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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.
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 52 TITLE: DOORS - CARGO - INPECTION OF FWD AND AFT CARGO DOOR
PAINT PEEL OFF ON FRAME FORK **CONF ALL
MODIFICATIONS None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Inspection on structure assembly level revealed that paint peeling might be present on the forward and aft cargo door frame forks around the hook bolt hole.
This Mandatory Inspection Service Bulletin requests to perform a one time Detailed Inspection of the frame forks around the hook bolt hole on the FWD and AFT Cargo Door and defines corrective actions in case of findings.
In case of paint - peeling finding, application of the corrective action will restore the surface treatment to the required level to tackle corrosion, abrasion effect due to the environment severity.
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 NOTE
(1) : Service Bulletin must be accomplished.
DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
SUMMARY
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 52P011D01R00 1
50.00 Cotter Pin
EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :
FIN HVN QTR
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU
52.33.00.012 OEB None AOT None SIL None ISI 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 52P011-832-848-001: Inspection
TOTAL MANHOURS
18.00
ELAPSED TIME (HOURS)
9.00
APPENDICES Appendix 01 - Affected Part Numbers and Serial Numbers Appendix 02 - Gantt Chart DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
SUMMARY **CONF ALL A A Z822 Z821 A FR26A FR26 FR25A FR25 FR24A FR24 FR23A FR23FR81A FR81 FR80A FR80 FR79A FR79 FR78A FR78 FWD AFT FWD AFT FWD AFT FWD AFT FWD AFT FWD AFT FWD AFT FWD AFT B
TYPICAL P_SB_52P011_6_SAAA_01_00 Figure A-GSAAA - Sheet 01 DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
SUMMARY **CONF ALL B C
TYPICAL FRAME C
TYPICAL FRAME FORK
OUTER LOFT
INSPECTION AREA
VIEW LOOKING FORWARD
AFT VIEW SIMILAR P_SB_52P011_6_SAAA_02_00 Figure A-GSAAA - Sheet 02 DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 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
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 52 TITLE: DOORS - CARGO - INPECTION OF FWD AND AFT CARGO DOOR
PAINT PEEL OFF ON FRAME FORK 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 NOTE : The MSN’s are given for information, reference should be taken on both PN and SN listed in Appendix 01 - Affected Part Numbers and Serial Numbers .
(1) Models 350-941
(2) Effectivity by MSN 0006-0020
(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 FIN 0018 0019 0020 DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN
OPERATOR MSN HVN 0014 0015 0016 0017 QTR 0006 0007 0008 0009 0010 0011 0012 0013
(4) Configuration by MSN MSN
CONFIGURATION 0006 0007 0008 0009 0010 0011 0012 0013 0014 0015 0016 0017 0018 0019 0020 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 52P011D01R00 1 Consumable CMLD01 1 B. CONCURRENT REQUIREMENTS None C. REASON
(1) History Inspection on structure assembly level revealed that paint peeling might be present on the forward and aft cargo door frame forks around the hook bolt hole.
(2) Objective/Action This Mandatory Inspection Service Bulletin requests to perform a one time Detailed Inspection of the frame forks around the hook bolt hole on the FWD and AFT Cargo Door and defines corrective actions in case of findings.
(3) Advantages In case of paint - peeling finding, application of the corrective action will restore the surface treatment to the required level to tackle corrosion, abrasion effect due to the environment severity.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN Task 52P011-832-848-001: Inspection
(1) Open the Fwd Cargo Door and Identify the Part Number (PN) and Serial Number (SN)
(2) Do a Detailed Visual Inspection for Paint Peel Off on the FWD Cargo Door
(3) Open the AFT Cargo Door and Identify the Part Number (PN) and Serial Number (SN)
(4) Do a Detailed Visual Inspection for Paint Peel Off on the AFT Cargo Door
(5) Restore the Anti - Corrosion Protection of the Frame Forks on the FWD Cargo Door
(6) Close the FWD Cargo Door
(7) Restore the Anti - Corrosion Protection of the Frame Forks on the Aft Cargo Door
(8) Close the AFT Cargo Door E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale Accomplishment of this Service Bulletin must be done 3 years from entry into service (EIS).
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 and/or intervals and/or date) 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.
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.
DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
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 52P011-832-848-001: Inspection Get Access
1.00 On Aircraft Open the Fwd Cargo Door and Identify the Part Number (PN) and Serial Number (SN)
0.25 Do a Detailed Visual Inspection for Paint Peel Off on the FWD Cargo Door
3.00 Open the AFT Cargo Door and Identify the Part Number (PN) and Serial Number (SN)
0.25 Do a Detailed Visual Inspection for Paint Peel Off on the AFT Cargo Door
3.00 Restore the Anti - Corrosion Protection of the Frame Forks on the FWD Cargo Door
4.50 Close the FWD Cargo Door
0.25 Restore the Anti - Corrosion Protection of the Frame Forks on the Aft Cargo Door
4.50 Close the AFT Cargo Door
0.25 Close-Up
1.00
TOTAL MANHOURS
18.00
ELAPSED TIME (HOURS)
9.00 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-GAAAA given in Appendix 02.
NOTE : The minimum man-hours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply.
H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES Aircraft Structural Repair (ASR) 51-42-XX 51-75-12 Consumable Material List (CML) Electrical Standard Practices (ESP) 20-55-XX DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN Maintenance Procedure (MP) 20-51-50 24-41-XX 52-33-71 52-33-72 52-3X-XX Non Destructive Test (NDT) 51-99-XX Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-14 Process and Material Specification (PMS) 01-02-61 Process and Material Specification (PMS) 01-02-63 Process and Material Specification (PMS) 02-16-00 System Description (SD) 06-2X-XX 06-3X-XX 06-4X-XX Standards Manual (SM) K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN This Page Intentionally Left Blank DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 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 52P011D01R00 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:
A350/A380: +49 40 743 51775
(2) Price and Availability Kit 52P011D01R00 Cost
50.00 USD Availability 90 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 AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
B. INDUSTRY SUPPORT INFORMATION AIRBUS will credit the man-hours indicated in this Service Bulletin for inspections that are performed on aircraft in warranty at the time of such inspection. Credit will be at the agreed in-house warranty labor rate. Claims for labor allowance should be received no later than 90 days after completion of the last affected warranted aircraft.
For those aircraft in warranty at the time of such inspection with findings further to inspection as per this Service Bulletin, Airbus will credit the man-hours indicated in this Service Bulletin for corrections that are performed on aircraft in warranty at the time of such correction. Credit will be at the agreed in-house warranty labor rate. Claims for labor allowance should be received no later than 90 days after completion of the last affected warranted aircraft.
For those aircraft in warranty at the time of such inspection with findings further to inspection as per this Service Bulletin, AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at no charge for orders placed before Apr 30/19.
DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 7 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A350
SERVICE BULLETIN This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit management department.
AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX France E-mail : monitored.retrofit@airbus.com C. LIST OF COMPONENTS Kit 52P011D01R00 ITEM NEW PART N˚
QTY (UM)
KEYWORD ITEM OLD PART N˚ INT SEE NOTES 1 MS24665-376 8 PIN 2 MS24665-372 8 PIN 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.
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials Consumable CMLD01 ITEM
DESCRIPTION
REFERENCE TO CML MAT. No.
QTY PER A/C SEE NOTES Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required Top Coat Polyurethane - Grey Internal Structure 04JME4 As required Varnish Polyurethane - Internal Structure 04SMM4 As required Polysulfide Sealant - General Purpose Fillet 06AAB1 As required Surface Pretreatment-Light Alloys Chemical Conver 10ABC1 As required Surface Pretreatment-Light Alloys Chemical Conver 10ABE1 As required Corrosion Preventive Compound - Water Displacing So 12ABC1 As required
(2) Components None DATE: May 12/17 SERVICE BULLETIN No.: A350-52-P011 REVISION No.: 00 - May 12/17 Page: 8 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.