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A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 1
CONF ALL AIRBUS 2, ROND POINT EMILE DEWOITINE 31700 BLAGNAC FRANCE
The content of this document is the property of Airbus. All rights including copyrights are reserved.
It is supplied in confidence and commercial security on its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons.
It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus.
MANDATORY MANDATORY MANDATORY ATA SYSTEM: 44 TITLE: CABIN SYSTEMS - TV/ DATA BROADBAND TRANSCEIVER SYSTEM -
INSPECTION - PANASONIC ADAPTER PLATE MODIFICATION No.:
None
A380
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 2 ATA SYSTEM: 44 TITLE: CABIN SYSTEMS - TV/ DATA BROADBAND TRANSCEIVER SYSTEM -
INSPECTION - PANASONIC ADAPTER PLATE
REVISION TRANSMITTAL SHEET This page transmits Revision No. 01 of Service Bulletin No. A380-44-8145.
A. ADDITIONAL WORK No additional work is required by this revision.
B. REASON Revision No. 01 issued to:
- Correct the VSB reference in the reason paragraph
- Update the accomplishment timescale appendix C. CHANGES
PLANNING INFORMATION REASON PANASONIV VSB number update from DPA- RDAA903141-01-44-00 to RDAA903141-01-44-00
APPENDIX
ACCOMPLISHMENT TIMESCALE Fig.AA Sol.AA Accomplishment Timescale compliance table aligned with IAS44R0006-23 REV00A D. 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.
E. HISTORY OF PREVIOUS REVISIONS No previous revision F. REVISION SEQUENCE ORIGINAL: Dec 22/23 REVISION No. : 01 - Apr 22/24
A380
SERVICE BULLETIN
SUMMARY REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 3 ATA SYSTEM: 44 TITLE: CABIN SYSTEMS - TV/ DATA BROADBAND TRANSCEIVER SYSTEM -
INSPECTION - PANASONIC ADAPTER PLATE
SUMMARY This summary is for information only and is not approved for modification of the aircraft.
A. MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR None MINOR None 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.
B. REASON
(1) History During the Louver check, an operator found corrosion and cracks on the adapter plate.
(2) Objective/Action This Service Bulletin consists to cover the PANASONIC VSB RDAA903141-01-44-00, which removes the Radome to allow a General Visual Inspection (GVI) of the Plate and Skirt Assy-Adapter. Depending on results of GVI, maintenance coordination with HAECO Cabin Solutions may be required, involving the removal of the Adapter Plate.
(3) Advantages None
(4) Operational/Maintenance Consequences None C. GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY COST SAVING NO
A/C OPERATION
AFFECTED
NO VENDOR SB YES
CANCELS INSPECTION SB NO ETOPS AFFECTED NO
PAX COMFORT AFFECTED NO POTENTIAL AD YES
RELIABILITY AFFECTED NO STRUCTURAL LIFE EXTENSION NO
LIFE LIMIT NO LINE MAINTENANCE AFFECTED NO NOTE: Service Bulletin must be accomplished.
D. MAINTENANCE CONFIGURATION No specific aircraft maintenance configuration required.
E. MATERIAL PRICE INFORMATION
A380
SERVICE BULLETIN
SUMMARY REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 4
(1) Do a General Visual Inspection (GVI) of the Adapter Plate
(a) T ask set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate No material F. APPLICABILITY This Service Bulletin is applicable to this (these) operator(s):
ANA DLH ETD UAE G. CONCURRENT REQUIREMENTS None H. NATURE OF THE WORK
(1) Do a General Visual Inspection (GVI) of the Adapter Plate
(a) T ask set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate
AIRCRAFT YES
EQUIPMENT NO I. MANPOWER
(1) Do a General Visual Inspection (GVI) of the Adapter Plate
(a) T ask set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate
MANPOWER TOTAL MAN-HOURS 3.10 h ELAPSED TIME (HOURS) 3.10 h Additional man-hours related to Vendor SB; refer to:
Do a GVI of the PANASONIC Adapter Plate with a DPA Ref. PANASONIC AVIONICS CORPORATION (1UL05) VSB RDAA903141-01-44-00
A380
SERVICE BULLETIN
SUMMARY Figure ICN-A380-A-44XX8145-A-FAPE3-0182E-A-002-01 Fig.SA Sol.AA SHEET 1/1 REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 General Overview Page 5 J. GENERAL OVERVIEW
CONF ALL FR75 FR76 FR79 FR80 A A Z290
INSPECTION OF THE RADOME ADAPTER PLATE ICN-A380-A-44XX8145-A-FAPE3-0182E-A-002-01
A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 6 ATA SYSTEM: 44 TITLE: CABIN SYSTEMS - TV/ DATA BROADBAND TRANSCEIVER SYSTEM -
INSPECTION - PANASONIC ADAPTER PLATE
1. PLANNING INFORMATION A. APPLICABILITY NOTE: This Service Bulletin is only applicable to aircraft on which MOD No. 73057T81961 or 77993T87510 (Service Bulletin No. A380-44-8112 and A380-44-8113) are embodied.
(1) Models ON A/C 0146, 0149, 0175, 0177, 0262, 0263, 0266 380-841 ON A/C 0162, 0167, 0225-0229, 0232, 0234, 0236, 0238-0242, 0244, 0248-0250, 0252, 0256- 0261, 0264, 0267-0272 380-842 ON A/C 0030, 0042, 0056, 0080, 0086, 0098, 0101, 0111-0113, 0116, 0119, 0133, 0134, 0138-0142, 0147, 0150, 0153, 0154, 0157-0159, 0164-0166, 0168-0172, 0174, 0176, 0178, 0180, 0182, 0184, 0186-0188, 0190, 0191, 0195, 0198-0211, 0213, 0214, 0216-0224, 0233, 0237 380-861
CONF ALL
(2) Applicability by MSN 0030 0042 0056 0080 0086 0098 0101 0111-0113 0116 0119 0133 0134 0138-0142 0146 0147 0149 0150 0153 0154 0157-0159 0162 0164-0172 0174-0178 0180 0182 0184 0186-0188 0190 0191 0195 0198-0211 0213 0214 0216-0229 0232-0234 0236- 0242 0244 0248-0250 0252 0256-0264 0266-0272
(3) MSN by configuration
MSN CONFIGURATION 0030 0042 0056 0080 0086 0098 0101 0111 0112 0113 0116 0119 0133 0134 0138 0139 0140 0141 0142 0146 0147 0149 0150 0153 0154 0157 0158 0159 0162 0164 0165 0166 0167 0168 0169 0170 0171 0172 0174 0175 0176 0177 0178 0180 0182 0184 0186 0187 0188 0190 0191 0195 0198 0199 0200 0201 0202 0203 0204 0205 0206 0207 0208 0209 0210 0211 0213 0214 0216 0217 0218 0219 0220 0221 0222 0223 0224 0225 0226 0227 0228 0229 0232 0233 0234 0236 0237 0238 0239 0240 0241 0242 0244 0248 0249 0250 0252 0256 0257 0258 0259 0260 0261 0262 0263 0264 0266 0267 0268 0269 0270 0271 0272 001
(4) Configuration definition Configuration 001 CONF 001 is applicable for all the aircraft affected by this Service Bulletin as a standard configuration.
B. CONCURRENT REQUIREMENTS None
A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 7 C. REASON
(1) History During the Louver check, an operator found corrosion and cracks on the adapter plate.
(2) Objective/Action This Service Bulletin consists to cover the PANASONIC VSB RDAA903141-01-44-00, which removes the Radome to allow a General Visual Inspection (GVI) of the Plate and Skirt Assy-Adapter. Depending on results of GVI, maintenance coordination with HAECO Cabin Solutions may be required, involving the removal of the Adapter Plate.
(3) Advantages None
(4) Operational/Maintenance Consequences None D. DESCRIPTION T o accomplish this Service Bulletin it is necessary to:
(1) Do a General Visual Inspection (GVI) of the Adapter Plate
(a) T ask set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate 1 Do a GVI of the PANASONIC Adapter Plate with a DPA 2 Complete and Send the Inspection Report sheet E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Union Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and intervals given but reference should be made to the AD for confirmation of the mandated accomplishment timescale.
Accomplishment of this Service Bulletin must be done in accordance with the Appendix ACCOMPLISHMENT TIMESCALE.
F. APPROVAL The technical content of this document is approved under the authority of the Design Organisation Approval ref. EASA.21J.031.
If an aircraft listed in the applicability 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.
A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 8
(1) Do a General Visual Inspection (GVI) of the Adapter Plate
(a) T ask set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate
PREPARATION Job Set-Up 1.50 h
PROCEDURE Complete and Send the Inspection Report sheet 0.10 h
PREPARATION FOR TEST None TEST None
CLOSE-UP Close-up 1.50 h TOTAL MAN-HOURS 3.10 h ELAPSED TIME (HOURS) 3.10 h Additional man-hours related to Vendor SB; refer to:
Do a GVI of the PANASONIC Adapter Plate with a DPA Ref. PANASONIC AVIONICS CORPORATION (1UL05) VSB RDAA903141-01-44-00 NOTE: The minimum man-hours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional man-hours can apply.
H. WEIGHT AND BALANCE Not changed I. ELECTRICAL LOAD DATA Not changed J. REFERENCES
(1) Do a General Visual Inspection (GVI) of the Adapter Plate
(a) T ask set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate
AIRCRAFT MAINTENANCE MANUAL (AMM) 06-20-00, Page Block 00 06-31-53, Page Block 00 T ask 12-34-24-869-002 T ask 44-33-24-000-801 T ask 44-33-24-400-801
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM) 20-55-00
IN SERVICE INFORMATION (ISI)
00.00.00179
VENDOR SERVICE BULLETIN (VSB) PANASONIC AVIONICS CORPORATION (1UL05) VSB RDAA903141-01-44-00 K. PUBLICATION AFFECTED
A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 9 None L. INDUSTRY SUPPORT INFORMATION This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign. For detailed support, please refer to the related RIL L44M23002624.
For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department: monitored.retrofit@airbus.com.
A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 10
2. MATERIAL INFORMATION A. MATERIAL APPLICABILITY Material for task set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate
MATERIAL QTY SEE NOTES Referenced tools See SB Referenced consumables See SB B. TOOLING Referenced tools for task set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate T o accomplish this Service Bulletin it is necessary to use the tools listed in:
Ref. AMM T ask 44-33-24-000-801 Ref. AMM T ask 44-33-24-400-801 C. CONSUMABLES Referenced consumables for task set A380-A-44-XX-8145-01000-93BA-A Do a GVI of the Adapter Plate T o accomplish this Service Bulletin it is necessary to use the consumable materials listed in:
Ref. AMM T ask 44-33-24-400-801 D. LIST OF NEW PARTS No parts E. LIST OF EXISTING PARTS No parts
A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 11
3. ACCOMPLISHMENT INSTRUCTIONS Task set A380-A-44-XX-8145-01000-93BA-A (A380-A-44-XX-8145-01ZZZ-93BZ-A) Do a GVI of the Adapter Plate 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 A 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 ESP Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words “refer to” are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words “in accordance with” are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin.
Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD.
T o allow more flexibility, the rule "refer to" and "in accordance with" will apply to these paragraphs 3.C. and 3.E. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition.
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions, including Required for Compliance paragraph contained herein, contact AIRBUS for further instructions and approval.
A. TASK SET ASSOCIATED INFORMATION Task Manpower TOTAL MAN-HOURS 3.10 h ELAPSED TIME (HOURS) 3.10 h Additional man-hours related to Vendor SB; refer to:
PANASONIC AVIONICS CORPORATION (1UL05) VSB RDAA903141-01-44-00
A380
SERVICE BULLETIN REV 00 Dec 22/23 A380-44-8145 REV 01 Apr 22/24 Page 12 B. PREPARATION
(1) Task A380-A-44-XX-8145-01001-540A-A (A380-A-44-XX-8145-01ZZZ-540Z-A) Job Set-Up Job Set-Up Information Manpower/Resources/Skills Man-hours 1.50 h Minimum Number of person 1 Elapsed Time 1.50 h Referenced Information Manuals/Drawings References/Sheets AMM T ask 12-34-24-869-002T ask 44-33-24-000-801 VSB PANASONIC AVIONICS CORPORATION (1UL05)VSB RDAA903141-01-44-00 Procedure NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction - Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM T ask 12-34- 24-869-002.
(b) Put an access platform in position in zone Zone 290.
(c) Do the job set-up procedure as specified in the removal of the antenna radome, refer to Ref. AMM T ask 44-33-24-000-801.
(d) For the removal of the antenna radome, refer to Ref. PANASONIC AVIONICS CORPORATION (1UL05) VSB RDAA903141-01-44-00.
C. PROCEDURE
(1) Task A380-A-44-XX-8145-01001-300A-A (A380-A-44-XX-8145-01ZZZ-300Z-A) Do a GVI of the PANASONIC Adapter Plate with a DPA Job Set-Up Information Working Area Impacted Zone Access / Work Location 290 Work location From Frame 75 to Frame 80 Referenced Information Manuals/Drawings References/Sheets AMM 06-20-00, Page Block 0006-31-53, Page Block 00 VSB PANASONIC AVIONICS CORPORATION (1UL05)VSB RDAA903141-01-44-00 Procedure
(a) Standard practices given in this procedure:
1 For the Frame (FR) identification, refer to Ref. AMM 06-31-53, Page Block
00.