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@A300
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 ATA SYSTEM: 28 TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL FUEL PUMP CANISTER
WITH NEW HOOD/MESH IN INNER AND CENTER TANK POSITIONS MODIFICATION No.: 13644H5743 13739H5755 This page transmits Revision No.01 of Service Bulletin No.A300-28-0092
ADDITIONAL WORK **CONF ALL Additional work is required by this revision for aircraft modified by the original issue of this Service Bulletin.
REASON Revision No. 01 issued to:
- add modification No. 13739H5755 (Introduction of Longer Screws at the outer positions on the canister hoods for Post-MOD 13644)
- update the procurement address in paragraph 2.A.(1).
The opportunity is taken to make minor format changes.
CHANGES
FRONT MATTER
MODIFICATIONS
MODIFICATION NUMBER(S) UPDATED R
SUMMARY
MODIFICATIONS
MODIFICATION CLASSIFICATION UPDATED R
MANPOWER
MANPOWER UPDATED R
MANPOWER UPDATED R
PLANNING INFORMATION
EFFECTIVITY
EFFECTIVITY RELATED INFORMATION
UPDATED R Configuration definition CONF 002
CONFIGURATION DEFINITION UPDATED R Material Effectivity
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL SET UPDATED R DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL SET UPDATED R
APPROVAL
APPROVAL UPDATED R
MANPOWER
MANPOWER UPDATED R
MANPOWER UPDATED
CONFIGURATION UPDATED R
MANPOWER UPDATED
CONFIGURATION UPDATED R
REFERENCES
REFERENCED DOCUMENTATION UPDATED R
REFERENCED DOCUMENTATION UPDATED R
INTERCHANGEABILITY/MIXABILITY
INTERCHANGEABILITY/MIXABILITY UPDATED R
INTERCHANGEABILITY/MIXABILITY UPDATED R
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY Procurement Addresses
PROCUREMENT ADDRESSES UPDATED R
LIST OF MATERIALS - OPERATOR
SUPPLIED Equipment Equipement BFEB01
PART MATERIAL SET UPDATED
PART NUMBER UPDATED R Equipement BFEB02
PART MATERIAL SET UPDATED
PART NUMBER UPDATED R
PARTS TO BE RE-IDENTIFIED BY
OPERATOR
PARTS TO BE RE-IDENTIFIED BY OPERATOR
UPDATED R Reidentified part set REIDB01
PART MATERIAL SET UPDATED
PART NUMBER UPDATED R Reidentified part set REIDB02
PART MATERIAL SET UPDATED
QUANTITY UPDATED
PART NUMBER UPDATED R Reidentified part set REIDB03
PART MATERIAL SET ADDED N Reidentified part set REIDB04
PART MATERIAL SET ADDED N
ACCOMPLISHMENT INSTRUCTIONS TASK 280092- 831-895-001-Modification
TASK SOLUTION UPDATED
CAUTION UPDATED
NOTE UPDATED R Task associated data - 001
ZONE UPDATED
PANEL UPDATED R Subtask 280092-910-401-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 280092-910-401-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 280092-941-401-001
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 280092-941-401-002
SUBTASK SOLUTION UPDATED
NOTE UPDATED R DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Subtask 280092-831-401-001
SUBTASK SOLUTION UPDATED
PANEL UPDATED
ZONE UPDATED
PART NUMBER UPDATED
LOCATION UPDATED
MATERIAL LIST UPDATED R Subtask 280092-930-401-001
SUBTASK SOLUTION UPDATED
PART NUMBER UPDATED
MATERIAL LIST UPDATED R Subtask 280092-831-401-002
SUBTASK SOLUTION UPDATED
PART NUMBER UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
MATERIAL LIST UPDATED R Subtask 280092-930-401-002
SUBTASK SOLUTION UPDATED
PART NUMBER UPDATED
MATERIAL LIST UPDATED R Subtask 280092-700-401-001
SUBTASK SOLUTION UPDATED R Subtask 280092-700-401-001
SUBTASK SOLUTION UPDATED R Subtask 280092-942-401-001
SUBTASK SOLUTION UPDATED R Subtask 280092-942-401-002
SUBTASK SOLUTION UPDATED R TASK 280092- 831-896-001-Modification for aircraft that have accomplished this Service Bulletin at Rev 00 - ADDITIONAL WORK
TASK SOLUTION ADDED N Task associated data - 001
TASK ASSOCIATED DATA ADDED N Task associated data - 002
TASK ASSOCIATED DATA ADDED N Subtask 280092-910-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-839-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-910-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-839-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-941-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-941-402-002
SUBTASK SOLUTION ADDED N Subtask 280092-831-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-930-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-831-402-002
SUBTASK SOLUTION ADDED N Subtask 280092-930-402-002
SUBTASK SOLUTION ADDED N Subtask 280092-700-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-700-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-942-402-001
SUBTASK SOLUTION ADDED N Subtask 280092-942-402-002
SUBTASK SOLUTION ADDED N Appendix 01 - Elapsed Time Assumption Fig. A-UAAAB
FIGURE SOLUTION ADDED N Fig. A-UAAAB Sheet 01
SHEET ADDED N Fig. A-UABAA
FIGURE SOLUTION UPDATED
CONFIGURATION UPDATED R Fig. A-UABAA Sheet 01
SHEET UPDATED R DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Fig. A-UABAB
FIGURE SOLUTION ADDED N Fig. A-UABAB Sheet 01
SHEET ADDED N
FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS No previous revision
REVISION SEQUENCE ORIGINAL: Dec 12/13 REVISION No. : 01 - Aug 29/14 DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
SUMMARY AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 This summary is for information only and is not approved for modification of the aircraft.
ATA SYSTEM: 28 TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL FUEL PUMP CANISTER
WITH NEW HOOD/MESH IN INNER AND CENTER TANK POSITIONS **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR 13644H5743 MINOR 13739H5755 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 Fuel pump canisters are located in pairs in all fuel tanks. There is a fabricated aluminium hood (in two halves) which forms a surface between the fuel pump inlet mesh and the fuel pump canister body.
Some operators have reported cases of cracking on the hood in the inner wing fuel tanks. On one aircraft, part of the hood detached and was found inside the fuel tank.
Fuel pump canister hoods are currently subject to a mandatory inspection in accordance with Inspection Service Bulletin A300-28-0089.
Following the investigation into in-service failures, this Service Bulletin introduces new canister hoods for the wing inner tank and the center tank fuel pumps (where fitted) only. No other fuel pump positions are affected by this Service Bulletin.
The new design consists of a new two part stainless steel hood assembly that is installed over the existing inlet mesh as before. To account for tolerances in the inlet mesh diameter and to avoid installation pre-stress, each hood half has an enlarged central hole, through which a stepped fastener is installed.
Accomplishment of this Service Bulletin will reduce the scope of the Inspection Service Bulletin A300-28-0089 and will be captured in any future Airworthiness Directive. Accomplishment of this Service Bulletin will also cancel the repeat inspection requirement of the inner wing and center tanks (only).
The installation of a new fuel pump canister hood changes the part number of the canister assembly.
DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
SUMMARY
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE RECOMMENDED (1)
CANCELS INSPECTION SB NO
POTENTIAL AD NO
A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO
DEFUEL/VENTILATION YES
PRE-ENTRY CHECKLIST YES NOTE
(1) : Service Bulletin recommended to be accomplished to prevent significant operational disruptions.
MATERIAL PRICE INFORMATION **CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Equipment BFEB01 4 See SB Hood Halves and Attachments **CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Equipment BFEB01 4 See SB Hood Halves and Attachments Equipment BFEB02 2 See SB Hood Halves and Attachments
EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :
001 50W 81T ABR AFG F2I IAW IRA IRM KZU MNB MSR RUN
SOP TIW TNO TSY
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
SUMMARY OTHER None
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT YES HARD NO SOFT NO OBRM NO
MANPOWER **CONF 001 Task 280092-831-895-001: Modification
TOTAL MANHOURS
11.00
ELAPSED TIME (HOURS)
7.00 Task 280092-831-896-001: Modification for aircraft that have accomplished this Service Bulletin at Rev 00 - ADDITIONAL WORK
TOTAL MANHOURS
7.00
ELAPSED TIME (HOURS)
5.00 **CONF 002 Task 280092-831-895-001: Modification
TOTAL MANHOURS
15.00
ELAPSED TIME (HOURS)
9.00 Task 280092-831-896-001: Modification for aircraft that have accomplished this Service Bulletin at Rev 00 - ADDITIONAL WORK
TOTAL MANHOURS
9.00
ELAPSED TIME (HOURS)
6.00
APPENDICES **CONF ALL Appendix 01 - Elapsed Time Assumption DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
SUMMARY **CONF 001
TYPICAL TYPICAL RIB2
LH WING SHOWN
RH WING SIMILAR Z542 (Z642)A A A B B C C
BEFORE AFTER NOTE:
AREA OF MODIFICATION.
FUEL PUMP
CANISTER
HOOD HALF
FUEL PUMP
CANISTER
HOOD HALF A_SB_280092_7_SAAA_01_01 Figure A-USAAA - Sheet 01 DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
SUMMARY **CONF 002 A B BEFORE
TYPICAL AFTER
TYPICAL C D RIB2
LH WING SHOWN
RH WING SIMILAR FR46 FR47 Z542 (Z642) A B
FUEL PUMP
CANISTER
HOOD HALF
FUEL PUMP
CANISTER
HOOD HALF C C C NOTE:
AREA OF MODIFICATION.
D A_SB_280092_7_SBAA_01_00 − Z142Z141 B Figure A-USBAA - Sheet 01 DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 5 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
SUMMARY This Page Intentionally Left Blank DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 6 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 ATA SYSTEM: 28 TITLE: FUEL - MAIN FUEL PUMP SYSTEM - INSTALL FUEL PUMP CANISTER
WITH NEW HOOD/MESH IN INNER AND CENTER TANK POSITIONS MODIFICATION No.: 13644H5743 13739H5755 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 B4-203 B4-2C C4-203 F4-203
(2) Effectivity by MSN 0003 0045 0055 0075 0080 0090 0101 0105 0107 0117 0126 0129 0139 0151-0152 0154 0157 0160 0173 0175 0180 0183 0185 0187 0200 0203-0204 0210 0212 0218 0220 0226-0227 0234-0236 0239 0244 0247 0255-0256 0259 0261 0274 0277 0292 0299 0302
(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 001 0203 0218 50W 0003 81T 0157 0277 0292 ABR 0152 0220 0259 0274 DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300
SERVICE BULLETIN
OPERATOR MSN AFG 0180 F2I 0235 IAW 0239 IRA 0080 0139 0151 0173 0185 0187 0226 0256 0299 0302 IRM 0055 0090 0160 0175 0204 0244 KZU 0101 0117 MNB 0212 MSR 0200 0255 RUN 0075 0105 0107 0154 0183 SOP 0126 TIW 0234 0236 0261 TNO 0045 0210 0227 0247 TSY 0129
(4) Configuration by MSN MSN
CONFIGURATION 0003 0080 0090 0160 0185 0187 0226 0244 001 0045 0055 0075 0101 0105 0107 0117 0126 0129 0139 0151 0152 0154 0157 0173 0175 0180 0183 0200 0203 0204 0210 0212 0218 0220 0227 0234 0235 0236 0239 0247 0255 0256 0259 0261 0274 0277 0292 0299 0302 002
(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 aircraft without a center tank installed (Aircraft Model B2).
**CONF 002 Config. 002 is applicable to aircraft with a center tank installed (Aircraft Model B4).
(6) Material Effectivity **CONF 001
MATERIAL
QTY PER A/C
SEE NOTES Consumable CMLB01 As required Equipment BFEB01 4
(1) Reidentified part set REIDB01 1 Reidentified part set REIDB03 1 (2 ) NOTE
(1) : One Kit BFEB01 is required for each Wing Inner Tank Fuel Pump Canister.
DATE: Dec 12/13 SERVICE BULLETIN No.: A300-28-0092 REVISION No.: 01 - Aug 29/14 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.