### AIRWORTHINESS LIMITATIONS SECTION

REVISION: 05 

# A330



# ALS Part 1

-

Safe Life

Airworthiness Limitation Items

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document.

This document and all information contained herein is the sole property of AIRBUS SAS. No

intellectual property rights are granted by the delivery of this document or the disclosure of its

content. This document shall not be reproduced or disclosed to a third party (except for the

purposes of performing the tasks described hereunder and provided that any recipient of such

document shall comply with the conditions herein) without the express written consent of

AIRBUS SAS. This document and its content shall not be used for any purpose other than that

for which it is supplied.

### AIRWORTHINESS LIMITATIONS SECTION

ALS PART 1

SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

LIST OF EFFECTIVE PAGES

PART MVT PAGE ISSUE PART MVT PAGE ISSUE

ISSUE: JUL 29/10 ALS PART 1 PAGE: 1-LEP

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1 R 1-LEP JUL 29/10

1 1-TOC JAN 28/10

1 R 1-ROR JUL 29/10

1 R 2-ROR JUL 29/10

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ALS PART 1

SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

TABLE OF CONTENTS

SUBJECT PART

ISSUE: JAN 28/10 ALS PART 1 PAGE: 1-TOC

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

RECORDS OF REVISIONS ROR

INTRODUCTION 1-0

ILLUSTRATIONS 1-1

LIFE LIMITS 1-2

DEMONSTRATED FATIGUE LIVES 1-3

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ALS PART 1

SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

ISSUE: JUL 29/10 ALS PART 1 PAGE: 1-ROR

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

The European Aviation Safety Agency (EASA) Certification Directorate approves the ALS

Par t 1. Variations must also be approved.

REVISION

NUMBER SUB

- PARTS APPROVED BY

EASA EASA AD INSERTION IN

MAINT. PROG.

00 1

- 2

1

- 3 MAR 23/06 2006

- 0129

01 ROR

1

- 2

1

- 3 MAR 30/07 2007

- 0133

02 ROR

1

- 2

1

- 3 APR 28/08 2008

- 0152

03 ROR

1

- 2

1

- 3 NOV 04/08 Not Applicable

R 04 ROR

1

- 2

1

- 3 JAN 28/10 2010

- 0131

N 05 ROR

1

- 2

1

- 3 JUL 29 /10

Note: The A330 ALS Part 1 is covered by the Certification Document 00G050AM091/C01.

Revision 05 is approved by EASA under reference 10031148

.

REVISION 05 COMPLIANCE TIME:

1. Except as stated in paragraphs 4. and 5. of this Record Of Revisions (ROR), it is mandatory

to comply with the replacement requirement and airworthiness limitations defined in the

A330 ALS Part 1 revision 05 from 29 -Jul- 2011

.

2. From 29 -Jul- 2010 to 27-Jan-2011, it is mandatory to comply with the replacement

requirement and airworthiness limitations defined, either:

- In the A330 ALS Part 1 at revision 03, except as stated in paragraph 4. of this ROR,

or,

- In the A330 ALS Part 1 at revision 04, R

R

D

N

N

N

N

N

N

N

N

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ALS PART 1

SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

ISSUE: JUL 29/10 ALS PART 1 PAGE: 2-ROR

EASA APPROVED

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# A330

or,

- In the A330 ALS Part 1 at revision 05.

3. From 28-Jan-2011 to 28 -Jul- 2011 , it is mandatory to comply with the replacement

requirement and airworthiness limitations defined, either:

- In the A330 ALS Part 1 at revision 04,

or,

- In the A330 ALS Part 1 at revision 05.

4. From 29 -Jul- 2010 , it is mandatory to comply with the replacement requirement and

airworthiness limitations defined in the A340 ALS Part 1 revision 04 or revision 05, for the

main landing gear main fitting (LH) PNR 201488324, PNR 2 01488335, and PNR 50

-

2107001 -00 and main fitting (RH) PNR 201488325, PNR 201488336 and PNR 50- 2108001

- 00, whose SNR is identified as ‘S3’ in Messier -Dowty Service Letter A33-34 A20 revision 05,

dated 31-Jul- 2009. N

N

N

N

N

N

N

N

N

N

N

N

N

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-0 PAGE: 1

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# A330

Sub-part 1-0 INTRODUCTION

1. GENERAL

From revision 06 and on, the content of

A330 Maintenance Planning Document

Section 9-1

Life Limits/Monitored parts

that provided life limitations applicable to A330 models, has been transferred to the

A330 Airworthiness Limitations Section

Part 1

Safe Life Airworthiness Limitation Items

This change is part of a process to provide Operators and Maintenance, Repair and

Overhaul Organizations (MRO) with a series of stand-alone documents in a location

dedicated to the mandatory limitations.

The data provided under Part 1 has been established with the following rules:

Compliance with the requirements contained in this document is mandatory. No

person may operate an aircraft to which an ALS applies except in accordance with

the requirements of that ALS, unless otherwise agreed with the Authority of the State

of aircraft registry.

Consultation with the State of design should be made by the State of aircraft registry,

in consideration of any deviation from the ALS requirements. This is indicated in the

International Civil Aviation Organization (ICAO) Airworthiness manual (Doc. 9760),

Volume II, Part A, Chapter 3.

A. Sub-part 1-2: Life limits

Parts listed under this sub-part are those having a life limit less than the Limit Of Validity

(LOV) due to failure during fatigue tests and whose failure could result in a catastrophic

failure of the airplane.

B. Sub-part 1-3: Demonstrated fatigue lives

Parts listed under this sub-part are those having a demonstrated fatigue life without

failure but whose failure could result in a catastrophic failure of the airplane.

Where the values are less than the LOV, fatigue tests are still on going. For these parts,

the life limitation provided (in flight hours and/or flight cycles and/or landings and/or

calendar time, as applicable) is temporary waiting for finalization of the tests. If the

demonstrated fatigue life reaches the LOV, it will remain in sub-part 1-3, if the part fails

before the LOV, its Part NumbeR (PNR) together with the life limit(s) will be transferred

to sub-part 1- 2.

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# A330

C. Traceability and replacement requirements

In order to maintain aircraft airworthiness, it is mandatory to replace parts listed

under sub-parts 1-2 and 1-3 at or prior to whichever of the life limitations occurs

first, after any necessary adjustment of the stated life limitations in accordance

with the instructions of paragraph 6 of this sub-part.

Therefore, it is necessary to assure traceability and monitoring of these parts.

Non-compliance with these requirements could suspend the validity of t he

Certificate of Airworthiness.

For a given item of the ALS Part 1, new PNR are introduced as a result of modifications

and Service Bulletins (SB) Airbus publishes. These new PNR may not be listed in the

sub-part 1-3, when the related modifications and/or SB have been released between

two scheduled revisions of the ALS Part 1.

However, it is required to assure traceability and monitoring of such items whatever

their detail PNR.

The next scheduled ALS Part 1 revision will confirm the applicable life limitation(s).

For further guidance, Operators are requested to contact Airbus.

Note: In the context of the ALS Part 1, traceability means records that clearly

demonstrate the history of each part back to initial entry into service of the part, so

that life limitations are accurately applied. Traceability records may comprise, but

are not limited to, the following:

- Application history (aircraft type, model, weight variant, MSN i.e.

Manufacturer Serial Number, etc...),

- Maintenance actions carried out (Airworthiness Directives, modifications,

repairs, inspections, etc...),

- Life accumulation (accounting for any individual aircraft to which a part may

have been fitted).

Where the complete life history of a part is not known, Operators are requested to refer

to the Service Information Letter (SIL) 32-100 for guidance. It provides the means to

manage such parts. It has been issued in agreement with the European Aviation Safety

Agency (EASA).

Note: Traceability and monitoring of parts listed in sub-parts 1-2 and 1-3 is not required

when a systematic replacement applies.

D. Disposal/quarantine action

When the parts reach the life limitations, disposal/quarantine action must be taken

depending on the following categories:

- For parts listed in the ALS sub-part 1-2: They must be mutilated beyond repair

limits to prevent rework to appear to be airworthy.

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# A330

Note: Some means may exist to extend their life potential provided they are applied

prior to reaching the life limit (e.g. Service Bulletin: POST SB PNR in the ALS

sub- par t 1 -3).

- For parts listed in the ALS sub-part 1-3: Appropriate means must be implemented

to deter their installation on aircraft pending possible extension of their life

limitations. Examples of means are:

- Record keeping system,

- Non-permanent marking s, - Segregation (parts stored separately from those currently eligible for

installation).

The ultimate solution is the mutilation beyond repair limits to prevent rework to

appear to be airworthy.

Note: When parts are removed by way of a systematic replacement, they must be

mutilated beyond repair limits to prevent rework to appear to be airworthy.

E. ALS Part 1 applicability

Sub-parts 1-2 and 1-3 are approved by the EASA.

The applicability of this ALS Part 1 revision is restricted to the aircraft series, models

and Weight Variants (WV) listed in the table below:

Aircraft series Aircraft models WV

A330

- 200 A330

- 201 020, 023, 024, 050, 052, 054, 055, 056, 059,

060

A330

- 202 020, 021, 022, 023, 050, 052, 053, 054, 055,

056, 059, 060

A330

- 203 020, 022, 023, 026, 050, 051, 052, 054, 055,

056, 059, 060

A330

- 223 020, 021, 022, 023, 050, 052, 054, 055, 056,

059, 060 , 061 R

A330

- 243 020, 021, 022, 023, 024, 025, 026, 027, 050,

052, 054, 055, 056, 059, 060

N A3 30

- 200F A330

- 223F 000, 001

N A330

- 243F 000, 001

A330

- 300 A330

- 301 000, 001, 002, 003, 004, 010, 051

A330

- 302 050, 052, 053

A330

- 303 050, 052

A330

- 321 000, 002, 003, 004, 010, 011, 012, 013 A330

- 322

A330

- 323 020, 022, 025, 050, 05 2

A330

- 341 000, 002, 003, 004, 010, 011, 012, 013, 014

A330

- 342 000, 002, 003, 004, 010, 011, 012, 013, 014,

022, 052

A330

- 343 020, 022, 024, 050, 052

### AIRWORTHINESS LIMITATIONS SECTION

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# A330

Note: The engine Time Limits and Maintenance Checks are not included in this manual:

Refer to the relevant Engine Manufacturer Chapter 05 manual.

2. DEFINITIONS

The initial entry into service of the part is the date at which the part accomplishes the

first flight for which it will undertake its intended function.

Note: Unless otherwise stated, this means for parts delivered on new aircraft (i.e. from

Airbus Final Assembly Line) that the life accumulated before the aircraft delivery

date/transfer of title date (e.g. as a result of test flights) must be taken into account.

Calendar times (Cal.): Airworthiness limitations in Years (Ye), in Months (Mo), etc... must

be counted from the date of initial entry into service of the part,

unless otherwise stated. Storage, maintenance, etc... do not freeze

calendar time accumulation.

Flight Cycle (FC): A complete take-off and landing sequence.

Flight Hour (FH): The accumulated time intervals between ‘wheels

- off’ and ‘wheels

on’.

Landing (LDG): An operation of an aircraft touching the runway and coming to a full

stop or performing a ‘touch and go’.

Li mit Of Validity (LOV): The LOV, as stated in the ALS Part 1, is the time at which the

maintenance programme defined in that Part ceases to be valid. The

applicable LOV are indicated in sub-part 1-0, paragraph 5.

Touch and go: A landing in which an aircraft touches the runway and does not

come to a full stop prior to commencing an additional flight.

3. APPLICABILITY SYSTEM

A. General

ALS sub-part 1-2 and 1-3 tables provide the applicable life limitations only when PNR

installations have been authorized. These tables do not ensure that a PNR has been

validated for a specific individual aircraft MSN.

PNR are authorized for installation on individual aircraft MSN by SB (and the associated

modifications), which are published by Airbus.

B. Aircraft model applicability

ALS sub-part 1-2 and 1- 3 table headers indicate aircraft models. When ‘x’ is entered in

the model number, it stands for any number within the limits of the list of models given

in the paragraph 1.E. of this sub-part, e.g.:

A330- 30x stands for: A330-301, A330-302 and A330- 303.

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-0 PAGE: 5

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# A330

Life limitation applicability is allocated according to the aircraft model affected, e.g.:

X stands for: All A330 models defined by the applicability of the column.

- 321 stands for: A330-321 model only, defined by the applicability of the

column.

- 321/

- 341 stands for: A330-321 and A330-341 models only, defined by the

applicability of the column.

excl. - 341 stands for: All A330 models defined by the applicability of the column,

except the model A330- 341.

C. Weight Variant applicability

ALS sub-part 1-2 and 1- 3 table headers indicate aircraft WV. When ‘x’ is entered in the

WV number, it stands for any number within the limits of the list of WV defined in the

tables of the paragraph 1.E or 8 of this sub-part.

It is under Operators’ responsibility to refer to the applicable WV.

The list of the approved WV is provided in the Type Certification Data Sheet (TCDS)

N°A.004 issued by the EASA, together with the associated modification

configuration(s).

To determine the applicable WV at the time of aircraft delivery, refer to the list of

modifications embodied during production, provided to the initial Operator of the aircraft,

in the delivery documentation (Aircraft Inspection Report ‘Conformity to Design

Standard Requirements’)

. A WV status may change as a result of the embodiment of Airbus’ SB.

Note 1: The paragraph 8 of the present sub-part reminds the modifications and SB

associated to the approved WV.

Note 2: - Life limitations applicable to A330-243 WV020 also apply to aircraft POST

MOD 50302 (A330-200 series with dual MTOW 230/192 tons).

- Life limitations applicable to A330-243 WV022 also apply to aircraft POST

MOD 50830 or POST SB A330- 00 -3027 (A330-200 series with triple MTOW

233/230/220 tons).

- Life limitations applicable to A330-302 WV050 also apply to aircraft POST

MOD 52910 (A330-300 series with dual MTOW 230/205 tons).

- Life limitations applicable to A330-202 WV050 also apply to aircraft POST

MOD 53108 (A330-200 series with dual MTOW 230/210 tons).

- Life limitations applicable to A330-203 WV052 also apply to aircraft POST

MOD 54105 (A330-200 series with triple MTOW 233/230/192 tons).

- Life limitations applicable to A330-243 WV020 also apply to aircraft POST

MOD 54518 or POST SB A330- 00 -3044 (A330-200 series with quadruple

MTOW 230/220/202/192 tons).

### AIRWORTHINESS LIMITATIONS SECTION

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# A330

N

N

N

N - Life limitations applicable to A330-202 WV052 also apply to aircraft POST

MOD 57441 (A330-200 series with quadruple MTOW 233/220/202/192 tons).

- Life limitations applicable to A330-202 WV054 also apply to aircraft POST

MOD 58324 (A330-200 series with quadruple MTOW 230/220/202/192 tons).

- Life limitations applicable to A330-202 WV052 also apply to aircraft POST

MOD 200099 (A330-200 series with dual MTOW 233/202 tons).

D. Aircraft Manufacturer Serial Number applicability

Life limitation applicability may be allocated according to the aircraft MSN affected, e.g.:

XXX

– YYY

stands for: From aircraft MSN XXX to aircraft MSN YYY (for all aircraft

defined by the applicability of the column).

XYX, XXZ stands for: For aircraft MSN XYX and aircraft MSN XXZ.

XZX stands for: For aircraft MSN XZX only

. excl. XXX stands for: All aircraft MSN defined by the applicability of the column,

excluding aircraft MSN XXX.

4. LIMITATION/REPLACEMENT TIME INDICATION

A. General

In computing the part’s accumulated life, calculations must include flight hours

and/or flight cycles and/or landings and/or calendar time (as applicable) since the

initial entry into service of the part (unless otherwise stated).

The life limitation indicated against PNR originally fitted is counted from the

part’s initial entry into service.

The life limitation indicated against PNR evolutions is also to be counted from the

part’s initial entry into service (unless otherwise stated).

B. ALS Part 1 life limitations

Life limitations quoted in sub-parts 1-2 and 1-3 are applicable to the undamaged detail

parts as listed, not to the assembly or the aircraft on which they are installed. The

limitation/replacement time indication is quoted on the same line/block of lines as the

PNR.

For a given PNR, when more than one set of limitations (FH/FC/Cal) is published for the

same application, it is the Operator/MRO's responsibility to select the appropriate set

depending on the aircraft utilisation. Combining the limitations from different sets is not

permitted.

C. Production/Repair concessions, ALS Variation and Alternative Method Of Compliance

Limitations of the ALS Part 1 may be negated by instructions given in either a

Production concession, a Repair design Approval Sheet (RAS)

, an ALS Variation (AV)

or an Alternative Method Of Compliance (AMOC). R

R

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# A330

It is Operator’s responsibility to refer to the applicable limitations.

When limitations change in a revision of the ALS Part 1 subsequent to the issuance

date of the Production concession/RAS/ AV/ AMOC, Operators are requested to contact

Airbus for guidance.

The restrictions of limitation(s) indicated in the RAS/ AV/ AMOC (or absence thereof)

depend on the part's accumulated life considered during the original evaluation of the

repair solution/ AV/

AMOC. Occasionally, repair solutions/ AV/ AMOC are evaluated on

the basis of a part's accumulated life that includes a conservative life calculation (refer

to SIL 32-100). Such AV/ AMOC/repair solutions MUST be re-evaluated by Airbus

before Operators can take credit of the history partially or completely rebuilt after

application for the repair solution/ AV/ AMOC.

Production concessions are provided to the initial Operator of the aircraft in the delivery

documentation (Aircraft Insp ection Report ‘Recordable concessions’).

Note: For spare parts, restrictions of life limitation(s), if any, are indicated in EASA Form

1 block 13 (directly or by reference to another document).

D. Modifications/repairs not developed under Airbus DOA Certificate EASA.21J.031

If an aircraft/a part has a modification or repair embodied that has not been developed

under the Design Organisation Approval (DOA) Certificate EASA.21J.031 and which

affects the content of the ALS Part 1, the Operator is responsible for obtaining approval

by the relevant Airworthiness Authority for any necessary adaptations of the

airworthiness limitations. For example, Supplemental Type Certificates (STC), which

have been designated by Airbus Corporate Jet Centre (ACJC) or which have been

transferred from former Airbus Deutschland, or other entity, under DOA Certificate

EASA.21J.031 are not considered in this ALS Part 1.

When such an aircraft/a part is transferred from an Owner/Operator to another, the

associated approvals and documents indicating the necessary adaptations of limitations

have to be transferred as well.

5. LIMIT OF VALIDITY (LOV)

A. Landing Gear Safe Life Airworthiness Limitation Items

Main Landing Gear (MLG) LOV

Flight Hours Landings

A330

- 300 series WV000’s & WV010’s

PNR 201252 series (basic) 0 75000 50000

A330

- 200/

- 300 series WV020’s & WV050’s

PNR 201490 series (growth) 0 75000 50000

PNR 10

- 210 series (enhanced) 125000 50000

A330

- 200 series WV060’s

PNR 10

- 210 series (enhanced) 125000 50000

A330

- 200 F series WV000’s

PNR 10

- 210 series (enhanced) 125000 50000 R

R

N

N R

R

R

R

R

R

R

N

N

N

### AIRWORTHINESS LIMITATIONS SECTION

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# A330

Nose Landing Gear (NLG) LOV

Flight Hours Landings

A330

- 300 series WV000’s & WV010’s

PNR D23285 series (basic) 0 75000 50000

PNR D23581 series (reinforced) 0 75000 50000

A330

- 200/

- 300 ser ies WV020’s & WV050’s

PNR D23581 series (reinforced) 0 75000 50000

A330

- 200 series WV 060’s

PNR D23581 series (reinforced) 0 75000 50000

A330

- 200F series WV000’s

PNR D23581 series (reinforced) 125000 50000

Note: Life limitations listed in sub-part 1-3 may exceed the LOV stated above as a result

of a fatigue test carried out for another aircraft application having a greater LOV.

B. Airframe Safe Life Airworthiness Limitation Items

Aircraft series LOV

Flight Hours Flight Cycles

A330

- 200 WV020’s or 0 60000 40000

100000 33000

A330

- 200 WV050’s & WV 060’s 100000 33000

A330

- 200F WV000’s 100000 33000

A330

- 300 WV000’s, WV010’s & WV020’s or 0 60000 40000

100000 33000

A330

- 300 WV050’s 100000 33000

Note: Life limitations applicable to some airframe parts may exceed the airframe LOV.

They may have been set to a greater value to be consistent with the landing gear

LOV, for example.

6. TRANSFERS OF PARTS BETWEEN AIRCRAFT APPLICATIONS

The airworthiness limitation(s) for a part fitted to an application (aircraft type, aircraft model,

weight variant, etc...) may be different when the part is transferred to another application. In

this case, the part’s remaining operational life must be calculated us ing the following

formula:

with:

Tr i = part’s re maining life for operation on current application i.

Ca j = part’s accumulated life on previous application j.

Cp j = part’s airworthiness limitation in previous application j.

Cp i = part’s airworthiness limitation in current application i. R

R

N R

N

N

R

R

R

R

R

R

R

R

R

### AIRWORTHINESS LIMITATIONS SECTION

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# A330

Note 1: When using the above formula, Tr i, Ca j, Cp j, Cp i are expressed in the same usage

parameter (FH or FC or LDG): Usage parameters cannot be mixed in the same

calculation.

Note 2: The remaining life calculation must be reassessed every time the part’s

airworthines s limitation(s) change(s) for current and/or previous aircraft

application(s) to which the part is/was fitted.

7. ASSOCIATED TECHNICAL DOCUMENTATION

PNR provided by sub-parts 1-2 and 1-3 relate to detail parts. They may not all be listed in

Illustrated Parts Catalogue (IPC) issued by Airbus.

For wing structure and landing gear parts manufactured by Airbus, detail PNR are listed in

the relevant Airbus engineering drawings/Component Maintenance Manual manufacturer

(CMMm) issued by Airbus.

For landing gears, detail PNR are listed in the relevant Illustrated Parts List

(IPL)/Component Maintenance Manual (CMM) issued by vendors.

Messier-Dowty SB have been/will be issued to provide information on procurable

replacement PNR, detail PNR and applicable SB:

- Messier-Dowty Ltd Service Bulletin number:

- A33/34- 32

- 85 (main landing gear PRE MOD 43029

– ‘basic’),

- A33/34- 32

- 88 (main landing gear POST MOD 43029

– ‘growth’ or POST

MOD 47487

– ‘growth scallop’),

- A33/34- 32

- 258 (main landing gear POST MOD 54500

– ‘enhanced’).

- Messier-Dowty SA Service Bulletin number:

- D23285- 32

- 040 (nose landing gear). R

R R

R

N

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-0 PAGE: 10

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

8. LANDING GEAR LRUs APPLICABILITY

A. A330- 200 series WV020’s installations

A330

- 201 X X X

A330

- 202 X X X X

A330

- 203 X X X X

A330

- 223 X X X X

A330

- 243 X X X X X X X X

WEIGHT VARIANT 020 021 022 023 024 025 026 027

MTOW 230 230 233 233 202 220 192 220

MLW 180 182 182 180 180 182 180 180

MZFW 168 170 170 168 168 170 168 168

Top assembly PNR

Mai n Landing Gear Main Strut and Dressings

201254 SERIES NOT AUTHORIZED

201489001/002

- xxx X X X X X X X X

201489003/004

- xxx X X X X X X X X

10

- 210501/601

- xxx X X X X X X X X

Main Landing Gear Bogie and Dressings

201274 SERIES NOT AUTHO RIZED

201486001

- xxx X X X X X X X X

201486002

- xxx X X X X X X X X

201486003

- xxx X X X X X X X X

201486004

- xxx X X X X X X X X

10

- 211501

- xxx X X X X X X X X

Main Landing Gear Complete Side Stay

201457 SERIES NOT AUTHORIZED

201484001/002

- xxx X X X X X X X X

10

- 211901/2001

- xxx X X X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-0 PAGE: 11

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

A330

- 201 X X X

A330

- 202 X X X X

A330

- 203 X X X X

A330

- 223 X X X X

A330

- 243 X X X X X X X X

WEIGHT VARIANT 020 021 022 023 024 025 026 027

MTOW 230 230 233 233 202 220 192 220

MLW 180 182 182 180 180 182 180 180

MZFW 168 170 170 168 168 170 168 168

Top assembly PNR

Nose Landing Gear Leg

D23285 SERIES NOT AUTHORIZED

D23581100

- x X X X X X X X X

D23581150

- x X X X X X X X X

Nose Landing Gear Main Fitting

– Shock Absorber Structure

D23286 SERIES NOT AUTHORIZED

D23582100

- x X X X X X X X X

Nose Landing Gear Drag Stay Upper Arm

D23303 SERIES NOT AUTHORIZED

D23444000 X X X X X X X X

Nose Landing Gear Lock Link

D23297000 X X X X X X X X



### Weight variant number allocation (refer to the EASA Type Certificate Data Sheet

– TCDS N°A.004):

WV020: Basic aircraft.

WV021: Aircraft POST MOD 46892 or POST SB A330- 00

- 3019.

WV022: Aircraft POST MOD 47784 or POST SB A330- 00

- 3026.

WV023: Aircraft POST MOD 47888.

WV024: Aircraft POST MOD 49819.

WV025: Aircraft POST MOD 50864 or POST SB A330- 00

- 3028.

WV026: Aircraft POST MOD 51712.

WV027: Aircraft POST MOD 54519.

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-0 PAGE: 12

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

THE ABOVE TABLE INDICATES THE LANDING GEAR LRUs THAT CAN BE INSTALLED FOR EACH

AIRCRAFT MODEL WEIGHT VARIANT BUT IT DOES NOT:

- ENSURE THAT A LRU PNR HAS BEEN VALIDATED FOR A SPECIFIC INDIVIDUAL AIRCRAFT MSN,

- PROVIDE ANY INTERCHANGEABILITY OR MIX POSSIBILITIES.

Refer to Airbus and Messier-Dowty publications (Illustrated Parts Catalogue, Service Bulletins, Component

Maintenance Manuals, etc...) for the applicability of LRUs compared with individual aircraft MSN and for

the interchangeabilities/mixabilities of LRUs.

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 13

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

B. A330- 200 series, WV050’s and WV060’s installations

A330

- 201 X X X X X X X

A330

- 202 X X X X X X X X

A330

- 203 X X X X X X X X

R A330

- 223 X X X X X X X X

A330

- 243 X X X X X X X

R WEIGHT VARIANT 050 051 052 053 054 055 056 059 060 061

R MTOW 230 192 233 210 230 192 233 202 2 20 230

R MLW 180 180 182 180 182 182 180 182 182 182

R MZFW 168 168 170 168 170 170 168 170 170 168

Top assembly PNR

Main Landing Gear Main Strut and Dressings

201254 SERIES NOT AUTHORIZED

201489001/002

- xxx X X X X X X X X

201489003/004

- xxx X X X X X X X X

R 10

- 210501/601

- xxx X X X X X X X X X X

Main Landing Gear Bogie and Dressings

201274 SERIES NOT AUTHORIZED

201486001

- xxx X X X X X X X X

201486002

- xxx X X X X X X X X

201486003

- xxx X X X X X X X X

201486004

- xxx X X X X X X X X

R 10

- 211501

- xxx X X X X X X X X X X

Main Landing Gear Complete Side Stay

201457 SERIES NOT AUTHORIZED

201484001/002

- xxx X X X X X X X X

R 10

- 211901/2001

- xxx X X X X X X X X X X

Nose Landing Gear Le g

D23285 SERIES NOT AUTHORIZED

R D23581100

- x X X X X X X X X X X

R D23581150

- x X X X X X X X X X X 

### R

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 14

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

A330

- 201 X X X X X X X

A330

- 202 X X X X X X X X

A330

- 203 X X X X X X X X

R A330

- 223 X X X X X X X X

A330

- 243 X X X X X X X

R WEIGHT VARIANT 050 051 052 053 054 055 056 059 060 061

R MTOW 230 192 233 210 230 192 233 202 2 20 230

R MLW 180 180 182 180 182 182 180 182 182 182

R MZFW 168 168 170 168 170 170 168 170 170 168

Top assembly PNR

Nose Landing Gear Main Fitting

– Shock Absorber Structure

D23286 SERIES NOT AUTHORIZED

R D23582100

- x X X X X X X X X X X

Nose Landing Gear D rag Stay Upper Arm

D23303 SERIES NOT AUTHORIZED

R D23444000 X X X X X X X X X X

Nose Landing Gear Lock Link

R D23297000 X X X X X X X X X X



### Weight variant number allocation (refer to the EASA Type Certificate Data Sheet

– TCDS N°A.004):

WV050: Aircraft POST MOD 51802.

WV051: Aircraft POST MOD 51803.

WV052: Aircraft POST MOD 51804.

WV053: Aircraft POST MOD 53109.

WV054: Aircraft POST MOD 54106.

WV055: Aircraft POST MOD 54107.

WV056: Aircraft POST MOD 55813.

WV059: Aircraft POST MOD 57439.

WV 060: Aircraft POST MOD 57440.

WV061: Aircraft POST MOD 200561. N

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-0 PAGE: 15

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

THE ABOVE TABLE INDICATES THE LANDING GEAR LRUs THAT CAN BE INSTALLED FOR EACH

AIRCRAFT MODEL WEIGHT VARIANT BUT IT DOES NOT:

- ENSURE THAT A LRU PNR HAS BEEN VALIDATED FOR A SPECIFIC INDIVIDUAL AIRCRAFT MSN,

- PROVIDE ANY INTERCHANGEABILITY OR MIX POSSIBILITIES.

Refer to Airbus and Messier-Dowty publications (Illustrated Parts Catalogue, Service Bulletins, Component

Maintenance Manuals, etc...) for the applicability of LRUs compared with individual aircraft MSN and for

the interchangeabilities/mixabilities of LRUs.

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 16

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

C. A330- 200F series WV000’s installations

N A330

- 223F X X

N A330

- 243F X X

N WEIGHT VARIANT 000 001

N MTOW 233 227

N MLW 182 187

N MZFW 173 178

N Top assembly PNR

N Main Landing Gear Main Strut and Dressings

N 201254 SERIES NOT AUTHORIZED

N 201489 SERIES NOT AUTHORIZED

N 10

- 210501/601

- xxx X X

N Main Landing Gear Bogie a nd Dressings

N 201274 SERIES NOT AUTHORIZED

N 201486 SERIES NOT AUTHORIZED

N 10

- 211501

- xxx X X

N Main Landing Gear Complete Side Stay

N 201457 SERIES NOT AUTHORIZED

N 201484 SERIES NOT AUTHORIZED

N 10

- 211 901/2001

- xxx X X

N Nose Landing Gear Leg

N D23285 SERIES NOT AUTHORIZED

N D23581100

- x X X

N D23581150

- x X X

N Nose Landing Gear Main Fitting

– Shock Absorber Structure

N D23286 SERIES NOT AUTHORIZED

N D23 582100

- x X X

N Nose Landing Gear Drag Stay Upper Arm

N D23303 SERIES NOT AUTHORIZED

N D23444000 X X 

### N

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 17

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

N A330

- 223F X X

N A330

- 243F X X

N WEIGHT VARIANT 000 001

N MTOW 233 227

N MLW 182 187

N MZFW 173 178

N Top assembly PNR

N Nose Landing Gear Lock Link

N D23297000 X X



### Weight variant number allocation (refer to the EASA Type Certificate Data Sheet

– TCDS N°A.004):

WV000: Basic Aircraft POST MOD 200589.

WV001: Aircraft POST MOD 58981.

THE ABOVE TABLE INDICATES THE LANDING GEAR LRUs THAT CAN BE INSTALLED FOR EACH

AIRCRAFT MODEL WEIGHT VARIANT BUT IT DOES NOT:

- ENSURE THAT A LRU PNR HAS BEEN VALIDATED FOR A SPECIFIC INDIVIDUAL AIRCRAFT MSN,

- PROVIDE ANY INTERCHANGEABILITY OR MIX POSSIBILITIES.

Refer to Airbus and Messier-Dowty publications (Illustrated Parts Catalogue, Service Bulletins, Component

Maintenanc e Manuals, etc...) for the applicability of LRUs compared with individual aircraft MSN and for

the interchangeabilities/mixabilities of LRUs. N

N

N

N

N

N

N

N

N

N

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 18

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

D. A330-300 series WV000’s and WV010’s installations

A330

- 301 X X X X X X

A330

- 302

A330

- 303

A330

- 321 X X X X X X X X

A330

- 322 X X X X X X X X

A330

- 323

A330

- 341 X X X X X X X X X

A330

- 342 X X X X X X X X X

A330

- 343

WEIGHT VARIANT 000 001 002 003 004 (*) 010 011 012 013 014

MTOW 212 184 2 12 215 209/215 217 212 218 215 205

MLW 174 174 177 177 182/177 179 177 182 177 182

MZFW 164 164 167 167 172/167 169 167 172 167 172

Top assembly PNR

Main Strut and Dressings

201254001/002

- xxx X X X X X X X X X X

201254003/004

- xxx X X X X X X X X X X

201254005/006

- xxx X X X X X X X X X X

201254007/008

- xxx X X X X X X X X X X

201254009/010

- xxx X X X X X X X X X X

201254011/012

- xxx X X X X X X X X X X

201254013/014

- xxx X X X X X X X X X X

201254015/016

- xxx X X X X X X X X X X

201254017/018

- xxx X X X X X X X X X X

201254021/022

- xxx X X X X X X X X X X

201254023/024

- xxx X X X X X X X X X X

201254025/026

- xxx X X X X X X X X X X

201254027/028

- xxx X X X X X X X X X X

201254029/030

- xxx X X X X X X X X X X

201254031/032

- xxx X X X X X X X X X X 

### R

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 19

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

A330

- 301 X X X X X X

A330

- 302

A330

- 303

A330

- 321 X X X X X X X X

A330

- 322 X X X X X X X X

A330

- 323

A330

- 341 X X X X X X X X X

A330

- 342 X X X X X X X X X

A330

- 343

WEIGHT VARIANT 000 001 002 003 004 (*) 010 011 012 013 014

MTOW 212 184 2 12 215 209/215 217 212 218 215 205

MLW 174 174 177 177 182/177 179 177 182 177 182

MZFW 164 164 167 167 172/167 169 167 172 167 172

Top assembly PNR

201254035/036

- xxx X X X X X X X X X X

201489 SERIES NOT AUTHORIZED

Main Landing Gear Bogie and Dressings

201274001

- xxx X X X X X X X X X X

201274002

- xxx X X X X X X X X X X

201274003

- xxx X X X X X X X X X X

201486001

- xxx NOT AUTHORIZED

201486002

- xxx NOT AUTHORIZED

201486003

- xxx X X X X X X X X X X

201486004

- xxx X X X X X X X X X X

Main Landing Gear Complete Side Stay

201457001/002

- xxx X X X X X X X X X X

201484 SERIES NOT AUTHORI ZED

Nose Landing Gear Leg

D23285001

- xxx X X X X X X X X X X

D23285051

- xxx X X X X X X X X X X

D23285101

- xxx X X X X X X X X X X

D23285151

- xxx X X X X X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 20

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

A330

- 301 X X X X X X

A330

- 302

A330

- 303

A330

- 321 X X X X X X X X

A330

- 322 X X X X X X X X

A330

- 323

A330

- 341 X X X X X X X X X

A330

- 342 X X X X X X X X X

A330

- 343

WEIGHT VARIANT 000 001 002 003 004 (*) 010 011 012 013 014

MTOW 212 184 2 12 215 209/215 217 212 218 215 205

MLW 174 174 177 177 182/177 179 177 182 177 182

MZFW 164 164 167 167 172/167 169 167 172 167 172

Top assembly PNR

D23581100

- x X X X X X X X X X X

D23581150

- x X X X X X X X X X X

Nose La nding Gear Main Fitting

– Shock Absorber Structure

D23286001

- xx X X X X X X X X X X

D23286100

- xx X X X X X X X X X X

D23582100

- x X X X X X X X X X X

Nose Landing Gear Drag Stay Upper Arm

D23303000

- x X X X X X X X X X X

D23444000 X X X X X X X X X X

Nose Landing Gear Lock Link

D23297000 X X X X X X X X X X



### Notes:

(*) WV004: Linear variation between the indicated weights.

Weight variant number allocation (refer to the EASA Type Certificate Data Sheet

– TCDS N°A.004):

WV000: Basic aircraft.

WV001: Aircraft POST MOD 42200.

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 21

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

WV002: Aircraft POST MOD 42600 or POST SB A330- 00 -3003 or, POST MOD 44700 or POST SB A330- 00

- 3006.

WV003: Aircraft POST MOD 44270 or POST SB A330- 00

- 3004.

WV004: Aircraft POST MOD 44849.

WV010: Aircraft POST MOD 43308 or POST SB A330- 00

- 3014.

WV011: Aircraft POST MOD 44803.

WV012: Aircraft POST MOD 45086 or POST SB A330- 00

- 3020.

WV013: Aircraft POST MOD 46688 or POST SB A330- 00

- 3015.

WV014: Aircraft POST MOD 48377 or POST SB A330- 00

- 3024.

THE ABOVE TABLE INDICATES THE LANDING GEAR LRUs THAT CAN BE INSTALLED FOR EACH

AIRCRAFT MODEL WEIGHT VARIANT BUT IT DOES NOT:

- ENSURE THAT A LRU PNR HAS BEEN VALIDATED FOR A SPECIFIC INDIVIDUAL AIRCRAFT MSN,

- PROVIDE ANY INTERCHANGEABILITY OR MIX POSSIBILITIES.

Refer to Airbus and Messier-Dowty publications (Illustrated Parts Catalogue, Service Bulletins, Component

Maintenance Manuals, etc...) for the applicability of LRUs compared with individual aircraft MSN and for

the interchangeabilities/mixabilities of LRUs.

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 22

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

E. A 330

- 300 series WV020’s and WV050’s installations

A330

- 301 X

A330

- 302 X X X

A330

- 303 X X

A330

- 321

A330

- 322

A330

- 323 X X X X X

A330

- 341

A330

- 342 X X

A330

- 343 X X X X X

WEIGHT VARIANT 020 022 024 025 050 051 052 053

MTOW 230 233 205 217 230 212 233 205

MLW 185 187 185 179 185 187 187 185

MZFW 173 175 173 169 173 175 175 173

Top assembly PNR

Main Strut and Dressings

201254 SERI ES NOT AUTHORIZED

201489001/002

- xxx X X X X X X X X

201489003/004

- xxx X X X X X X X X

10

- 210501/601

- xxx X X X X X X X X

Main Landing Gear Bogie and Dressings

201274 SERIES NOT AUTHORIZED

201486001

- xxx X X X X X X X X

2014860 02

- xxx X X X X X X X X

201486003

- xxx X X X X X X X X

201486004

- xxx X X X X X X X X

10

- 211501

- xxx X X X X X X X X

Main Landing Gear Complete Side Stay

201457 SERIES NOT AUTHORIZED

201484001/002

- xxx X X X X X X X X

10

- 211901/2 001

- xxx X X X X X X X X 

### R

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 23

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

A330

- 301 X

A330

- 302 X X X

A330

- 303 X X

A330

- 321

A330

- 322

A330

- 323 X X X X X

A330

- 341

A330

- 342 X X

A330

- 343 X X X X X

WEIGHT VARIANT 020 022 024 025 050 051 052 053

MTOW 230 233 205 217 230 212 233 205

MLW 185 187 185 179 185 187 187 185

MZFW 173 175 173 169 173 175 175 173

Top assembly PNR

Nose Landing Gear Leg

D23285 SERIES NOT AUTHORIZED

D23581100

- x X X X X X X X X

D23581150

- x X X X X X X X X

Nose Landing Gear Main Fitting

– Shock Absorber Structure

D23286 SERIES NOT AUTHORIZED

D23582100

- x X X X X X X X X

Nose Landing Gear Drag Stay Upper Arm

D23303000

- x NOT AUTHORIZED

D23444000 X X X X X X X X

Nose Landing Gear Lock Link

D23297000 X X X X X X X X



### Weight variant number allocation (refer to the EASA Type Certificate Data Sheet

– TCDS N°A.004):

WV020: Aircraft POST MOD 46028.

WV022: Aircraft POST MOD 47785 or POST SB A330- 00 -3023 or, POST MOD 50943 or POST SB A330- 00

- 3039.

WV024: Aircraft POST MOD 48350.

WV025: Aircraft POST MOD 49651.

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-0 PAGE: 24

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

WV050: Aircraft POST MOD 51805 or, POST MOD 53107 or SB A330- 00

- 3036.

WV051: Aircraft POST MOD 51806.

WV052: Aircraft POST MOD 51807 or POST SB A330- 00

- 3035.

WV053: Aircraft POST MOD 52924.

THE ABOVE TABLE INDICATES THE LANDING GEAR LRUs THAT CAN BE INSTALLED FOR EACH

AI RCRAFT MODEL WEIGHT VARIANT BUT IT DOES NOT:

- ENSURE THAT A LRU PNR HAS BEEN VALIDATED FOR A SPECIFIC INDIVIDUAL AIRCRAFT MSN,

- PROVIDE ANY INTERCHANGEABILITY OR MIX POSSIBILITIES.

Refer to Airbus and Messier-Dowty publications (Illustrated Parts Catalogue, Service Bulletins, Component

Maintenance Manuals, etc...) for the applicability of LRUs compared with individual aircraft MSN and for

the interchangeabilities/mixabilities of LRUs.

END OF SUB

- PART 1

- 0

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 1

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A 3 3 0

Sub-part 1-1 ILLUSTRATIONS

(*) Location, Item not illustrated.



### MAIN LANDING GEAR - FIG. 01 Brake rod pin

(x2) (*) Lower torque

link

Lower torque

link pin Torque link

apex pin nut

Wheel axle

(x2)

Bogie beam

pivot pin (*)

Brake rod

(x4) Main fitting

Bogie beam Upper torque

link pin

Upper torque

link

Torque link

apex pin Complete

side stay

FWD FWD

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 2

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A 3 3 0

MAIN LANDING GEAR - FIG. 02 Aft pintle pin Aft pintle

bearing

Aft pintle pin

nut Forward pintle pin

lock bolt Main fitting Forward pintle pin FWD

FWD

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 3

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A3 3 0

(*) Location, item not illustrated on 3D view.



### MAIN LANDING GEAR - FIG. 03 Adjustable

link

Bellcrank

(subassembly)

Shortening

link (upper)

Pin SM8 (*)

Shortening

link (lower)

Pin SM9 (*)

Upper piston Pin SM7 (*) Bellcrank link

FWD FWD

Main fitting Connecting

link (SM)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 4

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A3 3 0

MAIN LANDING GEAR - FIG. 04 Upper piston

Upper gland

housing

Recoil nut

Sliding piston

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 5

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A3 3 0

MAIN LANDING GEAR - FIG. 05 Side stay

upper pin Upper cardan

pin

Side stay

center pin

Lower side

stay

Lower cardan

nut Side stay

lower pin Lock link

(subassembly)

Lower cardan

pin

Pivot link

bracket

Pivot link

center pin

Lock link/Side

stay pin Lower spring

bracket Spring bracket

lower bolt Upper spring

bracket Pivot link bracket

bolts (x4) Upper cardan

nut

Upper side

stay

Spring bracket

upper bolts (x3)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 6

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A3 3 0

MAIN LANDING GEAR - FIG. 06 Lock link

upper pin Cardan link

Pivot link Upper lock

link

Lock link

center pin

Connecting link/Lock

link/Upper spring pin

Connecting

link Landing gear

safety pin

Connecting

link/Pivot link pin

Lower spring/Pivot

link pin Lower lock

link Cardan link

pin

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 7

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A3 3 0

NOSE LANDING GEAR - FIG. 07 Drag stay

upper pin

Lock link

upper arm

Drag stay

upper arm Lock link

center pin

Main fitting

Drag stay

lower arm

Drag stay

upper pin

Pintle pin Drag stay lower

arm/Main fitting pin

Upper torque

link pin

Sliding tube Torque link

apex pin

Upper flange Lock link

lower arm

Lower torque

link pin Lower torque

link Upper torque

link

Main fitting Drag stay center

pin (x2) Lock link upper arm/

Main fitting pin

Main fitting hinge

pin (x2)

Turning

sleeve

Airframe FWD

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 28/10 ALS PART 1-1 PAGE: 8

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A3 3 0

WING STRUCTURE - FIG. 08

END OF SUB-PART 1-1 Retraction

jack fitting

Gear support

rib Forward

pintle fitting Side stay

fitting

FWD

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 1

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Sub-part 1-2 LIFE LIMITS

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

ATA 32

- 11

- 00 MAIN LANDING GEAR (FIG. 01 to 06)

MAIN STRUT AND DRESSINGS ( FIG. 01 & 02)

(1) Embodime nt of MOD 46902/SB A330

- 32

- 3096 introduces a different PNR. MOD 46902 factory embodied on original landing gear of MSN 271 and subsequent.

(2) Embodiment of MOD 46903/SB A330

- 32

- 3096 introduces a different PNR. MOD 46903 factory embodied on original land ing gear of MSN 271 and subsequent.

(3) Embodiment of MOD 46904/SB A330

- 32

- 3095 introduces a different PNR. MOD 46904 factory embodied on original landing gear of MSN 271 and subsequent.

(4) Parts that have been installed on any A330

- 300 series aircraf t must not be fitted to any A340 aircraft models.

(5) These minimum general life limits can be increased depending on individual aircraft utilisation: Refer to OIT 999.0022/03/CL dated 20

- Feb

- 2003.

Forward pintle pin 201275616 (2) 50000 13000 10 Ye X X

201428608 (2) 50000 13000 10 Ye X X

201489623 (2) 75000 50000 10 Ye X X

75000 37600 10 Ye X X X

Upper torque link pin 201269626 (1) (5) 47425 23780 10 Ye X X

201489600 (1) 60000 19700 10 Ye X X

60000 1 2100 10 Ye X X X

Upper torque link 201254349 (4) 42650 14350 10 Ye X X

201269308 (4) 42650 14350 10 Ye X X

201428303 (4) 42650 14350 10 Ye X X

201489303 57000 13200 N/A X X

48000 12200 N/A X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 2

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Lower torque link 201254350 (4) 42650 14350 10 Ye X X

201269309 (4) 42650 14350 10 Ye X X

201428304 (4) 42650 14350 10 Ye X X

201489304 57000 13200 N/A X X

48000 12200 N/A X X X

Lower torque link pin 2012696 31 (1) (5) 26240 12570 10 Ye X X

201489601 (1) 60000 14300 10 Ye X X

50000 9000 10 Ye X X X

Bogie beam pivot pin 201269612 (3) 6250 4500 5 Ye X X

201489621 (3) 19000 4000 5 Ye X X

19000 3800 5 Ye X X X

MAIN STRUT (FIG. 01 to 03)

(1) Embodiment of MOD 46904/SB A330

- 32

- 3095 introduces a different PNR. MOD 46904 factory embodied on original landing gear of MSN 271 and subsequent.

(2) Parts that have been installed on any A330

- 300 series aircraft must no t be fitted to any A340 aircraft models.

(3) Rework in accordance with SB A330

- 32

- 3053/VSB A33/34

- 32

- 90 (MOD 45480) introduces a different PNR.

(4) Rework in accordance with VSB A33/34

- 32

- 82 (MOD 45479) introduces a different PNR.

(5) Both FH and LDG limits apply from the time the part was reworked in accordance with VSB A33/34

- 32

- 82. Nevertheless, the sum of the accumulated lives PRE

and POST VSB A33/34

- 32

- 82 must not exceed the applicable LOV defined in sub

- part 1

- 0 paragraph 5.

(6) Rework in acco rdance with SB A330

- 32

- 3215/VSB A33/34

- 32

- 257 (MOD 56498) introduces a different PNR.

(7) These limits apply to parts identified as ‘S1’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(8) These limits apply to parts identifi ed as ‘S3’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(9) These limits apply to parts on which SB A330

- 32

- 3215/VSB A33/34

- 32

- 257 (MOD 56498) has been performed at or before accumulation of 8750 LDG.

.../...

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 3

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

(10) These limi ts apply to parts on which SB A330

- 32

- 3215/VSB A33/34

- 32

- 257 (MOD 56498) has been performed after accumulation of 8750 LDG.

(11) These limits apply to parts identified as ‘S2C’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(12) These limits apply to parts on which SB A330

- 32

- 3215/VSB A33/34

- 32

- 257 (MOD 56498) has been performed at or before accumulation of 1840 LDG.

(13) These limits apply to parts on which SB A330

- 32

- 3215/VSB A33/34

- 32

- 257 (MOD 56498) has been performed a fter accumulation of 1840 LDG.

(14) These limits apply to parts NOT identified in notes (7), (8) and (11) above.

(15) These limitations apply to parts on which SB A330

- 32

- 3215/VSB A33/34

- 32

- 257 (MOD 56498) has been performed at or before accumulation o f 14000 LDG.

(16) These limits apply to parts on which SB A330

- 32

- 3215/VSB A33/34

- 32

- 257 (MOD 56498) has been performed after accumulation of 14000 LDG.

Main fitting (LH) 201428311 (2) 42650 14350 10 Ye X X

201428349 (2) 42650 14350 10 Ye X X

201428363 (2) 42650 14350 10 Ye X X

201428371 (2) 42650 14350 10 Ye X X

201428373 (2) 42650 14350 10 Ye X X

201488301 (6) 53000 22000 N/A X X

44500 22000 N/A X X X

201488318 (6) 75000 22000 N/A X X X X X X X

201488320 (6) 75000 22000 N/A X X X X X

201488322 (6) 53000 22000 N/A X X

.../... 44500 22000 N/A X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 4

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Main fitting (LH)

201488324 (6) 46870 13750 N/A X (7) X (7) X ( 7) X (7) X (7) X (7) X (7)

36000 11920 N/A X (8) X (8)

57000 16685 N/A X (8) X (8)

51000 16500 N/A X (8) X (8) X (8)

9860 2890 31

- Mar

- 09 X (11) X (11) X (11) X (11) X (11) X (11) X (11)

75000 22000 N/A X (14) X (14) X (14) X (14) X (14) X (14) X (14)

201488326 (6) 75000 22000 N/A X X X X X

201488329 75000 37600 N/A X (15) X (15) X (15) X (15) X (15)

75000 22000 N/A X (16) X (16) X (16) X (16) X (16)

201488331 75000 37600 N/A X (15) X (15) X (15) X (15) X (15)

75000 22000 N/A X (16) X (16) X (16) X (16) X (16)

201488333 75000 28000 N/A X (15) X (15)

75000 37600 N/A X (15) X (15) X (15) X (15) X (15)

.../... 75000 22000 N/A X (16) X (16) X (16) X (16) X (16) X (16) X (16)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 5

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Main fitting (LH)

201488335 46870 17500 N/A X (7) (9) X (7) (9)

46870 23500 N/A X (7) (9) X (7) (9) X (7) (9) X (7) (9) X ( 7) (9)

46870 13750 N/A X (7) (10) X (7) (10) X (7) (10) X (7) (10) X (7) (10) X (7) (10) X (7) (10)

36000 11920 N/A X (8) (9) X (8) (9)

57000 16685 N/A X (8) (9) X (8) (9)

51000 16500 N/A X (8) (9) X (8) (9) X (8) (9)

36000 11920 N/A X (8) (10) X (8) (10)

57000 16685 N/A X (8) (10) X (8) (10)

51000 16500 N/A X (8) (10) X (8) (10) X (8) (10)

9860 3680 31

- Mar

- 09 X (11) (12) X (11) (12)

9860 4945 31

- Mar

- 09 X (11) (12) X (11) (12) X (11) (12) X (11) (12) X (11) (12)

9860 2890 31

- Mar

- 09 X (11) (13) X (11) (13) X (11) (13) X (11) (13) X (11) (13) X (11) (13) X (11) (13)

75000 28000 N/A X (14) (15) X (14) (15)

75000 37600 N/A X (14) (15) X (14) (15) X (14) (15) X ( 14) (15) X (14) (15)

75000 22000 N/A X (14) (16) X (14) (16) X (14) (16) X (14) (16) X (14) (16) X (14) (16) X (14) (16)

201488337 53000 35000 N/A X (15) X (15)

44500 29200 N/A X (15) X (15) X (15)

53000 22000 N/A X (16) X (16)

.../... 44500 22000 N/A X (16) X (16) X (16)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 6

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Main fitting (LH)

201488339 53000 35000 N/A X (15) X (15)

44500 29200 N/A X (15) X (15) X (15)

53000 22000 N/A X (16) X (16)

4 4500 22000 N/A X (16) X (16) X (16)

Main fitting (RH) 201428312 (2) 42650 14350 10 Ye X X

201428350 (2) 42650 14350 10 Ye X X

201428364 (2) 42650 14350 10 Ye X X

201428372 (2) 42650 14350 10 Ye X X

201428374 (2) 4 2650 14350 10 Ye X X

201488300 (6) 53000 22000 N/A X X

44500 22000 N/A X X X

201488319 (6) 75000 22000 N/A X X X X X X X

201488321 (6) 75000 22000 N/A X X X X X

201488323 (6) 53000 22000 N/A X X

44500 22000 N/ A X X X

201488325 (6) 46870 13750 N/A X (7) X (7) X (7) X (7) X (7) X (7) X (7)

36000 11920 N/A X (8) X (8)

57000 16685 N/A X (8) X (8)

51000 16500 N/A X (8) X (8) X (8)

9860 2890 31

- Mar

- 09 X (11) X (11) X (11) X (11) X (11) X (11) X (11)

75000 22000 N/A X (14) X (14) X (14) X (14) X (14) X (14) X (14)

.../... 201488327 (6) 75000 22000 N/A X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 7

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Main fitting (RH)

201488330 75000 37600 N/A X (15) X (15) X (15) X (15) X (15)

75000 22000 N/A X (16) X (16) X (16) X (16) X (16)

201488332 75000 37600 N/A X (15) X (15) X (15) X (15) X (15)

75000 22000 N/A X (16) X (16) X (16) X (16) X (16)

201488334 75000 28000 N/A X (15) X (15)

75000 37600 N/A X (15) X (15) X (15) X (15) X (15)

75000 22000 N/A X (16) X (16) X (16) X (16) X (16) X (16) X (16)

201488336 46870 17500 N/A X (7) (9) X (7) (9)

46870 23500 N/A X (7) (9) X (7) (9) X (7) (9) X (7) (9) X (7) (9)

46870 13750 N/A X (7) (10) X (7) (10) X (7) (1 0) X (7) (10) X (7) (10) X (7) (10) X (7) (10)

36000 11920 N/A X (8) (9) X (8) (9)

57000 16685 N/A X (8) (9) X (8) (9)

51000 16500 N/A X (8) (9) X (8) (9) X (8) (9)

36000 11920 N/A X (8) (10) X (8) (10)

57000 1668 5 N/A X (8) (10) X (8) (10)

51000 16500 N/A X (8) (10) X (8) (10) X (8) (10)

9860 3680 31

- Mar

- 09 X (11) (12) X (11) (12)

9860 4945 31

- Mar

- 09 X (11) (12) X (11) (12) X (11) (12) X (11) (12) X (11) (12)

9860 2890 31

- Mar

- 09 X (11) (13) X (11) (13) X (11) (13) X (11) (13) X (11) (13) X (11) (13) X (11) (13)

75000 28000 N/A X (14) (15) X (14) (15)

75000 37600 N/A X (14) (15) X (14) (15) X (14) (15) X (14) (15) X (14) (15)

.../... 75000 22000 N/A X (14) (16) X (14) (16) X (14) (16) X (14) (16) X (14) (16) X (14) (16) X (14) (16)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 8

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Main fitting (RH)

201488338 53000 35000 N/A X (15) X (15)

44500 29200 N/A X (15) X (15) X (15)

53000 22000 N/A X (16) X (16)

44500 22000 N/A X (16) X (16) X (16)

201488340 53000 35000 N/A X (15) X (15)

44500 29200 N/A X (15) X (15) X (15)

53000 22000 N/A X (16) X (16)

44500 22000 N/A X (16) X (16) X (16)

Aft pintle bearing 201042273 40000 14000 N/A X X

Pin SM7 201428650 (1) 6250 4500 5 Ye X X

201488610 (1) 19000 4000 5 Ye X X

19000 3800 5 Ye X X X

Shortening link (upper) 201428317 (3) 26500 10000 N/A X X

Pin SM8 201275789 (1) 6250 4500 5 Ye X X

201488607 (1) 19000 4000 5 Ye X X

19000 3800 5 Ye X X X

Shortening link (lower) 201428328 (4) 26500 10000 N/A X X

201478309 (5) 41750 13900 N/A X X

Pin SM9 201275790 (1) 6250 4500 5 Ye X X

201488606 (1) 19000 4000 5 Ye X X

19000 3800 5 Ye X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 9

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

SHOCK STRUT (FIG. 03 & 04)

(1) The 10

- year limit applies to parts that have been operated on any A330 before 31

- Oct

- 1998, regardless of subsequent applications they have been fitted to.

(2) Rework in accord ance with SB A330

- 32

- 3204/VSB A33/34

- 32

- 233 or VSB A33/34

- 32

- 234 (MOD 55801) introduces a different PNR.

(3) These limits apply to parts identified as ‘S1’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(4) These limits appl y to parts NOT identified in note (3) above.

Upper piston 201270311 75000 47390 N/A X X

201270312 75000 47390 N/A X X

201270318 75000 47390 N/A X X

201270320 75000 47390 N/A X X

201270322 75000 47390 N/A X X

2 01270324 75000 47390 N/A X X

Sliding piston 201270304 (1) 42600 14350 10 Ye X X

201270305 (1) 42600 14350 10 Ye X X

201270313 (1) 42600 14350 10 Ye X X

201270315 (1) 42600 14350 10 Ye X X

201270316 (1) 42600 1435 0 10 Ye X X

201270323 (1) 42600 14350 10 Ye X X

201487300 (2) 36900 12200 N/A X X

67500 18900 N/A X X

.../... 62100 15300 N/A X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 10

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Sliding piston

201487307 (2) 23060 7625 N/A X (3) X (3)

42180 11810 N/A X (3) X (3)

38810 9560 N/A X (3) X (3) X (3)

36900 12200 N/A X (4) X (4)

67500 18900 N/A X (4) X (4)

62100 15300 N/A X (4) X (4) X (4)

BOGIE AND DRESSINGS (FIG. 01)

BOGIE ASSEMB LY (FIG. 01)

(1) These limits apply to parts identified as ‘S2A’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(2) These limits apply to parts identified as ‘S2B’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, date d 31

- Jul

- 2009.

(3) These limits apply to parts identified as ‘S2C’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(4) These limits apply to parts NOT identified in notes (1), (2) and (3) above.

Bogie beam

201272304 42610 2 8405 N/A X (1) X (1) X (1) X (1) X (1) X (1) X (1)

12710 8470 N/A X (2) X (2) X (2) X (2) X (2) X (2) X (2)

9860 6575 31

- Mar

- 09 X (3) X (3) X (3) X (3) X (3) X (3) X (3)

75000 50000 N/A X (4) X (4) X (4) X (4) X (4) X (4) X (4)

N

20127230 7 42610 28405 N/A X (1) X (1) X (1) X (1) X (1) X (1) X (1)

N 12710 8470 N/A X (2) X (2) X (2) X (2) X (2) X (2) X (2)

N 9860 6575 31

- Mar

- 09 X (3) X (3) X (3) X (3) X (3) X (3) X (3)

N .../... 75000 50000 N/A X (4) X (4) X (4) X (4) X (4) X (4) X ( 4)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 11

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Bogie beam

50

- 2117002

- 00 69520 25340 N/A X (1) X (1)

54710 25340 N/A X (1) X (1) X (1)

N 42610 17045 N/A X (1)

20740 7555 N/A X (2) X (2)

16320 7555 N/A X (2) X (2) X (2)

N 1 2710 5080 N/A X (2)

R 9860 3945 31

- Mar

- 09 X (3) X (3) X (3) X (3) X (3) X (3)

122300 44600 N/A X (4) X (4)

96300 44600 N/A X (4) X (4) X (4)

N 75000 30000 N/A X (4)

N

50

- 2117002

- 01 69520 25340 N/A X (1) X (1)

N 54710 25340 N/A X (1) X (1) X (1)

N 42610 17045 N/A X (1)

N 20740 7555 N/A X (2) X (2)

N 16320 7555 N/A X (2) X (2) X (2)

N 12710 5080 N/A X (2)

N 9860 3945 31

- Mar

- 09 X (3) X (3) X (3) X (3) X (3) X (3)

N 122300 44600 N/A X (4) X (4)

N 96300 44600 N/A X (4) X (4) X (4)

N 75000 30000 N/A X (4)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 12

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

COMPLETE SIDE STAY (FIG. 01, 05 & 06)

(BASIC) SIDE STAY (FIG. 05)

(1) Must be replaced by a new on e every time it is removed from upper side stay PNR 201458301 PRE MOD 42735 (VSB A33/34

- 32

- 23) but no later than 10400

LDG since its installation.

Spring bracket upper

bolt NAS6606D13 N/A (1) N/A X X

LOCK LINK (FIG. 06)

Lower lock link 201482 300 N/A 35500 N/A X X X X X

201482305 N/A 35500 N/A X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-2 PAGE: 13

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the

assy title. LIFE LIMITS (*) LIFE LIMITS APPLICABILITY

R

Nomenclat ure Part Number FH LDG Cal. A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

ATA 32

- 21

- 00 NOSE LANDING GEAR (FIG. 07)

NOSE LANDING GEAR LEG (FIG. 07)

MAIN FITTING

- SHOCK ABSORBER STRUCTURE (FIG. 07)

Drag stay lower

arm/Main fitting pin D64007 46400 30950 N/A X X

54700 36475 N/A X X X X X

Lower torque link D62721 17535 8000 N/A X X



### END OF SUB

- PART 1

- 2

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 1

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Sub part 1-3 DEMONSTRATED FATIGUE LIVES

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

ATA 32

- 11

- 00 MAIN LANDING GEAR (FIG. 01 to 06)

R (1) ‘xx’ at the end of the PNR stands for any number between 00 and 99

, including unused digits

.

(2) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(3) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330

- 32

- 3212 (POST MOD 56214).

(4) These limitations apply to parts fitted to aircraft PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(5) These limitations apply to parts fitted to aircraft POST SB A330

- 32

- 3212 (POST MOD 56214).

Aft pintle pin (LH) (1)

F32150058000xx 75000 50000 X X

100000 33000 X X

F32155011000xx 75000 50000 X (4) X (2) X X (2) X X (4) X (2)

100000 33000 X (4) X (2) X X (2) X X (4) X (2)

125000 50000 X (5) X (3) X (3) X (5) X (3)

F3 2155021000xx 75000 50000 X (4) X (2) X X (2) X X (4) X (2)

100000 33000 X (4) X (2) X X (2) X X (4) X (2)

R 125000 50000 X X (5) X (3) X (3) X (5) X (3)

Aft pintle pin (RH) (1)

F32150058001xx 75000 50000 X X

100000 33000 X X

F32155011001xx 75000 50000 X (4) X (2) X X (2) X X (4) X (2)

100000 33000 X (4) X (2) X X (2) X X (4) X (2)

125000 50000 X (5) X (3) X (3) X (5) X (3)

F32155021001xx 75000 50000 X (4) X (2) X X (2) X X (4) X (2)

100000 33000 X (4) X (2) X X (2) X X (4) X (2)

R 125000 50000 X X (5) X (3) X (3) X (5) X (3)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 2

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

R Aft pintle pin nut

SLN40789 M130X2R 75000 50000 X X

100000 33000 X X

R SLN40874 M130X2R 75000 50000 X X

100000 33000 X X

SLN40 927 75000 50000 X (4) X (2) X X (2) X X (4) X (2)

100000 33000 X (4) X (2) X X (2) X X (4) X (2)

R 125000 50000 X X (5) X (3) X (3) X (5) X (3)

SLN41180 75000 50000 X (4) X (2) X X (2) X X (4) X (2)

100000 33000 X (4) X (2) X X (2) X X (4) X (2)

R 125000 50000 X X (5) X (3) X (3) X (5) X (3)

MAIN STRUT AND DRESSINGS (FIG. 01 & 02)

Forward pintle pin 201478611 75000 27000 X X

201478620 75000 27000 X X

201489752 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2105042

- 00 75000 30000 X X X X X X

Forward pintle pin lock bolt

201275895 75000 27000 X X

50000 35000 X X

.../... 44000 28000 X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 3

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Forward pintle pin lock bolt

201589601 75000 27000 X X

50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2105058

- 00 75000 30000 X X X X X X

Upper torque link pin 201254926 40000 14 000 X X

201489753 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X X X

R 55

- 2105055

- 00 75000 30000 X X X X X X

Upper torque link

201676300 75000 50000 X X

75000 46950 X X X X X

R 50

- 2105021

- 00 75000 30000 X X X X X X

Torque link apex pin 201269624 75000 27000 X X

201489602 50000 35000 X X

44000 28000 X X X

201676600 75000 27000 X X

50000 35000 X X

75000 32500 X X

4400 0 28000 X X X

75000 26000 X X X

R 55

- 2105054

- 00 75000 30000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 4

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Torque link apex pin nut

201269656 75000 27000 X X

50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

201269699 75000 27000 X X

50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2105072

- 00 75000 30000 X X X X X X

Lower torque link

201676301 75000 50000 X X

75000 46950 X X X X X

R 50

- 2105020

- 00 75000 30000 X X X X X X

Lower torque link pin 201254927 42000 14400 X X

201489754 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X X X

R 55

- 2105056

- 00 75000 30000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 5

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Bogie beam pivot pin 201254925 75000 27000 X X

201489751 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2105029

- 0 0 75000 30000 X X X X X X

Brake rod pin 201269636 75000 27000 X X

201489619 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2105091

- 00 75000 30000 X X X X X X

Brake rod

201254352 75000 43300 X X

75000 50000 X X

75000 49650 X X X

201269304 75000 43300 X X

201490300 75000 50000 X X

75000 49650 X X X

R 50

- 2105025

- 00 75000 30000 X X X X X X

MAIN STRUT (FIG. 01 to 03)

(1) Th ese limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(2) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330

- 32

- 3212 (POST MOD 56214).

(3) These limitations apply to par ts fitted to aircraft PRE SB A330

- 32

- 3212 (PRE MOD 56214).

.../...

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 6

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

(4) These limitations apply to parts fitted to aircraft POST SB A330

- 32

- 3212 (POST MOD 56214).

(5) These limitations apply to parts identified as ‘S1’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(6) These limitations apply to parts identified as ‘S3’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(7) These limitations apply to parts NOT identified in notes (5) and (6) above.

Main fitting (LH)

201488341 75000 28000 X X

75000 37600 X X X X X

R

50

- 2107001

- 00 46870 18750 X (5) X (5) X (5) X (5) X (5) X (5)

R 75000 30000 X (6) X (6) X (6) X (6) X (6) X (6)

R 75000 30000 X (7) X (7) X (7) X (7) X (7) X (7)

Main fitting (RH)

201488342 75000 28000 X X

75000 37600 X X X X X

R

50

- 2108001

- 00 46870 18750 X (5) X (5) X (5) X (5) X (5) X (5)

R 75000 30000 X (6) X (6) X (6) X (6) X (6) X (6)

R 75000 30000 X (7) X (7) X (7) X (7) X (7) X (7)

Aft pintle bearing

201042565 75000 27000 X X

50000 35000 X (3) X (1)

75000 32500 X (3) X (1)

44000 28000 X (1) X (3) X (1)

75000 26000 X (1) X (3) X (1)

R .../... 75000 30000 X X (4) X (2) X (2) X (4) X (2)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 7

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Aft pintle bearing

450250952 75000 27000 X X

50000 35000 X (3) X (1)

75000 32500 X (3) X (1)

44000 28000 X (1) X (3) X (1)

75000 26000 X (1) X (3) X (1)

450250953 75000 27000 X X

50000 35000 X (3) X (1)

75000 32500 X (3) X (1)

44000 28000 X (1) X (3) X (1)

75000 26000 X (1) X (3) X (1)

450250954 75000 27000 X X

50000 35000 X (3) X (1)

75 000 32500 X (3) X (1)

44000 28000 X (1) X (3) X (1)

75000 26000 X (1) X (3) X (1)

450250955 75000 27000 X X

50000 35000 X (3) X (1)

75000 32500 X (3) X (1)

44000 28000 X (1) X (3) X (1)

.../..

. 75000 26000 X (1) X (3) X (1)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 8

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Aft pintle bearing

450250956 75000 27000 X X

50000 35000 X (3) X (1)

75000 32500 X (3) X (1)

44000 28000 X (1) X (3) X (1)

75000 26000 X (1) X (3) X (1)

450250957 75000 27000 X X

50000 35000 X (3) X (1)

75000 32500 X (3) X (1)

44000 28000 X (1) X (3) X (1)

75000 26000 X (1) X (3) X (1)

Pin SM7 201478618 75000 50000 X X

201478635 75000 50000 X X

201488652 75000 50000 X X X X X

201488685 75000 50000 X X X X X

R 55

- 2107009

- 00 75000 30000 X X X X X X

Shortening link (upper) 201428359 75000 50000 X X

201428375 75000 50000 X X

2 01428376 75000 50000 X X

201478310 75000 50000 X X

201488302 75000 50000 X X

70000 50000 X X X

.../... 75000 40000 X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 9

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Shortening link (upper)

201488328 75000 50000 X X

70000 50 000 X X X

75000 40000 X X X

R 50

- 2107003

- 00 75000 30000 X X X X X X

Pin SM8 201478617 69300 50000 X X

201478646 75000 50000 X X

201488651 75000 50000 X X X X X

201488690 75000 50000 X X X X X

201488707 7500 0 50000 X X X X X

R 55

- 2107008

- 00 75000 30000 X X X X X X

Shortening link (lower) 201428345 75000 50000 X X

201488304 75000 50000 X X

64800 50000 X X X

75000 39000 X X X

R 50

- 2107002

- 00 75000 30000 X X X X X X

Pin SM9 201478616 75000 50000 X X

201478643 75000 50000 X X

201488650 75000 50000 X X X X X

201488691 75000 50000 X X X X X

201488699 75000 50000 X X X X X

R 55

- 2107007

- 00 75000 30000 X X X X X X

R 55

- 2107093

- 00 750 00 30000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 10

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

SHOCK STRUT (FIG. 03 & 04)

(1) These limitations apply to parts identified as ‘S1’ in Messier

- Dowty Service Letter A33

- 34 A20 revision 05, dated 31

- Jul

- 2009.

(2) These limitations apply to parts NO T identified in note (1) above.

Upper piston 201487301 75000 50000 X X X X X

201487304 75000 50000 X X X X X

201487306 75000 50000 X X X X X

201496300 75000 50000 X X X X X

201496301 75000 50000 X X X X X

201496302 75000 500 00 X X X X X

R 50

- 2109002

- 00 75000 30000 X X X X X X

Recoil nut

201270730 N/A 50000 X X

N/A 35000 X X

N/A 28000 X X X

201411604 N/A 50000 X X

N/A 35000 X X

N/A 28000 X X X

R 50

- 2109008

- 00 N/A 30700 X X X X X X

Sliding piston

201487308 75000 35900 X X

75000 50000 X X X X X

201487309 46870 22430 X (1) X (1)

46870 31250 X (1) X (1) X (1) X (1) X (1)

75000 35900 X (2) X (2)

.../... 75000 50000 X (2) X (2) X (2) X (2) X (2)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 11

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Sliding piston

201487310 75000 35900 X X

75000 50000 X X X X X

R

50

- 2109001

- 01 46870 18750 X (1) X (1) X (1) X (1) X (1) X (1)

R 75000 30000 X (2) X (2) X (2) X (2) X (2) X (2)

BOGIE AND DRESSING S (FIG. 01)

BOGIE ASSEMBLY (FIG. 01)

Bogie beam 201272300 63500 26000 X X

201272302 75000 50000 X X X X X X X

N 201272305 63500 26000 X X

N 201272306 75000 50000 X X X X X X X

201485300 75000 50000 X X X X X

N 201485301 7 5000 50000 X X X X X

Wheel axle 201272638 75000 40200 X X

201272644 75000 40200 X X

75000 50000 X X

75000 44500 X X X

201272649 75000 40200 X X

75000 50000 X X

75000 44500 X X X

20148560 1 75000 50000 X X

75000 44500 X X X

201485615 75000 50000 X X

75000 44500 X X X

R 55

- 2117003

- 00 75000 30000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 12

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

COMPLETE SIDE STAY (FIG. 01, 05 & 06)

(1) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(2) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330

- 32

- 3212 (POST MOD 56214).

(3) These limitations apply to parts fitted to aircraft PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(4) These limitations apply to parts fitted to aircraft POST SB A330

- 32

- 3212 (POST MOD 56214).

(5) Must be replaced by a new one every time it is removed from the upper side stay.

Pivot link center pin

201442614 N/A 50000 X X

N/A 3 5500 X X X X X

201442651 N/A 35500 X (3) X (1) X (1) X (3) X (1)

R N/A 50000 X X (4) X (2) X X (2) X X (4) X (2)

Pivot link bracket

201441605 N/A 50000 X X

N/A 35500 X X X X X

201457607 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 2119008

- 00 N/A 50000 X X X X X X

R Pivot link bracket bolt NAS6606D10 N/A (5) X X X X X X X X

Lock link/Side stay pin 201268618 N/A 50000 X X

201482609 N/A 35500 X (3) X (1) X (1) X (3) X (1)

R N/A 50000 X X (4) X (2) X ( 2) X (4) X (2)

(BASIC) SIDE STAY (FIG. 05)

(1) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(2) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330

- 32

- 321 2 (POST MOD 56214).

(3) These limitations apply to parts fitted to aircraft PRE SB A330

- 32

- 3212 (PRE MOD 56214).

.../...

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 13

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

(4) These limitations apply to parts fitted to aircraft POST SB A330

- 32

- 3212 (POST MOD 56214).

(5) Must be replaced by a new one ev ery time it is removed from the upper side stay.

Upper cardan nut

201267639 75000 27000 X X

50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

201267642 75000 27000 X X

50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 1221042

- 01 75000 30000 X X X X X X

Upper cardan pin 201267600 75000 27000 X X

201483600 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2121003

- 00 75000 30000 X X X X X X

Side stay upper pin 201267602 75000 27000 X X

201483602 50000 35000 X X

75000 32500 X X

44000 28000 X X X

.../... 75000 26000 X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 14

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

R Side stay upper pin 55

- 2121005

- 00 75000 30000 X X X X X X

Upper side stay 201458301 75000 27000 X X

201483301 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 50

- 2121001

- 00 75000 30000 X X X X X X

Upper spring bracket

201441602 N/A 50000 X X

N/A 35500 X X X X X

201483636 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 1221012

- 01 N/A 50000 X X X X X X

Lower spring bracket

201441604 N/A 50000 X X

N/A 35500 X X X X X

201458611 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 1221026

- 01 N/A 50000 X X X X X X

R Spring bracket upper bolt MS21250H06016 N/A (5) X X X X X X X X

Spring bracket lower bolt

201441607 N/A 50000 X X

N/A 35500 X X X X X

201458612 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 1221029

- 01 N/A 50000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 15

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Side stay center pin 201267605 75000 27000 X X

201483605 50000 35000 X (3) X (1)

75000 32500 X (3) X (1)

R 75000 30000 X X (4) X (2) X (2) X (4) X (2)

44000 28000 X (1) X (3) X (1)

75000 26000 X (1) X (3) X (1)

Lower side stay 201267620 75000 27000 X X

201483606 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2121002

- 00 75000 30000 X X X X X X

Side stay lower pin 201267635 75000 27000 X X

201483609 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2121007

- 00 125000 50000 X X X X X X

Lower cardan pin 201267304 53500 50000 X X

201483304 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 50

- 2121004

- 00 75000 30000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 16

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Lower cardan nut 201267640 75000 27000 X X

201267643 75000 27000 X X

201483621 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

201483635 50000 35000 X X

75000 32500 X X

44000 28000 X X X

75000 26000 X X X

R 55

- 2121009

- 00 75000 30000 X X X X X X

LOCK LINK (FIG. 06)

(1) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(2 ) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330

- 32

- 3212 (POST MOD 56214).

(3) These limitations apply to parts fitted to aircraft PRE SB A330

- 32

- 3212 (PRE MOD 56214).

(4) These limitations apply to parts fitted to a ircraft POST SB A330

- 32

- 3212 (POST MOD 56214).

Cardan link pin

201442618 N/A 35500 X (3) X (1) X (1) X (3) X (1)

R N/A 50000 X X (4) X (2) X X (2) X X (4) X (2)

Cardan link

201442617 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 2123003

- 0 0 N/A 50000 X X X X X X

Lock link upper pin 201442619 N/A 50000 X X

201482612 N/A 35500 X (3) X (1) X (1) X (3) X (1)

R N/A 50000 X X (4) X (2) X (2) X (4) X (2)

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 17

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Upper lock link 201442305 N/A 50000 X X

201442600 N/A 50000 X X

201482301 N/A 35500 X X X X X

201482304 N/A 35500 X X X X X

R 50

- 2123001

- 00 N/A 50000 X X X X X X

Lock link center pin 201268615 N/A 50000 X X

201482610 N/A 35500 X (3) X (1) X (1) X (3) X (1)

R N/A 50000 X X (4) X (2) X (2) X (4) X (2)

Lower lock link 201442300 N/A 50000 X X

201442306 N/A 50000 X X

201482312 N/A 35500 X X X X X

R 50

- 2123002

- 00 N/A 50000 X X X X X X

Connecting link/Lock link/Upper

spring pin 201442628 N/A 50000 X X

201442633 N/A 50000 X X

N/A 35500 X X X X X

201442646 N/A 35500 X (3) X (1) X (1) X (3) X (1)

R N/A 50000 X X (4) X (2) X X (2) X X (4) X (2)

Connecting link

201442606 N/A 50000 X X

N/A 35500 X X X X X

201442649 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 1223011

- 01 N/A 50000 X X X X X X

Connecting link/Pivot link pin

201442615 N/A 50000 X X

.../... N/A 35500 X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 18

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Connecting link/Pivot link pin

201442650 N/A 35500 X (3) X (1) X (1) X (3) X (1)

R N/A 50000 X X (4) X (2) X X (2) X X (4) X (2)

Pivot link

201442609 N/A 50000 X X

N/A 35500 X X X X X

201442648 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 1223013

- 01 N/A 50000 X X X X X X

Lower spring/Pivot link pin

201442613 N/A 50000 X X

N/A 35500 X X X X X

201442647 N/A 50000 X X

N/A 35500 X X X X X

R 55

- 1223029

- 01 N/A 50000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 19

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

ATA 32

- 21

- 00 NOSE LANDING GEAR (FIG. 07)

R (1) ‘xx’ at the end of the PNR stands for any number between 00 and 99

, including unused digits

.

Pintle pin (1)

F 53112339200xx 75000 50000 X X X X

125000 41250 X X X

F53120581200xx 75000 50000 X X X X

R 125000 41250 X X X X

DRAG STAY UPPER ARM ASSEMBLY (FIG. 07)

Drag stay upper pin D61848 75000 50000 X X

D64034 75000 50000 X X X X X X X

N 125000 50000 X

Drag stay upper arm D62667 75000 50000 X X

D62667

- 1 75000 50000 X X

D62667

- 10 75000 50000 X X

D64033 75000 50000 X X X X X X X

N 125000 50000 X

Drag stay center pin D61854 750 00 50000 X X

D64036 75000 50000 X X X X X X X

N 125000 50000 X

NOSE LANDING GEAR LEG (FIG. 07)

Drag stay lower arm D61844 75000 50000 X X

D64037 75000 50000 X X X X X X X

N 125000 50000 X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 20

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

MAIN FITTING

- SHOCK ABSORBER STRUCTURE (FIG. 07)

Drag stay lower arm/Main fitting

pin D61687 75000 50000 X X

D66331 75000 50000 X X X X X X X

N 35980 18000 X

Upper flange D61684 75000 50000 X X

D64000 75000 50000 X X X X X X X

N 125000 32610 X

Turning sleeve D62717 75000 50000 X X

D63998 75000 50000 X X X X X X X

D67634 47330 37370 X X

75000 50000 X X X X X

N 125000 50000 X

D67674 75000 50000 X X

Upper torqu e link pin D62720 75000 50000 X X

D64006 75000 50000 X X X X X X X

N 125000 50000 X

Upper torque link D62719 75000 50000 X X

D64002 75000 50000 X X X X X X X

N 125000 50000 X

Torque link apex pin

D62660 75000 500 00 X X X X X X X

N 125000 50000 X

Lower torque link D63710 75000 50000 X X

D64001 75000 50000 X X X X X X X

N 125000 50000 X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 21

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

Lower torque link pin D61688 75000 50000 X X

D64005 75000 50000 X X X X X X X

N 125 000 50000 X

D67247 75000 50000 X X X X X X X

N 125000 50000 X

D67247

- 1 75000 50000 X X X X X X X

N 125000 50000 X

N D67763 75000 50000 X X

D67790 75000 50000 X X X X X X X

N

D 125000 50000 X

Slidin g tube D62701 75000 50000 X X

D65046 75000 50000 X X X X X X X

D67201 75000 50000 X X X X X X X

N 60400 18000 X

D67338 75000 50000 X X X X X X X

N 60400 18000 X

D67511 75000 50000 X X

Main fitting D62714 750 00 50000 X X

D63407 75000 50000 X X

D63996 75000 50000 X X X X X X X

N 125000 18000 X

Main fitting hinge pin D62729 75000 50000 X X

D64003 75000 50000 X X X X X X X

N 125000 50000 X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 22

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMO NSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH LDG A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV01x WV02x WV05x

LOCK LINK (FIG. 07)

Lock link upper arm/Main fitting

pin D61693 75000 50000 X X X X X X X

N 125000 50000 X

D61693

- 1 75000 50000 X X X X X X X

N 125000 50000 X

D67788 75000 50000 X X X X X X X

N 125000 50000 X

Lock link upper arm

D61 845 75000 50000 X X X X X X X

N 125000 32870 X

Lock link center pin

D61870 75000 50000 X X X X X X X

N 125000 40540 X

D61870

- 1 75000 50000 X X X X X X X

N 125000 40540 X

D67789 75000 50000 X X X X X X X

N 125000 40540 X

Lock link lower arm

D61846 75000 50000 X X X X X X X

N 125000 50000 X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 23

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMONSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH FC A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV 01x WV02x WV05x

ATA 57

- 00

- 00 WING STRUCTURE (FIG. 08)

(1) This item is not transferable from an aircraft to an another: Traceability at aircraft level is authorized.

R (2) ‘xx’ at the end of the PNR stands for any number between 00 and 99

, including u nused digits

.

Gear support rib (LH) (1) (2)

F57550239000xx 60000 40000 X X

100000 33000 X X

F57555013000xx 60000 40000 X X X X

100000 33000 X X X X X X X

F57555013002xx 100000 33000 X X X

F57555114000xx 60000 40000 X X

R 100000 33000 X X X X X X

F57555542000xx 60000 40000 X X

100000 33000 X X

Gear support rib (RH) (1) (2)

F57550239001xx 60000 40000 X X

100000 33000 X X

F57555013001xx 60000 40000 X X X X

10000 0 33000 X X X X X X X

F57555013003xx 100000 33000 X X X

F57555114001xx 60000 40000 X X

R 100000 33000 X X X X X X

F57555542001xx 60000 40000 X X

100000 33000 X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 24

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMONSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH FC A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV 01x WV02x WV05x

Forward pintle fitting (LH) (1) (2)

F57550018000xx 60000 40000 X X

100000 33000 X X

F57555024000xx 60000 40000 X X

100000 33000 X X

F57555024002xx 60000 40000 X X X X

R 100000 33000 X X X X X X X X

Forward pintle fitt ing (RH) (1)

(2) F57550018001xx 60000 40000 X X

100000 33000 X X

F57555024001xx 60000 40000 X X

100000 33000 X X

F57555024003xx 60000 40000 X X X X

R 100000 33000 X X X X X X X X

Side stay fitting (LH) (1) (2)

F57550022000xx 60000 40000 X X

100000 33000 X X

F57555017000xx 60000 40000 X X

100000 33000 X X

F57555017002xx 60000 40000 X X

R 100000 33000 X X X X X X

Side stay fitting (RH) (1) (2)

F57550022001xx 6000 0 40000 X X

100000 33000 X X

F57555017001xx 60000 40000 X X

100000 33000 X X

F57555017003xx 60000 40000 X X

R 100000 33000 X X X X X X

### AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUL 29/10 ALS PART 1-3 PAGE: 25

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Note: Explanations on the applicability system are provided in the sub

- part 1

- 0 paragraph 3.

(*) Whichever occurs first.

Explanation notes are located under the assembly title. DEMONSTRATED

FATIGUE LIVES (*) DEMONSTRATED FATIGUE LIVES APPLICABILITY

R

Nomenclature Part Number FH FC A330

- 2xxF A330

- 2xx A330

- 30x A330

- 32x / A330

- 34x

R WV00x WV02x WV05x

WV06 x WV00x

WV01x WV05x WV00x

WV 01x WV02x WV05x

Retraction jack fitting (LH) (1)

(2) F57550028000xx 60000 40000 X X X X

100000 33000 X X X X X X X

R F57551977000xx 100000 33000 X X X X

Retraction jack fitting (RH) (1)

(2) F57550028001xx 60000 40000 X X X X

100000 33000 X X X X X X X

R F57551977001xx 100000 33000 X X X X



### END OF SUB

- PART 1

- 3

### AIRWORTHINESS LIMITATIONS SECTION

ALS PART 1

SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

HISTORY FILE

ISSUE: JUL 29/10 ALS PART 1 HISTORY FILE PAGE: 1/6

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

1- GENERAL

- A330 ALS Part 1 revision 00:

The A330 ALS Part 1 revision 00 was dedicated to transfer the content of the MPD 9-1 revision

05 into the subject document and to introduce the A330- 200/ -300 Enhanced Main Landing Gear

(EMLG). ATA 57 SL ALI have also been introduced.

- A330 ALS Part 1 revision 01:

The A330 ALS Part 1 revision 01 was dedicated to introduce a life reduction factor for parts

made of out- of -specification material. At the opportunity of this revision, life limitation assigned

to Enhanced MLG have been increased and their applicability have been extend to A330

WV020’s and WV050’s originally delivered equipped with P/N 201490 series MLG.

- A330 ALS Part 1 revision 02:

A330 ALS Part 1 revision 02 was mainly dedicated to assign new life reduction factors

applicable to MLG main fittings, bogie beams and sliding pistons made of out- of -specification

material. This revision was also dedicated to increase life limitations assigned to Enhanced

MLG parts and to introduce reworked MLG main fittings (Post MOD 56498).

- A330 ALS Part 1 revision 03:

A330 ALS Part 1 revision 03 was mainly dedicated to introduce the Intermediate Service Goal

figures for ATA 57 SL ALI. This revision was also dedicated to transfer the retraction actuator

chain items to the A330 ALS Part 4.

- A330 ALS Part 1 revision 04:

A330 ALS Part 1 revision 04 was mainly dedicated to introduce a new set of adapted

airworthiness limitations for main fittings made of out- of -specification material.

For some SL ALI, this revision also introduces an alternative set of airworthiness limitations

(trade off LDG for more FH).

- A330 ALS Part 1 revision 05:

A330 ALS Part 1 revision 05 is mainly dedicated to introduce the new A330-200F series.

### AIRWORTHINESS LIMITATIONS SECTION

ALS PART 1

SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

HISTORY FILE

ISSUE: JUL 29/10 ALS PART 1 HISTORY FILE PAGE: 2/6

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

2- SUMMARY OF CHANGES:

The following summarizes the changes with respect to the previous issue of the A330 ALS Part

1 (revision 04 ).

New items:

SUB -PART 1-0 LANDING GEAR LRUs APPLICABILITY:

* A330- 200F series:

Introduction of A330-223F and A330-243F models.

Introduction of WV000 (MOD 200589) and WV001 (MOD 58981).

* A330- 223 model:

Introduction of WV061 (MOD 200561).

SUB -PART 1- 2:

None.

SUB -PART 1- 3:

None.

Amendments:

SUB -PART 1-0 LANDING GEAR LRUs APPLICABILITY:

None.

SUB -PART 1- 2:

Table header amended.

* Main landing gear, bogie and dressings, bogie assembly:

Bogie beam PNR 50- 2117002 -00: Limits and limits applicability amended, PNR

201272307 and PNR 50

- 2117002 -01: PNR added (MOD 58896).

SUB -PART 1- 3:

Table header amended.

* Main landing gear:

Note (1) amended.

Aft pintle pin PNR (LH) F32155021000xx: Limitations applicability amended.

Aft pintle pin PNR (RH) F32155021001xx: Limitations applicability amended.

Aft pintle pin nut PNR SLN40789M130X2R and PNR SLN40874M130X2R: PNR

amended.

### AIRWORTHINESS LIMITATIONS SECTION

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ISSUE: JUL 29/10 ALS PART 1 HISTORY FILE PAGE: 3/6

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# A330

Aft pintle pin nut PNR SLN40927 and PNR SLN41180 : Limitations applicability

amended.

* Main landing gear, main strut and dressings:

Forward pintle pin PNR 55- 2105042 -00: Limitations applicability amended.

Forward pintle pin lock bolt PNR 55- 2105058 -00: Limitations applicability amended.

Upper torque link pin PNR 55- 2105055 -00: Limitations applicability amended.

Upper torque link PNR 50- 2105021 -00: Limitations applicability amended.

Torque link apex pin PNR 55- 2105054 -00: Limitations applicability amended.

Torque link apex pin nut PNR 55- 2105072 -00: Limitations applicability amended.

Lower torque link PNR 50

- 2105020

- 00 : Limitations applicability amended.

Lower torque link pin PNR 55- 2105056 -00: Limitations applicability amended.

Bogie beam pivot pin PNR 55- 2105029 -00: Limitations applicability amended.

Brake rod pin PNR 55-2105091-00: Limitations applicability amended.

Brake rod PNR 50-2105025-00: Limitations applicability amended.

* Main landing gear, main strut and dressings, main strut:

Main fitting (LH) PNR 50- 2107001 -00: Limitations applicability amended.

Main fitting (RH) PNR 50- 2108001 -00: Limitations applicability amended.

Aft pintle bearing PNR 201042565: Limitations applicability amended.

Pin SM7 PNR 55- 2107009 -00: Limitations applicability amended.

Shortening link (upper) PNR 50- 2107003 -00: Limitations applicability amended.

Pin SM8 PNR 55- 2107008 -00: Limitations applicability amended.

Shortening link (lower) PNR 50- 2107002 -00: Limitations applicability amended.

Pin SM9 PNR 55- 2107007 -00 and PNR 55- 2107093 -00: Limitations applicability

amended.

* Main landing gear, main strut and dressings, shock strut:

Upper piston PNR 50-2109002-00: Limitations applicability amended.

Recoil nut PNR 50-2109008-00: Limitation applicability amended.

Sliding piston PNR 50-2109001-01: Limitations applicability amended.

* Main landing gear, bogie and dressings, bogie assembly:

Bogie beam PNR 201272305, PNR 201272306, PNR 201485301: PNR added (MOD

58896).

Wheel axle PNR 55-2117003-00: Limitations applicability amended.

* Main landing gear, complete side stay:

Pivot link center pin 201442651: Limitation applicability amended.

Pivot link bracket PNR 55- 2119008 -00: Limitation applicability amended.

Pivot link bracket bolt PNR NAS6606D10: Limitation applicability amended.

Lock link/Side stay pin PNR 201482609: Limitation applicability amended.

### AIRWORTHINESS LIMITATIONS SECTION

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SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

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ISSUE: JUL 29/10 ALS PART 1 HISTORY FILE PAGE: 4/6

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# A330

* Main landing gear, complete side stay, (basic) side stay:

Upper cardan nut PNR 55- 1221042 -01: Limitations applicability amended.

Upper cardan pin PNR 55- 2121003 -00: Limitations applicability amended.

Side stay upper pin PNR 55- 2121005 -00: Limitations applicability amended.

Upper side stay PNR 50- 2121001 -00: Limitations applicability amended.

Upper spring bracket PNR 55- 1221012 -01: Limitation applicability amended.

Lower spring bracket PNR 55- 1221026 -01: Limitation applicability amended.

Spring bracket upper bolt PNR MS21250H06016: Limitation applicability amended.

Spring bracket lower bolt PNR 55- 1221029 -01: Limitation applicability amended.

Side stay center pin PNR 201483605: Limitations applicability amended.

Lower side stay PNR 55- 2121002

- 00: Limitations applicability amended.

Side stay lower pin PNR 55- 2121007 -00: Limitations applicability amended.

Lower cardan pin PNR 50- 2121004 -00: Limitations applicability amended.

Lower cardan nut PNR 55- 2121009 -00: Limitations applicability amended.

* Main landing gear, complete side stay, lock link:

Cardan link pin PNR 201442618: Limitation applicability amended.

Cardan link PNR 55-2123003-00: Limitation applicability amended.

Lock link upper pin PNR 201482612: Limitation applicability amended.

Upper lock link PNR 50- 2123001 -00: Limitation applicability amended.

Lock link center pin PNR 201482610: Limitation applicability amended.

Lower lock link PNR 50- 2123002 -00: Limitation applicability amended.

Connecting link/Lock link/Upper spring pin PNR 201442646 : Limitation applicability

amended.

Connecting link PNR 55- 1223011 -01: Limitation applicability amended.

Connecting link/Pivot link pin PNR: 201442650: Limitation applicability amended.

Pivot link PNR 55-1223013-01: Limitation applicability amended.

Lower spring/Pivot link pin PNR 55- 1223029 -01: Limitation applicability amended.

* Nose landing gear:

Note (1) amended.

Pintle pin PNR F53120581200xx: Limitations applicability amended.

* Nose landing gear, drag stay upper arm assembly:

Drag stay upper pin PNR D64034: Limitations and limitations applicability amended.

Drag stay upper arm PNR D64033: Limitations and limitations applicability amended.

Drag stay center pin PNR D64036: Limitations and limitations applicability amended.

* Nose landing gear, nose landing gear leg:

Drag stay lower arm PNR D64037: Limitations and limitations applicability amended.

### AIRWORTHINESS LIMITATIONS SECTION

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SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

HISTORY FILE

ISSUE: JUL 29/10 ALS PART 1 HISTORY FILE PAGE: 5/6

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

* Nose landing gear, nose landing gear leg, main fitting shock absorber structure:

Drag stay lower arm/Main fitting pin PNR D66331: Limitations and limitations applicability

amended.

Upper flange PNR D64000: Limitations and limitations applicability amended.

Turning sleeve PNR D67634: Limitations and limitations applicability amended.

Upper torque link pin PNR D64006: Limitations and limitations applicability amended.

Upper torque link PNR D64002: Limitations and limitations applicability amended.

Torque link apex pin PNR D62660: Limitations and limitations applicability amended.

Lower torque link PNR D64001: Limitations and limitations applicability amended.

Lower torque link pin PNR D64005, PNR D67247, PNR D67247-1 and PNR D67790:

Limitations and limitations applicability amended, PNR sorted in ascending sequence.

Sliding tube PNR D67201 and PNR D67338: Limitations and limitations applicability

amended.

Main fitting PNR D63996: Limitations and limitations applicability amended.

Main fitting hinge pin PNR D64003: Limitations and limitations applicability amended.

* Nose landing gear, nose landing gear leg, lock link:

Lock link upper arm/Main fitting pin PNR D61693, PNR D61693-1 and PNR D67788:

Limitations and limitations applicability amended.

Lock link upper arm PNR D61845: Limitations and limitations applicability amended.

Lock link center pin PNR D61870, PNR D61870-1 and PNR D67789: Limitations and

limitations applicability amended.

Lock link lower arm PNR D61846: Limitations and limitations applicability amended.

* Wing structure:

Note (1) amended.

Gear support rib (LH) PNR F57555114000xx: Limitations applicability amended.

Gear support rib (RH) PNR F5755 5114001xx: Limitations applicability amended.

Forward pintle fitting (LH) PNR F57555024002xx: Limitations applicability amended.

Forward pintle fitting (RH) PNR F57555024003xx: Limitations applicability amended.

Side stay fitting (LH) PNR F57555017002xx: Limitations applicability amended.

Side stay fitting (RH) PNR F57555017003xx: Limitations applicability amended.

Retraction jack fitting (LH) PNR F57551977000xx: Limitations applicability amended.

Retraction jack fitting (RH) PNR F57551977001xx: Limitations applicability amended.

### AIRWORTHINESS LIMITATIONS SECTION

ALS PART 1

SAFE LIFE AIRWORTHINESS LIMITATION ITEMS

HISTORY FILE

ISSUE: JUL 29/10 ALS PART 1 HISTORY FILE PAGE: 6/6

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

# A330

Deletions:

SUB -PART 1-0 LANDING GEAR LRUs APPLICABILITY:

None.

SUB -PART 1- 2:

None.

SUB -PART 1- 3:

None.