC Part Number SIC5077-4 must accomplish either: - Service Bulletin No. A300-28-6038 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No. A300-28-6093 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled). References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 Service Information Letter (SIL) 28-024

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 15 7

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# @A300-600 SERVICE BULLETIN (a) Install as applicable one of these FQICs (15QT) (Refer to AMM 28-42-38, Page Block 401 and SIL 28-024): Install a 1 Computer-Fuel Quantity SIC5077-2

or a 1 Computer-Fuel Quantity SIC5077-3

or a 1 Computer-Fuel Quantity SIC5077-4
D. TEST (1) Subtask 286024-710-401-001 - Operational Test of the Type 2 FQIC (15QT) Manpower Resources Skills AIRFRAME 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 132VU FUEL/FQI/SUPPLY & IND 1QT 321/P59 132VU FUEL/FQI/CHAN SUPPLY 1 3QT 321/P60 132VU FUEL/FQI/CHAN SUPPLY 2 4QT 321/P61 (b) Do the operational test of the Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 501). (2) Subtask 286024-720-401-001 - Functional Test of the Type 2 FQIC (15QT) Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 501 (a) Do the functional test of the Type 2 FQIC 15QT (Refer to AMM 28-42-38, Page Block 501).

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 16 7

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# @A300-600 SERVICE BULLETIN
E. CLOSE-UP (1) Subtask 286024-942-401-001 - Close-up Manpower Resources Skills UTILITY 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 access door 121BL. (c) Close the FWD cargo compartment access door 132AZ (Refer to AMM 52-52-00, Page Block 001). (d) Close the cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (e) Remove the access platform.

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 17 7

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# @A300-600 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 18 7

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# @A300-600 SERVICE BULLETIN
Task 286024-832-895-001 - 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 Zone 120 Modified FIN 15QT Access Door 132AZ Manpower TOTAL MANHOURS 2.25 ELAPSED TIME (HOURS) 2.25 A. GENERAL (1) Subtask 286024-839-402-001 - 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 286024-941-402-001 - Job Set-up Manpower Resources Skills UTILITY

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 19 7

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# @A300-600 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 (a) Do the Job Set-up procedure as specified in AMM Task ’Fuel Quantity Computer 15QT - Removal/Installation’ (Refer to AMM 28-42-38, Page Block 401). C. PROCEDURE (1) Subtask 286024-832-401-001 - Inspect the FQIC (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 UTILITY (a) Do an inspection of the FQIC (15QT) to check the part number on the label on the front of the FQIC: 1 If the part number of the FQIC (15QT) is SIC5077-2, SIC5077-3 or SIC5077-4, no action is necessary. Go to SUBTASK 286024-942-402 001 Close-up . 2 If the part number of the FQIC (15QT) is SIC5051-1, SIC5051-2, SIC5051-3, SIC5051-4, SIC5051-5 or SIC5051-6, do SUBTASK 286024-831-401 001 Modification - Replace the Type 1 FQIC (15QT) with a Type 2 FQIC (15QT) . (2) Subtask 286024-831-401-001 - 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 ELECTRICAL Material necessary to do the job Component COMPB01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5077-2 FQIC

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 20 7

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# @A300-600 SERVICE BULLETIN
Component COMPB02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5077-3 FQIC Component COMPB03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES SIC5077-4 FQIC (1) NOTE (1): Operators who wish to install an FQIC Part Number SIC5077-4 must accomplish either: - Service Bulletin No. A300-28-6038 (Mod. No. 10506H5332 and 10862H5388) - Change Auto Fuel Feed System Fault Detection Circuit (with outer tank feeding warning enabled) OR - Service Bulletin No. A300-28-6093 (Mod. No. 13161H5661) - Install A New FQI Computer Standard (with outer tank feeding warning disabled). References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 Service Information Letter (SIL) 28-024 (a) Open, safety and tag this (these) circuit breaker(s): PANEL DESIGNATION FIN LOCATION SEE NOTES 132VU FUEL/FQI/SUPPLY & IND 1QT 321/P59 132VU FUEL/FQI/CHAN SUPPLY 1 3QT 321/P60 132VU FUEL/FQI/CHAN SUPPLY 2 4QT 321/P61 (b) Remove the Type 1 FQIC (15QT) as follows (Refer to AMM 28-42-38, Page Block 401): Remove 1 Computer-Fuel Quantity SIC5051-1 Discard

or remove 1 Computer-Fuel Quantity SIC5051-2 Discard

or remove 1 Computer-Fuel Quantity SIC5051-3 Discard

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 21 7

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# @A300-600 SERVICE BULLETIN

or remove 1 Computer-Fuel Quantity SIC5051-4 Discard

or remove 1 Computer-Fuel Quantity SIC5051-5 Discard

or remove 1 Computer-Fuel Quantity SIC5051-6 Discard (c) Install a Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 401 and SIL 28-024): Install a 1 Computer-Fuel Quantity SIC5077-2

or a 1 Computer-Fuel Quantity SIC5077-3

or a 1 Computer-Fuel Quantity SIC5077-4
D. TEST (1) Subtask 286024-710-402-001 - Operational Test of the Type 2 FQIC (15QT) Manpower Resources Skills AIRFRAME 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 132VU FUEL/FQI/SUPPLY & IND 1QT 321/P59 132VU FUEL/FQI/CHAN SUPPLY 1 3QT 321/P60 132VU FUEL/FQI/CHAN SUPPLY 2 4QT 321/P61 (b) Do the operational test of the Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 501).

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 22 7

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# @A300-600 SERVICE BULLETIN (2) Subtask 286024-720-402-001 - Functional Test of the Type 2 FQIC (15QT) Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 501 (a) Do the functional test of the Type 2 FQIC (15QT) (Refer to AMM 28-42-38, Page Block 501). E. CLOSE-UP (1) Subtask 286024-942-402-001 - Close-up Manpower Resources Skills UTILITY References Aircraft Maintenance Manual (AMM) 28-42-38, Page Block 401 (a) Do the Close-up procedure as specified in AMM Task ’Fuel Quantity Computer 15QT - Removal/Installation’ (Refer to AMM 28-42-38, Page Block 401).

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 23 7

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# @A300-600 SERVICE BULLETIN

**CONF ALL

FR20

FR1 

### A

Z120



## B 90VU 

## A 15QT

D_SB_286024_5_CAAA_01_01 92VU 

### B

Figure A-FCAAA - Sheet 01 Location of the FQI Computer
DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 24 7

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# @A300-600 SERVICE BULLETIN

**CONF ALL

Figure A-FBAAA - Sheet 01 Modification of the Wiring in the Electronics Rack 90VU
DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 25 7

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# @A300-600 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 2842−0839 CF24 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 A9000095094995 A = ADDED WIRE
Figure A-FBBAA - Sheet 01 Hook-up Chart
DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 26 7

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# @A300-600 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUEL - FUEL QUANTITY INDICATING SYSTEM - FQIC INTERCHANGEABILITY MODIFICATION No.: 08121H5245 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: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 1 7

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# @A300-600 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: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024 REVISION No.: 02 - Jan 19/11 Page: 1 7

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