@A300

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 PUMP SYSTEM - INSPECTION OF THE FUEL PUMP

CANISTER HOOD

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A300-28-0089

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision 01 issued to add the Equipment BFEB02 for the Canister Hood PN 3C93-129 (part of Fuel

Pump Canister PN C93R51-601).

CHANGES

SUMMARY

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition CONFIGURATION LIST UPDATED R

Material Effectivity MATERIAL EFFECTIVITY UPDATED R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET QUANTITY UPDATED

MATERIAL SET UPDATED

R

APPROVAL APPROVAL UPDATED R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

LIST OF MATERIALS - OPERATOR

SUPPLIED

Equipment EQUIPMENT UPDATED R

Equipement BFEB01 PART MATERIAL SET UPDATED

NOTE UPDATED

R

Equipement BFEB02 PART MATERIAL SET ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 280089- 832-895-001-INSPECTION TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 280089-941-401-001 SUBTASK SOLUTION UPDATED R

Subtask 280089-832-401-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

Subtask 280089-832-402-002 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

TASK 280089- 833-895-001-REPAIR

Subtask 280089-833-403-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Fig. A-UAAAA

Fig. A-UAAAA Sheet 01 SHEET UPDATED R

Fig. A-UBAAA

Fig. A-UBAAA Sheet 01 SHEET UPDATED R

Fig. A-UBCAA

Fig. A-UBCAA Sheet 01 SHEET UPDATED R

Fig. A-UCAAA

Fig. A-UCAAA Sheet 01 SHEET UPDATED R

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

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Jan 13/11

REVISION No. : 01 - Apr 15/11

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

REVISION No.: 01 - Apr 15/11 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

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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 PUMP SYSTEM - INSPECTION OF THE FUEL PUMP

CANISTER HOOD

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Some operators have reported cases of cracking on the hood of the inboard and outboard fuel pump

canisters located in the inner fuel tanks. The hood is part of the fuel pump canister and forms a surface

between the pump inlet mesh and the canister body. The hood is fabricated from thin aluminium alloy in

two halves.

On one aircraft the detached parts were reported as consisting of two separate pieces. One annular

section was subsequently found in the fuel tank.

This Inspection Service Bulletin (ISB) introduces a repetitive Detailed Visual Inspection (DVI) of all fuel

pump locations (center, wing-inner and wing-outer). The inspection will also assess which locations are

subject to such cracking, hood halves with cracks must be replaced. The Inspection must be done not

more than 30 months after the issue date of this Service Bulletin and repeated every 30 months.

Replacement of failed hood halves will prevent possible contamination issues and establish which

locations are subject to cracking. Replace both hood halves if cracks are found in one of the two

halves. You must find and remove all broken pieces from the fuel tanks.

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

DEFUEL/VENTILATION YES PRE-ENTRY CHECKLIST YES

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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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

Equipment BFEB01 1 See SB Hood Halves

Equipment BFEB02 1 See SB Hood Halves

EFFECTIVITY

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

50W 69X 72U ABR AFG C2A DHL F2I FLM IAW IRA IRM JLJ

KYE KZU MIX MNB MSR NTR P2A RUN SOP TNO TSY

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 28.21.13.001

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 280089-832-895-001: INSPECTION

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 5.00

Task 280089-833-895-001: REPAIR

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

APPENDICES

Inspection Findings - Reporting Sheet

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@A300

SERVICE BULLETIN

SUMMARY

**CONF ALL

B

LH WING SHOWN

RH WING SIMILAR

RIB14

RIB2

Z550 (Z650)

TYPICAL

Z540 (Z640)

A_SB_280089_7_SAAA_01_01

A

FR47

FR46

C

C

C

C

C

A

Z141 Z142 − 

B

Figure A-USAAA - Sheet 01

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

REVISION No.: 01 - Apr 15/11 Page: 4

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@A300

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 PUMP SYSTEM - INSPECTION OF THE FUEL PUMP

CANISTER HOOD

MODIFICATION No.: None

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

B2-1C B2-203 B2K-3C B4-103 B4-120 B4-203 B4-2C C4-203

F4-203

(2) Effectivity by MSN

0003 0019 0041 0045 0047 0053 0055 0075 0079-0080 0082-0085 0090 0094-0095

0100-0101 0105 0107 0116-0117 0123-0126 0128-0129 0133-0137 0139 0141

0147-0152 0154-0157 0160 0170 0173 0175-0176 0180 0183-0185 0187 0189-0190

0196 0199-0200 0203-0204 0208 0210-0212 0216 0218-0220 0226-0227 0234-0236

0239 0243-0244 0247 0249-0250 0255-0256 0259 0261 0265 0274 0277 0289 0292

0299 0302 0304

(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.

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@A300

SERVICE BULLETIN

OPERATOR MSN

50W 0003

69X 0095

72U 0079

ABR 0148 0152 0184 0189 0199 0208 0219 0220 0234 0236 0250 0259

0274 0289

AFG 0180 0190

C2A 0211

DHL 0084 0085 0141 0149 0249 0265

F2I 0083 0094 0128 0133 0135 0136 0137 0156 0170 0235 0243

FLM 0082

IAW 0239

IRA 0080 0139 0151 0173 0185 0187 0226 0256 0299 0302

IRM 0055 0090 0160 0175 0204 0244

JLJ 0176

KYE 0053 0100 0216

KZU 0041 0101 0117

MIX 0125 0134 0157 0196 0203 0218

MNB 0019 0047 0123 0212 0277 0292 0304

MSR 0200 0255

NTR 0124 0155 0261

P2A 0116 0150

RUN 0075 0105 0107 0147 0154 0183

SOP 0126

TNO 0045 0210 0227 0247

TSY 0129

(4) Configuration by MSN

MSN CONFIGURATION

0003 0019 0041 0045 0047 0053 0055 0075 0079 0080 0082

0083 0084 0085 0090 0094 0095 0100 0101 0105 0107 0116

0117 0123 0124 0125 0126 0128 0129 0133 0134 0135 0136

0137 0139 0141 0147 0148 0149 0150 0151 0152 0154 0155

0156 0157 0160 0170 0173 0175 0176 0180 0183 0184 0185

0187 0189 0190 0196 0199 0200 0203 0204 0208 0210 0211

0212 0216 0218 0219 0220 0226 0227 0234 0235 0236 0239

0243 0244 0247 0249 0250 0255 0256 0259 0261 0265 0274

0277 0289 0292 0299 0302 0304

001

(5) Configuration definition

NOTE: This Service Bulletin is only applicable to A300 aircraft that have Fuel

Pump Canister Hood PN 205481 (part of Fuel Pump Canister PN

2052C11 or PN 2052C12) or PN 3C93-129 (part of Fuel Pump Canister

PN C93R51-601) installed.

**CONF 001

Config. 001 is applicable to all the aircraft listed in the effectivity of this Service Bulletin

as a standard configuration.

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SERVICE BULLETIN

(6) Material Effectivity

NOTE: One BFEB01 or BFEB02 is required for each Fuel Pump Canister. The

total quantity of BFE kits will be determined by the result of the

inspection requirements of this Service Bulletin.

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEB01 1

Equipment BFEB02 1

Consumable CMLB01 As required

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Some operators have reported cases of cracking on the hood of the inboard and

outboard fuel pump canisters located in the inner fuel tanks. The hood is part of the fuel

pump canister and forms a surface between the pump inlet mesh and the canister body.

The hood is fabricated from thin aluminium alloy in two halves.

On one aircraft the detached parts were reported as consisting of two separate pieces.

One annular section was subsequently found in the fuel tank.

(2) Objective/Action

This Inspection Service Bulletin (ISB) introduces a repetitive Detailed Visual Inspection

(DVI) of all fuel pump locations (center, wing-inner and wing-outer). The inspection will

also assess which locations are subject to such cracking, hood halves with cracks must

be replaced. The Inspection must be done not more than 30 months after the issue date

of this Service Bulletin and repeated every 30 months.

(3) Advantages

Replacement of failed hood halves will prevent possible contamination issues and

establish which locations are subject to cracking. Replace both hood halves if cracks are

found in one of the two halves. You must find and remove all broken pieces from the

fuel tanks.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 280089-832-895-001: INSPECTION

(1) INSPECTION OF THE WING TANKS (INNER/OUTER) PUMP CANISTER HOOD

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SERVICE BULLETIN

HALVES

(2) INSPECTION OF THE CENTER TANK PUMP CANISTER HOOD HALVES (IF

FITTED)

Task 280089-833-895-001: REPAIR

(1) REPAIR THE FUEL PUMP CANISTER HOOD HALVES

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Do this Inspection not more than 30 months after the date you receive this Service

Bulletin and repeat every 30 months.

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 (thresholds and/or intervals

and/or date) given above but reference should be made to the AD for confirmation of the

mandated accomplishment timescale.

F. APPROVAL

The technical content of this document is approved under authority of Design Organization

Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

Task 280089-832-895-001: INSPECTION

Get Access 2.00

On Aircraft

INSPECTION OF THE WING TANKS (INNER/OUTER)

PUMP CANISTER HOOD HALVES

4.00

INSPECTION OF THE CENTER TANK PUMP

CANISTER HOOD HALVES (IF FITTED)

1.00

Close-Up 2.00

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

Task 280089-832-895-001: INSPECTION

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 5.00

Task 280089-833-895-001: REPAIR

On Aircraft

REPAIR THE FUEL PUMP CANISTER HOOD

HALVES

0.50

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-21-00 06-21-53 06-21-57

28-00-00 28-10-00 28-11-00

28-11-14 28-21-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-55-00

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Vendor parts are to be procured from:

Equipment BFEB01

Equipment BFEB02

INTERTECHNIQUE

M. Jean_Pierre Michel

Bd Sagnat BP3

4220 ROCHE-LA-MOLIERE, FRANCE

(2) Price and Availability

Procurement terms for the equipment must be negotiated with the equipment supplier.

(MATERIAL INFORMATION).

B. INDUSTRY SUPPORT INFORMATION

Refer to the paragraph: ’Price and Availability’.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

Equipment BFEB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 205481 2 HOODHALF (1) 205481 (1) (2) (1)

(2)

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NOTE (1): One BFEB01 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 205481 for Fuel Pump Canister PN 2052C11 or PN

2052C12.

Equipment BFEB02

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

4 3C93-129 2 HOODHALF (4) 3C93-129 (1) (2) (1)

(2)

NOTE (1): One BFEB02 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 280089-832-895-001 - INSPECTION

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

141 142 542 550 642 650

Modified FIN

280014 280015 280016 280017 280018 280019 280020 280021 280022 280023

Access

Door 147AZ 148AZ 542CB 550BB 642CB 650BB

Manpower

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 5.00

A. GENERAL

(1) Subtask 280089-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-21-00

06-21-53

06-21-57

28-00-00, Page Block 301

28-10-00, Page Block 301

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(a) For the identification of Access Panels (Refer to AMM 06-21-57 and AMM

06-21-53).

(b) For the identification of Zones (Refer to AMM 06-21-00).

(c) Obey the safety procedures when you do work in a fuel tank (Refer to AMM

28-10-00, Page Block 301 and AMM 28-00-00, Page Block 301).

(2) Subtask 280089-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

(1) Subtask 280089-941-401-001 - JOB SET-UP - WING AND CENTER TANKS (IF

FITTED)

Work Zones and Access Panels

Zone Access/Work location

542 Access Door 542CB

550 Access Door 550BB

642 Access Door 642CB

650 Access Door 650BB

141 Access Door 147AZ

142 Access Door 148AZ

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

28-10-00, Page Block 301

28-11-00, Page Block 601

28-11-14, Page Block 401

28-21-00, Page Block 601

Consumable Material List (CML)

WARNING: YOU MUST OBEY ALL THE SAFETY PROCEDURES WHEN YOU DO

WORK IN OR NEAR A FUEL TANK. IF YOU DO NOT OBEY THE

SAFETY PROCEDURES, THERE IS A RISK OF:

- DEATH OR INJURY TO PERSONS

- DAMAGE TO THE AIRCRAFT OR TO OTHER EQUIPMENT.

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(a) Prepare the aircraft as specified in AMM Task ’STORAGE - SERVICING (Fuel

Tank Draining, Venting and Entry)’ (Refer to AMM 28-10-00, Page Block 301).

1 Before you go into a fuel tank you must complete the Pre-Entry Checklist

(Refer to AMM 28-10-00, Page Block 301).

(b) Put platforms in position to get access to the applicable zones (Refer to AMM

06-21-00, Page Block 001):

1 Wing tanks inner - Zones 542 LH (642 RH) (Refer to AMM 28-11-14, Page

Block 401 and (Refer to AMM 28-21-00, Page Block 601).

2 Wing tanks outer - Zones 550 LH (650 RH) (Refer to AMM 28-11-14, Page

Block 401 and AMM 28-21-00, Page Block 601).

3 Center tank (if fitted) - Zones 141 and 142 (Refer to AMM 28-11-14, Page

Block 401 and AMM 28-21-00, Page Block 601).

(c) Remove the applicable manhole covers:

1 Wing tanks inner 542CB LH (642CB RH) (Refer to AMM 28-11-14, Page Block

401 and AMM 28-21-00, Page Block 601).

2 Wing tanks outer 550BB LH (650BB RH) (Refer to AMM 28-11-14, Page Block

401 and AMM 28-21-00, Page Block 601).

3 Center tank (if fitted) 147AZ LH and 148AZ RH (Refer to AMM 28-11-14, Page

Block 401 and AMM 28-21-00, Page Block 601).

(d) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Material List (CML).

C. PROCEDURE

NOTE: Operators can have the Fuel Pump Canister Hood PN 205481 (part of Fuel

Pump Canister PN 2052C11 or PN 2052C12) or PN 3C93-129 (part of Fuel

Pump Canister PN C93R51-601) installed.

(1) Subtask 280089-832-401-001 - INSPECTION OF THE WING TANKS (INNER/OUTER)

PUMP CANISTER HOOD HALVES

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills AIRFRAME

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UAAAA

Inspection Flowchart

Sheet 01

Fig. A-UBAAA

Fuel Pump Canister Hood Halves

Inspection - Wing Tanks

Sheet 01

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

(a) Clean the

2 Hood Half 205481 Item (1)

with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

(b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the

wing tanks:

- Wing tank (LH) - inboard FIN 280014 and FIN 280016 and outboard FIN

280018 and FIN 280020

- Wing tank (RH) - inboard FIN 280015 and FIN 280017 and outboard FIN

280019 and FIN 280021.

(Refer to Fig. A-UAAAA, and Fig. A-UBAAA).

1 No cracks found in

2 Hood Half 205481 Item (1)

a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

2 Cracks are found in

2 Hood Half 205481 Item (1)

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SERVICE BULLETIN

a Replace the Hood Halves.

(Refer to TASK 280089-833-895 001 REPAIR and Fig. A-UCAAA).

b Make sure that all broken parts and unwanted materials are removed from the

related tank.

c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

(c) Send the inspection results to AIRBUS (Refer to Inspection Findings - Reporting

Sheet ).

(2) Subtask 280089-832-402-002 - INSPECTION OF THE CENTER TANK PUMP

CANISTER HOOD HALVES (IF FITTED)

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UAAAA

Inspection Flowchart

Sheet 01

Fig. A-UBCAA

Fuel Pump Canister Hood Halves

Inspection - Center Tank

Sheet 01

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

(a) Clean the

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

with a

Lint-Free Cotton

Cloth

19-003 As required

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

made moist with

Solvent 11-583 As required

(b) Do a Detailed Visual Inspection (DVI) to the fuel pump canister hood halves in the

center tank (if fitted) - LH FIN 280022 and RH FIN 280023 (Refer to Fig. A-UAAAA,

and Fig. A-UBCAA).

1 No cracks found in

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

a Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

2 Cracks are found in

2 Hood Half 205481 Item (1)

or

2 Hood Half 3C93-129 Item (4)

a Replace the Hood Halves.

(Refer to TASK 280089-833-895 001 REPAIR and Fig. A-UCAAA).

b Make sure that all broken parts and unwanted materials are removed from the

related tank.

c Make a record of the results (Refer to Inspection Findings - Reporting Sheet ).

(c) Send the inspection results to AIRBUS (Refer to Inspection Findings - Reporting

Sheet ).

D. TEST

None

E. CLOSE-UP

(1) Subtask 280089-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

(a) Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING

(Fuel Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM

28-10-00, Page Block 301).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

Task 280089-833-895-001 - REPAIR

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

Manpower

TOTAL MANHOURS 0.50

ELAPSED TIME (HOURS) 0.50

A. GENERAL

(1) Subtask 280089-839-402-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

C. PROCEDURE

(1) Subtask 280089-833-403-001 - REPAIR THE FUEL PUMP CANISTER HOOD

HALVES

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Equipment BFEB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 205481 2 HOODHALF (1) (2)

NOTE (1): One BFEB01 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 205481 for Fuel Pump Canister PN 2052C11 or PN

2052C12.

Equipment BFEB02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 3C93-129 2 HOODHALF (1) (2)

NOTE (1): One BFEB02 is required for each Fuel Pump Canister. The total

quantity of BFE kits will be determined by the result of the inspection

requirements of this Service Bulletin.

NOTE (2): Canister Hood PN 3C93-129 for Fuel Pump Canister PN C93R51-601.

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-583 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UCAAA

Repair the Fuel Pump Canister Hood

Halves - Typical

Sheet 01

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

REVISION No.: 01 - Apr 15/11 Page: 18

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SERVICE BULLETIN

(a) Replace the fuel pump canister hood halves, do the steps that follow (Refer to Fig.

A-UCAAA Sheet 01):

1 Clean the surface area of the fuel pump canister with a

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent 11-583 As required

2 Remove:

6 Screw Item (2) Retain

6 Washer Item (3) Retain

2 Hood Half 205481 Item (1) Discard

or

2 Hood Half 3C93-129 Item (4) Discard

NOTE: If there are defective parts they must be replaced (Refer to the

Vendor Intertechnique for replacement parts).

NOTE: The discarded hood halves have to be replaced with a new

ones with the same Part Number.

3 Install:

2 Hood Half 205481 Item 1

or

2 Hood Half 3C93-129 Item 4

with:

6 Screw Item (2) Retained at

removal

6 Washer Item (3) Retained at

removal

(b) Make sure that all broken parts and unwanted materials are removed from the

related tank.

D. TEST

None

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

E. CLOSE-UP

(1) Subtask 280089-942-402-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 28-10-00, Page Block 301

Do the Close Up procedure as specified in AMM Task ’STORAGE - SERVICING (Fuel

Tank Draining, Venting and Entry - Leaving the Fuel Tank)’ (Refer to AMM 28-10-00,

Page Block 301).

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

**CONF ALL

NO YES

INSPECTION OF CANISTER

HOODS INSTALLED ON FUEL

PUMP CANISTER P/Ns 2052C11

OR 2052C12 OR C93R51−601

REPORT

TO

AIRBUS

IS THE

CANISTER

HOOD

CRACKED?

REPLACE

CANISTER

HOOD

RECORD

LOCATION

(FIN)

REPORT

LOCATION (FIN)

TO AIRBUS

A_SB_280089_7_AAAA_01_03

PERFORM REPEAT

INSPECTION WITHIN

30 MONTHS OF

PREVIOUS

INSPECTION

PERFORM REPEAT

INSPECTION WITHIN

30 MONTHS OF

PREVIOUS

INSPECTION

Figure A-UAAAA - Sheet 01

Inspection Flowchart

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

**CONF ALL

LH WING SHOWN

RH WING SIMILAR

FUEL PUMP

CANISTER

TYPICAL DAMAGE

HOOD

HALF

HOOD

HALF

SCREW AND

WASHER

(6 OFF)

B

A

RIB14

RIB2

Z550 (Z650)

A

TYPICAL

A

FILTER

B

Z542 (Z642)

A_SB_280089_7_BAAA_01_03

HOOD

HALF

Figure A-UBAAA - Sheet 01

Fuel Pump Canister Hood Halves Inspection - Wing Tanks

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

**CONF ALL

TYPICAL DAMAGE

TYPICAL

FR47

FR46

Z141 Z142 − 

A

FUEL PUMP

CANISTER

HOOD

HALF

HOOD

HALF

SCREW AND

WASHER

(6 OFF) FILTER

B

B

A

B

C

C

A_SB_280089_7_BCAA_01_02

HOOD

HALF

Figure A-UBCAA - Sheet 01

Fuel Pump Canister Hood Halves Inspection - Center Tank

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

**CONF ALL

FUEL PUMP

CANISTER

A A

A

TYPICAL

A_SB_280089_7_CAAA_01_01

(2) (3)

(1) 1

(4) 4

(3)

(2)

(2) (3)

Figure A-UCAAA - Sheet 01

Repair the Fuel Pump Canister Hood Halves - Typical

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SERVICE BULLETIN

Inspection Findings - Reporting Sheet

**CONF ALL

Complete the Table below by ticking the appropriate finding for each inspection location:

SERVICE BULLETIN NO.

A300-28-0089

A/C MSN: Date of Inspection:

FLIGHT HOURS:

FLIGHT CYCLES

LOCATION FIN FINDING

YES NO

280014

280015

280016

280017

280018

280019

280020

280021

280022

280023

INSPECTION REPORT

Return the completed Inspection Report to AIRBUS.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FUEL - FUEL PUMP SYSTEM - INSPECTION OF THE FUEL PUMP

CANISTER HOOD

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

REVISION No.: 01 - Apr 15/11 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: Jan 13/11 SERVICE BULLETIN No.: A300-28-0089

REVISION No.: 01 - Apr 15/11 Page: 1

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