@AIRBUS

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

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PART LIST

SPRING STRUT

PN : A2104001020200
A2104001025200

Issue: Jun 01/77 36-14-16 Rev: Jul 01/09

 @AIRBUS
COMPONENT MAINTENANCE MANUAL
A2104001020200

HIGHLIGHTS

Revision No. 12 - Jul 01/09

LOCATIONS CHG DESCRIPTIONS OF CHANGE

CODE
REPAIR
TASK 36-14-16-300-801-A01 R CONSUMABLE MATERIAL DATA
UPDATED

HIGHLIGHTS
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COMPONENT MAINTENANCE MANUAL
A2104001020200

LIST OF EFFECTIVE CONTENT

Revision No. 12 - Jul 01/09

CONTENT CHG LAST REVISION

CODE DATE
INTRODUCTION
TASK 36-14-16-871-801-A01 Mar 01/09

DESCRIPTION AND OPERATION

TASK 36-14-16-870-802-A01 Mar 01/09
TASK 36-14-16-870-803-A01 Mar 01/09
FIGURE 36-14-16-991-001-A01 Mar 01/09

TESTING AND FAULT ISOLATION

TASK 36-14-16-700-801-A01 Mar 01/09
Subtask 36-14-16-700-001-A01 Mar 01/09

DISASSEMBLY
TASK 36-14-16-000-801-A01 Mar 01/09
Subtask 36-14-16-000-001-A01 Mar 01/09
TASK 36-14-16-000-802-A01 Mar 01/09
Subtask 36-14-16-000-002-A01 Mar 01/09

CLEANING
TASK 36-14-16-100-801-A01 Mar 01/09
Subtask 36-14-16-100-001-A01 Mar 01/09

INSPECTION/CHECK
TASK 36-14-16-210-801-A01 Mar 01/09
Subtask 36-14-16-200-001-A01 Mar 01/09

REPAIR
TASK 36-14-16-300-801-A01 R Jul 01/09
Subtask 36-14-16-300-001-A01 Mar 01/09

ASSEMBLY

L.E.C.
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CONTENT CHG LAST REVISION

CODE DATE
TASK 36-14-16-400-801-A01 Mar 01/09
Subtask 36-14-16-400-001-A01 Mar 01/09

FITS AND CLEARANCES

TASK 36-14-16-820-804-A01 Mar 01/09
TASK 36-14-16-820-805-A01 Mar 01/09

STORAGE INCLUDING TRANSPORTATION

TASK 36-14-16-550-801-A01 Mar 01/09
Subtask 36-14-16-530-001-A01 Mar 01/09
Subtask 36-14-16-550-001-A01 Mar 01/09

ILLUSTRATED PARTS LIST

IPL Introduction
TASK 36-14-16-872-801-A01 Mar 01/09
VENDOR LIST Mar 01/09
Figure 01
FIGURE 36-14-16-991-801-001 Mar 01/09
Parts List Mar 01/09

L.E.C.
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COMPONENT MAINTENANCE MANUAL
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LIST OF SERVICE BULLETINS

SB No REV No MOD No INCORP. TITLE

DATE
*** NO SB ***

SBL
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COMPONENT MAINTENANCE MANUAL
A2104001020200

INTRODUCTION

**For PN’s ALL

TASK 36-14-16-871-801-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
ACM Abbreviated Component Maintenance Manual
AEB Airline Engineering Bulletin
ASD Aero Space and Defence Industries Association of Europe
ATA Air Transport Association of America
ATLAS Abbreviated Test Language for All Systems
CMM Component Maintenance Manual
CMS Component Maintenance Sheet
FIN Functional Item Number

INTRO
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COMPONENT MAINTENANCE MANUAL
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IPC Illustrated Parts Catalog

IPL Illustrated Parts List
ID Inside Diameter
MFG Manufacturing
MFR Manufacturer
MOD Modification
MTOSS Maintenance Task Oriented Support System
NTF Non Textile Floor
OD Outside Diameter
PA Poly-Amide
PARA Paragraph
PC Poly-Carbonate
PMS Process and Materials Specification
PN Part Number
PU Poly-Urethane
PV Poly-Venyl-Fluorite
SB Service Bulletin
SERNO Serial Number
STE Simplified Technical English
TBD To Be Determined
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 36-14-16-870-802-A01
General
1. Technical Data
Length: 4 in (101.6 mm)
Height: 0.5 in (12.7 mm)
Weight: 0.551 lb (0.25kg)
Technical Data
TABLE 1

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**For PN’s ALL

TASK 36-14-16-870-803-A01
Description and Operation
1. The spring strut consists of a spring housing (60) and a spring rod (40) incorporating an internal
spring (50), the housing and rod are attached by a headed pin (30) which slides in a slot.
The strut has a compressing action and the length movement is governed by the slot in the housing.
On installation, to a ventilation valve with an actuator fitted, the spring rod (40) is set to the center
of slot when valve is closed, so that a continuous load is being applied to the butterfly valve.

NOTE : Refer to FIGURE 36-14-16-991-001-A.

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F_CM_361416_1_0010101_01_00

Spring Strut
FIGURE-36-14-16-991-001-A01

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COMPONENT MAINTENANCE MANUAL
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TESTING AND FAULT ISOLATION

**For PN’s ALL

TASK 36-14-16-700-801-A01
Functional Test
1. Reason for the Job
Self explanatory.
2. Procedure

Subtask 36-14-16-700-001-A01
A. Functional Test
(1) Check strut for full freedom of movement, extending to 3.44/3.52 in. (87.4/89.4 mm)
between attachment holes. Ensure that spring is under compression of 0.06 in. (1.5 mm)
minimum when strut is fully extended.

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COMPONENT MAINTENANCE MANUAL
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DISASSEMBLY

**For PN’s ALL

TASK 36-14-16-000-801-A01
Checks before Disassembly
1. Reason for the Job
Self explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 36-14-16-210-801-A01 TASK 36-14-16-210-801-A01-Metal Component
TASK 36-14-16-100-801-A01 TASK 36-14-16-100-801-A01-Cleaning
Referenced Information
TABLE 1

3. Procedure

Subtask 36-14-16-000-001-A01
A. Checks before Disassembly
(1) Examine the history or defect card, (if there is one), to find any defective areas which you
must look at. You must clean and examine the components (Refer to TASK
36-14-16-210-801-A01TASK 36-14-16-100-801-A01) to find the condition and/or the cause
of the problem (if there is one). The procedure that follows is for the complete disassembly.
Do all the operations an a clean, soft work surface to prevent damage to the components.
(2) Locking devices such as cotter pins, peened pins and bolts, are to be discarded and must
not be re-used.

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**For PN’s ALL

TASK 36-14-16-000-802-A01
Detailed Disassembly
1. Reason for the Job
Self explanatory.
2. Procedure

Subtask 36-14-16-000-002-A01
A. Detailed Disassembly

NOTE : Refer to IPL_FIGURE_01.

(1) Remove cotter pin (10), washer (20) and headed pin (30).
(2) Withdraw spring rod (40), collect spring (50) from spring housing (60).

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COMPONENT MAINTENANCE MANUAL
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CLEANING

**For PN’s ALL

TASK 36-14-16-100-801-A01
Cleaning
1. General

WARNING : BE CAREFUL WHEN YOU USE SOLVENTS/CLEANING AGENTS, SEALANTS AND

OTHER MATERIALS. OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS
AND THE LOCAL REGULATIONS. MAKE SURE THAT THERE IS A GOOD FLOW
OF AIR THROUGH THE WORK AREA. DO NOT BREATHE THE FUMES. DO NOT
SMOKE. DO NOT USE THESE MATERIALS NEAR A FLAME, SPARKS OR
SOURCES OF HEAT. USE PROTECTIVE CLOTHING, GOGGLES AND GLOVES. IF
YOU GET ONE OF THESE MATERIALS ON YOUR SKIN OR IN YOUR EYES,
FLUSH IT AWAY WITH A FLOW OF CLEAN WATER. IF YOU GET ONE OF
THESE MATERIALS IN YOUR MOUTH, GET IMMEDIATE MEDICAL AID. IN
GENERAL, THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN
IRRITANTS.

CAUTION : USE ONLY SPECIFIED CLEANING MATERIALS AND SOLUTIONS OR THEIR

EQUIVALENTS. THE SURFACE PROTECTION COULD BE DAMAGED IF
UNSPECIFIED MATERIALS ARE USED. IT IS IMPORTANT THAT THE
MANUFACTURER’S MIXING, APPLICATION AND TREATMENT INSTRUCTIONS
ARE FOLLOWED.
-
-

NOTE : Use Genklene Material No. 11-577 to clean all components not painted.

NOTE : Use dry Cleaning Solvent Material No. 11-524 to clean all the components.

NOTE : If necessary, use Titanine Material No. 11-576 to remove dirt, from the components.

NOTE : Dry the parts with a jet of dry and clean compressed air. If necessary remove traces of dry
Cleaning Solvent Material No. 11-524 with Material No. 19-003 Lint-Free Cotton Cloth.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
19-003 Lint-Free Cotton Cloth
Consumable Materials
TABLE 1

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3. Procedure

Subtask 36-14-16-100-001-A01
A. Sealed Bearings
(1) Use Material No. 19-003 Lint-Free Cotton Cloth to clean any traces of dirt or grease from
the external surfaces of the sealed bearings.

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COMPONENT MAINTENANCE MANUAL
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INSPECTION/CHECK

**For PN’s ALL

TASK 36-14-16-210-801-A01
Metal Component
1. Reason for the Job
Self explanatory.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 36-14-16-820-805-A01 TASK 36-14-16-820-805-A01-Fits and Clearance
Referenced Information
TABLE 1

3. Procedure

Subtask 36-14-16-200-001-A01
A. Metal Component
(1) Cleanliness.
(2) Distortion.
(3) Cracks - should serviceability be suspect the part to either magnetic (ferrous) or penetrant
dye (non-ferrous) flaw detection.
(4) Scoring or abrasions.
(5) Evidance of wear. Refer to TASK 36-14-16-820-805-A01 charts for permissible wear limits.
(6) Deterioration of protective treatment - corrosion.

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REPAIR

**For PN’s ALL

TASK 36-14-16-300-801-A01
Repair
1. Reason for the Job
Self explanatory.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
Epoxide Primer Mat. No. 16-504
Polyurethane Finish Mat. No. 16-511
Consumable Materials
TABLE 1

3. Procedure

Subtask 36-14-16-300-001-A01
A. General
(1) Repair will usually be by renewal of any damaged or worn items with a new spare part.
(2) For type of protective finish refer to TABLE 2.
IPL FIG. AND ITEM DESCRIPTION MATERIAL PROTECTIVE
NO. SPECIFICATION FINISH
1 - 60A Housing S. 98 Phosphate - Parker
GM internal only.
Cadmium plate plus
Epoxide Primer Mat.
No. 16-504
elsewhere.

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IPL FIG. AND ITEM DESCRIPTION MATERIAL PROTECTIVE

NO. SPECIFICATION FINISH
1 - 60B Spring Housing S. 98 Phosphate - Parker
GM internal and
outside diameters.
Epoxide Primer Mat.
No. 16-504 and
Polyurethane Finish
Mat. No. 16-511
externally.
Protective Finish
TABLE 2

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COMPONENT MAINTENANCE MANUAL
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ASSEMBLY

**For PN’s ALL

TASK 36-14-16-400-801-A01
Detailed Assembly
1. General
A. Renew all locking devices, with a dual inspection of all such locking during the assembly
procedure.
-

NOTE : Coat spring and internal surfaces with synthetic grease Material No. 04-522 on
assembly.
2. Job Set-up Information
A. Consumable Materials
REFERENCE DESIGNATION
synthetic grease Material No. 04-522
Consumable Materials
TABLE 1

B. Referenced Information
REFERENCE DESIGNATION
TASK 36-14-16-820-805-A01 TASK 36-14-16-820-805-A01-Fits and Clearance
Referenced Information
TABLE 2

3. Procedure

Subtask 36-14-16-400-001-A01
A. Detailed Assembly
(1) Detailed Assembly

NOTE : Refer to IPL_FIGURE_01.

(a) Lubricate internal bore of spring housing (60), spring (50) and external shaft of spring
rod (40) with synthetic grease Material No. 04-522.
(b) Fit spring (50) into spring housing (60), push in spring rod (40) and attach together
through slot with pin (30), washer (20) and cotter pin (10), ensuring spring is under
compression refer to FIT AND CLEARANCE TASK 36-14-16-820-805-A01.

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FITS AND CLEARANCES

**For PN’s ALL

TASK 36-14-16-820-804-A01
Fits and Clearance Introduction
1. General
A. How to use the Fits and Clearances Table (See Sample TABLE 1)
(1) A NOTE above the table gives the reference to the related CMM figure.
(2) Column 1 gives the location number (LOC NO.) of the part.
(3) Column 2 gives links to the IPL figure item numbers of the mating parts.
(4) Column 3 gives the dimensions and the assembly clearances of the original manufacturer
(MFR) limits.
(5) Column 4 gives the dimension limits and the maximum allowable clearance of the in-
service wear limits.

NOTE : It is necessary to replace the parts which are not in the limits (See
DISASSEMBLY, REPAIR and ASSEMBLY).
B. Sample of Fits and Clearances
1 2 3 4
MFR LIMITS IN-SERVICE WEAR LIMITS
MATING MAX
IPL ASSEMBLY DIMENSION ALLOWABLE
LOC FIGURE DIMENSION CLEARANCE LIMITS CLEARANCES
NO. AND millimeters millimeters millimeters millimeters
ITEM NO. (inches) (inches) (inches) (inches)
MIN MAX MIN MAX MIN MAX
Sample
TABLE 1

NOTE : See FIGURE XXX

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**For PN’s ALL

TASK 36-14-16-820-805-A01
Fits and Clearance
1. Chart Table
ORIGINAL MFR LIMITS IN-SERVICE WEAR LIMITS
IPL DIMENSION (INCH) ASSEMBLY DIMENSION MAXIMUM
FIGURE MM CLEARANCE LIMITS (INCH) MM ALLOWABLE
AND (INCH) MM CLEARANCE
ITEM MIN MAX MIN MAX MIN MAX (INCH)
NUMBER MM
OD 1- 40 0.3432 0.3436 0.3420
(8.717) (8.727) 0.0002 0.0015 (8.687) 0.0040
ID 1-60 0.3438 0.3477 (0.005) (0.038) FOOTNOTE0.3460 (0.101)
(8.732) (8.755) (8.788)
OD 1- 30 0.1840 0.1860 0.1830
(4.674) (4.724) 0.0015 0.0042 (4.648) 0.0080
ID 1- 40 0.1875 0.1882 (0.038) (0.106) FOOTNOTE0.1920 (0.203)
1- 60 (4.762) (4.780) (4.851)
Only apply while there is a thickness of chromeplating on the bearing surfaces.
Chart
TABLE 1

2. Spring Loading
IPL FIG. ITEM NO. DESIGNATION FREE LENGTH IN COMPRESSED
(MM) LENGTH IN (MM)
1- 50 Spring 1.20 in. (30.48 mm) 0.93 to 0/98 in. (24.5
to 25.8 mm) with load
of 3 kg applied
Spring Loading
TABLE 2

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COMPONENT MAINTENANCE MANUAL
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STORAGE INCLUDING TRANSPORTATION

**For PN’s ALL

TASK 36-14-16-550-801-A01
Storage including Transportations
1. General
A. The component should be stored in its original packing if available. Avoid damage caused by
excessive weight, if stacked storage is used. For the weight of the component refer to
Description/Operation - Data
B. Store the packed component in a clean dry, well ventilated room. Keep the storage temperature
between 18 deg. C (64 deg. F) and 28 deg. C (82 deg. F), preferably nearer the lower limit. If
rubber parts are installed on the component, the temperature should not exceed +20 deg. C
(+68 deg. F).
C. The relative humidity should be between 25% and 65%.
D. Do not store the packed component in the vicinity of corrosive fluids or near heat or ozone
generating sources.
E. Position package so that the identification label can be checked easily.
2. Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
TASK 36-14-16-870-802-A01 TASK 36-14-16-870-802-A01-General
Referenced Information
TABLE 1

3. Procedure

Subtask 36-14-16-530-001-A01
A. Packing
(1) Pack the component either in the original packing, or in a suitable container, in accordance
with Air Transport Association Specification Number 300 (ATA 300).
(2) If a container is used, provide cushioning material and bracing to prevent accidental
damage. For dimensions of the component refer to Description/Operation TASK
36-14-16-870-802-A01.

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Subtask 36-14-16-550-001-A01
B. Identification Label
(1) Affix an identification label to the component so that it is easily discernable both before
and after packing. If necessary, an additional identification label must be affixed to the
outside of the package.
(2) The identification label must contain all relevant details, including the date of receipt into
storage and dates of condition checks during storage.

NOTE : If the identification label is missing, the components cannot be approved for
installation or storage.

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ILLUSTRATED PARTS LIST

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INTRODUCTION

**For PN’s ALL

TASK 36-14-16-872-801-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.

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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.

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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 TBIL
V06329 TBIL
V60996 TBIL
V6D833 TBIL
V70347 TBIL
V80205 TBIL
V84114 TBIL
V8K160 TBIL
V96906 TBIL
VC5543 TBIL
VC5729 TBIL
VF0188 TBIL
VFAPE3 TBIL
VH2776 TBIL

IPL INTRO
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DETAILED PARTS LIST

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F_PL_361416_01_0_01_00

STRUT ASSY-SPRING
Figure 01 / FIGURE-36-14-16-950-801-01

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FIG-ITEM PART NUMBER NOMENCLATURE USAGE UNIT

1234567 FROM PER
TO ASSY
01 - 001A A2104001020200 STRUT ASSY-SPRING VFAPE3 RF
01 - 001B A2104001025200 STRUT ASSY-SPRING VFAPE3 RF
01 010A MS24665-155 . PIN-COTTER V96906 001
Optional Vendor Code 04795, 06329, 60996, 84114,
8K160, C5543, C5729
used on 001A, 001B
01 020A AN960PD4L . WASHER (NP) 001
NAS1149DN416J 80205
used on 001A, 001B
01 030A MS20392-1C15 . PIN V96906 001
Optional Vendor Code 04795, 06329, 6D833, 70347,
C5543, C5729, F0188, H2776
used on 001A, 001B
01 040A A2104002420000 . ROD-SPRING VFAPE3 001
used on 001A, 001B
01 050A A2104002220000 . SPRING VFAPE3 001
used on 001A, 001B
01 060A A2104002320000 . HOUSING VFAPE3 001
used on 001A
01 060B A2104002330000 . HOUSING-SPRING VFAPE3 001
used on 001A, 001B
- ITEM NOT ILLUSTRATED

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