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@A350
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: 53 TITLE: FUSELAGE - FORWARD FUSELAGE - INTRODUCE IMPROVED CARGO DOOR SURROUND ALU LATCH FITTINGS IN SECTION 13/14 - SB ONLY **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR None MINOR 109227L31617 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 During inspection on an AIRBUS test aircraft, cracks have been detected on parts made of forging aluminum 7037 due to an unexpected behavior of this material. AIRBUS decided to redesign the FWD door latch fittings with the material change to aluminum 7010T7652. This design change has been applied in production from Manufacturer Serial Number (MSN) 0040.
For aircraft with MSN 0006 thru MSN 0039 the FWD cargo door latch fittings must be replaced due to the material improvement from aluminum 7037 to aluminum 7010T7652.
This Service Bulletin details the installation of new FWD cargo-door latch fittings at FR24, FR24A, FR25 and FR25A in the lower part of the cargo door surround.
Accomplishment of this Service Bulletin cancels the requirements of Service Bulletin No.A350-53-P046.
The accomplishment of this Service Bulletin will ensure the 6 years threshold for the first General Visual Inspection (GVI) in these affected areas.
In addition, interference fit of the latch fitting bushes has been increased to avoid a rotation of the bushes which has been detected on a A350 test aircraft. This change has been implemented in production from MSN 0064.
DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
SUMMARY
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE RECOMMENDED (1)
CANCELS INSPECTION SB YES
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 NOTE
(1) : Service Bulletin recommended to be accomplished to prevent significant operational disruptions.
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 53P011D01R00 1 63,500.00 Latch fitting assembly, edge protection Kit 53P011D02R05 1 1,700.00 Angle, bolts, nuts, cotter pins, washers TOTAL 65,200.00 Standard tool TOOLD01 1 See SB
EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :
CPA FIN HVN QTR SIA TAM
CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s):
Service Bulletin No. A350-53-P046.
NOTE : Service Bulletin No. A350-35-P046 (F USELAGE - FORWARD F UGELAGE - INSPECT
EXTERNAL LUGS OF THE CARGO DOOR SURROUND ALU LATCH FITTINGS IN SECTION 13/14).
REFERENCES / REPERCUSSIONS TFU
53.40.00.008 OEB None AOT None SIL None ISI None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None OTHER None DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
SUMMARY
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT NO
MANPOWER Task 53P011-831-848-001: Modification
TOTAL MANHOURS
48.50
ELAPSED TIME (HOURS)
36.75
APPENDICES Appendix 01 - Manpower Gantt Chart Appendix 02 - Check of the Latch Fittings Alignment DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
SUMMARY **CONF ALL A
DOOR IN OPEN CONDITION A Z821
REPLACEMENT OF CARGO
DOOR LATCH FITTINGS P_SB_53P011_6_SAAA_01_01 Figure A-GSAAA - Sheet 01 DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
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: 53 TITLE: FUSELAGE - FORWARD FUSELAGE - INTRODUCE IMPROVED CARGO DOOR SURROUND ALU LATCH FITTINGS IN SECTION 13/14 - SB ONLY MODIFICATION No.: 109227L31617 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 applicable by Service Bulletin only.
(1) Models 350-941
(2) Effectivity by MSN 0006-0039
(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 CPA 0029 0032 0034 0038 0039 FIN 0018 0019 0020 0022 0023 0028 HVN 0014 0015 0016 0017 QTR 0006 0007 0008 0009 0010 0011 0012 0013 0021 0025 0033 0036 DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
OPERATOR MSN SIA 0026 0030 0031 0037 TAM 0024 0027 0035
(4) Configuration by MSN MSN
CONFIGURATION 0006 0007 0008 0009 0010 0011 0012 0013 0014 0015 0016 0017 0018 0019 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029 0030 0031 0032 0033 0034 0035 0036 0037 0038 0039 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 53P011D01R00 1 Kit 53P011D02R05 1 Consumable CMLD01 1 Standard tool TOOLD01 1 B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s):
Service Bulletin No. A350-53-P046.
NOTE : Service Bulletin No. A350-35-P046 (FUSELAGE - FORWARD FUGELAGE
- INSPECT EXTERNAL LUGS OF THE CARGO DOOR SURROUND ALU LATCH FITTINGS IN SECTION 13/14).
C. REASON
(1) History During inspection on an AIRBUS test aircraft, cracks have been detected on parts made of forging aluminum 7037 due to an unexpected behavior of this material. AIRBUS decided to redesign the FWD door latch fittings with the material change to aluminum 7010T7652. This design change has been applied in production from Manufacturer Serial Number (MSN) 0040.
For aircraft with MSN 0006 thru MSN 0039 the FWD cargo door latch fittings must be replaced due to the material improvement from aluminum 7037 to aluminum 7010T7652.
DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
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SERVICE BULLETIN
(2) Objective/Action This Service Bulletin details the installation of new FWD cargo-door latch fittings at FR24, FR24A, FR25 and FR25A in the lower part of the cargo door surround.
(3) Advantages Accomplishment of this Service Bulletin cancels the requirements of Service Bulletin No.A350-53-P046.
The accomplishment of this Service Bulletin will ensure the 6 years threshold for the first General Visual Inspection (GVI) in these affected areas.
In addition, interference fit of the latch fitting bushes has been increased to avoid a rotation of the bushes which has been detected on a A350 test aircraft. This change has been implemented in production from MSN 0064.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
Task 53P011-831-848-001: Modification
(1) Remove Latch Fitting at Frame 25A
(2) Install Latch Fitting at Frame 25A
(3) Remove of Latch Fitting at Frame 25
(4) Install Latch Fitting at Frame 25
(5) Remove Latch Fitting at Frame 24A
(6) Install Latch Fitting at Frame 24A
(7) Remove Latch Fitting at Frame 24
(8) Install Latch Fitting at Frame 24
(9) Apply the Surface Protection to the Fasteners and Latch Fittings E. COMPLIANCE
(1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions.
DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
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SERVICE BULLETIN
(2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available.
F. APPROVAL The technical content of this document is approved under the authority of Design Organisation 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 53P011-831-848-001: Modification Get Access
11.00 On Aircraft Remove Latch Fitting at Frame 25A
2.00 Install Latch Fitting at Frame 25A
3.00 Remove of Latch Fitting at Frame 25
2.00 Install Latch Fitting at Frame 25
3.00 Remove Latch Fitting at Frame 24A
2.00 Install Latch Fitting at Frame 24A
3.00 Remove Latch Fitting at Frame 24
2.00 Install Latch Fitting at Frame 24
3.00 Apply the Surface Protection to the Fasteners and Latch Fittings
0.50 Tests
4.50 Close-Up
12.50
TOTAL MANHOURS
48.50
ELAPSED TIME (HOURS)
36.75 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-GAAAA given in Appendix 01 - Manpower Gantt Chart .
DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN H. WEIGHT AND BALANCE The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator’s items. For the definition of MEW and operator’s items, refer to the Weight and Balance Manual (WBM).
Manufacturers Empty Weight +0.2 KG (+0.5 LB) Effect on Balance +3.6 KGM (+26.2 LB.FT ) I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES Aircraft Structural Repair (ASR) 51-24-XX 51-42-XX 51-43-XX 51-4X-XX Consumable Material List (CML) Electrical Standard Practices (ESP) 20-51-20 20-55-XX Maintenance Procedure (MP) 20-46-XX 20-51-20 20-51-50 24-41-XX 25-81-72 50-18-61 50-1X-XX 50-23-XX 52-33-XX 52-3X-XX Process and Material Specification (PMS) System Description (SD) 06-3X-XX Standards Manual (SM) Weight and Balance Manual (WBM) K. PUBLICATION AFFECTED Maintenance Illustrated Part Data (MIPD) 53-25-74 Structural Repair IPD (SRIPD) 53-21-63 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES Latch Assy V5327439200200 Latch Assy V5327439200400 The parts listed here must not be installed anymore on aircraft which have accomplished this Service Bulletin or which have the equivalent production modification embodied.
DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN This Page Intentionally Left Blank DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 6 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses 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:
Kit 53P011D01R00 Kit 53P011D02R05 AIRBUS Material, Logistics and Suppliers
ATP II B, Hein-Sass-Weg 24 21129 HAMBURG
GERMANY For ordering by internet:
http://spares.airbus.com For ordering by E-mail: airbus.kit@airbus.com Telephone Hotline: +49 40 743 51775
(2) Price and Availability Kit 53P011D01R00 Cost 63,500.00 USD Availability 99 calendar days from receipt of order The availability given above is the standard lead time from the date of your purchase order. If items are required 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.
The latest valid price and lead time for ordering purposes shall be obtained through the AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 53P011D02R05 Cost 1,700.00 USD Availability 99 calendar days from receipt of order The availability given above is the standard lead time from the date of your purchase order. If items are required 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.
The latest valid price and lead time for ordering purposes shall be obtained through the AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
B. INDUSTRY SUPPORT INFORMATION AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at no charge for orders placed before Dec 31/21.
DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 7 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN AIRBUS will credit the man hours indicated in this Service Bulletin at the agreed in-house warranty labor rate for claims received no later than 90 days after completion of the last affected aircraft of your fleet, for the accomplishment of this Service Bulletin before Dec 31/21.
For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department: monitored.retrofit@airbus.com.
C. LIST OF COMPONENTS Kit 53P011D01R00 ITEM NEW PART N˚
QTY (UM)
KEYWORD ITEM OLD PART N˚ INT SEE NOTES 1 V5327412220000 1 PLATE 28 V5327439201800 2 LATCH 29 V5327439202000 2 LATCH Kit 53P011D02R05 ITEM NEW PART N˚
QTY (UM)
KEYWORD ITEM OLD PART N˚ INT SEE NOTES 2 DAN169E3-7 9 SCREW 8 NAS1149D0316K 14 WASHER 9 ASNA2069N3 18 WASHER 10 NAS1726C3E 6 NUT 17 NSA5191-3V8 12 BOLT 18 MS24665-86 2 PIN 19 NSA5059E3 2 NUT 23 MS21042L3 2 NUT 26 MS24665-372 1 PIN 27 NSA5059E10 1 NUT 30 EN6115B4E4 30 BOLT 31 EN6115B4E5 26 BOLT 32 EN6115B4E6 8 BOLT 33 EN6115B4E7 10 BOLT 35 ABS0873B3E6 32 BOLT 36 ABS0873B3E7 16 BOLT 37 ABS0873B3E8 16 BOLT 38 ABS0873B4E8 24 BOLT 40 ABS0873B4E10 8 BOLT 41 ABS1738K3 64 NUT 42 ABS1738K4 106 NUT 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.
DATE: Dec 17/18 SERVICE BULLETIN No.: A350-53-P011 REVISION No.: 00 - Dec 17/18 Page: 8 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.