@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

MANDATORY MANDATORY MANDATORY

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

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

Material Effectivity Minor editorial or document structure change N

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

APPROVAL Minor editorial or document structure change N

Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

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

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

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

TASK 286024- 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

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

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

MANDATORY MANDATORY MANDATORY

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

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

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

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

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

MANDATORY MANDATORY MANDATORY

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

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

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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. EASA 21J.031.

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024

REVISION No.: 02 - Jan 19/11 Page: 3

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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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(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

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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

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This Page Intentionally Left Blank

DATE: Feb 27/91 SERVICE BULLETIN No.: A300-28-6024

REVISION No.: 02 - Jan 19/11 Page: 18

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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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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

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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

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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

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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

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**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

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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

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**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

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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

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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

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