@AIRBUS

AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
31707 Blagnac Cedex
FRANCE

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PART LIST

ARM ASSY - GUIDE

PN : A5217213300200
A5217213300400
A5217213300600
A5217213300800

Issue: Jul 01/87 52-12-12 Rev: Jul 01/09

 @AIRBUS
COMPONENT MAINTENANCE MANUAL
A5217213300200

HIGHLIGHTS

Revision No. 7 - Jul 01/09

LOCATIONS CHG DESCRIPTIONS OF CHANGE

CODE
REPAIR
TASK 52-12-12-370-801-A01 R CONSUMABLE MATERIAL DATA
UPDATED

HIGHLIGHTS
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LIST OF EFFECTIVE CONTENT

Revision No. 7 - Jul 01/09

CONTENT CHG LAST REVISION

CODE DATE
INTRODUCTION
TASK 52-12-12-871-801-A01 Mar 01/09

DESCRIPTION AND OPERATION

TASK 52-12-12-870-802-A01 Mar 01/09

INSPECTION/CHECK
TASK 52-12-12-210-801-A01 Mar 01/09
Subtask 52-12-12-210-001-A01 Mar 01/09
Subtask 52-12-12-210-002-A01 Mar 01/09
FIGURE 52-12-12-991-001-A01 Mar 01/09

REPAIR
TASK 52-12-12-370-801-A01 R Jul 01/09
Subtask 52-12-12-370-001-A01 Mar 01/09

SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

TASK 52-12-12-940-803-A01 Mar 01/09

ILLUSTRATED PARTS LIST

IPL Introduction
TASK 52-12-12-872-801-A01 Mar 01/09
VENDOR LIST Mar 01/09
Figure 02
FIGURE 52-12-12-991-802-001 Mar 01/09
Parts List Mar 01/09
Figure 03
FIGURE 52-12-12-991-803-001 Mar 01/09
Parts List Mar 01/09

L.E.C.
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LIST OF SERVICE BULLETINS

SB No REV No MOD No INCORP. TITLE

DATE
*** NO SB ***

SBL
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INTRODUCTION

**For PN’s ALL

TASK 52-12-12-871-801-A01
Introduction
1. General
A. This manual is written to the iSpec 2200 and in ASD Simplified Technical English (STE). The
international SI units of measurement are used in this manual, with imperial units shown in
parentheses.
B. The manual contains data about maintenance on the component in a workshop. It does not
contain data about maintenance on the component when it is installed in the aircraft.
C. Only approved persons with the necessary skills are permitted to do the maintenance procedures
in this manual.
D. Maintenance Task Oriented Support System (MTOSS) task and subtask identification is used in
this manual. The maintenance tasks and other data have special MTOSS numbers for Electronic
Data Processing (EDP). The user of the manual can ignore the MTOSS numbers.
E. This manual contains:
- Technical data for the component
- Maintenance and repair procedures about the component
- An Illustrated Parts List (IPL) with data for the component parts. Parts are identified in all
sections of the manual by the IPL-Figure and item number.
F. We verified the DISASSEMBLY, TESTING and ASSEMBLY procedures by simulation.
2. How to use the Manual
A. Make sure that the manual contains the information applicable to your component.
B. If you need to identify a part or find a part number, use the search function.
C. You must use the instructions in this manual for all the component maintenance. Read all the
applicable WARNINGS and CAUTIONS before you do the work on the component.
3. List of Abbreviations
ABP Airbus Process
AECMA European Association of Aerospace Industries
ANSI American National Standards Institute
ASD AeroSpace and Defence Industries Association of Europe
ATA Air Transport Association of America
ATE Automatic Test Requirements
BITE Built In Test Equipment
CDIM Component Data Information Manual

INTRO
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CML Consumable Materials List

EDP Electronic Data Processing
IEC International Electrical Commission
IPC Illustrated Parts Catalog
IPL Illustrated parts list
ISO International Standards Organization
LH Left Hand
LRU Line Replaceable Unit
MTOSS Maintenance Task Oriented Support System
NHA Next Higher Assembly
NI/ALPH Numeric Index/Alphabetical
NTM Nondestructive Testing Manual
PMS Process and Materials Specification
RH Right Hand
SAE Society of Automotive Engineers
SB Service Bulletin
SBL Service Bulletin List
SI Systéme International (French)
SPC Spare Part Classification
SRM Structural Repair Manual
STE Simplified Technical English
TBD To Be Determined
TID Tool Identifier
TOC Table of Contents
TPG-CMM Technical Publications Guide-CMM
List of Abbreviations
TABLE 1

INTRO
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COMPONENT MAINTENANCE MANUAL
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DESCRIPTION AND OPERATION

**For PN’s ALL

TASK 52-12-12-870-802-A01
General
1. The Guide Arm Assy serves as a guide during opening and closing of the MID and AFT
passenger/crew doors.
2. Technical Data (approx.):
Length: 700 mm (27.60 in.)
Width: 110 mm (4.30 in.)
Height: 30 mm (1.18 in.)
Weight: 0.590 kg (1.300 lb.)
Technical Data Table
TABLE 1

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INSPECTION/CHECK

**For PN’s ALL

TASK 52-12-12-210-801-A01
Check of the Guide Arm Assy
1. Reason for the Job
Self explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 52-12-12-370-801-A01 TASK 52-12-12-370-801-A01-Reworking
FIGURE 52-12-12-991-001-A FIGURE 52-12-12-991-001-A-Deformation of Guide Arm Assy
Referenced Information
TABLE 1

3. Procedure

Subtask 52-12-12-210-001-A01
A. Check guide arms for cracks.
(1) Cracks are not permitted.
(2) Replace the guide arm which has cracks.

Subtask 52-12-12-210-002-A01
B. Check the guide arm for deformation.
(1) Parts with more than 6 deg. deformation are not reworkable (Refer to FIGURE
52-12-12-991-001-A).
(2) For reworking of parts with Less than 6 deg. deformation refer to TASK 52-12-12-370-801-
A01.

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**For PN’s ALL

F_CM_521212_1_0010101_01_00

Deformation of Guide Arm Assy

FIGURE-52-12-12-991-001-A01

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REPAIR

**For PN’s ALL

TASK 52-12-12-370-801-A01
REWORKING
1. General
-
-

NOTE : Refer to TASK 52-12-12-940-803-A01 for Milling and Crimping Device.

2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
16-020 Wash Primer
16-001 Anti Corrosion Primer (Polyurethane)
16-002 Polyurethane Topcoat Grey (for Internal Applic.)
Consumable Materials
TABLE 1

B. Fixtures, Tools, Test and Support

REFERENCE DESIGNATION
98F52108009000 Milling and Crimping Device - Passenger/Crew Doors
Fixtures, Tools, Test and Support
TABLE 2

C. Referenced Information
REFERENCE DESIGNATION
TASK 52-12-12-940-803-A01 TASK 52-12-12-940-803-A01-Special Tools, Fixtures and
Equipment
PMS 01-05-27
Referenced Information
TABLE 3

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3. Procedure

Subtask 52-12-12-370-001-A01
A. Rework deformation of guide arm assy as follows:
(1) Remove paintwork from guide arm assy with a suitable tool.
(2) Remove self-aligning bearing from guide arm with Milling and Crimping Device-
Passenger/Crew Doors.
(3) Remove slide bearings with suitable tools.
(4) Check guide arm for cracks using an approved nondestructive test.

CAUTION : REWORK MUST BE CARRIED OUT USING HEAT TREATMENT FACILITIES

AND HEATABLE TOOLS.

CAUTION : COLD FORMING IS NOT ALLOWED FOR THE GUIDE ARM.

(5) Carry out reworking of guide arm using hot forming procedure in accordance with TABLE
4.
(6) After reworking carry out nondestructive test and make certain that no cracks exist.

NOTE : Before beginning the heat treatment, identify the material of the guide arm in
accordance with TABLE 4.
(7) Guide Arm Material Table
FIG ITEM NO. MATERIAL NO. TREATMENT TREATMENT
OF GUIDE ARM TEMPERATURE DURATION
2,3 50A, C 3.4364T7351 160 deg. C within 60
(320deg. F) minutes
2,3 50B 3.1354T351 160 deg. C within 45
(320deg. F) minutes
Guide Arm Material
TABLE 4

(8) If the guide arm is free from cracks, carry out conductivity test (NTM, 51-30-00, Part 1).
(9) Install slide bearings in accordance with PMS 01-05-27.
(10) Install slide-aligning bearing with 98F52108009000 Milling and Crimping Device -
Passenger/Crew Doors (Refer to TASK 52-12-12-940-803-A01.
(11) Renew Paintwork

WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-020 WASH PRIMER.
OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS.
(a) Apply 16-020 Wash Primer and allow to dry.

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WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-001 ANTI

CORROSION PRIMER (POLYURETHANE). OBEY THE MATERIAL
MANUFACTURER’S INSTRUCTIONS.
(b) Apply 16-001 Anti Corrosion Primer (Polyurethane) and allow to dry.

WARNING : BE CAREFUL WHEN YOU USE MATERIAL NO. 16-002 POLYURETHANE

TOPCOAT GREY (FOR INTERNAL APPLIC.). OBEY THE MATERIAL
MANUFACTURER’S INSTRUCTIONS.
(c) Apply 16-002 Polyurethane Topcoat Grey (for Internal Applic.) and allow to dry.

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SPECIAL TOOLS,FIXTURES,EQUIPMENT AND CONSUMABLES

**For PN’s ALL

TASK 52-12-12-940-803-A01
Special Tools, Fixtures and Equipment
1. Special Tools, Fixtures and Equipment List
SUPPLIERS CODE
PART No. DESCRIPTION OR NAME AND WHERE USED TID
ADDRESS
98F52108009000 Milling and Crimping Device FAPE3 TASK
- Passenger/Crew Doors 52-12-12-370-801-
A01
DefaultCategory
TABLE 1

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ILLUSTRATED PARTS LIST

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INTRODUCTION

**For PN’s ALL

TASK 52-12-12-872-801-A01
Introduction Illustrated Parts List (IPL)
1. General
A. The procedure recommended for finding a part number, or details of a part are in paragraph 2
of this introduction.
B. The IPL contains:
- illustrations that show an exploded view of the parts,
- the related detailed Parts Lists.
C. The IPL is used to identify, to get, keep and issue replacement aircraft parts and units.
D. AIRBUS S.A.S. has no responsibility for parts and/or units deleted or revised as a result if
airline initiated modifications are included.
E. Part numbers shown in this document are written to Air Transport Association of America
(ATA) Specification ISPEC 2200.
F. Illustrations are applicable to more than one customer.
G. In the Detailed Parts List, each figure has its own page numbering system that starts at zero.
2. How to use the IPL
A. To find a Part Number (P/N) in a Figure or Illustration you can either:
- Enter the PN in the SEARCH tool within the AirN@v / Workshop. This will show you the
Figure or Figures where this appears. Click on your chosen Fig/Item number to go open the
Figure.
- Or refer to the Alph/Numeric Parts List and find the PN. In the Fig/Item column it will
show you all the figures where this PN exists, and the Item number. Click one of these to
open the Figure.
3. Plan of the IPL
A. Indenture System of the Detailed Parts List
(1) The indenture system shows how parts and assemblies relate to their next higher
assemblies (NHA) as follows:
1234567
Assembly
Attaching parts for assembly
.Detail parts for assembly
.Sub-assembly
..Detailed parts for sub-assembly
..Sub-sub-assembly

IPL INTRO
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...Detailed parts for sub-sub-assembly.

B. AIRBUS Part -- Numbering System
(1) The example that follows shows the identification of a part/assembly:
Basic Part Number L 57 4 6 0200 000 00
DRAWING NUMBER PARTS LIST DATA
AIRBUS Part -- Numbering System
TABLE 1

(1) L Aircraft A = AIRBUS A310/A300/A300-600 Aircraft

D = AIRBUS A320 Aircraft
F = AIRBUS A340 Aircraft
L = AIRBUS A380 Aircraft
NOTE: Initial aircraft type the part assembly was
first used on.
(2) 57 ATA Chapter Design and Manufacturing requirements of the
above breakdown will not always be the same as
those in the ATA Specification and the IPL.
(3) 4 ATA Section Changes with the ATA Chapter.
(4) 6 Drawing The Engineering Department that is responsible
Responsibility for the Design.
(5) 0200 Drawing Number The Drawing number.
(6) 000 Part or Assembly Part/assembly number.
(7) 00 Technical Manufacturing or spares requirements suffix.
Specification
AIRBUS Part -- Numbering System
TABLE 2

C. Suffixes
SUFFIXES DEFINITION REMARKS
00 and 40 to 49 Production Part to drawing The same as the Production
01 to 39 Production Part not to drawing Part.
50 Spare Part to drawing Spare part is not the same as the
51 to 59 Spare Part not to drawing Production Part
60 to 89 Spare Part not to drawing and Number for Product Support
not storable Breakout, but not for Production
99 Spare Part to drawing and not
storable
90 to 94 Specific Part for Repair Kits

IPL INTRO
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SUFFIXES DEFINITION REMARKS

95 to 98 Specific Part for Service Bulletin
Kits
Suffixes
TABLE 3

D. D. Detailed composition for an IPL

Column Column 2 Column 3 Column 4 Column
1 5
FIG- PART NUMBER 1234567 NOMENTLATURE USAGE UNIT
ITEM FROM TO PER
ASSY
1 -- 1A L5217605100000 ARM ASSY-SUPPORT EFF//NHA RF
1 -- 2A L5217605100100 ARM ASSY-SUPPORT EFF//NHA RF
10A L5217605100100 .SUPPORT ASSY (LH) ) (V2D671) 1
SEE 52-10-50-02 FOR DET
20A L5217605500300 .SUPPORT ASSY (RH) (V2D671) 1
SEE 52-10-50-02 FOR DET
*** L5217605501100 .SUPPORT ASSY (V2D671) SPARE
30A L5217609020000 .SHEET-BONDING (V2D671) 2
40A ABS0114T3-1 .BOLT V2D671) 18
50A NAS1149C0363R .WASHER (V80205) 21
60A L9247100502400 .STRAP-BONDING (V2D671) 3
70A L9247100500400 .STRAP-BONDING (V2D671) 1
80A L9247100501400 .STRAP-BONDING (V2D671) 1
90A L5217608620000 .BRACKET-DOOR (V2D671) 1
100A ABS0114T5-25 .BOLT (V2D671) 1
110A L5217608720000 .WASHER-TOOTHED (V2D671) 2
120A NAS1149C0532R .WASHER (V80205) 1
130A NAS1291C5M .NUT (V80205) 1
OPT TO H42-5 (V15653)
OPT TO PLH55M
(VF0224)
OPT TO VN300D054
(V92215)
140A L5217605600000 .BRACKET ASSY (V2D671) 2

IPL INTRO
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Column Column 2 Column 3 Column 4 Column

1 5
*** L5217605600200 .BRACKET ASSY (V2D671) SPARE
145A L5217605620000 ..BRACKET (V2D671) EFF/NHA 1
USED WITH
L5217605600000
*** L5217605620200 ..BRACKET (V2D671) SPARE
150A MS21209F4-15 ..INSERT (V96906) EFF/NHA 1
USED WITH
L5217605600000
160A L5217607600000 .BUMPER ASSY (LH) (V2D671) 1
170A L5217607600100 .BUMPER ASSY (RH) (V2D671) 1
180A L5217607800000 ..BRACKET ASSY (LH) (V2D671) 1
190A L5217607800100 ..BRACKET ASSY (RH) (V2D671) 1
200A L5217607820000 ...BRACKET (LH) (V2D671) 1
210A L5217607820100 ...BRACKET (RH) (V2D671) 1
220A D5237111620400 ...BUSHING-SHOULDERED (V2D671) 1
230A L5217608000000 ..STOP ASSY (V2D671) 1
240A L5217608120000 ...STOP (V2D671) 1
250A L5217608220000 ...SUPPORT (V2D671) 1
260A ABS0114T5-15 ..BOLT (V2D671) 1
270A NAS1291C5M ..NUT (V80205) 1
OPT TO H42-5 (V15653)
OPT TO PLH55M
(VF0224)
OPT TO VN300D054
(V92215)
Detailed composition for an IPL
TABLE 4

IPL INTRO
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(1) Help for the IPL-Page example

Column 1 Figure Number The figure number refers to its
related illustration.
Modifications and system
variants can cause a different
figure. It will be added with a
sequential alpha-suffix, e.g.
modified versions of Figure 1
would be Figure 1A then Figure
1B and so on.
Non-Illustrated Parts The dash before an item
number shows it is not
illustrated.
Item Number Initially, only every tenth
number is used for item
numbers so that other items
can be added later.
Column 2 AIRBUS Part AIRBUS manufactured parts e.
g. L5217605600000
Standard Part A standard part such as AN,
MS, NAS ...., is not given a
supplier code.
Column 3 See XX-XX-XX-XX for DET or Identifies correctly:
NHA - the location of the full
breakdown of a sub-assembly
in the IPL
- the location of the NHA of
the item in the IPL.
Usage From To In the Usage From To field the
statement ”EFF//NHA”
related to an NHA. At the
same time in the Nomenclature
Field under the description of
the Part A Statement ”Used
With ***” will state the NHA
PNR.
Symmetrical Parts LH or RH identifies the left
hand or right hand position of
the part. If a part is only on
one assembly, (LH side) or (RH
side) follows its name.

IPL INTRO
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VENDOR CODE A supplier code is given to the

parts manufactured by firms
other then AIRBUS.
Non-Procurable Item (NP) Identifies an item that is not
supplied.
Column 4 Usage From To In the Usage From To field the
statement ”EFF//NHA”
related to an NHA. At the
same time in the Nomenclature
Field under the description of
the Part A Statement ”Used
With ***” will state the NHA
PNR.
Column 5 Quantity The number in the Units Per
Assy column shows the
quantity of parts used for each
NHA or installation.
AR = as required
RF = reference (quantity
shown in the NHA figure).
Help for the IPL-Page example
TABLE 5

E. Other Notes
(1) ORDER OVRLGTH MPN XXXXXXXXXX
- Identifies a part number with more than fifteen characters that cannot fit in the part
number column.
(2) SB XX-XXX
- Identifies the Service Bulletin (SB) which adds to or changes the Detailed Parts List.
When the SB number shown in the name column is related to an AIRWORTHINESS
DIRECTIVE (AD), the letters AD and its number are shown in parenthesis. Also they
will follow the SB number, for example: PRE SB XX XXX (AD XXXX), POST SB XX
XXX (AD XXXX), ADDED by SB XX XXX (AD XXXX), DELETED BY SB XX XXX
(AD XXX), etc.
(3) SEL FROM
- Identifies a group of alternative parts from which you can take the necessary ones.
(4) OVERSIZE/UNDERSIZE
- Identifies a part as oversize or undersize.
(5) OPT TO
- Identifies an optional part that is fully interchangeable with the initial part.

IPL INTRO
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(6) ALT FROM PN XXXXXXXXXX

- Identifies an alternate part number (this is a part that is fully interchangeable with the
initial part after it has had a change(s)).
(7) BUY PN XXXXXXXXXX
- Identifies the replacement part for the part in the part number column.
(8) LM = LOCAL MANUFACTURE
- Identifies the part number of the basic material (e.g. for seals, hinge strips, extrusion
etc...) from which the part in the part number column is manufactured.
- Identifies the unit of measurement followed by the dimensions or quantity.
(9) SEE CMM OR ACMM
- Refer to the Component Maintenance Manual or Abbreviated Component Maintenance
Manual for the part listed in the Detailed Parts List.
(10) MADE FROM JXXXX, MADE BY VXXXXX, MM XXX
- Identifies a part that is made from bulk material e.g. seals extrusions etc. and, if
necessary, the unit of measurement and quantity.
(11) USED ON MPN
- Identifies the NHA for a part in the part number column. This is used when the NHA
is not clear from the Usage Code (almost the same assemblies with details that are not
the same but have a single breakdown).
(12) VENDOR CODE
(a) These codes agree with the current issue of the Manufacturers Cataloging Handbook
H4/HB:
- Federal Supply Code for Manufacturing (FSCM) or Commercial and Government
Entity (CAGE) code (United States and Canada only).
- NATO Supply Code for Manufacturers (NSCM) codes (does not include United
States and Canada)
(b) The letter ’V’ comes before the vendors code. For suppliers with no official code,
AIRBUS has given a provisional code. These codes are identified in the supplier table
by the information ”DUMMY CODE”.
- AIRBUS standard parts (Prefix DAN, NSA etc...) are given the supplier code of
the seller of the parts. If there is more than one seller, a dummy supplier code
VT0000 is assigned to the related P/N. In this case, the additional cross-
reference table gives, for each P/N the various supplier codes and their own P/N
if applicable.

NOTE : Suppliers who manufacture parts for which AIRBUS S.A.S. has an exclusive
sale right are not given a vendor code.

NOTE : All relevant Supplier Codes are shown in the ’Vendors Name and Code
List’, which is a part of the IPL INTRO.

IPL INTRO
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VENDOR LIST

CODE NAME AND ADDRESS

V04795 HONEYWELL INTERNATIONAL INC/DIV HARDWARE PRODUCT GROUP/875W
ELLIOT RD SUITE 106/AZ-85284/TEMPE/USA
V50632 KAMATICS CORP/SUB OF KAMAN CORP/1330 BLUE HILLS AVENUE/3/CT
06002-1304/BLOOMFIELD/USA
VC5543 INTERTURBINE LOGISTIK GMBH/KISDORFER WEG
36-38/24568/KALTENKIRCHEN/D
VC5729 HONEYWELL HPG/LADEMANNBOGEN 128/22339/HAMBURG,/D
VC7239 NMB MINEBA GMBH/SIEMENSTRASSE 30/63225/LANGEN/GER
VD3279 FRANKENJURA INDUSTRIE GMBH.FLUGWERKLAGER/GARTENHAEUSER WEG
19/91462/DACHSBACH/GER
VF0222 SKF AEROSPACE FRANCE/1 AVENUE MARC SEGUIN/BP 29/26241/ST VALLIER
CEDEX/FR
VF0234 ADR LES APPLICATIONS DU ROULEMENT/CHEMIN DES PRES/BP
3/77810/THOMERY/FR
VF5442 EADS NORMALISATION STANDARD ASN/REFER TO OPT VENDORS/37
BOULEVARD DE MONTMORENCY/75781/PARIS/FR
VFAPE3 AIRBUS SAS (FOR ORDERING REFER TO CAGE CODE D4296)/1 ROND-POINT
MAURICE BELLONTE/31707/BLAGNAC/FRA
VH1822 STORK FOKKER AESP BV/INDUSTRIEWEG 4/1/3351 LB/PAPENDRECHT/NL
VK0685 ICORE INTERNATIONAL LTD/LEIGH ROAD SLOUGH TRADING ESTATE/SL1
4BB/SLOUGH BERKS/GB
VK5269 SKF (U.K) LTD AEROSPACE DIVISION/108 STRODE ROAD/BS21 6QQ/CLEVEDON
AVON/UK
VS0352 NIPPON MINIATURE BEARING COMPANY LTD/00389/TOKYO/JAP

IPL INTRO
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DETAILED PARTS LIST

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12, 5, V4.0
3, 8
F_PL_521212_02_0_01_00

ARM ASSY-GUIDE
Figure 02 / FIGURE-52-12-12-950-802-01

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FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
02 - 001A A5217213300200 ARM ASSY-GUIDE VFAPE3 RF
02 - 001B A5217213300600 ARM ASSY-GUIDE VFAPE3 RF
02 - 001C A5217213300800 ARM ASSY-GUIDE VFAPE3 RF
02 010A NSA8147-10-24 . BEARING VF5442 001
OPT TO AJF10C24NSA S0352
OPT TO BFA1-10-24 F0234
OPT TO F0N6-8932-10C24 H1822
Optional Vendor Code 04795, C5543, C5729, C7239
used on 001A, 001B, 001C
02 020A NSA8147-08-20 . BEARING VF5442 001
OPT TO AJF08C20NSA S0352
OPT TO BFA1-08-20 F0234
OPT TO F0N6-8932-08C20 H1822
OPT TO KSF0810P K5269
Optional Vendor Code 04795, 50632, C5543, C5729,
C7239, F0222
used on 001A, 001B, 001C
02 030A NSA5100-021 . RETAINER-BEARING VF5442 001
Optional Vendor Code 04795, D3279
used on 001A, 001B, 001C
02 040A NSA8135-04X . BEARING-SPHERICAL VF5442 001
OPT TO ABWT4-2020 K0685
OPT TO RWR04FF F0234
OPT TO XRL6-35X F0222
Optional Vendor Code 04795, C5543, C5729, C7239,
S0352
used on 001A, 001B, 001C
02 050A A5217213420200 . ARM-GUIDE VFAPE3 001
used on 001A
02 050B A5217240820000 . ARM-GUIDE VFAPE3 001
used on 001B
02 050C A5217240820400 . ARM-GUIDE VFAPE3 001
used on 001C
- ITEM NOT ILLUSTRATED

Page 10002-1
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
A5217213300200

12, 5, V4.0
3, 8
F_PL_521212_03_0_01_00

ARM ASSY-GUIDE
Figure 03 / FIGURE-52-12-12-950-803-01

Page 10003-0
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 @AIRBUS
COMPONENT MAINTENANCE MANUAL
A5217213300200

FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
03 - 001A A5217213300400 ARM ASSY-GUIDE VFAPE3 RF
OPT TO X5217213300400 FAPE3
03 - 001B A5217213300600 ARM ASSY-GUIDE VFAPE3 RF
03 - 001C A5217213300800 ARM ASSY-GUIDE VFAPE3 RF
03 010A NSA8147-10-24 . BEARING VF5442 001
OPT TO AJF10C24NSA S0352
OPT TO BFA1-10-24 F0234
OPT TO F0N6-8932-10C24 H1822
Optional Vendor Code 04795, C5543, C5729, C7239
used on 001A, 001B, 001C
03 020A NSA8147-08-20 . BEARING VF5442 001
OPT TO AJF08C20NSA S0352
OPT TO BFA1-08-20 F0234
OPT TO F0N6-8932-08C20 H1822
OPT TO KSF0810P K5269
Optional Vendor Code 04795, 50632, C5543, C5729,
C7239, F0222
used on 001A, 001B, 001C
03 030A NSA5100-021 . RETAINER-BEARING VF5442 001
Optional Vendor Code 04795, D3279
used on 001A, 001B, 001C
03 040A NSA8135-04X . BEARING-SPHERICAL VF5442 001
OPT TO ABWT4-2020 K0685
OPT TO RWR04FF F0234
OPT TO XRL6-35X F0222
Optional Vendor Code 04795, C5543, C5729, C7239,
S0352
used on 001A, 001B, 001C
03 050A A5217213420400 . ARM-GUIDE VFAPE3 001
used on 001A
03 050B A5217240820000 . ARM-GUIDE VFAPE3 001
used on 001A, 001B
03 050C A5217240820400 . ARM-GUIDE VFAPE3 001
used on 001C
- ITEM NOT ILLUSTRATED

Page 10003-1
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