# Airbus Service Bulletin A350-25-P182

Copy: No revision named ("SB_25-P182_r00"), 29 pages: PDF https://openairdocs.org/files/sha256/f0/96/f0969a3eb90d52cb3ac942e007bb3cf9bf2edac4920b74534d5fa60fb839feb1; text https://openairdocs.org/service-documents/airbus/a350-25-p182/file/f0969a3eb90d.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2022-0686, the docket of AD 2022-17-07. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A350-25-P182
- Page: https://openairdocs.org/service-documents/airbus/a350-25-p182

## Text (29 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2022-0686, the docket of AD 2022-17-07. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
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: 25
TITLE: EQUIPMENT/FURNISHINGS - EMERGENCY - MODIFY IFAR ON SINGLE
LANE SLIDE-RAFTS ON DOOR 3 RH FOR -900
MODIFICATION No.:
CONF 001
116436L39345
CONF 002
116357L39340

### Page 2

A350
SERVICE BULLETIN
SUMMARY
REV 00 Jul 22/21 A350-25-P182
Page 2
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - EMERGENCY - MODIFY IFAR ON SINGLE
LANE SLIDE-RAFTS ON DOOR 3 RH FOR -900
CONF ALL
SUMMARY
This summary is for information only and is not approved for modification of the aircraft.
A. MODIFICATIONS
CONF 001
MODIFICATION CLASSIFICATION
MAJOR 116436L39345
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.
CONF 002
MODIFICATION CLASSIFICATION
MAJOR 116357L39340
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.
CONF ALL
B. REASON
(1) History
Inflatable Free Aisle Restrictor (IFAR) was introduced on A350–900 single lane slide/
rafts to address concerns of a dual lane flow of evacuees coming through a type A
door (de-rated to type C) and entering a single lane slide inflatable.
A potential unsafe condition has been identified at door 3 single lane slide, the IFAR
showed inconsistent release behavior in aft wind conditions, in some cases rendering
the slide unusable for evacuation.
(2) Objective/Action
This Service Bulletin is published to advise all operators of A350 aircraft of the issue of
AIR CRUISERS COMPANY Service Bulletin No. 006–25–08 which upgrades the slide/raft
IFAR on door 3 Right Hand (RH).
(3) Advantages
The accomplishment of this Service Bulletin will restrain the IFAR to avoid that
potential interference and/or entanglement of the upper part of the IFAR with slide/raft
cover/door structure in aft wind conditions. It will maintain the slide/raft reliability.
(4) Operational/Maintenance Consequences
None

### Page 3

A350
SERVICE BULLETIN
SUMMARY
REV 00 Jul 22/21 A350-25-P182
Page 3
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
CONF 001
No specific aircraft maintenance configuration required.
CONF 002
No specific aircraft maintenance configuration required.
CONF ALL
E. MATERIAL PRICE INFORMATION
CONF 001
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AA-A Option 1: Modification of the Packed
Slide/Raft in accordance with VSB
No material
(b) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Equipment See SB See Note Raft
NOTE: Price information to be obtained from the given supplier.
CONF 002
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Equipment See SB See Note Raft
NOTE: Price information to be obtained from the given supplier.

### Page 4

A350
SERVICE BULLETIN
SUMMARY
REV 00 Jul 22/21 A350-25-P182
Page 4
CONF ALL
F. APPLICABILITY
This Service Bulletin is applicable to this (these) operator(s):
CES CPA MAS QTR SAS SIA
G. CONCURRENT REQUIREMENTS
CONF 001
None
CONF 002
Accomplishment of this Service Bulletin requires the simultaneous accomplishment of this
Service Bulletin:
Service Bulletin(s) Modification(s)
Ref. SB A350-25-P181 116357L39340
NOTE: Service Bulletin No. A350–25–P181 (EQUIPMENT/FURNISHINGS - EMERGENCY —
MODIFY IFAR ON SINGLE LANE SLIDE-RAFTS ON DOOR 3 LH FOR -900) CONF 002.
CONF ALL
H. NATURE OF THE WORK
CONF 001
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AA-A Option 1: Modification of the Packed
Slide/Raft in accordance with VSB
AIRCRAFT NO
EQUIPMENT YES
(b) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
AIRCRAFT NO
EQUIPMENT YES
CONF 002
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
AIRCRAFT NO
EQUIPMENT YES
CONF ALL
I. MANPOWER
CONF 001
(1) Modification of the Packed Slide/Raft

### Page 5

A350
SERVICE BULLETIN
SUMMARY
REV 00 Jul 22/21 A350-25-P182
Page 5
(a) T ask set A350-A-25-XX-P182-01000-93AA-A Option 1: Modification of the Packed
Slide/Raft in accordance with VSB
MANPOWER
TOTAL MAN-HOURS 9.25 h
ELAPSED TIME (HOURS) 3.25 h
Additional man-hours related to Vendor SB; refer to:
Modify the Packed Slide/Raft in
accordance with VSB
Ref. AIR CRUISERS COMPANY
(70167) VSB 006-25-08
BENCH
(b) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
MANPOWER
TOTAL MAN-HOURS 9.25 h
ELAPSED TIME (HOURS) 3.25 h
CONF 002
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
MANPOWER
TOTAL MAN-HOURS 9.25 h
ELAPSED TIME (HOURS) 3.25 h

### Page 6

A350
SERVICE BULLETIN
SUMMARY
Figure ICN-A350-A-25XXP182-A-FAPE3-05XMD-A-001-01 Fig.SA Sol.AA SHEET 1/1
REV 00 Jul 22/21 A350-25-P182General Overview
Page 6
CONF ALL
J. GENERAL OVERVIEW
CONF ALL
A
PAX DOOR 3
Z843
A
REPLACE PACKED SLIDE/RAFT 7915MX
ICN-A350-A-25XXP182-A-FAPE3-05XMD-A-001-01

### Page 7

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 7
ATA SYSTEM: 25
TITLE: EQUIPMENT/FURNISHINGS - EMERGENCY - MODIFY IFAR ON SINGLE
LANE SLIDE-RAFTS ON DOOR 3 RH FOR -900
1. PLANNING INFORMATION
A. APPLICABILITY
NOTE: Modification No. 116358L39341 is applicable by Service Bulletin only.
NOTE: This Service Bulletin is only applicable to aircraft on which MOD No. 100881L39024
(E/F - CABIN ESCAPE FACILITIES - DEF/INST SINGLE LANE SLIDE-RAFT ON DOOR 3
LH/RH - CHANGE SLIDE FROM DUAL- TO SINGLE LANE) or MOD No. 109222L39126
(EQUIPMENT/FURNISHINGS - CABIN ESCAPE FACILITIES - INSTALL MODIFIED SINGLE
LANE SLIDE-RAFT ON DOOR 3 LH/RH) is embodied.
NOTE: Modification No. 116357L39340 is embodied before delivery on aircraft with
Manufacturer Serial Number (MSN) 0393, 0460, 0470, 0472, 0485, 0489, 0494,
0505, 0540, 0561, 0564, 0569, 0573, 0577, 0591, 0593, 0599, 0609 and 0613.
(1) Models
ON A/C 0006-0013, 0021, 0025, 0026, 0029-0034, 0036-0039, 0041, 0042, 0046, 0047, 0053,
0054, 0058, 0061-0063, 0068-0070, 0072, 0075-0078, 0081, 0083-0085, 0090, 0093, 0096,
0099-0101, 0106, 0107, 0109, 0114, 0116, 0119, 0122, 0126, 0128, 0132, 0133, 0137, 0140,
0143, 0148, 0154, 0155, 0158, 0159, 0163, 0165, 0170, 0172, 0183, 0186, 0195, 0203,
0207, 0211, 0213, 0214, 0216, 0220, 0223, 0230, 0232, 0237, 0238, 0244, 0248, 0249,
0254, 0257, 0261, 0263, 0269, 0272, 0276, 0278, 0291, 0294, 0305, 0307, 0309, 0316,
0322, 0324, 0328, 0329, 0337, 0341, 0344, 0348, 0358, 0364, 0369, 0371, 0373, 0378,
0379, 0385, 0391, 0394, 0396, 0401, 0408, 0413, 0418, 0423, 0436, 0439, 0445, 0447,
0452, 0464, 0469, 0475, 0484, 0499
350-941
CONF ALL
(2) Applicability by MSN
0006-0013 0021 0025 0026 0029-0034 0036-0039 0041 0042 0046 0047 0053 0054
0058 0061-0063 0068-0070 0072 0075-0078 0081 0083-0085 0090 0093 0096 0099-
0101 0106 0107 0109 0114 0116 0119 0122 0126 0128 0132 0133 0137 0140 0143
0148 0154 0155 0158 0159 0163 0165 0170 0172 0183 0186 0195 0203 0207 0211
0213 0214 0216 0220 0223 0230 0232 0237 0238 0244 0248 0249 0254 0257 0261
0263 0269 0272 0276 0278 0291 0294 0305 0307 0309 0316 0322 0324 0328 0329
0337 0341 0344 0348 0358 0364 0369 0371 0373 0378 0379 0385 0391 0394 0396
0401 0408 0413 0418 0423 0436 0439 0445 0447 0452 0464 0469 0475 0484 0499
(3) MSN by configuration
CONF 001
MSN CONFIGURATION
0006 0007 0008 0009 0010 0011 0012 0013 0021 0025 0026
0029 0030 0031 0032 0033 0034 0036 0037 0038 0039 0041
0042 0046 0047 0053 0054 0058 0061 0062 0063 0068 0069
0070 0072 0075 0076 0077 0078 0081 0083 0084 0085 0090
0093 0096 0099 0100 0101 0106 0107 0109 0114 0116 0119
0122 0126 0128 0132 0133 0137 0140 0143 0148 0154 0155
0158 0159 0163 0165 0170 0172 0183 0186 0195 0203 0207
0211 0213 0214 0216 0220 0223 0230 0232 0237 0238 0244
001

### Page 8

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 8
MSN CONFIGURATION
0248 0249 0254 0257 0261 0263 0269 0272 0276 0278 0291
0294 0305 0307 0309 0316 0322 0324 0328 0329 0337 0341
0344 0348 0358 0364 0369 0371 0373 0378 0379 0385 0391
0394 0396 0401 0408 0413 0418 0423 0436 0439 0445 0447
0452 0464 0469 0475 0484 0499
CONF 002
MSN CONFIGURATION
0006 0007 0008 0009 0010 0011 0012 0013 0021 0025 0026
0029 0030 0031 0032 0033 0034 0036 0037 0038 0039 0041
0042 0046 0047 0053 0054 0058 0061 0062 0063 0068 0069
0070 0072 0075 0076 0077 0078 0081 0083 0084 0085 0090
0093 0096 0099 0100 0101 0106 0107 0109 0114 0116 0119
0122 0126 0128 0132 0133 0137 0140 0143 0148 0154 0155
0158 0159 0163 0165 0170 0172 0183 0186 0195 0203 0207
0211 0213 0214 0216 0220 0223 0230 0232 0237 0238 0244
0248 0249 0254 0257 0261 0263 0269 0272 0276 0278 0291
0294 0305 0307 0309 0316 0322 0324 0328 0329 0337 0341
0344 0348 0358 0364 0369 0371 0373 0378 0379 0385 0391
0394 0396 0401 0408 0413 0418 0423 0436 0439 0445 0447
0452 0464 0469 0475 0484 0499
002
CONF ALL
(4) Configuration definition
CONF 001
Configuration 001
CONF 001 is applicable to aircraft on which Part Number (PN) 67963-106 will be
installed.
CONF 001 retrofits following modifications: 116436L39345.
CONF 002
Configuration 002
CONF 002 is applicable to aircraft on which PN 67963-108 will be installed.
CONF 002 retrofits following modifications: 116357L39340.
CONF ALL
B. CONCURRENT REQUIREMENTS
CONF 001
None
CONF 002
Accomplishment of this Service Bulletin requires the simultaneous accomplishment of this
Service Bulletin:
Service Bulletin(s) Modification(s)
Ref. SB A350-25-P181 116357L39340
NOTE: Service Bulletin No. A350–25–P181 (EQUIPMENT/FURNISHINGS - EMERGENCY —
MODIFY IFAR ON SINGLE LANE SLIDE-RAFTS ON DOOR 3 LH FOR -900) CONF 002.

### Page 9

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 9
CONF ALL
C. REASON
(1) History
Inflatable Free Aisle Restrictor (IFAR) was introduced on A350–900 single lane slide/
rafts to address concerns of a dual lane flow of evacuees coming through a type A
door (de-rated to type C) and entering a single lane slide inflatable.
A potential unsafe condition has been identified at door 3 single lane slide, the IFAR
showed inconsistent release behavior in aft wind conditions, in some cases rendering
the slide unusable for evacuation.
(2) Objective/Action
This Service Bulletin is published to advise all operators of A350 aircraft of the issue of
AIR CRUISERS COMPANY Service Bulletin No. 006–25–08 which upgrades the slide/raft
IFAR on door 3 Right Hand (RH).
(3) Advantages
The accomplishment of this Service Bulletin will restrain the IFAR to avoid that
potential interference and/or entanglement of the upper part of the IFAR with slide/raft
cover/door structure in aft wind conditions. It will maintain the slide/raft reliability.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
NOTE: T o accomplish this Service Bulletin, you have two options.
T o accomplish this Service Bulletin it is necessary to:
(1) Modification of the Packed Slide/Raft
CONF 001
(a) T ask set A350-A-25-XX-P182-01000-93AA-A Option 1: Modification of the Packed
Slide/Raft in accordance with VSB
1 Remove and Retain the Packed Slide/Raft
2 Modify the Packed Slide/Raft in accordance with VSB
3 Install the Modified Packed Slide/Raft
CONF ALL
(b) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
CONF 001
1 Replace the Packed Slide/Raft
CONF 002
1 Replace the Packed Slide/Raft
CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.

### Page 10

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 10
(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. The accomplishment timescale,
which has not yet been defined, will be given in the AD.
NOTE: Only one option is required for the AD compliance.
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
CONF 001
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.
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AA-A Option 1: Modification of the Packed
Slide/Raft in accordance with VSB
PREPARATION
Job Set-up 0.50 h
PROCEDURE
Remove and Retain the Packed Slide/Raft 4.00 h
Install the Modified Packed Slide/Raft 4.00 h
PREPARATION FOR TEST
None
TEST
T est 0.25 h
CLOSE-UP
Close-up 0.50 h
TOTAL MAN-HOURS 9.25 h
ELAPSED TIME (HOURS) 3.25 h
Additional man-hours related to Vendor SB; refer to:
Modify the Packed Slide/Raft in
accordance with VSB
Ref. AIR CRUISERS COMPANY
(70167) VSB 006-25-08
BENCH
(b) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
PREPARATION
Job Set-up 0.50 h
PROCEDURE

### Page 11

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 11
Replace the Packed Slide/Raft 8.00 h
PREPARATION FOR TEST
None
TEST
T est 0.25 h
CLOSE-UP
Close-up 0.50 h
TOTAL MAN-HOURS 9.25 h
ELAPSED TIME (HOURS) 3.25 h
CONF 002
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.
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
PREPARATION
Job Set-up 0.50 h
PROCEDURE
Replace the Packed Slide/Raft 8.00 h
PREPARATION FOR TEST
None
TEST
T est 0.25 h
CLOSE-UP
Close-up 0.50 h
TOTAL MAN-HOURS 9.25 h
ELAPSED TIME (HOURS) 3.25 h
CONF ALL
H. WEIGHT AND BALANCE
Not changed
I. ELECTRICAL LOAD DATA
Not changed
J. REFERENCES
CONF 002
CONCURRENT SERVICE BULLETIN (SB)
A350-25-P181
CONF 001

### Page 12

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 12
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AA-A Option 1: Modification of the Packed
Slide/Raft in accordance with VSB
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-25-62-47-00ZZZ-520Z-A
A350-A-25-62-47-00ZZZ-720Z-A
SYSTEM DESCRIPTION (SD)
A350-A-06-3X-XX-01ZZZ-04CZ-A
VENDOR SERVICE BULLETIN (VSB)
AIR CRUISERS COMPANY (70167) VSB 006-25-08
(b) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
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-25-62-47-00ZZZ-520Z-A
A350-A-25-62-47-00ZZZ-720Z-A
SYSTEM DESCRIPTION (SD)
A350-A-06-3X-XX-01ZZZ-04CZ-A
CONF 002
(1) Modification of the Packed Slide/Raft
(a) T ask set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of the Packed
Slide/Raft as per MP
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-25-62-47-00ZZZ-520Z-A
A350-A-25-62-47-00ZZZ-720Z-A

### Page 13

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 13
SYSTEM DESCRIPTION (SD)
A350-A-06-3X-XX-01ZZZ-04CZ-A
CONF ALL
K. PUBLICATION AFFECTED
MAINTENANCE ILLUSTRATED PART DATA (MIPD)
L. INDUSTRY SUPPORT INFORMATION
AIRBUS will credit the man-hours indicated in this Service Bulletin at the agreed in-house
warranty labor rate for claims received no later than 90 days after completion of the last
affected aircraft of your fleet, for the accomplishment of this Service Bulletin within 36
months after the initial issue date of the Service Bulletin.
Industry support terms for the equipment must be negotiated with the equipment supplier.
Modification of removed equipment should be negotiated directly with the Vendor as per
instructions given in Vendor Service Bulletin No. 006–25–08.
Refer to Vendor Service Bulletin No. 006–25–08 for the industry support terms of the Vendor
Service Bulletin parts and labor.
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 retrofit
management department: monitored.retrofit@airbus.com.

### Page 14

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 14
2. MATERIAL INFORMATION
A. MATERIAL APPLICABILITY
CONF 001
Material for task set A350-A-25-XX-P182-01000-93AA-A Option 1: Modification of
the Packed Slide/Raft in accordance with VSB
MATERIAL QTY SEE NOTES
Referenced tools See SB
Re-identified parts See SB
Interchangeable parts See SB
Material for task set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of
the Packed Slide/Raft as per MP
MATERIAL QTY SEE NOTES
Referenced tools See SB
Equipment See SB
Interchangeable parts See SB
Spare parts See SB
CONF 002
Material for task set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement of
the Packed Slide/Raft as per MP
MATERIAL QTY SEE NOTES
Referenced tools See SB
Equipment See SB
Interchangeable parts See SB
Spare parts See SB
CONF ALL
B. TOOLING
CONF 001
Referenced tools for task set A350-A-25-XX-P182-01000-93AA-A Option 1:
Modification of the Packed Slide/Raft in accordance with VSB
T o accomplish this Service Bulletin it is necessary to use the tools listed in:
Ref. MP A350-A-25-62-47-00ZZZ-520Z-A
Ref. MP A350-A-25-62-47-00ZZZ-720Z-A
Ref. AIR CRUISERS COMPANY (70167) VSB 006-25-08
Referenced tools for task set A350-A-25-XX-P182-01000-93AB-A Option 2:
Replacement of the Packed Slide/Raft as per MP
T o accomplish this Service Bulletin it is necessary to use the tools listed in:
Ref. MP A350-A-25-62-47-00ZZZ-520Z-A
Ref. MP A350-A-25-62-47-00ZZZ-720Z-A
CONF 002
Referenced tools for task set A350-A-25-XX-P182-01000-93AB-A Option 2:
Replacement of the Packed Slide/Raft as per MP

### Page 15

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 15
T o accomplish this Service Bulletin it is necessary to use the tools listed in:
Ref. MP A350-A-25-62-47-00ZZZ-520Z-A
Ref. MP A350-A-25-62-47-00ZZZ-720Z-A
CONF ALL
C. CONSUMABLES
No consumables
D. LIST OF NEW PARTS
CONF 001
Equipment for task set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement
of the Packed Slide/Raft as per MP
Procurement address 70167
AIR CRUISERS COMPANY
1747 State Route 34
07727-3935 WALL TOWNSHIP
UNITED STATES
Phone: +1 732–681–3527
E-mail: T echPubs@SafranGroup.com
NOTE(S)
Vendor parts are to be procured from the address given above.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
67963-106 (70167) 1 RAFT (1) (2) (3)
NOTE(S)
(1): Procurement terms for the equipment must be negotiated with the equipment
supplier.
(2): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
(3): After applying this modification, PN 67963–108 can replace PN 67963–106 and PN
67963–106 can replace PN 67963–108.
CONF 002
Equipment for task set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement
of the Packed Slide/Raft as per MP
Procurement address 70167
AIR CRUISERS COMPANY
1747 State Route 34
07727-3935 WALL TOWNSHIP
UNITED STATES
Phone: +1 732–681–3527
E-mail: T echPubs@SafranGroup.com
NOTE(S)
Vendor parts are to be procured from the address given above.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
67963-108 (70167) 1 RAFT (1) (2) (3)
NOTE(S)
(1): Procurement terms for the equipment must be negotiated with the equipment
supplier.
(2): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.

### Page 16

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REV 00 Jul 22/21 A350-25-P182
Page 16
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
(3): After applying this modification, PN 67963–108 can replace PN 67963–106 and PN
67963–106 can replace PN 67963–108.
CONF ALL
E. LIST OF EXISTING PARTS
CONF 001
Re-identified parts for task set A350-A-25-XX-P182-01000-93AA-A Option 1:
Modification of the Packed Slide/Raft in accordance with VSB
ITEM NEW PART No. KEYWORD ITEM OLD PART No. SEE NOTES
67963-106 RAFT 67963-102 (1) (2) (3)
67963-106 RAFT 67963-104 (1) (2) (3)
NOTE(S)
(1): Refer to the AIR CRUISERS COMPANY Vendor Service Bulletin No. 006–25–08 for the
equipment modification sales terms.
(2): Parts are re-identified in accordance with Vendor Service Bulletin No. 006–25–08.
(3): After applying this modification, PN 67963–108 can replace PN 67963–106 and PN
67963–106 can replace PN 67963–108.
Interchangeable parts for task set A350-A-25-XX-P182-01000-93AA-A Option 1:
Modification of the Packed Slide/Raft in accordance with VSB
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTES
RAFT-ESCAPE
SLIDE,DOOR 3 RH 67963-102 67963-106 01 (1)
RAFT-ESCAPE
SLIDE,DOOR 3 RH 67963-104 67963-106 01 (1)
NOTE(S)
For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter
2).
(1): The interchangeability possibilities are for new or modified parts introduced by the
accomplishment of this Service Bulletin.
Interchangeable parts for task set A350-A-25-XX-P182-01000-93AB-A Option 2:
Replacement of the Packed Slide/Raft as per MP
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTES
RAFT-ESCAPE
SLIDE,DOOR 3 RH 67963-102 67963-106 01 (1)
RAFT-ESCAPE
SLIDE,DOOR 3 RH 67963-104 67963-106 01 (1)
NOTE(S)
For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter
2).
(1): The interchangeability possibilities are for new or modified parts introduced by the
accomplishment of this Service Bulletin.
CONF 002
Interchangeable parts for task set A350-A-25-XX-P182-01000-93AB-A Option 2:
Replacement of the Packed Slide/Raft as per MP

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Page 17
DESCRIPTION OLD PART No. NEW PART No. INT SEE NOTES
RAFT-ESCAPE
SLIDE,DOOR 3 RH 67963-104 67963-108 01 (1)
NOTE(S)
For definitions of interchangeability codes in column INT. refer to ATA (CSDD Chapter
2).
(1): The interchangeability possibilities are for new or modified parts introduced by the
accomplishment of this Service Bulletin.
CONF 001
Spare parts for task set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement
of the Packed Slide/Raft as per MP
DESCRIPTION OLD PART No. SEE NOTES
RAFT-ESCAPE SLIDE,DOOR 3 RH 67963-102 (1)
RAFT-ESCAPE SLIDE,DOOR 3 RH 67963-104 (1)
NOTE(S)
(1): The parts listed here must not be installed anymore on aircraft which have
accomplished this Service Bulletin or which have the equivalent production
modification embodied.
CONF 002
Spare parts for task set A350-A-25-XX-P182-01000-93AB-A Option 2: Replacement
of the Packed Slide/Raft as per MP
DESCRIPTION OLD PART No. SEE NOTES
RAFT-ESCAPE SLIDE,DOOR 3 RH 67963-104 (1)
NOTE(S)
(1): The parts listed here must not be installed anymore on aircraft which have
accomplished this Service Bulletin or which have the equivalent production
modification embodied.

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Page 18
CONF ALL
3. ACCOMPLISHMENT INSTRUCTIONS
CONF 001
Task set A350-A-25-XX-P182-01000-93AA-A (A350-A-25-XX-P182-01ZZZ-93AZ-A)
Option 1: Modification of the Packed Slide/Raft in accordance with VSB
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 Ref. ESP A350-A-20-55-XX-01ZZZ-
042Z-A.
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 9.25 h
ELAPSED TIME (HOURS) 3.25 h

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A350
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REV 00 Jul 22/21 A350-25-P182
Page 19
Additional man-hours related to Vendor SB; refer to:
AIR CRUISERS COMPANY (70167) VSB 006-25-08
B. PREPARATION
(1) Task A350-A-25-XX-P182-01001-540A-A (A350-A-25-XX-P182-01ZZZ-540Z-A)
Job Set-up
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
INTRO A350-A-00-61-04-11ZZZ-018Z-D
MP A350-A-24-41-XX-00ZZZ-170Z-AA350-A-25-62-47-00ZZZ-520Z-A
SD A350-A-06-3X-XX-01ZZZ-04CZ-A
Procedure
NOTE: For the basic Aircraft configuration, refer to Ref. INTRO A350-A-00-61-04-
11ZZZ-018Z-D “Maintenance Procedure - Introduction”.
(a) Standard practice given in this procedure:
1 For identification of zones, refer to Ref. SD A350-A-06-3X-XX-01ZZZ-04CZ-A.
(b) Make sure that the aircraft is electrically grounded, refer to Ref. MP A350-A-24-
41-XX-00ZZZ-170Z-A.
(c) Put an access platform in position at Zone 843.
(d) Do the job set-up procedure as specified in the removal of the packed slide/raft
(FIN 7915MX), refer to Ref. MP A350-A-25-62-47-00ZZZ-520Z-A.
C. PROCEDURE
(1) Task A350-A-25-XX-P182-01001-520A-A (A350-A-25-XX-P182-01ZZZ-520Z-A)
Remove and Retain the Packed Slide/Raft
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
843
Manpower/Resources/Skills
Man-hours 4.00 h
Minimum Number of person 4
Elapsed Time 1.00 h
Skills Airframe

### Page 20

A350
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Page 20
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-520Z-A
SD A350-A-06-3X-XX-01ZZZ-04CZ-A
Procedure
(a) Standard practices given in this procedure:
1 For identification of zones, refer to Ref. SD A350-A-06-3X-XX-01ZZZ-04CZ-A.
2 T ag all the parts you must remove and retain to make the subsequent
installation easier.
(b) Remove the packed slide/raft (FIN 7915MX), refer to Ref. MP A350-A-25-62-47-
00ZZZ-520Z-A.
NOTE: Retained for modification.
(2) Task A350-A-25-XX-P182-01001-920A-C (A350-A-25-XX-P182-01ZZZ-920Z-C)
Modify the Packed Slide/Raft in accordance with VSB
Job Set-Up Information
Material necessary to do the job
Re-identified Part Set
ITEM NEW PART No. KEYWORD ITEM OLD PART No. SEE NOTES
67963-106 RAFT 67963-102 (1) (2)
67963-106 RAFT 67963-104 (1) (2)
NOTE(S)
(1): Parts are re-identified in accordance with Vendor Service Bulletin No. 006–25–08.
(2): After applying this modification, PN 67963–108 can replace PN 67963–106 and PN
67963–106 can replace PN 67963–108.
Referenced Information
Manuals/Drawings References/Sheets
VSB AIR CRUISERS COMPANY (70167) VSB 006-25-08
Procedure
(a) Modify the packed slide/raft (FIN 7915MX) in accordance with Ref. AIR CRUISERS
COMPANY (70167) VSB 006-25-08.
(b) After the modification:
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-102    
becomes
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-106  
OR
FIN 7915MX

### Page 21

A350
SERVICE BULLETIN
REV 00 Jul 22/21 A350-25-P182
Page 21
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-104    
becomes
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-106  
(3) Task A350-A-25-XX-P182-01001-720A-A (A350-A-25-XX-P182-01ZZZ-720Z-A)
Install the Modified Packed Slide/Raft
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
843
Manpower/Resources/Skills
Man-hours 4.00 h
Minimum Number of person 4
Elapsed Time 1.00 h
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-720Z-A
SD A350-A-06-3X-XX-01ZZZ-04CZ-A
Procedure
(a) Standard practice given in this procedure:
1 For identification of zones, refer to Ref. SD A350-A-06-3X-XX-01ZZZ-04CZ-A.
(b) Install the modified packed slide/raft (FIN 7915MX), refer to Ref. MP A350-A-25-
62-47-00ZZZ-720Z-A.
D. PREPARATION FOR TEST
None
E. TEST
(1) Task A350-A-25-XX-P182-01001-320A-A (A350-A-25-XX-P182-01ZZZ-320Z-A)
Test
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-720Z-A
Procedure

### Page 22

A350
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REV 00 Jul 22/21 A350-25-P182
Page 22
(a) Do the operational test as specified after the installation of the packed slide/raft
(FIN 7915MX), refer to Ref. MP A350-A-25-62-47-00ZZZ-720Z-A.
F. CLOSE-UP
(1) Task A350-A-25-XX-P182-01001-740A-A (A350-A-25-XX-P182-01ZZZ-740Z-A)
Close-up
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-720Z-A
Procedure
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up procedure as specified in the installation of the packed slide/raft
(FIN 7915MX), refer to Ref. MP A350-A-25-62-47-00ZZZ-720Z-A.
(c) Remove the access platform.
(d) Put the aircraft back to its initial configuration.
G. ADMINISTRATIVE
(1) Task A350-A-25-XX-P182-01001-90AA-A (A350-A-25-XX-P182-01ZZZ-90AZ-A)
Administrative
Procedure
Confirm in the applicable aircraft records that you have completed all the work defined
in this Service Bulletin task set as required.

### Page 23

A350
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Page 23
CONF ALL
Task set A350-A-25-XX-P182-01000-93AB-A (A350-A-25-XX-P182-01ZZZ-93AZ-A)
Option 2: Replacement of the Packed Slide/Raft as per MP
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 Ref. ESP A350-A-20-55-XX-01ZZZ-
042Z-A.
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.
NOTE: Discarded parts must be managed at the operator's discretion.
A. TASK SET ASSOCIATED INFORMATION
Task Manpower
CONF 001
TOTAL MAN-HOURS 9.25 h

### Page 24

A350
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Page 24
CONF 002
TOTAL MAN-HOURS 9.25 h
CONF 001
ELAPSED TIME (HOURS) 3.25 h
CONF 002
ELAPSED TIME (HOURS) 3.25 h
CONF ALL
B. PREPARATION
(1) Task A350-A-25-XX-P182-02001-540A-A (A350-A-25-XX-P182-02ZZZ-540Z-A)
Job Set-up
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
INTRO A350-A-00-61-04-11ZZZ-018Z-D
MP A350-A-24-41-XX-00ZZZ-170Z-AA350-A-25-62-47-00ZZZ-520Z-A
SD A350-A-06-3X-XX-01ZZZ-04CZ-A
Procedure
NOTE: For the basic Aircraft configuration, refer to Ref. INTRO A350-A-00-61-04-
11ZZZ-018Z-D “Maintenance Procedure - Introduction”.
(a) Standard practice given in this procedure:
1 For identification of zones, refer to Ref. SD A350-A-06-3X-XX-01ZZZ-04CZ-A.
(b) Make sure that the aircraft is electrically grounded, refer to Ref. MP A350-A-24-
41-XX-00ZZZ-170Z-A.
(c) Put an access platform in position at Zone 843.
(d) Do the job set-up procedure as specified in the removal of the packed slide/raft
(FIN 7915MX), refer to Ref. MP A350-A-25-62-47-00ZZZ-520Z-A.
C. PROCEDURE
CONF 001
(1) Task A350-A-25-XX-P182-02001-920A-A (A350-A-25-XX-P182-02ZZZ-920Z-A)
Replace the Packed Slide/Raft
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
843
Manpower/Resources/Skills
Man-hours 8.00 h
Minimum Number of person 4

### Page 25

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Page 25
Elapsed Time 2.00 h
Skills Airframe
Material necessary to do the job
Equipment
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
67963-106 1 RAFT (1)
NOTE(S)
(1): After applying this modification, PN 67963–108 can replace PN 67963–106 and PN
67963–106 can replace PN 67963–108.
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-520Z-AA350-A-25-62-47-00ZZZ-720Z-A
SD A350-A-06-3X-XX-01ZZZ-04CZ-A
Procedure
(a) Standard practice given in this procedure:
1 For identification of zones, refer to Ref. SD A350-A-06-3X-XX-01ZZZ-04CZ-A.
(b) Remove the packed slide/raft (FIN 7915MX), refer to Ref. MP A350-A-25-62-47-
00ZZZ-520Z-A.
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-102   Discard
OR
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-104   Discard
(c) Install the packed slide/raft (FIN 7915MX), refer to Ref. MP A350-A-25-62-47-
00ZZZ-720Z-A.
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-106  
CONF 002
(1) Task A350-A-25-XX-P182-02002-920A-A (A350-A-25-XX-P182-02ZZZ-920Z-A)
Replace the Packed Slide/Raft
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
843
Manpower/Resources/Skills
Man-hours 8.00 h
Minimum Number of person 4
Elapsed Time 2.00 h

### Page 26

A350
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REV 00 Jul 22/21 A350-25-P182
Page 26
Skills Airframe
Material necessary to do the job
Equipment
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
67963-108 1 RAFT (1)
NOTE(S)
(1): After applying this modification, PN 67963–108 can replace PN 67963–106 and PN
67963–106 can replace PN 67963–108.
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-520Z-AA350-A-25-62-47-00ZZZ-720Z-A
SD A350-A-06-3X-XX-01ZZZ-04CZ-A
Procedure
(a) Standard practice given in this procedure:
1 For identification of zones, refer to Ref. SD A350-A-06-3X-XX-01ZZZ-04CZ-A.
(b) Remove the packed slide/raft (FIN 7915MX), refer to Ref. MP A350-A-25-62-47-
00ZZZ-520Z-A.
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-104    
(c) Install the packed slide/raft (FIN 7915MX), refer to Ref. MP A350-A-25-62-47-
00ZZZ-720Z-A.
FIN 7915MX
1 RAFT-ESCAPE
SLIDE,DOOR 3 RH
67963-108  
CONF ALL
D. PREPARATION FOR TEST
None
E. TEST
(1) Task A350-A-25-XX-P182-02001-320A-A (A350-A-25-XX-P182-02ZZZ-320Z-A)
Test
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-720Z-A
Procedure

### Page 27

A350
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REV 00 Jul 22/21 A350-25-P182
Page 27
(a) Do the operational test as specified after the installation of the packed slide/raft
(FIN 7915MX), refer to Ref. MP A350-A-25-62-47-00ZZZ-720Z-A.
F. CLOSE-UP
(1) Task A350-A-25-XX-P182-02001-740A-A (A350-A-25-XX-P182-02ZZZ-740Z-A)
Close-up
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Referenced Information
Manuals/Drawings References/Sheets
MP A350-A-25-62-47-00ZZZ-720Z-A
Procedure
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the close-up procedure as specified in the installation of the packed slide/raft
(FIN 7915MX), refer to Ref. MP A350-A-25-62-47-00ZZZ-720Z-A.
(c) Remove the access platform.
(d) Put the aircraft back to its initial configuration.
G. ADMINISTRATIVE
(1) Task A350-A-25-XX-P182-02001-90AA-A (A350-A-25-XX-P182-02ZZZ-90AZ-A)
Administrative
Procedure
Confirm in the applicable aircraft records that you have completed all the work defined
in this Service Bulletin task set as required.

### Page 28

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APPENDIX
REV 00 Jul 22/21 A350-25-P182
Page 28
APPENDIX
A. REPORTING SHEET
TITLE: EQUIPMENT/FURNISHINGS - EMERGENCY - MODIFY IFAR ON SINGLE
LANE SLIDE-RAFTS ON DOOR 3 RH FOR -900
MODIFICATION No.: 116357L39340 116436L39345
(1) SB Reporting status
This Service Bulletin will only be incorporated into affected customized Maintenance
and Flight Operations Products if it is duly reported to Airbus.
(2) GENERAL information
The SB Reporting policy is published in ISI 00.00.00135. This document provides
information regarding: the SB Reporting means and benefits, the update of
customized Maintenance Products and customized Flight Operations Products.
If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations
Products" for further information on the update of affected Flight Operations Products.
(3) SB Reporting procedure
Standard practice to report SB is to use the online reporting application on
AirbusWorld.
Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus, Question 2 "What are
the 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.

### Page 29

A350
SERVICE BULLETIN
APPENDIX
REV 00 Jul 22/21 A350-25-P182
Page 29
B. QUALITY PERCEPTION FORM
Use 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 to
take 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 1
Quality rating of the Accomplishment Instructions 4 3 2 1
Quality rating of the Illustrations 4 3 2 1
Is 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) and
give a short description of the issue.
Planning Material Instructions
X Applicability X T ooling X Preparation
X Reason X List of Materials
Operator Supplied
X Mod/Inspection
X Manpower X Kit content X T est
X References X Re-identification X Close-up
X Publication X Illustrations
X Industry Support
Comments :
Operator : Date :
Name/Title
Please return this form to :
AIRBUS
2, ROND POINT EMILE DEWOITINE
31700 BLAGNAC
FRANCE
Or via your Resident Customer Support Office.

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