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A350SERVICE BULLETIN
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CONF ALLAIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFRANCE The content of this document is the property of Airbus.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 informationcontained 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 thecopyright. Requests for reproduction of any data in this document and the media authorized for it mustbe addressed to Airbus.
ATA SYSTEM: 32
TITLE: LANDING GEAR - LANDING GEAR MANAGEMENT SYSTEM -INTRODUCE BCS SOFTWARE STANDARD S5B, WSCS SOFTWARESTANDARD S5B AND LGERS SOFTWARE S5A
MODIFICATION No.:CONF 001111399L43339CONF ALL114420L04028114434L48204114420L04027CONF 003 005115009L48441CONF 005 006113846L48153
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ATA SYSTEM: 32
TITLE: LANDING GEAR - LANDING GEAR MANAGEMENT SYSTEM -INTRODUCE BCS SOFTWARE STANDARD S5B, WSCS SOFTWARESTANDARD S5B AND LGERS SOFTWARE S5A
CONF ALLSUMMARY
This summary is for information only and is not approved for modification of the aircraft.A. MODIFICATIONS
CONF 001
MODIFICATION CLASSIFICATIONMAJOR 111399L43339 114420L04027 114420L04028MINOR 114434L48204
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF 002
MODIFICATION CLASSIFICATIONMAJOR 114420L04027 114420L04028MINOR 114434L48204
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF 003
MODIFICATION CLASSIFICATIONMAJOR 114420L04027 114420L04028MINOR 114434L48204 115009L48441
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF 004
MODIFICATION CLASSIFICATIONMAJOR 114420L04027 114420L04028MINOR 114434L48204
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF 005
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MODIFICATION CLASSIFICATIONMAJOR 114420L04027 114420L04028MINOR 113846L48153 114434L48204 115009L48441
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF 006
MODIFICATION CLASSIFICATIONMAJOR 114420L04027 114420L04028MINOR 113846L48153 114434L48204
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
CONF ALLB. REASON
(1) HistoryThe Braking Control System (BCS) S5B software and Wheel Steering Control System(WSCS) S5B software developments were launched to address in-service limitationsrelated to the braking and steering system. These BCS and WSCS software arecompatible for A350-900 and A350-1000.Landing Gear Extension and Retraction (LGERS) S5A software is the A350-1000 entry-into-service software and offers maturity improvement for A350-900 as well.
(2) Objective/ActionBCS and WSCS software S5B :
- Address limitations related to software which have been identified in-service,
- Correct Braking and Steering Control System (BSCS) Built-In Test Equipment(BITE) issues,
- Merge A350-900 and A350-1000 BCS in one single software standard,- Merge A350-900 and A350-1000 WSCS in one single software standard.On A350-1000, BCS software S5B allows :
- In combination with the installation of RBCU hardware H4-3 (MOD 113626 /L04011), removal of the temporary documentary unit (TDU) and AFM TemporaryRevision No. 94 associated with ECAM Temporary Change (ETC) 32AS for thealerts BRAKES A-SKID FAULT ON ALL WHEELS and BRAKES A-SKID OFF.
- Deactivation of ECAM Temporary Change (ETC) code 29BF.
NOTE: For further details about the improvements brought by BCS and WSCS S5Bsoftware, refer to:- TFU (Technical Follow Up) 32.40.00.044,- TFU MOI (Modification Operational Impact) 32.81.00.006.
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(3) AdvantagesIncorporation of this Service Bulletin will ensure :
- A more robust operational reliability for:- Braking Control System (BCS)- Wheel Steering Control System (WSCS)- Landing Gear Extension Retraction System (LGERS)
- A single software standard compatible on A350-900 and A350-1000 for:- BCS software- WSCS software- LGERS software
- On A350-1000, desactivation of ETC code 29BF and ETC code 32AS (incombination with RBCU hardware H4-3).
(4) Operational/Maintenance ConsequencesThe Operational/Maintenance Consequences of this Service Bulletin are covered bythe update of the affected publications detailed in "PLANNING INFORMATION".This Service Bulletin has an impact on flight operations documentation; refer toAirbusWorld to consult the Modification Operational Impact (MOI) No.32.81.00.006described in Technical Follow-up (TFU) 32.40.00.044.
C. GENERAL EVALUATION
EVALUATION TABLECOMPLIANCE RECOMMENDED COST SAVING NOA/C OPERATIONAFFECTED
YES VENDOR SB NO
CANCELS INSPECTION SB NO ETOPS AFFECTED NOPAX COMFORT AFFECTED NO POTENTIAL AD NORELIABILITY AFFECTED YES STRUCTURAL LIFE EXTENSION NOLIFE LIMIT NO LINE MAINTENANCE AFFECTED NO
NOTE: Service Bulletin recommended to be accomplished to prevent significantoperational disruptions.
D. MAINTENANCE CONFIGURATIONCONF 001
No specific aircraft maintenance configuration required.CONF 002
No specific aircraft maintenance configuration required.CONF 003
No specific aircraft maintenance configuration required.CONF 004
No specific aircraft maintenance configuration required.CONF 005
No specific aircraft maintenance configuration required.CONF 006
No specific aircraft maintenance configuration required.
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CONF ALLE. MATERIAL PRICE INFORMATION
CONF 001(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
FLS kit 32P037N01R01 1 1200.00 USD SoftwareFLS kit 32P037N03R00 1 450.00 USD SoftwareTOTAL 1650.00 USD
CONF 002(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
FLS kit 32P037N01R01 1 1200.00 USD Software
CONF 003(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
FLS kit 32P037N02R01 1 1200.00 USD Software
CONF 004(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
FLS kit 32P037N02R01 1 1200.00 USD Software
CONF 005(1) Modification
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(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
FLS kit 32P037N02R01 1 1200.00 USD Software
CONF 006(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
FLS kit 32P037N02R01 1 1200.00 USD Software
CONF ALLF. APPLICABILITY
This Service Bulletin is applicable to this (these) operator(s):AAR BAW CAL CCA CES CHH CPA CRK CSC CSN DAL DLH ETD ETH EVE FBU FIN FWI HVN IBEJAL LAN MAS MAU PAL QTR SIA TAM THA VIR
G. CONCURRENT REQUIREMENTSCONF 003-006
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishmentof the following Service Bulletin(s):
Service Bulletin(s) Modification(s)Ref. SB A350-42-P009 111530L43360Ref. SB A350-42-P010 112312L43552
NOTE: Service Bulletin No. Ref. SB A350-42-P009 (INTEGRATED MODULAR AVIONICS -CPIOM - DEFINE AND INSTALL CPIOM S/W (RBCT AND MSL) B23 FOR CPIOM H6) is aconcurrent requirement if MOD No. 111530L43360 has not been embodied beforedelivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P010 (INTEGRATED MODULAR AVIONICS -CORE PROCESSING I/O MODULES (CPIOM) - DEFINEAND INSTALL CPIOM CORE S/WSTD S3.0.3) is a concurrent requirement if MOD No. 112312/L43552 has not beenembodied before delivery.
CONF 002Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishmentof the following Service Bulletin(s):
Service Bulletin(s) Modification(s)Ref. SB A350-32-P022 109449L42332 111134L43253 111405L43352Ref. SB A350-42-P009 111530L43360Ref. SB A350-42-P010 112312L43552
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NOTE: Service Bulletin No. Ref. SB A350-32-P022 (LANDING GEAR - LANDING GEARMANAGEMENT SYSTEM -INTRODUCE S4A2 SOFTWARE FOR BRAKING CONTROLSYSTEM (BCS) AND S4A1 SOFTWARE FOR WHEEL STEERING CONTROL SYSTEM(WSCS)) is a concurrent requirement if MOD No. 109449L42332 and MOD No.111134L43253 has not been embodied before delivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P009 (INTEGRATED MODULAR AVIONICS -CPIOM - DEFINE AND INSTALL CPIOM S/W (RBCT AND MSL) B23 FOR CPIOM H6) is aconcurrent requirement if MOD No. 111530L43360 has not been embodied beforedelivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P010 (INTEGRATED MODULAR AVIONICS -CORE PROCESSING I/O MODULES (CPIOM) - DEFINEAND INSTALL CPIOM CORE S/WSTD S3.0.3) is a concurrent requirement if MOD No. 112312/L43552 has not beenembodied before delivery.
CONF 001Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishmentof the following Service Bulletin(s):
Service Bulletin(s) Modification(s)Ref. SB A350-42-P007 110881L43236 110921L43235Ref. SB A350-32-P022 109449L42332 111134L43253 111405L43352Ref. SB A350-42-P009 111530L43360Ref. SB A350-42-P010 112312L43552
NOTE: Service Bulletin No. Ref. SB A350-42-P007 (INDICATING/RECORDING SYSTEMS -FLIGHT WARNING SYSTEM (FWS) - DEFINE AND INSTALL FWS S5/2.0 STANDARD)and (INDICATING/RECORDING SYSTEMS - CONTROL AND DISPLAY SYSTEM (CDS)- DEFINE AND INSTALL CDS S5 STANDARD) is a concurrent requirement if MODNo. 110881L43236 and MOD No. 110921L43235 has not been embodied beforedelivery.
NOTE: Service Bulletin No. Ref. SB A350-32-P022 (LANDING GEAR - LANDING GEARMANAGEMENT SYSTEM -INTRODUCE S4A2 SOFTWARE FOR BRAKING CONTROLSYSTEM (BCS) AND S4A1 SOFTWARE FOR WHEEL STEERING CONTROL SYSTEM(WSCS)) is a concurrent requirement if MOD No. 109449L42332 and MOD No.111134L43253 has not been embodied before delivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P009 (INTEGRATED MODULAR AVIONICS -CPIOM - DEFINE AND INSTALL CPIOM S/W (RBCT AND MSL) B23 FOR CPIOM H6) is aconcurrent requirement if MOD No. 111530L43360 has not been embodied beforedelivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P010 (INTEGRATED MODULAR AVIONICS -CORE PROCESSING I/O MODULES (CPIOM) - DEFINEAND INSTALL CPIOM CORE S/WSTD S3.0.3) is a concurrent requirement if MOD No. 112312/L43552 has not beenembodied before delivery.
CONF ALLH. NATURE OF THE WORK
CONF 001(1) Modification
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(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
AIRCRAFT NOEQUIPMENT YES
CONF 002(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
AIRCRAFT NOEQUIPMENT YES
CONF 003(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
AIRCRAFT NOEQUIPMENT YES
CONF 004(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
AIRCRAFT NOEQUIPMENT YES
CONF 005(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
AIRCRAFT NOEQUIPMENT YES
CONF 006(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
AIRCRAFT NOEQUIPMENT YES
CONF ALLI. MANPOWER
CONF 001(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MANPOWERTOTAL MAN-HOURS 3.25 hELAPSED TIME (HOURS) 3.25 h
CONF 002
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(1) Modification(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MANPOWERTOTAL MAN-HOURS 2.75 hELAPSED TIME (HOURS) 2.75 h
CONF 003(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MANPOWERTOTAL MAN-HOURS 3.00 hELAPSED TIME (HOURS) 3.00 h
CONF 004(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MANPOWERTOTAL MAN-HOURS 2.75 hELAPSED TIME (HOURS) 2.75 h
CONF 005(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MANPOWERTOTAL MAN-HOURS 3.00 hELAPSED TIME (HOURS) 3.00 h
CONF 006(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
MANPOWERTOTAL MAN-HOURS 3.00 hELAPSED TIME (HOURS) 3.00 h
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Figure ICN-A350-A-32XXP037-A-FAPE3-04T68-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037General overview
Page 10
CONF ALLJ. GENERAL OVERVIEW
CONF ALL
FR1
FR12
UPLOAD THE SOFTWARETHROUGH THE OMT
A
OMT
KEYBOARD-OMT
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04T68-A-001-01
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ATA SYSTEM: 32
TITLE: LANDING GEAR - LANDING GEAR MANAGEMENT SYSTEM -INTRODUCE BCS SOFTWARE STANDARD S5B, WSCS SOFTWARESTANDARD S5B AND LGERS SOFTWARE S5A
1. PLANNING INFORMATIONA. APPLICABILITY
(1) ModelsON A/C 0088, 0102, 0110, 0118, 0125, 0141, 0161, 0169, 0188, 0206, 0215, 0225, 0229,0233, 0241, 0252, 0258, 0262, 0266, 0274, 0286, 0290, 0296, 0298, 0306, 0315, 0319,0326, 0330, 0336
350-1041ON A/C 0005-0058, 0060-0064, 0066-0070, 0072-0087, 0089-0101, 0103-0107, 0109,0111-0117, 0119-0124, 0126-0130, 0132-0138, 0140, 0142-0151, 0153-0155, 0157-0160,0162-0165, 0167, 0168, 0170, 0172-0187, 0189-0193, 0195-0205, 0207-0214, 0216-0221,0223, 0224, 0226-0228, 0230-0232, 0234-0240, 0243-0251, 0254-0257, 0259-0261,0263-0265, 0267-0273, 0276-0285, 0287, 0289, 0291-0295, 0297, 0300-0303, 0305,0307-0314, 0316, 0318, 0321-0325, 0327-0329, 0333-0335, 0337, 0339, 0343
350-941CONF ALL
(2) Applicability by MSN0005-0058 0060-0064 0066-0070 0072-0107 0109-0130 0132-0138 0140-01510153-0155 0157-0165 0167-0170 0172-0193 0195-0221 0223-0241 0243-02520254-0274 0276-0287 0289-0298 0300-0303 0305-0316 0318 0319 0321-03300333-0337 0339 0343
(3) MSN by configurationCONF 001
MSN CONFIGURATION0005 0006 0007 0008 0009 0010 0011 0012 0013 0014 00150016 0017 0018 0019 0020 0021 0022 0023 0024 0025 00260027 0028 0029 0030 0031 0032 0033 0034 0035 0036 00370038 0039 0040 0041 0042 0043 0044 0045 0046 0047 00480049 0050 0051 0052 0053 0054 0055 0056 0057 0058 00600061 0062 0063 0064 0066 0067 0068 0069 0070 0072 00730074 0075 0076 0077 0078 0079 0080 0081 0082 0083 00840085 0086 0087 0089 0090 0091 0092 0093 0094 0095 00960097 0098 0099 0100 0101 0103 0104 0105 0106 0107 01090111 0112 0113 0114 0115 0116 0117 0119 0120 0121 01220123 0124 0126 0127 0128 0129 0130 0132 0133 0134 01350136 0137 0138 0140 0142 0143 0144 0145 0146 0147 01480149 0150 0151 0153 0154 0155 0157 0158 0159 0160 01620163 0164 0165 0167 0168 0170 0172 0173 0174 0175 01760177 0178 0179 0180 0181 0182 0183 0184 0185 0186 01870189 0190 0191 0192 0193 0195 0196 0197 0198 0199 02000201 0202 0203 0204 0205 0207 0208 0209 0210 0211 02120213 0214 0216 0217 0218 0219 0220 0221 0223 0224 02260227 0228 0230 0231 0232 0234 0235 0236 0237 0238 02390240 0243 0244 0245 0247 0248 0249 0250 0254 0255 02560259 0261 0263 0264 0265 0267 0268 0269 0271 0272 02730276 0277 0278 0279 0280 0281 0282 0284 0285 0287 0289
001
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MSN CONFIGURATION0291 0292 0293 0294 0295 0297 0300 0301 0302 0303 03050307 0309 0310 0311
CONF 002
MSN CONFIGURATION0246 0251 0257 0260 0270 0283 0308 0312 0313 0314 03160318 0321 0322 0323 0324 0325 0327 0328 0329 0333 03340335 0337 0339 0343
002
CONF 003
MSN CONFIGURATION0088 0102 0110 0118 0125 0141 0161 0169 0188 0206 02250233 0252 0258
003
CONF 004
MSN CONFIGURATION0088 0102 0110 0118 0125 0141 0161 0169 0188 0206 02250233 0252 0258
004
CONF 005
MSN CONFIGURATION0215 0229 0241 0262 0266 0274 0286 0290 0296 0298 03060315 0319 0326 0330 0336
005
CONF 006
MSN CONFIGURATION0215 0229 0241 0262 0286 0290 0296 0306 006
CONF ALL(4) Configuration definition
CONF 001Configuration 001
Config. 001 is applicable for A350-900 aircraft on which MOD No. 111399L43339(LGERS S5A) is not embodied.CONF 001 retrofits following modifications: 111399L43339, 114420L04027,114420L04028, 114434L48204.
CONF 002Configuration 002
Config. 002 is applicable for A350-900 aircraft on which MOD No. 113399L43339(LGERS S5A) is embodied.CONF 002 retrofits following modifications: 114420L04027, 114420L04028,114434L48204.
CONF 003Configuration 003
Config. 003 is applicable for A350-1000 aircraft on which MOD No.113626L04011 (Introduce RBCU H4-3 hardware) is not embodied and MOD No.
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114618L48398 (ACTIVATE ETC CODE 29BF) or Service Bulletin No. A350-42-P012(Batch6 Part1) is embodied.CONF 003 retrofits following modifications: 114420L04027, 114420L04028,114434L48204, 115009L48441.
CONF 004Configuration 004
Config. 004 is applicable for A350-1000 aircraft on which MOD No.113626L04011 (Introduce RBCU H4-3 hardware) is not embodied and MOD No.114618L48398 (ACTIVATE ETC CODE 29BF) or Service Bulletin No. A350-42-P012(Batch6 Part1) is not embodied.CONF 004 retrofits following modifications: 114420L04027, 114420L04028,114434L48204.
CONF 005Configuration 005
Config. 005 is applicable for A350-1000 aircraft on which MOD No.113626L04011 (Introduce RBCU H4-3 hardware) is embodied and MOD No.114618L48398 (ACTIVATE ETC CODE 29BF) or Service Bulletin No. A350-42-P012(Batch6 Part1) is embodied.CONF 005 retrofits following modifications: 113846L48153, 114420L04027,114420L04028, 114434L48204, 115009L48441.
CONF 006Configuration 006
Config. 006 is applicable for A350-1000 aircraft on which MOD No.113626L04011 (Introduce RBCU H4-3 hardware) is embodied and MOD No.114618L48398 (ACTIVATE ETC CODE 29BF) or Service Bulletin No. A350-42-P012(Batch6 Part1) is not embodied.CONF 006 retrofits following modifications: 113846L48153, 114420L04027,114420L04028, 114434L48204.
CONF ALLB. CONCURRENT REQUIREMENTS
CONF 003-006Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishmentof the following Service Bulletin(s):
Service Bulletin(s) Modification(s)Ref. SB A350-42-P009 111530L43360Ref. SB A350-42-P010 112312L43552
NOTE: Service Bulletin No. Ref. SB A350-42-P009 (INTEGRATED MODULAR AVIONICS -CPIOM - DEFINE AND INSTALL CPIOM S/W (RBCT AND MSL) B23 FOR CPIOM H6) is aconcurrent requirement if MOD No. 111530L43360 has not been embodied beforedelivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P010 (INTEGRATED MODULAR AVIONICS -CORE PROCESSING I/O MODULES (CPIOM) - DEFINEAND INSTALL CPIOM CORE S/WSTD S3.0.3) is a concurrent requirement if MOD No. 112312/L43552 has not beenembodied before delivery.
CONF 002
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Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishmentof the following Service Bulletin(s):
Service Bulletin(s) Modification(s)Ref. SB A350-32-P022 109449L42332 111134L43253 111405L43352Ref. SB A350-42-P009 111530L43360Ref. SB A350-42-P010 112312L43552
NOTE: Service Bulletin No. Ref. SB A350-32-P022 (LANDING GEAR - LANDING GEARMANAGEMENT SYSTEM -INTRODUCE S4A2 SOFTWARE FOR BRAKING CONTROLSYSTEM (BCS) AND S4A1 SOFTWARE FOR WHEEL STEERING CONTROL SYSTEM(WSCS)) is a concurrent requirement if MOD No. 109449L42332 and MOD No.111134L43253 has not been embodied before delivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P009 (INTEGRATED MODULAR AVIONICS -CPIOM - DEFINE AND INSTALL CPIOM S/W (RBCT AND MSL) B23 FOR CPIOM H6) is aconcurrent requirement if MOD No. 111530L43360 has not been embodied beforedelivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P010 (INTEGRATED MODULAR AVIONICS -CORE PROCESSING I/O MODULES (CPIOM) - DEFINEAND INSTALL CPIOM CORE S/WSTD S3.0.3) is a concurrent requirement if MOD No. 112312/L43552 has not beenembodied before delivery.
CONF 001Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishmentof the following Service Bulletin(s):
Service Bulletin(s) Modification(s)Ref. SB A350-42-P007 110881L43236 110921L43235Ref. SB A350-32-P022 109449L42332 111134L43253 111405L43352Ref. SB A350-42-P009 111530L43360Ref. SB A350-42-P010 112312L43552
NOTE: Service Bulletin No. Ref. SB A350-42-P007 (INDICATING/RECORDING SYSTEMS -FLIGHT WARNING SYSTEM (FWS) - DEFINE AND INSTALL FWS S5/2.0 STANDARD)and (INDICATING/RECORDING SYSTEMS - CONTROL AND DISPLAY SYSTEM (CDS)- DEFINE AND INSTALL CDS S5 STANDARD) is a concurrent requirement if MODNo. 110881L43236 and MOD No. 110921L43235 has not been embodied beforedelivery.
NOTE: Service Bulletin No. Ref. SB A350-32-P022 (LANDING GEAR - LANDING GEARMANAGEMENT SYSTEM -INTRODUCE S4A2 SOFTWARE FOR BRAKING CONTROLSYSTEM (BCS) AND S4A1 SOFTWARE FOR WHEEL STEERING CONTROL SYSTEM(WSCS)) is a concurrent requirement if MOD No. 109449L42332 and MOD No.111134L43253 has not been embodied before delivery.
NOTE: Service Bulletin No. Ref. SB A350-42-P009 (INTEGRATED MODULAR AVIONICS -CPIOM - DEFINE AND INSTALL CPIOM S/W (RBCT AND MSL) B23 FOR CPIOM H6) is aconcurrent requirement if MOD No. 111530L43360 has not been embodied beforedelivery.
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NOTE: Service Bulletin No. Ref. SB A350-42-P010 (INTEGRATED MODULAR AVIONICS -CORE PROCESSING I/O MODULES (CPIOM) - DEFINEAND INSTALL CPIOM CORE S/WSTD S3.0.3) is a concurrent requirement if MOD No. 112312/L43552 has not beenembodied before delivery.
CONF ALLC. REASON
(1) HistoryThe Braking Control System (BCS) S5B software and Wheel Steering Control System(WSCS) S5B software developments were launched to address in-service limitationsrelated to the braking and steering system. These BCS and WSCS software arecompatible for A350-900 and A350-1000.Landing Gear Extension and Retraction (LGERS) S5A software is the A350-1000 entry-into-service software and offers maturity improvement for A350-900 as well.
(2) Objective/ActionBCS and WSCS software S5B :
- Address limitations related to software which have been identified in-service,
- Correct Braking and Steering Control System (BSCS) Built-In Test Equipment(BITE) issues,
- Merge A350-900 and A350-1000 BCS in one single software standard,- Merge A350-900 and A350-1000 WSCS in one single software standard.On A350-1000, BCS software S5B allows :
- In combination with the installation of RBCU hardware H4-3 (MOD 113626 /L04011), removal of the temporary documentary unit (TDU) and AFM TemporaryRevision No. 94 associated with ECAM Temporary Change (ETC) 32AS for thealerts BRAKES A-SKID FAULT ON ALL WHEELS and BRAKES A-SKID OFF.
- Deactivation of ECAM Temporary Change (ETC) code 29BF.
NOTE: For further details about the improvements brought by BCS and WSCS S5Bsoftware, refer to:- TFU (Technical Follow Up) 32.40.00.044,- TFU MOI (Modification Operational Impact) 32.81.00.006.
(3) AdvantagesIncorporation of this Service Bulletin will ensure :
- A more robust operational reliability for:- Braking Control System (BCS)- Wheel Steering Control System (WSCS)- Landing Gear Extension Retraction System (LGERS)
- A single software standard compatible on A350-900 and A350-1000 for:- BCS software- WSCS software- LGERS software
- On A350-1000, desactivation of ETC code 29BF and ETC code 32AS (incombination with RBCU hardware H4-3).
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(4) Operational/Maintenance ConsequencesThe Operational/Maintenance Consequences of this Service Bulletin are covered bythe update of the affected publications detailed in "PLANNING INFORMATION".This Service Bulletin has an impact on flight operations documentation; refer toAirbusWorld to consult the Modification Operational Impact (MOI) No.32.81.00.006described in Technical Follow-up (TFU) 32.40.00.044.
D. DESCRIPTIONTo accomplish this Service Bulletin it is necessary to:(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A ModificationCONF 001 002
1 Upload the BCS S5B, the WSCS S5B, BSCS BITE S5B Software andSOFTWARE-CPIOM H6 CONFIG TABLE B24 to the CPIOM-H61 (8TF61),CPIOM-H62 (8TF62), CPIOM-H63 (8TF63) and CPIOM-64 (8TF64)
CONF 003-0061 Upload the BCS S5B, the WSCS S5B, BSCS BITE S5B Software and
SOFTWARE-CPIOM H6 CONFIG TABLE B24 to the CPIOM-H61 (8TF61),CPIOM-H62 (8TF62), CPIOM-H63 (8TF63) and CPIOM-64 (8TF64)
CONF 001 0022 Upload the BSCS MSL File Software (70GLSW3) to ASFC (1TC)
CONF 003-0062 Upload the BSCS MSL File Software (70GLSW3) to ASFC (1TC)
CONF 0013 Upload the LGERS S5A and LGERS BITE S5A Software to the CPIOM-H61
(8TF61), CPIOM-H62 (8TF62), CPIOM-H63 (8TF63) and CPIOM-H64 (8TF64)CONF 003
4 Desactivate the ETC Code 29BF for the ATQC EnvelopeCONF 005
4 Desactivate the ETC Codes 29BF and 32AS for the ATQC EnvelopeCONF 006
4 Desactivate the ETC Code 32AS for the ATQC EnvelopeCONF 001
5 Upload the LGERS MSL File Software (70GLSW1) to ASFC (1TC)CONF 001 002
6 Upload the RCBU software S5B (15GL1SW1, 15GL1SW2, 15GL2SW1,15GL2SW2) to the RBCU (10GL1 and 10GL2)
CONF 003-0066 Upload the RCBU software S5B (15GL1SW1, 15GL1SW2, 15GL2SW1,
15GL2SW2) to the RBCU (10GL1 and 10GL2)CONF ALL
E. COMPLIANCE
(1) ClassificationRECOMMENDED: Service Bulletin recommended to be accomplished to preventsignificant operational disruptions.
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(2) Accomplishment TimescaleAccomplishment of this Service Bulletin is recommended at the earliest opportunitywhere manpower and facilities are available.
F. APPROVALThe technical content of this document is approved under the authority of DesignOrganisation Approval No. EASA.21J.031.If an aircraft listed in the applicability has a modification or repair embodied that is notof AIRBUS origin, and which affects the content of this Service Bulletin, the operatoris responsible for obtaining approval by its airworthiness authority for any adaptationnecessary before incorporation of the Service Bulletin.
G. MANPOWERCONF 001
The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
PREPARATIONJob Set-up 0.25 h
PROCEDUREUpload the BCS S5B, the WSCS S5B, BSCS BITE S5BSoftware and SOFTWARE-CPIOM H6 CONFIG TABLE B24 tothe CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63(8TF63) and CPIOM-64 (8TF64)
1.00 h
Upload the BSCS MSL File Software (70GLSW3) to ASFC(1TC)
0.25 h
Upload the LGERS S5A and LGERS BITE S5A Software tothe CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63(8TF63) and CPIOM-H64 (8TF64)
0.25 h
Upload the LGERS MSL File Software (70GLSW1) to ASFC(1TC)
0.25 h
Upload the RCBU software S5B (15GL1SW1, 15GL1SW2,15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and 10GL2)
0.25 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 0.50 h
TOTAL MAN-HOURS 3.25 hELAPSED TIME (HOURS) 3.25 h
CONF 002
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The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
PREPARATIONJob Set-up 0.25 h
PROCEDUREUpload the BCS S5B, the WSCS S5B, BSCS BITE S5BSoftware and SOFTWARE-CPIOM H6 CONFIG TABLE B24 tothe CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63(8TF63) and CPIOM-64 (8TF64)
1.00 h
Upload the BSCS MSL File Software (70GLSW3) to ASFC(1TC)
0.25 h
Upload the RCBU software S5B (15GL1SW1, 15GL1SW2,15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and 10GL2)
0.25 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 0.50 h
TOTAL MAN-HOURS 2.75 hELAPSED TIME (HOURS) 2.75 h
CONF 003The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
PREPARATIONJob Set-up 0.25 h
PROCEDUREUpload the BCS S5B, the WSCS S5B, BSCS BITE S5BSoftware and SOFTWARE-CPIOM H6 CONFIG TABLE B24 tothe CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63(8TF63) and CPIOM-64 (8TF64)
1.00 h
Upload the BSCS MSL File Software (70GLSW3) to ASFC(1TC)
0.25 h
Desactivate the ETC Code 29BF for the ATQC Envelope 0.25 h
A350SERVICE BULLETIN
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Upload the RCBU software S5B (15GL1SW1, 15GL1SW2,15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and 10GL2)
0.25 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 0.50 h
TOTAL MAN-HOURS 3.00 hELAPSED TIME (HOURS) 3.00 h
CONF 004The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
PREPARATIONJob Set-up 0.25 h
PROCEDUREUpload the BCS S5B, the WSCS S5B, BSCS BITE S5BSoftware and SOFTWARE-CPIOM H6 CONFIG TABLE B24 tothe CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63(8TF63) and CPIOM-64 (8TF64)
1.00 h
Upload the BSCS MSL File Software (70GLSW3) to ASFC(1TC)
0.25 h
Upload the RCBU software S5B (15GL1SW1, 15GL1SW2,15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and 10GL2)
0.25 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 0.50 h
TOTAL MAN-HOURS 2.75 hELAPSED TIME (HOURS) 2.75 h
CONF 005The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.
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(1) Modification(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
PREPARATIONJob Set-up 0.25 h
PROCEDUREUpload the BCS S5B, the WSCS S5B, BSCS BITE S5BSoftware and SOFTWARE-CPIOM H6 CONFIG TABLE B24 tothe CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63(8TF63) and CPIOM-64 (8TF64)
1.00 h
Upload the BSCS MSL File Software (70GLSW3) to ASFC(1TC)
0.25 h
Desactivate the ETC Codes 29BF and 32AS for the ATQCEnvelope
0.25 h
Upload the RCBU software S5B (15GL1SW1, 15GL1SW2,15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and 10GL2)
0.25 h
PREPARATION FOR TESTNone
TESTTesting 0.50 h
CLOSE-UPClose-up 0.50 h
TOTAL MAN-HOURS 3.00 hELAPSED TIME (HOURS) 3.00 h
CONF 006The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
PREPARATIONJob Set-up 0.25 h
PROCEDUREUpload the BCS S5B, the WSCS S5B, BSCS BITE S5BSoftware and SOFTWARE-CPIOM H6 CONFIG TABLE B24 tothe CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63(8TF63) and CPIOM-64 (8TF64)
1.00 h
Upload the BSCS MSL File Software (70GLSW3) to ASFC(1TC)
0.25 h
Desactivate the ETC Code 32AS for the ATQC Envelope 0.25 hUpload the RCBU software S5B (15GL1SW1, 15GL1SW2,15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and 10GL2)
0.25 h
PREPARATION FOR TESTNone
A350SERVICE BULLETIN
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TESTTesting 0.50 h
CLOSE-UPClose-up 0.50 h
TOTAL MAN-HOURS 3.00 hELAPSED TIME (HOURS) 3.00 h
CONF ALLH. WEIGHT AND BALANCE
Not changedI. ELECTRICAL LOAD DATA
Not changedJ. REFERENCES
CONF 003-006
CONCURRENT SERVICE BULLETIN (SB)A350-42-P009 A350-42-P010
CONF 002
CONCURRENT SERVICE BULLETIN (SB)A350-32-P022 A350-42-P009A350-42-P010
CONF 001
CONCURRENT SERVICE BULLETIN (SB)A350-32-P022 A350-42-P007A350-42-P009 A350-42-P010
(1) Modification(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
ELECTRICAL STANDARD PRACTICES (ESP)A350-A-20-55-XX-01ZZZ-042Z-A
INTRODUCTION (INTRO)A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP)A350-A-24-41-XX-00ZZZ-170Z-A A350-A-31-63-XX-00ZZZ-133Z-AA350-A-32-31-XX-03ZZZ-343Z-A A350-A-32-42-XX-05ZZZ-343Z-AA350-A-32-81-XX-01ZZZ-752Z-A A350-A-32-82-XX-00ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-752Z-A
A350-A-45-46-XX-00ZZZ-752Z-A
A350-A-46-12-01-05ZZZ-752Z-A
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TECHNICAL FOLLOW UP (TFU)32.40.00.044
CONF 002(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
ELECTRICAL STANDARD PRACTICES (ESP)A350-A-20-55-XX-01ZZZ-042Z-A
INTRODUCTION (INTRO)A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP)A350-A-24-41-XX-00ZZZ-170Z-A A350-A-31-63-XX-00ZZZ-133Z-AA350-A-32-31-XX-03ZZZ-343Z-A A350-A-32-42-XX-05ZZZ-343Z-AA350-A-32-81-XX-01ZZZ-752Z-A A350-A-32-82-XX-00ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-752Z-A
A350-A-45-46-XX-00ZZZ-752Z-A
A350-A-46-12-01-05ZZZ-752Z-A
TECHNICAL FOLLOW UP (TFU)32.40.00.044
CONF 003(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
ELECTRICAL STANDARD PRACTICES (ESP)A350-A-20-55-XX-01ZZZ-042Z-A
INTRODUCTION (INTRO)A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP)A350-A-24-41-XX-00ZZZ-170Z-A A350-A-31-51-XX-02ZZZ-345Z-AA350-A-31-63-XX-00ZZZ-133Z-A A350-A-32-31-XX-03ZZZ-343Z-AA350-A-32-42-XX-05ZZZ-343Z-A A350-A-32-81-XX-01ZZZ-752Z-AA350-A-32-82-XX-00ZZZ-343Z-A A350-A-42-11-XX-01ZZZ-343Z-A
A350-A-42-11-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-A A350-A-46-12-01-05ZZZ-752Z-A
TECHNICAL FOLLOW UP (TFU)32.40.00.044
CONF 004(1) Modification
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(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
ELECTRICAL STANDARD PRACTICES (ESP)A350-A-20-55-XX-01ZZZ-042Z-A
INTRODUCTION (INTRO)A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP)A350-A-24-41-XX-00ZZZ-170Z-A A350-A-31-63-XX-00ZZZ-133Z-AA350-A-32-31-XX-03ZZZ-343Z-A A350-A-32-42-XX-05ZZZ-343Z-AA350-A-32-81-XX-01ZZZ-752Z-A A350-A-32-82-XX-00ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-752Z-A
A350-A-45-46-XX-00ZZZ-752Z-A
A350-A-46-12-01-05ZZZ-752Z-A
TECHNICAL FOLLOW UP (TFU)32.40.00.044
CONF 005(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
ELECTRICAL STANDARD PRACTICES (ESP)A350-A-20-55-XX-01ZZZ-042Z-A
INTRODUCTION (INTRO)A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP)A350-A-24-41-XX-00ZZZ-170Z-A A350-A-31-51-XX-02ZZZ-345Z-AA350-A-31-63-XX-00ZZZ-133Z-A A350-A-32-31-XX-03ZZZ-343Z-AA350-A-32-42-XX-05ZZZ-343Z-A A350-A-32-81-XX-01ZZZ-752Z-AA350-A-32-82-XX-00ZZZ-343Z-A A350-A-42-11-XX-01ZZZ-343Z-A
A350-A-42-11-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-A A350-A-46-12-01-05ZZZ-752Z-A
TECHNICAL FOLLOW UP (TFU)32.40.00.044
CONF 006(1) Modification
(a) Task set A350-A-32-XX-P037-03000-93AA-A Modification
ELECTRICAL STANDARD PRACTICES (ESP)A350-A-20-55-XX-01ZZZ-042Z-A
A350SERVICE BULLETIN
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INTRODUCTION (INTRO)A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP)A350-A-24-41-XX-00ZZZ-170Z-A A350-A-31-51-XX-02ZZZ-345Z-AA350-A-31-63-XX-00ZZZ-133Z-A A350-A-32-31-XX-03ZZZ-343Z-AA350-A-32-42-XX-05ZZZ-343Z-A A350-A-32-81-XX-01ZZZ-752Z-AA350-A-32-82-XX-00ZZZ-343Z-A A350-A-42-11-XX-01ZZZ-343Z-A
A350-A-42-11-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-A A350-A-46-12-01-05ZZZ-752Z-A
TECHNICAL FOLLOW UP (TFU)32.40.00.044
CONF ALLK. PUBLICATION AFFECTED
AIRCRAFT FAULT ISOLATION (AFI)FLIGHT CREW OPERATING MANUAL (FCOM)FLIGHT MANUAL (FM)MAINTENANCE ILLUSTRATED PART DATA (MIPD)MASTER MINIMUM EQUIPMENT LIST (MMEL)MAINTENANCE PROCEDURE (MP)SYSTEM DESCRIPTION (SD)This Service Bulletin has an impact on flight operations documentation. Refer to ISI00.00.00135 paragraph "Flight Operations Products" for further information on the updateof affected Flight Operations Products.Technical queries should be addressed through TechRequest on AirbusWorld using "TechnicalData/Support to report Service Bulletins" form.
L. INDUSTRY SUPPORT INFORMATIONAIRBUS will share the costs of accomplishment of this Service Bulletin by providing thematset at no charge for orders placed within 24 months after the initial issue date of theService Bulletin.AIRBUS will credit the man hours indicated in this Service Bulletin at the agreed in-housewarranty labor rate for claims received no later than 90 days after completion of the lastaffected aircraft of your fleet, for the accomplishment of this Service Bulletin within 24months after the issue date of the Service Bulletin.This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofitmanagement department: [email protected].
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2. MATERIAL INFORMATIONA. MATERIAL APPLICABILITY
CONF 001Material for task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL QTY SEE NOTESFLS kit 32P037N01R01 1FLS kit 32P037N03R00 1Interchangeable parts See SB
CONF 002Material for task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL QTY SEE NOTESFLS kit 32P037N01R01 1Interchangeable parts See SB
CONF 003Material for task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL QTY SEE NOTESFLS kit 32P037N02R01 1Interchangeable parts See SB
CONF 004Material for task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL QTY SEE NOTESFLS kit 32P037N02R01 1Interchangeable parts See SB
CONF 005Material for task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL QTY SEE NOTESFLS kit 32P037N02R01 1Interchangeable parts See SB
CONF 006Material for task set A350-A-32-XX-P037-03000-93AA-A Modification
MATERIAL QTY SEE NOTESFLS kit 32P037N02R01 1Interchangeable parts See SB
CONF ALLB. TOOLING
No toolsC. CONSUMABLES
No consumablesD. LIST OF NEW PARTS
A350SERVICE BULLETIN
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CONF 001 002FLS kit 32P037N01R01
Cost 1200.00 USDAvailability 007 d (calendar days from receipt of order)NOTE(S)
The availability given above is the standard lead-time from the date of your purchaseorder. If items are required before this time, please include a retrofit planningschedule with your order so that we can try to comply with your requirements.The sales terms (costs and availability) are estimated in relation to economicconditions. The latest valid price and lead-time for ordering purposes shall beobtained through the AIRBUS Spares portal or through a request for quotation [email protected].
Procurement address FAPE3
AIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFranceE-mail: [email protected]: http://spares.airbus.com
NOTE(S)All software Part Numbers required for accomplishment of this Service Bulletin will bedelivered through Electronic Delivery Service (EDS) and will have to be downloadedfrom airnavX MyLibrary application of AirbusWorld portal.Customers with aircraft shown in the applicability of this Service Bulletin should senda purchase order to AIRBUS at the address given above and quote the number of thisService Bulletin.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTESABF20A6T6ALCF0H 1 SOFTWAREABF45A6FYALED0T 1 SOFTWAREFMB5221608S05B2 1 SOFTWAREFMB5821601S05B1 1 SOFTWAREFMB5A21600S05B2 1 SOFTWAREFMB5A21603S05B1 1 SOFTWAREFMB5C21605S05B1 1 SOFTWAREFMB5D21604S05B1 1 SOFTWARE
CONF 003-006FLS kit 32P037N02R01
Cost 1200.00 USDAvailability 007 d (calendar days from receipt of order)NOTE(S)
The availability given above is the standard lead-time from the date of your purchaseorder. If items are required before this time, please include a retrofit planningschedule with your order so that we can try to comply with your requirements.The sales terms (costs and availability) are estimated in relation to economicconditions. The latest valid price and lead-time for ordering purposes shall be
A350SERVICE BULLETIN
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obtained through the AIRBUS Spares portal or through a request for quotation [email protected].
Procurement address FAPE3
AIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFranceE-mail: [email protected]: http://spares.airbus.com
NOTE(S)All software Part Numbers required for accomplishment of this Service Bulletin will bedelivered through Electronic Delivery Service (EDS) and will have to be downloadedfrom airnavX MyLibrary application of AirbusWorld portal.Customers with aircraft shown in the applicability of this Service Bulletin should senda purchase order to AIRBUS at the address given above and quote the number of thisService Bulletin.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTESABF20A6T6ALCF0H 1 SOFTWAREABF45A6FYALED0T 1 SOFTWAREFMB5221608S05B2 1 SOFTWAREFMB5821601S05B1 1 SOFTWAREFMB5A21600S05B2 1 SOFTWAREFMB5A21603S05B1 1 SOFTWAREFMB5C21605S05B1 1 SOFTWAREFMB5D21604S05B1 1 SOFTWARE
CONF 001FLS kit 32P037N03R00
Cost 450.00 USDAvailability 007 d (calendar days from receipt of order)NOTE(S)
The availability given above is the standard lead-time from the date of your purchaseorder. If items are required before this time, please include a retrofit planningschedule with your order so that we can try to comply with your requirements.The sales terms (costs and availability) are estimated in relation to economicconditions. The latest valid price and lead-time for ordering purposes shall beobtained through the AIRBUS Spares portal or through a request for quotation [email protected].
Procurement address FAPE3
AIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFranceE-mail: [email protected]: http://spares.airbus.com
NOTE(S)All software Part Numbers required for accomplishment of this Service Bulletin will bedelivered through Electronic Delivery Service (EDS) and will have to be downloadedfrom airnavX MyLibrary application of AirbusWorld portal.
A350SERVICE BULLETIN
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Customers with aircraft shown in the applicability of this Service Bulletin should senda purchase order to AIRBUS at the address given above and quote the number of thisService Bulletin.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTESABF57A6FYALEC0A 1 SOFTWAREFMB5321609S05A1 1 SOFTWAREFMB5C21606S05A1 1 SOFTWARE
CONF ALLE. LIST OF EXISTING PARTS
CONF 001Interchangeable parts for task set A350-A-32-XX-P037-03000-93AA-A Modification
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-LGERS ABF21A6FYALEC07 ABF57A6FYALEC0A 03 (1)SOFTWARE-CPIOMH6 CONFIG ABF2CA6T6ALCE0G ABF20A6T6ALCF0H 03 (1)
SOFTWARE-BSCSMSL FILE ABF55A6FYALED0D ABF45A6FYALED0T 03 (1)
SOFTWARE-BSCS,BITE FMB5321608S04A1 FMB5221608S05B2 03 (1)
SOFTWARE-LGERS,BITE FMB5621609S03B1 FMB5321609S05A1 03 (1)
SOFTWARE-BCS,COM FMB5821600S04A2 FMB5A21600S05B2 03 (1)SOFTWARE-BCS,MON FMB5921601S04A2 FMB5821601S05B1 03 (1)SOFTWARE-LGERS,COM FMB5A21606S03B2 FMB5C21606S05A1 03 (1)
SOFTWARE-RBCU FMB5B21603S04A2 FMB5A21603S05B1 03 (1)SOFTWARE-WSCS,MON FMB5E21605S04A1 FMB5C21605S05B1 03 (1)
SOFTWARE-WSCS,COM FMB5F21604S04A1 FMB5D21604S05B1 03 (1)
NOTE(S)For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter2).
(1): The interchangeability possibilities are for new or modified parts introduced by theaccomplishment of this Service Bulletin.
CONF 002Interchangeable parts for task set A350-A-32-XX-P037-03000-93AA-A Modification
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-CPIOMH6 CONFIG ABF2CA6T6ALCE0G ABF20A6T6ALCF0H 03 (1)
SOFTWARE-BSCSMSL FILE ABF55A6FYALED0D ABF45A6FYALED0T 03 (1)
SOFTWARE-BSCS,BITE FMB5321608S04A1 FMB5221608S05B2 03 (1)
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DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-BCS,COM FMB5821600S04A2 FMB5A21600S05B2 03 (1)SOFTWARE-BCS,MON FMB5921601S04A2 FMB5821601S05B1 03 (1)SOFTWARE-RBCU FMB5B21603S04A2 FMB5A21603S05B1 03 (1)SOFTWARE-WSCS,MON FMB5E21605S04A1 FMB5C21605S05B1 03 (1)
SOFTWARE-WSCS,COM FMB5F21604S04A1 FMB5D21604S05B1 03 (1)
NOTE(S)For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter2).
(1): The interchangeability possibilities are for new or modified parts introduced by theaccomplishment of this Service Bulletin.
CONF 003Interchangeable parts for task set A350-A-32-XX-P037-03000-93AA-A Modification
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-CPIOMH6 CONFIG ABF2CA6T6ALCE0G ABF20A6T6ALCF0H 03 (1)
SOFTWARE-BSCSMSL FILE ABF59A6FYALED0H ABF45A6FYALED0T 03 (1)
SOFTWARE-BSCS,BITE FMB5221608S05A1 FMB5221608S05B2 03 (1)
SOFTWARE-RBCU FMB5921603S05A1 FMB5A21603S05B1 03 (1)SOFTWARE-BCS,COM FMB5A21600S05A1 FMB5A21600S05B2 03 (1)SOFTWARE-BCS,MON FMB5B21601S05A1 FMB5821601S05B1 03 (1)SOFTWARE-WSCS,COM FMB5E21604S05A1 FMB5D21604S05B1 03 (1)
SOFTWARE-WSCS,MON FMB5F21605S05A1 FMB5C21605S05B1 03 (1)
NOTE(S)For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter2).
(1): The interchangeability possibilities are for new or modified parts introduced by theaccomplishment of this Service Bulletin.
CONF 004Interchangeable parts for task set A350-A-32-XX-P037-03000-93AA-A Modification
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-CPIOMH6 CONFIG ABF2CA6T6ALCE0G ABF20A6T6ALCF0H 03 (1)
SOFTWARE-BSCSMSL FILE ABF59A6FYALED0H ABF45A6FYALED0T 03 (1)
SOFTWARE-BSCS,BITE FMB5221608S05A1 FMB5221608S05B2 03 (1)
SOFTWARE-RBCU FMB5921603S05A1 FMB5A21603S05B1 03 (1)SOFTWARE-BCS,COM FMB5A21600S05A1 FMB5A21600S05B2 03 (1)
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DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-BCS,MON FMB5B21601S05A1 FMB5821601S05B1 03 (1)SOFTWARE-WSCS,COM FMB5E21604S05A1 FMB5D21604S05B1 03 (1)
SOFTWARE-WSCS,MON FMB5F21605S05A1 FMB5C21605S05B1 03 (1)
NOTE(S)For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter2).
(1): The interchangeability possibilities are for new or modified parts introduced by theaccomplishment of this Service Bulletin.
CONF 005Interchangeable parts for task set A350-A-32-XX-P037-03000-93AA-A Modification
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-CPIOMH6 CONFIG ABF2CA6T6ALCE0G ABF20A6T6ALCF0H 03 (1)
SOFTWARE-BSCSMSL FILE ABF59A6FYALED0H ABF45A6FYALED0T 03 (1)
SOFTWARE-BSCS,BITE FMB5221608S05A1 FMB5221608S05B2 03 (1)
SOFTWARE-RBCU FMB5921603S05A1 FMB5A21603S05B1 03 (1)SOFTWARE-BCS,COM FMB5A21600S05A1 FMB5A21600S05B2 03 (1)SOFTWARE-BCS,MON FMB5B21601S05A1 FMB5821601S05B1 03 (1)SOFTWARE-WSCS,COM FMB5E21604S05A1 FMB5D21604S05B1 03 (1)
SOFTWARE-WSCS,MON FMB5F21605S05A1 FMB5C21605S05B1 03 (1)
NOTE(S)For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter2).
(1): The interchangeability possibilities are for new or modified parts introduced by theaccomplishment of this Service Bulletin.
CONF 006Interchangeable parts for task set A350-A-32-XX-P037-03000-93AA-A Modification
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-CPIOMH6 CONFIG ABF2CA6T6ALCE0G ABF20A6T6ALCF0H 03 (1)
SOFTWARE-BSCSMSL FILE ABF59A6FYALED0H ABF45A6FYALED0T 03 (1)
SOFTWARE-BSCS,BITE FMB5221608S05A1 FMB5221608S05B2 03 (1)
SOFTWARE-RBCU FMB5921603S05A1 FMB5A21603S05B1 03 (1)SOFTWARE-BCS,COM FMB5A21600S05A1 FMB5A21600S05B2 03 (1)SOFTWARE-BCS,MON FMB5B21601S05A1 FMB5821601S05B1 03 (1)
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DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTESSOFTWARE-WSCS,COM FMB5E21604S05A1 FMB5D21604S05B1 03 (1)
SOFTWARE-WSCS,MON FMB5F21605S05A1 FMB5C21605S05B1 03 (1)
NOTE(S)For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter2).
(1): The interchangeability possibilities are for new or modified parts introduced by theaccomplishment of this Service Bulletin.
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CONF ALL3. ACCOMPLISHMENT INSTRUCTIONS
Task set A350-A-32-XX-P037-03000-93AA-AModification
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO Ref. ESP A350-A-20-55-XX-01ZZZ-042Z-A.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given inother 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 thisService 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 stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
CONF 001TOTAL MAN-HOURS 3.25 h
CONF 002TOTAL MAN-HOURS 2.75 h
CONF 003TOTAL MAN-HOURS 3.00 h
CONF 004TOTAL MAN-HOURS 2.75 h
CONF 005TOTAL MAN-HOURS 3.00 h
CONF 006TOTAL MAN-HOURS 3.00 h
CONF 001ELAPSED TIME (HOURS) 3.25 h
CONF 002ELAPSED TIME (HOURS) 2.75 h
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CONF 003ELAPSED TIME (HOURS) 3.00 h
CONF 004ELAPSED TIME (HOURS) 2.75 h
CONF 005ELAPSED TIME (HOURS) 3.00 h
CONF 006ELAPSED TIME (HOURS) 3.00 h
CONF ALLB. PREPARATION
CONF 001 002 004(1) Task A350-A-32-XX-P037-03001-540A-A - Job Set-up
Job Set-Up InformationWorking Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/SheetsINTRO A350-A-00-61-04-11ZZZ-018Z-D
MPA350-A-24-41-XX-00ZZZ-170Z-AA350-A-42-11-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-AA350-A-46-12-01-05ZZZ-752Z-A
Procedure
NOTE: For the basic Aircraft configuration, refer to Ref. INTRO A350-A-00-61-04-11ZZZ-018Z-D “Maintenance Procedure - Introduction”.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. MP A350-A-24-41-XX-00ZZZ-170Z-A.
(b) Do the Job Set-up procedure as specified in the uploading of the software to theCore Processing Input/Output Module (CPIOM) H6 ( FIN 8TF61, FIN 8TF62, FIN8TF63 and FIN 8TF64), refer to Ref. MP A350-A-42-11-XX-01ZZZ-752Z-A.
(c) Do the job set-up procedure as specified in the uploading of the MaintenanceSystem Load (MSL) file software component(s) to the Avionics Server FunctionCabinet (ASFC) (1TC), refer to Ref. MP A350-A-46-12-01-05ZZZ-752Z-A.
(d) Do the job set-up procedure as specified in the uploading of software toequipment, refer to Ref. MP A350-A-45-46-XX-00ZZZ-752Z-A.
(e) Make sure that these circuit breakers are closed:ON A/C 0246, 0251, 0257, 0260, 0270, 0283, 0308, 0312-0314, 0316, 0318, 0321-0325,0327-0329, 0333-0335, 0337, 0339, 0343ON A/C 0005-0058, 0060-0064, 0066-0070, 0072-0087, 0089-0101, 0103-0107, 0109,0111-0117, 0119-0124, 0126-0130, 0132-0138, 0140, 0142-0151, 0153-0155, 0157-0160,
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0162-0165, 0167, 0168, 0170, 0172-0187, 0189-0193, 0195-0205, 0207-0214, 0216-0221,0223, 0224, 0226-0228, 0230-0232, 0234-0240, 0243-0245, 0247-0250, 0254-0256, 0259,0261, 0263-0265, 0267-0269, 0271-0273, 0276-0282, 0284, 0285, 0287, 0289, 0291-0295,0297, 0300-0303, 0305, 0307, 0309-0311 (POST SB 42-P012)ON A/C 0088, 0102, 0110, 0118, 0125, 0141, 0161, 0169, 0188, 0206, 0225, 0233, 0252,0258 (PRE SB 42-P012)
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC1 C/B-RBCU1 CHAN-E 3203GL 3HH03
PANEL DESIGNATION FIN LOCATION SEE NOTESCBP1 C/B-RBCU1 CHAN-B 3201GL 5AH08
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC1 C/B-RBCU1 CHAN-A 3101GL 1KK04
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC2 C/B-RBCU2 CHAN-E 3202GL 4HJ03
PANEL DESIGNATION FIN LOCATION SEE NOTESCBP2 C/B-RBCU2 CHAN-B 3200GL 6AH08
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC2 C/B-RBCU2 CHAN-A 3100GL 2KD05
CONF 001 002 004(f) On panel 312VM, make sure that the A-SKID switch is set to the ON position.
CONF 003 005 006(1) Task A350-A-32-XX-P037-03002-540A-A - Job Set-up
Job Set-Up InformationWorking Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/SheetsINTRO A350-A-00-61-04-11ZZZ-018Z-D
MP
A350-A-24-41-XX-00ZZZ-170Z-AA350-A-31-51-XX-02ZZZ-345Z-AA350-A-42-11-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-AA350-A-46-12-01-05ZZZ-752Z-A
Procedure
NOTE: For the basic Aircraft configuration, refer to Ref. INTRO A350-A-00-61-04-11ZZZ-018Z-D “Maintenance Procedure - Introduction”.
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(a) Make sure that the aircraft is electrically grounded, refer to Ref. MP A350-A-24-41-XX-00ZZZ-170Z-A.
(b) Do the Job Set-up procedure as specified in the procedure to get access tothe Electronic Centralized Aircraft Monitoring (ECAM) Temporary Change CodeManagement of the Flight Warning System (FWS), refer to Ref. MP A350-A-31-51-XX-02ZZZ-345Z-A.
(c) Do the Job Set-up procedure as specified in the uploading of the software to theCore Processing Input/Output Module (CPIOM) H6 ( FIN 8TF61, FIN 8TF62, FIN8TF63 and FIN 8TF64), refer to Ref. MP A350-A-42-11-XX-01ZZZ-752Z-A.
(d) Do the job set-up procedure as specified in the uploading of the MaintenanceSystem Load (MSL) file software component(s) to the Avionics Server FunctionCabinet (ASFC) (1TC), refer to Ref. MP A350-A-46-12-01-05ZZZ-752Z-A.
(e) Do the job set-up procedure as specified in the uploading of software toequipment, refer to Ref. MP A350-A-45-46-XX-00ZZZ-752Z-A.
(f) Make sure that these circuit breakers are closed:ON A/C 0215, 0229, 0241, 0262, 0266, 0274, 0286, 0290, 0296, 0298, 0306, 0315, 0319,0326, 0330, 0336ON A/C 0088, 0102, 0110, 0118, 0125, 0141, 0161, 0169, 0188, 0206, 0225, 0233, 0252,0258 (POST SB 42-P012)
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC1 C/B-RBCU1 CHAN-E 3203GL 3HH03
PANEL DESIGNATION FIN LOCATION SEE NOTESCBP1 C/B-RBCU1 CHAN-B 3201GL 5AH08
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC1 C/B-RBCU1 CHAN-A 3101GL 1KK04
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC2 C/B-RBCU2 CHAN-E 3202GL 4HJ03
PANEL DESIGNATION FIN LOCATION SEE NOTESCBP2 C/B-RBCU2 CHAN-B 3200GL 6AH08
PANEL DESIGNATION FIN LOCATION SEE NOTESEPDC2 C/B-RBCU2 CHAN-A 3100GL 2KD05
CONF 003 005 006(g) On panel 312VM, make sure that the A-SKID switch is set to the ON position.
CONF ALLC. PROCEDURE
CONF 001 002(1) Task A350-A-32-XX-P037-01001-550A-A - Upload the BCS S5B, the WSCS S5B,
BSCS BITE S5B Software and SOFTWARE-CPIOM H6 CONFIG TABLE B24 to the
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CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63 (8TF63) and CPIOM-64(8TF64)Job Set-Up Information
Working Area
Impacted Zone Access / Work Location210 Access Door 831, Door 841
Manpower/Resources/Skills
Man-hours 1.00 hMinimum Number of person 1Elapsed Time 1.00 h
Material necessary to do the jobFLS kit 32P037N01R01ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
ABF20A6T6ALCF0H 1 SOFTWAREFMB5221608S05B2 1 SOFTWAREFMB5821601S05B1 1 SOFTWAREFMB5A21600S05B2 1 SOFTWAREFMB5C21605S05B1 1 SOFTWAREFMB5D21604S05B1 1 SOFTWARE
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-42-11-XX-01ZZZ-752Z-A
Procedure(a) Upload the BCS S5B, the WSCS S5B, BSCS BITE S5B Software and SOFTWARE-
CPIOM H6 CONFIG TABLE B24 to the CPIOM-H61 (8TF61), CPIOM-H62 (8TF62),CPIOM-H63 (8TF63) and CPIOM-64 (8TF64), refer to Ref. MP A350-A-42-11-XX-01ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For CPIOM-H61:
FIN 861TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 861TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL1SW11 SOFTWARE-BCS,COM FMB5821600S04A2
becomes:
FIN 12GL1SW11 SOFTWARE-BCS,COM FMB5A21600S05B2
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FIN 13GL1SW21 SOFTWARE-WSCS,MON FMB5E21605S04A1
becomes:
FIN 13GL1SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
FIN 12GL3SW21 SOFTWARE-BCS,MON FMB5921601S04A2
becomes:
FIN 12GL3SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL3SW11 SOFTWARE-WSCS,COM FMB5F21604S04A1
becomes:
FIN 13GL3SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL3SW11 SOFTWARE-BSCS,BITE FMB5321608S04A1
becomes:
FIN 14GL3SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
2 For CPIOM-H62:
FIN 862TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 862TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL2SW11 SOFTWARE-BCS,COM FMB5821600S04A2
becomes:
FIN 12GL2SW11 SOFTWARE-BCS,COM FMB5A21600S05B2
FIN 13GL2SW21 SOFTWARE-WSCS,MON FMB5E21605S04A1
becomes:
FIN 13GL2SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
FIN 12GL4SW21 SOFTWARE-BCS,MON FMB5921601S04A2
becomes:
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FIN 12GL4SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL4SW11 SOFTWARE-WSCS,COM FMB5F21604S04A1
becomes:
FIN 13GL4SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL4SW11 SOFTWARE-BSCS,BITE FMB5321608S04A1
becomes:
FIN 14GL4SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
3 For CPIOM-H63:
FIN 863TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 863TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL1SW21 SOFTWARE-BCS,MON FMB5921601S04A2
becomes:
FIN 12GL1SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL1SW11 SOFTWARE-WSCS,COM FMB5F21604S04A1
becomes:
FIN 13GL1SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL1SW11 SOFTWARE-BSCS,BITE FMB5321608S04A1
becomes:
FIN 14GL1SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
FIN 12GL3SW11 SOFTWARE-BCS,COM FMB5821600S04A2
becomes:
FIN 12GL3SW11 SOFTWARE-BCS,COM FMB5A21600S05B2
FIN 13GL3SW2
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1 SOFTWARE-WSCS,MON FMB5E21605S04A1 becomes:
FIN 13GL3SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
4 For CPIOM-H64:
FIN 864TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 864TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL2SW21 SOFTWARE-BCS,MON FMB5921601S04A2
becomes:
FIN 12GL2SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL2SW11 SOFTWARE-WSCS,COM FMB5F21604S04A1
becomes:
FIN 13GL2SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL2SW11 SOFTWARE-BSCS,BITE FMB5321608S04A1
becomes:
FIN 14GL2SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
FIN 12GL4SW11 SOFTWARE-BCS,COM FMB5821600S04A2
becomes:
FIN 12GL4SW11 SOFTWARE-BCS,COM FMB5A21600S05B2
FIN 13GL4SW21 SOFTWARE-WSCS,MON FMB5E21605S04A1
becomes:
FIN 13GL4SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 40
CONF 001 002
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
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CONF 003-006(1) Task A350-A-32-XX-P037-01003-550A-A - Upload the BCS S5B, the WSCS S5B,
BSCS BITE S5B Software and SOFTWARE-CPIOM H6 CONFIG TABLE B24 to theCPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63 (8TF63) and CPIOM-64(8TF64)Job Set-Up Information
Working Area
Impacted Zone Access / Work Location210 Access Door 831, Door 841
Manpower/Resources/Skills
Man-hours 1.00 hMinimum Number of person 1Elapsed Time 1.00 h
Material necessary to do the jobFLS kit 32P037N02R01ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
ABF20A6T6ALCF0H 1 SOFTWAREFMB5221608S05B2 1 SOFTWAREFMB5821601S05B1 1 SOFTWAREFMB5A21600S05B2 1 SOFTWAREFMB5C21605S05B1 1 SOFTWAREFMB5D21604S05B1 1 SOFTWARE
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-42-11-XX-01ZZZ-752Z-A
Procedure(a) Upload the BCS S5B, the WSCS S5B, BSCS BITE S5B Software and SOFTWARE-
CPIOM H6 CONFIG TABLE B24 to the CPIOM-H61 (8TF61), CPIOM-H62 (8TF62),CPIOM-H63 (8TF63) and CPIOM-64 (8TF64), refer to Ref. MP A350-A-42-11-XX-01ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For CPIOM-H61:
FIN 861TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 861TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL1SW11 SOFTWARE-BCS,COM FMB5A21600S05A1
becomes:
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FIN 12GL1SW11 SOFTWARE-BCS,COM FMB5A21600S05B2
FIN 13GL1SW21 SOFTWARE-WSCS,MON FMB5F21605S05A1
becomes:
FIN 13GL1SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
FIN 12GL3SW21 SOFTWARE-BCS,MON FMB5B21601S05A1
becomes:
FIN 12GL3SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL3SW11 SOFTWARE-WSCS,COM FMB5E21604S05A1
becomes:
FIN 13GL3SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL3SW11 SOFTWARE-BSCS,BITE FMB5221608S05A1
becomes:
FIN 14GL3SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
2 For CPIOM-H62:
FIN 862TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 862TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL2SW11 SOFTWARE-BCS,COM FMB5A21600S05A1
becomes:
FIN 12GL2SW11 SOFTWARE-BCS,COM FMB5A21600S05B2
FIN 13GL2SW21 SOFTWARE-WSCS,MON FMB5F21605S05A1
becomes:
FIN 13GL2SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
FIN 12GL4SW2
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1 SOFTWARE-BCS,MON FMB5B21601S05A1 becomes:
FIN 12GL4SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL4SW11 SOFTWARE-WSCS,COM FMB5E21604S05A1
becomes:
FIN 13GL4SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL4SW11 SOFTWARE-BSCS,BITE FMB5221608S05A1
becomes:
FIN 14GL4SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
3 For CPIOM-H63:
FIN 863TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 863TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL1SW21 SOFTWARE-BCS,MON FMB5B21601S05A1
becomes:
FIN 12GL1SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL1SW11 SOFTWARE-WSCS,COM FMB5E21604S05A1
becomes:
FIN 13GL1SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL1SW11 SOFTWARE-BSCS,BITE FMB5221608S05A1
becomes:
FIN 14GL1SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
FIN 12GL3SW11 SOFTWARE-BCS,COM FMB5A21600S05A1
becomes:
FIN 12GL3SW1
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 44
1 SOFTWARE-BCS,COM FMB5A21600S05B2
FIN 13GL3SW21 SOFTWARE-WSCS,MON FMB5F21605S05A1
becomes:
FIN 13GL3SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
4 For CPIOM-H64:
FIN 864TFSW21 SOFTWARE-CPIOM H6
CONFIGABF2CA6T6ALCE0G
becomes:
FIN 864TFSW21 SOFTWARE-CPIOM H6
CONFIGABF20A6T6ALCF0H
FIN 12GL2SW21 SOFTWARE-BCS,MON FMB5B21601S05A1
becomes:
FIN 12GL2SW21 SOFTWARE-BCS,MON FMB5821601S05B1
FIN 13GL2SW11 SOFTWARE-WSCS,COM FMB5E21604S05A1
becomes:
FIN 13GL2SW11 SOFTWARE-WSCS,COM FMB5D21604S05B1
FIN 14GL2SW11 SOFTWARE-BSCS,BITE FMB5221608S05A1
becomes:
FIN 14GL2SW11 SOFTWARE-BSCS,BITE FMB5221608S05B2
FIN 12GL4SW11 SOFTWARE-BCS,COM FMB5A21600S05A1
becomes:
FIN 12GL4SW11 SOFTWARE-BCS,COM FMB5A21600S05B2
FIN 13GL4SW21 SOFTWARE-WSCS,MON FMB5F21605S05A1
becomes:
FIN 13GL4SW21 SOFTWARE-WSCS,MON FMB5C21605S05B1
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 45
CONF 003-006
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 46
CONF 001 002(2) Task A350-A-32-XX-P037-04001-540A-A - Upload the BSCS MSL File Software
(70GLSW3) to ASFC (1TC)Job Set-Up Information
Working Area
Impacted Zone Access / Work Location210 Access Door 831, Door 841
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Material necessary to do the jobFLS kit 32P037N01R01ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
ABF45A6FYALED0T 1 SOFTWARE
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-46-12-01-05ZZZ-752Z-A
Procedure(a) Upload the BSCS MSL file software component(s) to the ASFC (1TC), refer to Ref.
MP A350-A-46-12-01-05ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For ASFC (1TC):
FIN 70GLSW31 SOFTWARE-BSCS MSL
FILEABF55A6FYALED0D
becomes:
FIN 70GLSW31 SOFTWARE-BSCS MSL
FILEABF45A6FYALED0T
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 47
CONF 001 002
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 48
CONF 003-006(2) Task A350-A-32-XX-P037-04003-540A-A - Upload the BSCS MSL File Software
(70GLSW3) to ASFC (1TC)Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Material necessary to do the jobFLS kit 32P037N02R01ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
ABF45A6FYALED0T 1 SOFTWARE
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-46-12-01-05ZZZ-752Z-A
Procedure(a) Upload the BSCS MSL file software component(s) to the ASFC (1TC), refer to Ref.
MP A350-A-46-12-01-05ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For ASFC (1TC):
FIN 70GLSW31 SOFTWARE-BSCS MSL
FILEABF59A6FYALED0H
becomes:
FIN 70GLSW31 SOFTWARE-BSCS MSL
FILEABF45A6FYALED0T
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 49
CONF 003-006
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 50
CONF 001(3) Task A350-A-32-XX-P037-05001-540A-A - Upload the LGERS S5A and LGERS
BITE S5A Software to the CPIOM-H61 (8TF61), CPIOM-H62 (8TF62), CPIOM-H63 (8TF63) and CPIOM-H64 (8TF64)Job Set-Up Information
Working Area
Impacted Zone Access / Work Location210 Access Door 831, Door 841
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Material necessary to do the jobFLS kit 32P037N03R00ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
FMB5321609S05A1 1 SOFTWAREFMB5C21606S05A1 1 SOFTWARE
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-42-11-XX-01ZZZ-752Z-A
Procedure(a) Upload the LGERS BITE software component(s) to the Core Processing Input/
Output Module (CPIOM) H6, refer to Ref. MP A350-A-42-11-XX-01ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For CPIOM-H61 (8TF61):
FIN 7GL1SW11 SOFTWARE-LGERS,COM FMB5A21606S03B2
becomes:
FIN 7GL1SW11 SOFTWARE-LGERS,COM FMB5C21606S05A1
and
FIN 7GL3SW31 SOFTWARE-LGERS,BITE FMB5621609S03B1
becomes:
FIN 7GL3SW31 SOFTWARE-LGERS,BITE FMB5321609S05A1
2 For CPIOM-H62 (8TF62):
FIN 7GL2SW11 SOFTWARE-LGERS,COM FMB5A21606S03B2
becomes:
FIN 7GL2SW1
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1 SOFTWARE-LGERS,COM FMB5C21606S05A1 and
FIN 7GL4SW31 SOFTWARE-LGERS,BITE FMB5621609S03B1
becomes:
FIN 7GL4SW31 SOFTWARE-LGERS,BITE FMB5321609S05A1
3 For CPIOM-H63 (8TF63):
FIN 7GL3SW11 SOFTWARE-LGERS,COM FMB5A21606S03B2
becomes:
FIN 7GL3SW11 SOFTWARE-LGERS,COM FMB5C21606S05A1
and
FIN 7GL1SW31 SOFTWARE-LGERS,BITE FMB5621609S03B1
becomes:
FIN 7GL1SW31 SOFTWARE-LGERS,BITE FMB5321609S05A1
4 For CPIOM-H64 (8TF64):
FIN 7GL4SW11 SOFTWARE-LGERS,COM FMB5A21606S03B2
becomes:
FIN 7GL4SW11 SOFTWARE-LGERS,COM FMB5C21606S05A1
and
FIN 7GL2SW31 SOFTWARE-LGERS,BITE FMB5621609S03B1
becomes:
FIN 7GL2SW31 SOFTWARE-LGERS,BITE FMB5321609S05A1
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 52
CONF 001
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 53
CONF 003(4) Task A350-A-32-XX-P037-03004-760A-A - Desactivate the ETC Code 29BF for
the ATQC EnvelopeJob Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-31-51-XX-02ZZZ-345Z-A
Procedure
NOTE: Check if the date is correct.
(a) Desactivate the ECAM Temporary Change (ETC) code for the Airbus TemporaryQuick Change (ATQC) envelopeRefer to Ref. Fig. Location of the OMT.1 Delete the ETC code No. 29BF – Remove FP9 inhibition for dual HYD alert,
refer to Ref. MP A350-A-31-51-XX-02ZZZ-345Z-A.
NOTE: ETC 29BF amends the ECAM procedure associated to the alerts:- HYD G+Y SYS LO PRESS.
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 54
CONF 003
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 55
CONF 005(4) Task A350-A-32-XX-P037-03006-760A-A - Desactivate the ETC Codes 29BF
and 32AS for the ATQC EnvelopeJob Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-31-51-XX-02ZZZ-345Z-A
Procedure
NOTE: Check if the date is correct.
(a) Desactivate the ECAM Temporary Change (ETC) code for the Airbus TemporaryQuick Change (ATQC) envelopeRefer to Ref. Fig. Location of the OMT.1 Delete the ETC code No. 32AS – Braking at 1000psi in case of a/skid fault,
refer to Ref. MP A350-A-31-51-XX-02ZZZ-345Z-A.
NOTE: ETC 32AS amends the ECAM procedure associated to the alerts:- BRAKES ANTI-SKID (A-SKID) alerts (BRAKES A-SKID FAULT ON
ALL WHEELS,- BRAKES A-SKID OFF.
2 Delete the ETC code No. 29BF – Remove FP9 inhibition for dual HYD alert,refer to Ref. MP A350-A-31-51-XX-02ZZZ-345Z-A.
NOTE: ETC 29BF amends the ECAM procedure associated to the alerts:- HYD G+Y SYS LO PRESS.
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 56
CONF 005
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 57
CONF 006(4) Task A350-A-32-XX-P037-03007-760A-A - Desactivate the ETC Code 32AS for
the ATQC EnvelopeJob Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-31-51-XX-02ZZZ-345Z-A
Procedure
NOTE: Check if the date is correct.
(a) Desactivate the ECAM Temporary Change (ETC) code for the Airbus TemporaryQuick Change (ATQC) envelopeRefer to Ref. Fig. Location of the OMT.1 Delete the ETC code No. 32AS – Braking at 1000psi in case of a/skid fault,
refer to Ref. MP A350-A-31-51-XX-02ZZZ-345Z-A.
NOTE: ETC 32AS amends the ECAM procedure associated to the alerts:- BRAKES ANTI-SKID (A-SKID) alerts (BRAKES A-SKID FAULT ON
ALL WHEELS,- BRAKES A-SKID OFF.
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 58
CONF 006
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 59
CONF 001(5) Task A350-A-32-XX-P037-07001-540A-A - Upload the LGERS MSL File
Software (70GLSW1) to ASFC (1TC)Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Material necessary to do the jobFLS kit 32P037N03R00ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
ABF57A6FYALEC0A 1 SOFTWARE
Referenced Information
Manuals/Drawings References/SheetsMP A350-A-46-12-01-05ZZZ-752Z-A
Procedure(a) Upload the LGERS file software component(s) to the ASFC (1TC), refer to Ref. MP
A350-A-46-12-01-05ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For ASFC (1TC):
FIN 70GLSW11 SOFTWARE-LGERS ABF21A6FYALEC07
becomes:
FIN 70GLSW11 SOFTWARE-LGERS ABF57A6FYALEC0A
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 60
CONF 001
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 61
CONF 001 002(6) Task A350-A-32-XX-P037-08001-540A-A - Upload the RCBU software S5B
(15GL1SW1, 15GL1SW2, 15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and10GL2)Job Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Material necessary to do the jobFLS kit 32P037N01R01ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
FMB5A21603S05B1 1 SOFTWARE
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-32-81-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-A
Procedure(a) Before uploading RBCU1 and RBCU2, confirm that P/N of RBCU1 and RBCU2 is
D24448004-2 or D24448004-3.(b) Upload the software (15GL1SW1, 15GL1SW2, 15GL2SW1 and 15GL2SW2) to the
RBCU (10GL1 and 10GL2), refer to Ref. MP A350-A-32-81-XX-01ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For RBCU (10GL1):
FIN 15GL1SW11 SOFTWARE-RBCU FMB5B21603S04A2
becomes:
FIN 15GL1SW11 SOFTWARE-RBCU FMB5A21603S05B1
FIN 15GL1SW21 SOFTWARE-RBCU FMB5B21603S04A2
becomes:
FIN 15GL1SW21 SOFTWARE-RBCU FMB5A21603S05B1
2 For RBCU (10GL2):
FIN 15GL2SW11 SOFTWARE-RBCU FMB5B21603S04A2
becomes:
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FIN 15GL2SW11 SOFTWARE-RBCU FMB5A21603S05B1
FIN 15GL2SW21 SOFTWARE-RBCU FMB5B21603S04A2
becomes:
FIN 15GL2SW21 SOFTWARE-RBCU FMB5A21603S05B1
(c) Do a check of the configuration of the uploaded software components inaccordance with configuration validation step D in MP Ref. MP A350-A-45-46-XX-00ZZZ-752Z-A (uploading of software to equipment) and if the "CONFIG TOBE VALIDATED" message is shown, validate their PNs.
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 63
CONF 001 002
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 64
CONF 003-006(6) Task A350-A-32-XX-P037-08003-540A-A - Upload the RCBU software S5B
(15GL1SW1, 15GL1SW2, 15GL2SW1, 15GL2SW2) to the RBCU (10GL1 and10GL2)Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 hMinimum Number of person 1Elapsed Time 0.25 h
Material necessary to do the jobFLS kit 32P037N02R01ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
FMB5A21603S05B1 1 SOFTWARE
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-32-81-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-A
Procedure(a) Before uploading RBCU1 and RBCU2, confirm that P/N of RBCU1 and RBCU2 is
D24448004-2 or D24448004-3.(b) Upload the software (15GL1SW1, 15GL1SW2, 15GL2SW1 and 15GL2SW2) to the
RBCU (10GL1 and 10GL2), refer to Ref. MP A350-A-32-81-XX-01ZZZ-752Z-A.Refer to Ref. Fig. Location of the OMT.1 For RBCU (10GL1):
FIN 15GL1SW11 SOFTWARE-RBCU FMB5921603S05A1
becomes:
FIN 15GL1SW11 SOFTWARE-RBCU FMB5A21603S05B1
FIN 15GL1SW21 SOFTWARE-RBCU FMB5921603S05A1
becomes:
FIN 15GL1SW21 SOFTWARE-RBCU FMB5A21603S05B1
2 For RBCU (10GL2):
FIN 15GL2SW11 SOFTWARE-RBCU FMB5921603S05A1
becomes:
FIN 15GL2SW11 SOFTWARE-RBCU FMB5A21603S05B1
FIN 15GL2SW2
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1 SOFTWARE-RBCU FMB5921603S05A1 becomes:
FIN 15GL2SW21 SOFTWARE-RBCU FMB5A21603S05B1
(c) Do a check of the configuration of the uploaded software components inaccordance with configuration validation step D in MP Ref. MP A350-A-45-46-XX-00ZZZ-752Z-A (uploading of software to equipment) and if the "CONFIG TOBE VALIDATED" message is shown, validate their PNs.
A350SERVICE BULLETIN
Figure ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01 SHEET 1/1REV 00 Jul 30/19 A350-32-P037Location of the OMT
Page 66
CONF 003-006
8TC
10TC
OMT
KEYBOARD-OMTFR1
FR12
A
A
Z210
ICN-A350-A-32XXP037-A-FAPE3-04TB9-A-001-01
A350SERVICE BULLETIN
REV 00 Jul 30/19 A350-32-P037Page 67
CONF ALLD. PREPARATION FOR TEST
NoneE. TEST
CONF 001 002 004(1) Task A350-A-32-XX-P037-04001-300A-A - Testing
Job Set-Up InformationManpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
MPA350-A-32-31-XX-03ZZZ-343Z-AA350-A-32-42-XX-05ZZZ-343Z-AA350-A-32-82-XX-00ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-343Z-A
Procedure(a) Do the BITE test of the Braking and Steering Control System (BSCS test) on
BSCS1 and BSCS2, refer to Ref. MP A350-A-32-42-XX-05ZZZ-343Z-A.- Confirm no BRAKES nor STEER Alert/Dispatch Message is shown.
(b) Do the BITE test of the LGERS (System Test) on LGERS1 and LGERS2, refer toRef. MP A350-A-32-31-XX-03ZZZ-343Z-A.BITE Test of the Landing Gear Extension and Retraction System (LGERS).
(c) Do the BITE test of LGMS (System Test) on LGMS1 and LGMS2, refer to Ref. MPA350-A-32-82-XX-00ZZZ-343Z-A.BITE Test of the Landing Gear Monitoring System (LGMS) (System Test)
(d) Do the BITE Test of CPIOM-H61, CPIOM-H62, CPIOM-H63 and CPIOM-H64, refer toRef. MP A350-A-42-11-XX-01ZZZ-343Z-A.BITE Test of the Core Processing Input/Output Module (CPIOM) (CPIOM InterfaceTest).
CONF 003(1) Task A350-A-32-XX-P037-04002-300A-A - Testing
Job Set-Up InformationManpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-31-51-XX-02ZZZ-345Z-AA350-A-32-31-XX-03ZZZ-343Z-A
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Manuals/Drawings References/SheetsA350-A-32-42-XX-05ZZZ-343Z-AA350-A-32-82-XX-00ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-343Z-A
Procedure(a) Do the BITE test of the Braking and Steering Control System (BSCS test) on
BSCS1 and BSCS2, refer to Ref. MP A350-A-32-42-XX-05ZZZ-343Z-A.- Confirm no BRAKES nor STEER Alert/Dispatch Message is shown.
(b) Do the BITE test of the LGERS (System Test) on LGERS1 and LGERS2, refer toRef. MP A350-A-32-31-XX-03ZZZ-343Z-A.BITE Test of the Landing Gear Extension and Retraction System (LGERS).
(c) Do the BITE test of LGMS (System Test) on LGMS1 and LGMS2, refer to Ref. MPA350-A-32-82-XX-00ZZZ-343Z-A.BITE Test of the Landing Gear Monitoring System (LGMS) (System Test)
(d) Do the BITE Test of CPIOM-H61, CPIOM-H62, CPIOM-H63 and CPIOM-H64, refer toRef. MP A350-A-42-11-XX-01ZZZ-343Z-A.BITE Test of the Core Processing Input/Output Module (CPIOM) (CPIOM InterfaceTest).
(e) Do a check of the desactivated ETCs list:1 After the validation of the modification to the list of ETC, refer to Ref. MP
A350-A-31-51-XX-02ZZZ-345Z-A, FWS1 and FWS2 will stop (FWS 1 + 2FAULT alert is displayed on Engine Warning Display (EWD)) and start againautomatically. The following check must be performed after FWS1 andFWS2 reset.
2 Check in the ETCs list that ETC code No. 29BF is not present, refer to Ref.MP A350-A-31-51-XX-02ZZZ-345Z-A.
CONF 005(1) Task A350-A-32-XX-P037-04003-300A-A - Testing
Job Set-Up InformationManpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
MP
A350-A-31-51-XX-02ZZZ-345Z-AA350-A-32-31-XX-03ZZZ-343Z-AA350-A-32-42-XX-05ZZZ-343Z-AA350-A-32-82-XX-00ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-343Z-A
Procedure(a) Do the BITE test of the Braking and Steering Control System (BSCS test) on
BSCS1 and BSCS2, refer to Ref. MP A350-A-32-42-XX-05ZZZ-343Z-A.- Confirm no BRAKES nor STEER Alert/Dispatch Message is shown.
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(b) Do the BITE test of the LGERS (System Test) on LGERS1 and LGERS2, refer toRef. MP A350-A-32-31-XX-03ZZZ-343Z-A.BITE Test of the Landing Gear Extension and Retraction System (LGERS).
(c) Do the BITE test of LGMS (System Test) on LGMS1 and LGMS2, refer to Ref. MPA350-A-32-82-XX-00ZZZ-343Z-A.BITE Test of the Landing Gear Monitoring System (LGMS) (System Test)
(d) Do the BITE Test of CPIOM-H61, CPIOM-H62, CPIOM-H63 and CPIOM-H64, refer toRef. MP A350-A-42-11-XX-01ZZZ-343Z-A.BITE Test of the Core Processing Input/Output Module (CPIOM) (CPIOM InterfaceTest).
(e) Do a check of the desactivated ETCs list:1 After the validation of the modification to the list of ETC, refer to Ref. MP
A350-A-31-51-XX-02ZZZ-345Z-A, FWS1 and FWS2 will stop (FWS 1 + 2FAULT alert is displayed on Engine Warning Display (EWD)) and start againautomatically. The following check must be performed after FWS1 andFWS2 reset.
2 Check in the ETCs list that ETC codes No. 29BF and No. 32AS are notpresent, refer to Ref. MP A350-A-31-51-XX-02ZZZ-345Z-A.
CONF 006(1) Task A350-A-32-XX-P037-04004-300A-A - Testing
Job Set-Up InformationManpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
MP
A350-A-31-51-XX-02ZZZ-345Z-AA350-A-32-31-XX-03ZZZ-343Z-AA350-A-32-42-XX-05ZZZ-343Z-AA350-A-32-82-XX-00ZZZ-343Z-AA350-A-42-11-XX-01ZZZ-343Z-A
Procedure(a) Do the BITE test of the Braking and Steering Control System (BSCS test) on
BSCS1 and BSCS2, refer to Ref. MP A350-A-32-42-XX-05ZZZ-343Z-A.- Confirm no BRAKES nor STEER Alert/Dispatch Message is shown.
(b) Do the BITE test of the LGERS (System Test) on LGERS1 and LGERS2, refer toRef. MP A350-A-32-31-XX-03ZZZ-343Z-A.BITE Test of the Landing Gear Extension and Retraction System (LGERS).
(c) Do the BITE test of LGMS (System Test) on LGMS1 and LGMS2, refer to Ref. MPA350-A-32-82-XX-00ZZZ-343Z-A.BITE Test of the Landing Gear Monitoring System (LGMS) (System Test)
(d) Do the BITE Test of CPIOM-H61, CPIOM-H62, CPIOM-H63 and CPIOM-H64, refer toRef. MP A350-A-42-11-XX-01ZZZ-343Z-A.BITE Test of the Core Processing Input/Output Module (CPIOM) (CPIOM InterfaceTest).
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(e) Do a check of the desactivated ETCs list:1 After the validation of the modification to the list of ETC, refer to Ref. MP
A350-A-31-51-XX-02ZZZ-345Z-A, FWS1 and FWS2 will stop (FWS 1 + 2FAULT alert is displayed on Engine Warning Display (EWD)) and start againautomatically. The following check must be performed after FWS1 andFWS2 reset.
2 Check in the ETCs list that ETC code No. 32AS is not present, refer to Ref.MP A350-A-31-51-XX-02ZZZ-345Z-A.
CONF ALLF. CLOSE-UP
(1) Task A350-A-32-XX-P037-03001-740A-A - Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 1Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
MP
A350-A-31-63-XX-00ZZZ-133Z-AA350-A-32-81-XX-01ZZZ-752Z-AA350-A-42-11-XX-01ZZZ-752Z-AA350-A-45-46-XX-00ZZZ-752Z-AA350-A-46-12-01-05ZZZ-752Z-A
Procedure(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.(b) Do the Control and Display System (CDS) stop procedure, refer to Ref. MP A350-
A-31-63-XX-00ZZZ-133Z-A.(c) Do the close-up procedure as specified in the uploading of software to
equipment, refer to Ref. MP A350-A-45-46-XX-00ZZZ-752Z-A (Uploading ofsoftware to equipment).
(d) Do the Close-up procedure as specified in the uploading of the MSL filesoftware component(s) to the ASFC ( FIN 1TC), refer to Ref. MP A350-A-46-12-01-05ZZZ-752Z-A.
(e) Do the Close-up procedure as specified in the uploading of the software to theCPIOM-H6 ( FIN 8TF61, FIN 8TF62, FIN 8TF63 and FIN 8TF64), refer to Ref. MPA350-A-42-11-XX-01ZZZ-752Z-A.
(f) Do the Close-Up procedure as specified in the Uploading of Software tothe Remote Braking Control Unit (RBCU), refer to Ref. MP A350-A-32-81-XX-01ZZZ-752Z-A.
(g) Put the aircraft back to its initial configuration.G. ADMINISTRATIVE
(1) Task A350-A-32-XX-P037-03001-90AA-A - Administrative
Procedure
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Write in the applicable aircraft records that you have done all the work given in thisService Bulletin.
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APPENDIX
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APPENDIXA. REPORTING SHEET
TITLE: LANDING GEAR - LANDING GEAR MANAGEMENT SYSTEM -INTRODUCE BCS SOFTWARE STANDARD S5B, WSCS SOFTWARESTANDARD S5B AND LGERS SOFTWARE S5A
MODIFICATION No.: 111399L43339 113846L48153 114420L04027 114420L04028114434L48204 115009L48441
(1) SB Reporting statusThis Service Bulletin will only be incorporated into affected customized Maintenanceand Flight Operations Products if it is duly reported to Airbus.
(2) GENERAL informationThe SB Reporting policy is published in ISI 00.00.00135. This document providesinformation regarding: the SB Reporting means and benefits, the update ofcustomized Maintenance Products and customized Flight Operations Products.If this Service Bulletin has an operational impact, refer to paragraph "Flight OperationsProducts" for further information on the update of affected Flight Operations Products.
(3) SB Reporting procedureStandard practice to report SB is to use the online reporting application onAirbusWorld.Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus, Question 2 "What arethe standard practices for SB Reporting?"
- If this SB requires previous or simultaneous accomplishment of other SBs,Question 3 "What about the reporting of prerequisite Service Bulletins?"
NOTE: ISI 00.00.00179 covers all the frequently asked questions about SB Reporting.It is revised on a regular basis.
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APPENDIX
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B. QUALITY PERCEPTION FORMUse this form to tell us what is your perception of the quality of this Service Bulletin.The reported data that you provide us will be used to analyse areas of difficulties and totake corrective action to further improve the quality of our Service Bulletin.We thank you for the time you have taken in completing this form.
Quality rating of this SB 4 3 2 1Quality rating of the Accomplishment Instructions 4 3 2 1Quality rating of the Illustrations 4 3 2 1Is this SB easy to understand ? Y / N
NOTE: Please rate on a scale of 1 to 4, with 4 being the highest score
If you have difficulties in the accomplishment of this SB please quote below the area(s) andgive a short description of the issue.
Planning Material InstructionsX Applicability X Tooling X PreparationX Reason X List of Materials
Operator SuppliedX Mod/Inspection
X Manpower X Kit content X TestX References X Re-identification X Close-upX Publication X IllustrationsX Industry Support
Comments :
Operator : Date :Name/TitlePlease return this form to :AIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFRANCEOr via your Resident Customer Support Office.