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@A318/A319/A320/A321
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
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 28 TITLE: FUEL - INDICATING - INTRODUCE COMMON FUEL LEVEL SENSOR
SUPPORT BRACKET MODIFICATION No.: 158133J4169 NOTE : This modification is related to an airworthiness issue which has been re-classified and confirmed by EASA as minor in acco rdance with EU Part 21.A.91. As such, this is handled by AIRBUS under its Design Organisation Approval No.
EASA.21J.031.
This page transmits Revision No.01 of Service Bulletin No.A320-28-1239
ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue.
REASON Revision No. 01 issued to:
- Update the effectivity
- Update the commercial policy
- Update KITB01 and KITB02 to give the corre ct left hand (LH) and right hand (RH) Bracket Assy- Support part numbers
- Correct the old and new Bracket Assy-Support par t number associations for both LH and RH parts
- Remove the Job Set-up and Close-up work steps relating to the transfer of fuel from/to the surge tanks.
CHANGES The main changes of this revision are:
- Aircraft added to the effectivity paragraph
- Effectivity by Operator updated DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
- Paragraph 1.L. INT ERCHANGEABILITY/MIXABILITY updated
- Commercial policy updated
- KITB01 updated to give correct LH Bracket Assy-Support part number
- KITB02 updated to give correct RH Bracket Assy-Support part number
- Job Set-up and Close-up updated to remove work steps relating to the transfer of fuel from/to the surge tanks
- Service Bulletin Information Transmission (SBIT) 16-0081 added to the REFERENCES / REPERCUSSIONS table.
SUMMARY
REASON/DESCRIPTION/OPERATIONAL
CONSEQUENCES
REASON UPDATED R
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
UPDATED R
EFFECTIVITY
OPERATOR LIST UPDATED R
REFERENCES / REPERCUSSIONS
REFERENCES/REPERCUSSIONS TABLE
UPDATED R
PLANNING INFORMATION
EFFECTIVITY
EFFECTIVITY RELATED INFORMATION
UPDATED R Configuration definition CONF 001
CONFIGURATION DEFINITION UPDATED R Material Effectivity
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET UPDATED R REASON Advantages
ADVANTAGES UPDATED R
REFERENCES
REFERENCED DOCUMENTATION UPDATED R
INTERCHANGEABILITY/MIXABILITY
INTERCHANGEABILITY/MIXABILITY UPDATED R
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY Procurement Addresses
PROCUREMENT ADDRESSES UPDATED
MATERIAL SET UPDATED R Price and Availability
PRICE AND AVAILABILITY UPDATED
MATERIAL AVAILABILITY UPDATED
MATERIAL SET UPDATED
MATERIAL PRICE UPDATED R
LIST OF COMPONENTS Kit 281239B01R02
PART MATERIAL SET UPDATED
MATERIAL SET LABEL UPDATED
PART NUMBER UPDATED R Kit 281239B02R02
PART MATERIAL SET UPDATED
MATERIAL SET LABEL UPDATED
PART NUMBER UPDATED R DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
ACCOMPLISHMENT INSTRUCTIONS TASK 281239- 831-895-001-Modification
TASK SOLUTION UPDATED
NOTE UPDATED
CAUTION UPDATED R Subtask 281239-941-401-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED R Subtask 281239-960-401-001
SUBTASK SOLUTION UPDATED
PART NUMBER UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED R Subtask 281239-960-402-001
SUBTASK SOLUTION UPDATED
PART NUMBER UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED R Subtask 281239-942-401-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
PANEL UPDATED
REFERENCES UPDATED R
FILING 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: Nov 22/16 REVISION No. : 01 - Sep 15/17 DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET This Page Intentionally Left Blank DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
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.
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 28 TITLE: FUEL - INDICATING - INTRODUCE COMMON FUEL LEVEL SENSOR
SUPPORT BRACKET **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR None MINOR 158133J4169 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.
NOTE : This modification is related to an airworthiness issue which has been re-classified and confirmed by EASA as minor in accordance with EU Part 21.A.91. As such, this is handled by AIRBUS under its D esign Organisation Approval No. EASA.21J.031.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Embodiment of production modification No. 160001J3282 has resulted in insufficient clearance between the fuel sensor cover mounted on Rib 24 and the crown of stringer (STGR) 15 on both the left hand (LH) and right hand (RH) wings.
This Service Bulletin introduces Modification Number (Mod No.) 158133J4169 which replaces the existing fuel sensor support brackets with new, offset fuel sensor support brackets as are currently installed on the A321 variant.
Accomplishment of this Service Bulletin will ensure that there is sufficient clearance between the fuel sensor cover and the crown of STGR 15.
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 DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO
DE-FUELLING/VENTILATION YES 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 281239B01R02 1
270.00 Support bracket assy LH Kit 281239B02R02 1
270.00 Support bracket assy RH TOTAL
540.00
EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :
AIB AXM CSN DLH FFT GOW IGO KZR LAN
NKS PGT QTR TAM
VIV VOI
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None ISI None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None OTHER Service Bulletin Information Transmission (SBIT) 16-0081
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT NO HARD NO SOFT NO OBRM NO
MANPOWER Task 281239-831-895-001: Modification
TOTAL MANHOURS
7.00
ELAPSED TIME (HOURS)
4.00 DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
APPENDICES Appendix 01 - Manpower Gantt Chart DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY **CONF ALL RIB24
LH SHOWN
RH SYMMETRICAL 550CB (650CB) NOTE:
AREA OF MODIFICATION B RIB24 FWD STGR16STGR15 A
VIEW LOOKING INBOARD ON RIB24 B A N_SB_281239_7_SAAA_01_00 Figure A-USAAA - Sheet 01 DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
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
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 28 TITLE: FUEL - INDICATING - INTRODUCE COMMON FUEL LEVEL SENSOR
SUPPORT BRACKET MODIFICATION No.: 158133J4169 NOTE : This modification is related to an airworthiness issue which has been re-classified and confirmed by EASA as minor in acco rdance with EU Part 21.A.91. As such, this is handled by AIRBUS under its Design Organisation Approval No.
EASA.21J.031.
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 NOTE : This modification is embodied before delivery on aircraft with Manufacturer Serial Number (MSN) 6642, 7129, 7175-7181, 7186-7209, 7249 and subsequent.
(1) Models 320-251N 320-271N
(2) Effectivity by MSN 6101 6286 6620 6720 6744 6772 6799 6801 6819 6829 6833 6849 6860 6864 6868 6904 6907 6914 6920 6946 6952 6967 6975 7001 7011 7033 7047 7051 7053 7060 7074 7078 7083 7094 7102-7103 7107 7124 7126 7140-7141 7147 7150 7162 7172 7185 7236 DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
(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 AIB 6101 6620 AXM 7150 7236 CSN 6975 DLH 6801 6864 6920 7078 7103 FFT 7141 GOW 7047 7074 7172 IGO 6720 6744 6772 6799 6819 6829 6849 6860 6868 6904 6914 6946 6952 6967 7001 7033 7053 KZR 7124 LAN 6286 NKS 6833 6907 7011 7094 PGT 7140 7147 7162 7185 QTR 7083 TAM 7126 VIV 7060 7107 VOI 7051 7102
(4) Configuration by MSN MSN
CONFIGURATION 6101 6286 6620 6720 6744 6772 6799 6801 6819 6829 6833 6849 6860 6864 6868 6904 6907 6914 6920 6946 6952 6967 6975 7001 7011 7033 7047 7051 7053 7060 7074 7078 7083 7094 7102 7103 7107 7124 7126 7140 7141 7147 7150 7162 7172 7185 7236 001
(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration.
(6) Material Effectivity
MATERIAL
QTY PER A/C
SEE NOTES Kit 281239B01R02 1 Kit 281239B02R02 1 Consumable CMLB01 1 B. CONCURRENT REQUIREMENTS None DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN C. REASON
(1) History Embodiment of production modification No. 160001J3282 has resulted in insufficient clearance between the fuel sensor cover mounted on Rib 24 and the crown of stringer (STGR) 15 on both the left hand (LH) and right hand (RH) wings.
(2) Objective/Action This Service Bulletin introduces Modification Number (Mod No.) 158133J4169 which replaces the existing fuel sensor support brackets with new, offset fuel sensor support brackets as are currently installed on the A321 variant.
(3) Advantages Accomplishment of this Service Bulletin will ensure that there is sufficient clearance between the fuel sensor cover and the crown of STGR 15.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
Task 281239-831-895-001: Modification
(1) Replace the LH Fuel Level Sensor Support Bracket
(2) Replace the RH Fuel Level Sensor Support Bracket E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale Accomplishment of this Service Bulletin must be done 12 years after first entry into service.
This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds given 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 the authority of Design Organisation Approval No. EASA.21J.031.
DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
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.
Task 281239-831-895-001: Modification Get Access
2.00 On Aircraft Replace the LH Fuel Level Sensor Support Bracket
1.00 Replace the RH Fuel Level Sensor Support Bracket
1.00 Tests
1.00 Close-Up
2.00
TOTAL MANHOURS
7.00
ELAPSED TIME (HOURS)
4.00 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-UAAAA given in Appendix 01 - Manpower Gantt Chart .
H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES Aircraft Maintenance Manual (AMM) 06-20-00 06-41-57 12-34-24 20-21-11 20-28-00 28-10-00 28-12-45 28-25-00 28-46-00 28-46-16 Consumable Material List (CML) ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-51-20 20-55-00 Standards Manual (SM) K. PUBLICATION AFFECTED Illustrated Parts Catalog (IPC) 28-46-85 DATE: Nov 22/16 SERVICE BULLETIN No.: A320-28-1239 REVISION No.: 01 - Sep 15/17 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.