# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

REV: 02 

# A318/A319/A320/A321

ALS Part 2

- Damage-Tolerant

Airworthiness Limitation Items

(DT ALI)

 AIRBUS SAS 2013. 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.

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

TABLE OF CONTENTS

SUBJECT

REV: 02 ALS PART 2 TOC PAGE: 1-TOC

 AIRBUS SAS 2013. All rights reserved. 

# TABLE OF CONTENTS

RECORD OF REVISIONS

SECTION 1 - INTRODUCTION

1.1 GENERAL

1.2 APPLICABILITY

1.2. A. General applicability

1.2. B. Weight Variant (WV) applicability

1.3 LIMIT OF VALIDITY (LOV)

1.4 RULES FOR COMPLIANCE DEMONSTRATION

1.4. A. General

1.4. B. Structure conditions for DT ALI requirements

1.4. C. Reporting

1.4. D. Superseding of ALS Part 2 Limitations

1.4. E. Modifications/repairs not developed by Airbus (TC holder)

SECTION 2 - DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS LIST

2.1 EXPLANATION OF SECTION 2.2 TABLE FORMAT

2.2 INSPECTION REQUIREMENTS

SECTION 3 - CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS

3.1 EXPLANATION OF CDCCL REQUIREMENTS

3.2 CDCCL TABLE

APPENDICES

APPENDIX A - SUMMARY OF CHANGES

APPENDIX B - ABBREVIATIONS

APPENDIX C - TERMS AND DEFINITIONS

APPENDIX D - MODIFICATIONS LIST

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

REV: 02 ALS PART 2 PAGE: 1-ROR

EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# The European Aviation Safety Agency (EASA) approves the ALS Part 2.

Variations must also be approved.

REVISION

NUMBER REASON EASA APPROVAL

DATE/REFERENCE

00 To include the ALI Document reference in the ALS N/A

01 To incorporate the ALI Document reference AI/SEM4/95A.0252/96, and to revise the LOV APR 04/12

10039054 Rev.1

02 To incorporate the sharklet requirements for A320

To introduce a new LOV for A321 POST 154881

To introduce Mod 152970, similar to Mod 34650 MAY 28/13

10045072 Rev.1

Note 1: The ALS Part 2 is covered by the Certification Document 00D050A0008 C11.

Note 2: Variations 0DVLG100004C0S, SAVLG100005C0S, 0JVLG110004C0S,

0DVLG120002C0S, and 0DVLG120009C0S are superseded by this revision.

COMPLIANCE TIME :

It is mandatory to be in compliance with the airworthiness limitations as defined in the

A318/A319/A320/A321 ALS Part 2 revision 02 from 28 MAY 2014, except as provided in

paragraph 3.

From 28 MAY 2013 to 27 MAY 2014, it is mandatory to be in compliance with the airworthiness

limitations defined in, either:

The A318/A319/A320/A321 ALS Part 2 at revision 01, except as provided in paragraph 3.

or,

The A318/A319/A320/A321 ALS Part 2 at revision 02.

For the revised tasks listed in table 1 a special compliance time to be counted from

A318/A319/A320/A321 ALS Part 2 revision 02 approval date can be applied, without exceeding

the A318/A319/A320/A321 ALS Part 2 revision 01 requirement:

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

REV: 02 ALS PART 2 PAGE: 2-ROR

EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# Table 1 :

Reduced

ALI task Changes Special

Compliance

Time Special Compliance

Time Applicability

534125-01-2 Threshold reduced from "33800 FC" to

"32100 FC" 1700 FC

OR

3400 FH GROUP 19-1A

PRE 160055

OR

GROUP 19-1B

PRE160055

534126-01-2 Threshold reduced from "30200 FC or

60000 FH" to "28700 FC or 57400 FH" 1500 FC

OR

3000 FH GROUP 19-1A

PRE 153073

PRE 160055

OR

GROUP 19-1B

PRE 153073

PRE160055

534172-01-2 Threshold and interval reduced from

"15500 FC or 31100 FH" to "15300 FC

or 30600 FH". 100 FC

OR

200 FH A320-200

POST 20449

OR

A320-200

POST 20029

PRE 21065

PRE 25354

OR

A321

PRE 22992

571101-02-1 Threshold reduced from "43600 FC or

87200 FH" to "37200 FC or 74400 FH" 24 MO GROUP 19-1A

OR

GROUP 19-1B

24 MO A320

PRE 160000

571170-01-1 Interval reduced from "20000 FC or

45900 FH" to "9100 FC or 18200 FH" 24 MO GROUP 19-1A

PRE 34650

OR

GROUP 19-1B

PRE 34650

571170-01-2 Interval reduced from "18700 FC or

37500 FH" to "9100 FC or 18200 FH" 24 MO A320-200

PRE 160000

572007-01-2 Threshold and interval reduced from

"16000 FC or 32000 FH" to "11900 FC

or 23800 FH" 24 MO A320-200

PRE 34650

PRE 160001

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

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EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# SECTION 1 - INTRODUCTION

1.1 GENERAL

This document together with the Safe Life ALIs (given in ALS Part 1), the Certification

Maintenance Requirements (given in ALS Part 3), the Ageing Systems Maintenance (given

in ALS Part 4), and the Fuel ALIs (given in ALS Part 5) satisfy the requirements given in JAR

Part 25.571/25.1529/appendix H25.4.

Compliance with the requirements contained in this document is mandatory. ALL

aircraft shall be operated in accordance with the requirements of ALS Part 2, unless

otherwise agreed with the Authority of the State of aircraft registry.

This document contains, in section 2.2, airworthiness limitations arising from fatigue and

damage tolerance evaluation of damage tolerant structural elements whose failure could

contribute to catastrophic failure of the aircraft (FAR/JAR 25.571). It also contains

airworthiness limitations arising from an initial evaluation of Widespread Fatigue Damage

(WFD).The requirements quoted in this document are classed as Damage-Tolerant

Airworthiness Limitation Items (DT ALIs).

Additional information concerning DT ALI requirements can be found in the following Airbus

supporting publications:

- Maintenance Planning Document (MPD)

- Aircraft Maintenance Manual (AMM)

- Non-Destructive Testing Manual (NTM)

- Structural Repair Manual (SRM)

- Maintenance Review Board Report (MRBR)

This document contains in Section 3 the Critical Design Configuration Control Limitations

(CDCCL). A CDCCL is a limitation requirement to preserve a critical feature of the aircraft

design that is necessary to prevent the occurrence of an unsafe condition.

1.2. APPLICABILITY

1.2. A General applicability

The ALS Part 2 covers the following aircraft models:

A318-111 A319-111 A320-111 A321-111

A318-112 A319-112 A320-211 A321-112

A318-121 A319-113 A320-212 A321-131

A318-122 A319-114 A320-214 A321-211

A319-115 A320-215 A321-212

A319-131 A320-216 A321-213

A319-132 A320-231 A321-231

A319-133 A320-232 A321-232

A320-233

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

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EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# 1.2. B Weight Variant (WV) applicability

DT ALIs may have different limitations depending on the Weight Variant (WV) of each

aircraft.

This DT ALI document is applicable to the following Weight Variants:

MODEL/SERIES WEIGHT VARIANTS SPECIFIC MODIFICATION GROUP

A318-100 000, 001, 002, 003, 004,

005, 006, 007, 008 N/A 18-1A

005 POST 39195 18-1E

A319-100 000, 001, 003 N/A 19-1A

002, 004, 005, 006, 007,

008, 009, 011, 012 N/A 19-1B

002, 005, 010, 013 POST 28162

POST 28238

POST 28342 19-1C

A320-100 000, 001, 002 N/A No Grouping

A320-200 000, 001, 002, 003, 004,

005, 006, 007, 008, 009,

010, 011, 012 ,013, 014,

015, 016, 017, 018 N/A

None N/A

N/A

A321-100 000, 002, 003, 004, 005,

006

, 007 N/A 21-1A

008 N/A 21-1B

A321-200 000, 004, 005, 006, 007,

008

, 009 N/A 21-2A

001, 002, 003, 010, 011 N/A

21-2B 000, 004, 005, 006, 007,

008

, 009 POST 28653 (Group 21-2A with two

A CTs )



# To minimise the number of individual DT ALI maintenance requirements, the WV

requirements may be grouped where they are similar. The group numbers are stated in the

above table.

It is the Operator’s responsibility to refer to the applicable WV, and to ensure that the tasks

performed are applicable to the WV of the concerned aircraft.

The applicable WV for each individual aircraft at delivery can be found in the Aircraft Cross

Reference table in the A318/A319/A320/A321 SRM Front Matter. This table does not

necessarily reflect the actual current status of the aircraft. This should be confirmed using

the Weight Variant Identification Information given in the SRM introduction (to check for the

possible embodiment of the referenced Service Bulletins).

For aircraft having mutliple WV configurations possibility, the limits of the WV of the highest

MTOW have to be applied.

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

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EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# 1.3. LIMIT OF VALIDITY

The airworthiness limitations contained herein allow operation up to the Limit of Validity

(LOV) in FC or FH whichever occurs first. The relevant LOV values are stated below.

The LOV reflects the limit of validity of the engineering data that supports the structural

maintenance programme.

MODEL /

SERIES WEIGHT VARIANTS CONFIGURATION GROUP LoV

PRE

37734

PRE

39020 LoV

POST

37734

(SB 00-

1198)

PRE

39020 LoV

POST 39020

(SB 02-1001) RESTRICTIONS /

REMARKS

A318-100 000, 001, 002, 003, 004, 005, 006,

007, 008 PRE 39195 18-1A 48000 FC

OR

60000 FH N/A N/A N/A

005 POST 39195 18-1E 13300 FC

OR

40000 FH N/A N/A N/A

A319-100 000, 001, 003 N/A 19-1A

48000 FC

OR

60000 FH N/A N/A N/A

002, 004, 005, 006, 007, 008, 009,

011, 012 N/A 19-1B N/A N/A N/A

002, 005, 010, 013 POST 28162

POST 28238

POST 28342 19-1C 18000 FC

OR

77400 FH N/A N/A N/A

A320-100 000, 001, 002 N/A None 48000 FC

OR

48000 FH N/A N/A N/A

A320-200 000, 001, 002, 003, 004, 005, 006,

007, 008, 009, 010, 013 N/A

None 48000 FC

OR

60000 FH 37500 FC

OR

80000 FH

60000 FC

OR

120000 FH N/A

011, 012, 014, 015, 016, 017, 018 N/A N/A Specific WVs

excluded from

POST 37734

LoV

N/A POST 25714 N/A Specific

Configuration

excluded from

POST 37734

LoV

N/A POST 26925 N/A Specific

Configuration

excluded from

POST 37734

LoV

All certified POST 160001 48000 FC

OR

96000 FH N/A N/A WTF and

Sharklets

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

REV: 02 ALS PART 2 PAGE: 4

EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. MODEL /

SERIES WEIGHT VARIANTS CONFIGURATION GROUP LoV

PRE

37734

PRE

39020 LoV

POST

37734

(SB 00-

1198)

PRE

39020 LoV

POST 39020

(SB 02-1001) RESTRICTIONS /

REMARKS

A320-200 All certified POST 34650

OR

POST 152970

None 48000 FC

OR

60000 FH N/A N/A Certification of

Russian

Operations

N/A POST 23002

PRE 24596 N/A N/A Specific

Configuration

excluded

from POST

37734 / 39020

LoV

N/A POST 20139

PRE 22129 N/A N/A Specific

Configuration

excluded from

POST 37734 /

39020 LoV

A321-100 000, 002, 003, 004, 005, 006, 007 N/A 21-1A

48000 FC

OR

60000 FH N/A N/A

008 N/A 21-1B N/A N/A Specific WV

structurally

identical to an

A321-200 WV

000

N/A POST 154881 N/A 37000 FC

OR

74000 FH N/A N/A

A321-200 000, 004, 005, 006, 007, 008, 009 PRE 28653 21-2A 48000 FC

OR

60000 FH N/A N/A

001, 002, 003, 010, 011 N/A

21-2B 48000 FC

OR

60000 FH N/A N/A N/A

000, 004, 005, 006, 007, 008, 009 POST 28653 N/A N/A N/A

N/A POST 154881 N/A 37000 FC

OR

74000 FH N/A N/A



# 1.4. RULES FOR COMPLIANCE DEMONSTRATION

1.4. A General

In order to maintain the airworthiness of the aircraft, the applicable maintenance

requirements of the ALS Part 2 shall be performed and repeated on DT ALI at or prior

to whichever of the limitations occurs first (either FC, FH, or calendar time, as

applicable).

The maintenance tasks shall be performed on all applicable aircraft with the quoted

inspection level and access.

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

REV: 02 ALS PART 2 PAGE: 5

EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# Thresholds and intervals of the DT ALIs cannot be increased, unless advised by the

manufacturer following approval by the Authority of the State of aircraft registry

.

The threshold is the time at which the maintenance task is first due.

- For FC or FH tasks, the thresholds are counted from first flight unless otherwise stated.

- For tasks in Calendar Time, the thresholds are counted from the date of initial delivery

from manufacturer, unless otherwise stated.

For repeat maintenance tasks, the interval us age parameters (years, FC or FH) are counted

from the time the task was previously performed.

In case where the first maintenance is accomplished very early, the next inspection can be

performed at the threshold if the period (years, FC or FH) between initial task accomplishment

and the threshold is greater than the interval.

When alternative inspection methods are provided, the next interval applicable is the one

associated with the inspection method used at the last inspection.

In the same way, when the method of inspection is revised to a more stringent one, the next

interval applicable is the one associated with the inspection method used at the last

inspection.

"Touch and Go" cycles can be neglected if they are less than 5% of the total number of

Flight Cycles up to threshold inspecti on or between two consecutive inspections.

Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold

inspection or between two consecutive inspections.

The ALS Part 2 requires also to control corrosion to Level 1 or better on all metallic structure

details, elements or assemblies, which contribute significantly to carrying flight, ground,

pressure or control loads and whose failure could result in catastr ophic failure of the aircraft.

Corrosion Level 1 is defined in the Structure Section of the A318/A319/A320/A321 MRB

Report as follows:

- Corrosion damage that does not require structural reinforcement or replacement.

Or

- Corrosion occuring between successive inspections that exceeds allowable limit but is

local and can be attributed to an event not typical of operator’s usage of other aircraft

in the same fleet (e.g. mercury spillage).

The Corrosion Prevention and Control Program (CPCP) defined in the Structure Section of

the A318/A319/A320/A321 MRB Report is an acceptable means of compliance.

Credit may be taken for the MRB Report Structures Section maintenance tasks, providing

that they are performed with the same ins pection level, as frequently, or more frequently,

than the inspection threshold and interval quoted in this document.

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

REV: 02 ALS PART 2 PAGE: 6

EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# 1.4. B Structure conditions for DT ALI requirements

Limitations quoted in Section 2-2 are applicable to the undamaged and unrepaired structure.

In cases of damage or repairs, the DT ALI maintenance requirements may have to be

adapted, or additional requirements may be required. In these cases the requirements that

are given in the relevant documents (SRM or specific Repair Approval Sheet (RAS)) must

be applied.

It is assumed that the structure to be inspected is in a state of cleanliness, which allows a

satisfactory inspection to be carried out at the required inspection level.

Where existing Temporary Protection System (TPS) permits unobscured assessment of the

condition of the structure, then that TPS may remain in place for the inspection.

If damage is found or suspected (such as bulging skin, paint discoloration) then the full

extent of any damage must be clearly identif ied using appropriate inspection techniques

and/or disassembly when necessary. This may require additional access to that stated for

the maintenance task.

Damage has to be evaluated and repaired in accordance with the A318/A319/A320/A321

SRM or other documentation acceptable to the relevant Airworthiness Authority.

If inspections indicate evidence of deterioration, appropriate further actions must be taken to

prevent similar deteriorations from occurring in the operator’s fleet.

1.4.C Reporting

As required by ICAO annex 8, any damage, su ch as a fatigue crack or corrosion greater

than Level 1, found at any time on a Principle Structural Element (PSE), Safe Life Item or

Fatigue Critical Structure (FCS), as identified in the SRM Chapter 51, shall be reported to

Airbus.

An appropriate reporting spreadsheet is available on the AirbusWorld eSite : Airbus World

Maintenance & Engineering > Prepare Maintenance > Optimize maintenance management

> Optimize maintenance program > Report my check records.

Guidance for completing the form is available at the same location.

All reports should be sent to MPDtask.Reports@Airbus.com . Any related questions should

be sent to the same address. Operators will receive an acknowledgement for data reports.

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

REV: 02 ALS PART 2 PAGE: 7

EASA APPROVED

 AIRBUS SAS 2013. All rights reserved. 

# 1.4. D. Superseding of ALS Part 2 limitations

Limitations of the ALS Part 2 may be superseded by instructions given in either

Airworthiness Directives (AD) or production Concessions or a Repair Approval Sheet (RAS)

or an Alternative Means Of Compliance (AMOC).

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

1.4. E. Modifications/repairs not developed by Airbus (TC holder)

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

Airbus (TC holder) under the Design Organisation Approval (DOA) Certificate

EASA.21J.031, then the Operator in accordance with his design organisation or

"Suplementary Type Certification holder" is respons ible for obtaining the certification of the

modification or repair embodied, as well as the approval by the relevant Airworthiness

Authority of any necessary adaptations of the ALS Part 2 limitations.

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/considered as well.A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2PAGE: 1EASA APPROVED©AIRBUS SAS 2013. Allrights reserved.SECTION 2 - DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS LIST2.1 EXPLANATION OF SECTION 2.2 TABLE FORMATDetailed information is given below concerning the section 2 table format of the DT ALI requirements provided on subsequent pages.REV.CODETASK REFERENCE ACCESS TASK DESCRIPTIONTHRESHOLDINTERVAL APPLICABILITY NOTE“REV CODE”This column indicates the revision code “status” of the DT ALI task requirement compared to previous issue of the document.<Blank> = No amendment.<R> = The DT ALI task requirement has been revised.<N> = The DT ALI task requirement is new.<D> = The DT ALI task requirement is deleted.“TASK REFERENCE”This column indicates the DT ALI task number, e.g. 531109-01-1. It is composed of 9 to 10 digits as follows:XXXXXX-YY-ZZZ = Applicability indexY = Sequence numberX = SSI numberThe SSI number is composed of six digits, e.g.531109-01-1. The first set of two digits, e.g.531109-01-1, is in accordance with theA318/A319/A320/A321 ATA 100 breakdown, showing the major section where the DT ALI is located, e.g. 53 fuselage. The second setof two digits, e.g. 531109-01-1, is also in accordance with the ATA 100 breakdown, showing the sub-section where the DT ALI islocated, e.g. 53-11 Fwd Fuselage. The third set of two digits, e.g. 521109-01-1, is a sequential number within the section e.g. 01, 02, 03up to 99.A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2PAGE: 2EASA APPROVED©AIRBUS SAS 2013. Allrights reserved.The Sequence number is composed of two digits, e.g. 531109-01-1. It follows the SSI number and is separated by a dash. It identifiesdifferent inspection level e.g. Detailed or Special Detailed. These two digits are also changed when the inspection areas are physicallydifferent (e.g. Rib 8 or Rib 9) or when the inspections have a major difference in access (e.g. actuator removal).The Applicability index is composed of one or two digits, e.g. 531109-01-1. It follows the Sequence number and is separated by a dash.It identifies the different applicability e.g. aircraft series, modstatus, group, etc. This digit is also used to differentiate between minoraccess differences e.g. different panel numbers.“ACCESS”This column indicates the access requirements to adequately perform the inspection, i.e. all items listed must be removed or opened(hinged panels/doors) unless otherwise stated (e.g. insulation to be displaced). For each DT ALI, the stated access is consideredsufficient to perform the task.“TASK DESCRIPTION”This column describes the task to be performed. It includes the inspection level, the description and the boundaries of the DTALI to beinspected. All items within this boundary are to be inspected e.g. fasteners, cutouts, attachments, unless otherwise stated. Additionalinformation may be added to clarify the inspection area. For Special Detailed Inspections the NDT method is to be stated betweenbrackets.Where applicable, Notes providing details such as alternative tasks, specific grace periods or tasks to be performed at the same time,will be included.“THRESHOLD”This column indicates the threshold when the inspection is due for the first time.“INTERVAL”This column indicates the repeat interval when the inspection is due the second and subsequent times.A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2PAGE: 3EASA APPROVED©AIRBUS SAS 2013. Allrights reserved.“APPLICABILITY”This column indicates the applicability of the task and lists the aircraft type, series, model, weight variant group or modification status towhich the DT ALI requirement is applicable. Some examples are given below. Details of modifications affecting the limitations are givenin Appendix E.Applicability Task applicable toALL All A318/A319/A320/A321 series aircraftA320 All A320 series aircraftA321-100 A321-100 series aircraft onlyA320PRE 25044ORA321PRE 25044All A320 and A321 series aircraft on which modification no. 25044 has not been embodiedA320POST 21003All A320 series aircraft on which modification no. 21003 has been embodiedA320-200POST 20062PRE 30748A320-200 series aircraft only on which modification no. 20062 has been embodied and modification no. 30748has not been embodiedGROUP 19-1A A319-100 series aircraft for Weight Variants 000, 001 or 003IAE All A318/A319/A320/A321 series aircraft installing IAE engines“NOTE”This column indicates if the task is widespread fatigue damage related by mentioning “WFD” in that case.A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 4EASA APPROVED©AIRBUS SAS 2013. All rights reserved.2.2 INSPECTION REQUIREMENTSREVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE521101-02-1 DELETED FROM ALS PART 2 AT REVISION 01521103-01-1 N/A GENERAL VISUAL INSPECTION OF FORWARDPASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE,LH/RH14800 FC 14800 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321521103-01-3 N/A GENERAL VISUAL INSPECTION OF FORWARDPASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE,LH/RH10800 FC 10800 FC GROUP 18-1EORGROUP 19-1C521301-02-1 DELETED FROM ALS PART 2 AT REVISION 01521303-01-1 N/A GENERAL VISUAL INSPECTION OF AFTPASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE,LH/RH14800 FC 14800 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321521303-01-3 N/A GENERAL VISUAL INSPECTION OF AFTPASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE,LH/RH10800 FC 10800 FC GROUP 18-1EORGROUP 19-1C522102-01-1 833 834 843844LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF EMERGENCY EXITS,INTERNAL STRUCTURE AND LOAD TRANSMITTINGPROFILE, LH/RH39300 FC 11400 FC GROUP 19-1APOST 32208ORGROUP 19-1BPOST 32208ORA320A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 5EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE522102-01-2 834 844LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF EMERGENCY EXITS,INTERNAL STRUCTURE AND LOAD TRANSMITTINGPROFILE, LH/RH39300 FC 11400 FC GROUP 18-1AORGROUP 19-1APRE 32208ORGROUP 19-1BPRE 32208522201-01-1 N/A GENERAL VISUAL INSPECTION OF FORWARDEMERGENCY EXITS, EXTERNAL SURFACE, LH/RH4500 FC 4500 FC A321522203-01-1 833 843 GENERAL VISUAL INSPECTION OF DOOR STOPASSEMBLIES AND LOCKING HOOK ON FORWARDEMERGENCY EXIT DOORS, LH/RH24000 FC 4500 FC A321522204-01-1 N/A GENERAL VISUALINSPECTION OF AFT EMERGENCYEXITS, EXTERNAL SURFACE, LH/RH4500 FC 4500 FC A321522206-01-1 834 844 GENERAL VISUAL INSPECTION OF DOOR STOPASSEMBLIES AND LOCKING HOOK ON AFT EMERGENCYEXIT DOORS, LH/RH24000 FC 4500 FC A321523101-01-1 N/A GENERAL VISUALINSPECTION OF FORWARD CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE12500 FCOR25000 FH12500 FCOR25000 FHGROUP 19-1AORGROUP 19-1BORA320ORA321523101-01-3 N/A GENERAL VISUALINSPECTION OF FORWARD CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE3000 FCOR14300 FH3000 FCOR14300 FHGROUP 19-1C523105-01-3 DELETED FROM ALS PART 2 AT REVISION 01523105-01-4 825 GENERAL VISUALINSPECTION OF FORWARD CARGOCOMPARTMENT DOOR, ACTUATOR ATTACH FITTINGS10000 FCOR43000 FH10000 FCOR43000 FHGROUP 19-1C523106-01-1 825LINING REMOVEDINSULATIONREMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION(ROTO) OF FORWARDCARGO COMPARTMENT DOOR SKIN, UNDERNEATHHINGE FITTINGS AT SELECTED BOLT HOLES40000 FCOR80000 FH23400 FCOR46900 FHA320PRE 24603ORA321PRE 24603523107-01-1 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 6EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE523108-01-1 825 DETAILED INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR, HINGE FITTINGS ANDATTACHMENT AREA, EXTERNAL51200 FCOR102400 FH14500 FCOR29000 FHGROUP 19-1AORGROUP 19-1BORA320ORA321523109-02-1 825 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF FORWARD CARGO COMPARTMENTDOOR AT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (6 PLACES)10300 FCOR20700 FH10300 FCOR20700 FHGROUP 19-1AORGROUP 19-1BORA320ORA321523109-02-2 825 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF FORWARD CARGO COMPARTMENTDOOR AT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (6 PLACES)10000 FCOR45300 FH10000 FCOR45300 FHGROUP 19-1C523111-01-1 N/A GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE12500 FCOR25000 FH12500 FCOR25000 FHA320ORA321523115-01-3 DELETED FROM ALS PART 2 AT REVISION 01523116-01-1 826LINING REMOVEDINSULATIONREMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION(ROTO) OF AFT CARGOCOMPARTMENT DOOR SKIN UNDERNEATH HINGEFITTINGS AT SELECTED BOLT HOLES40000 FCOR80000 FH23400 FCOR46900 FHA320PRE 24603ORA321PRE 24603523117-01-1 DELETED FROM ALS PART 2 AT REVISION 01523117-01-2 DELETED FROM ALS PART 2 AT REVISION 01523118-01-1 DELETED FROM ALS PART 2 AT REVISION 01523118-01-2 826 DETAILED INSPECTION OF AFT CARGO COMPARTMENTDOOR, HINGE FITTINGS AND ATTACHMENT AREA,EXTERNAL51200 FCOR102400 FH14500 FCOR29000 FHA320-200ORA321523119-02-1 826 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF AFT CARGO COMPARTMENT DOORAT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (6 PLACES)10300 FCOR20700 FH10300 FCOR20700 FHA320-100A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 7EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE523119-02-2 826 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF AFT CARGO COMPARTMENT DOORAT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (6 PLACES)10300 FCOR20700 FH10300 FCOR20700 FHA320-200ORA321523121-01-1 N/A GENERAL VISUALINSPECTION OF FORWARD CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE4500 FC 4500 FC GROUP 18-1A523121-01-2 N/A GENERAL VISUALINSPECTION OF FORWARD CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE4500 FCOR13500 FH4500 FCOR13500 FHGROUP 18-1E523125-01-1 DELETED FROM ALS PART 2 AT REVISION 01523127-01-1 825LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR, HINGE FITTINGS ATTACHMENTAREA, INTERNAL36500 FC 15000 FC GROUP 18-1A523128-01-1 825 DETAILED INSPECTION OF FORWARD CARGOCOMPARTMENTDOOR, HINGE FITTINGS ANDATTACHMENT AREA, EXTERNAL36500 FC 15000 FC GROUP 18-1A523129-02-1 825 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF FORWARD CARGO COMPARTMENTDOOR AT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (4 PLACES)13100 FC 13100 FC GROUP 18-1A523211-01-1 N/A GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE4500 FC 4500 FC GROUP 19-1AORGROUP 19-1B523211-01-3 N/A GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE3000 FCOR14300 FH3000 FCOR14300 FHGROUP 19-1C523215-01-1 DELETED FROM ALS PART 2 AT REVISION 01523215-01-2 826 GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR, ACTUATOR ATTACH FITTINGS10000 FCOR43000 FH10000 FCOR43000 FHGROUP 19-1C523217-01-1 826LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF AFT CARGO COMPARTMENTDOOR, HINGE FITTINGS ATTACHMENT AREA, INTERNAL35200 FC 15000 FC GROUP 19-1AORGROUP 19-1BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 8EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE523218-01-1 826 DETAILED INSPECTION OF AFT CARGO COMPARTMENTDOOR HINGE FITTINGS AND ATTACHMENT AREA,EXTERNAL48000 FCOR60000 FH14500 FCOR29000 FHGROUP 19-1AORGROUP 19-1B523219-02-1 826 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF AFT CARGO COMPARTMENT DOORAT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (6 PLACES)10300 FCOR20700 FH10300 FCOR20700 FHGROUP 19-1AORGROUP 19-1B523219-02-2 826 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF AFT CARGO COMPARTMENT DOORAT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (6 PLACES)10000 FCOR45300 FH10000 FCOR45300 FHGROUP 19-1C523221-01-1 N/A GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE4500 FC 4500 FC GROUP 18-1A523221-01-2 N/A GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE4500 FCOR13500 FH4500 FCOR13500 FHGROUP 18-1E523225-01-1 DELETED FROM ALS PART 2 AT REVISION 01523227-01-1 826LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF AFT CARGO COMPARTMENTDOOR, HINGE FITTINGS ATTACHMENT AREA, INTERNAL35200 FC 15000 FC GROUP 18-1A523228-01-1 826 DETAILED INSPECTION OF AFT CARGO COMPARTMENTDOOR HINGE FITTINGS AND ATTACHMENT AREA,EXTERNAL35200 FC 15000 FC GROUP 18-1A523229-02-1 826 GENERAL VISUALINSPECTION OF LOCKING HOOKS ANDFORK FITTINGS OF AFT CARGO COMPARTMENT DOORAT ALL FRAMES, BETWEEN LONGERON 4 ANDLONGERON 5 (4 PLACES)12200 FC 12200 FC GROUP 18-1A523301-01-1 N/A GENERAL VISUALINSPECTION OF BULK CARGOCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE7500 FC 7500 FC A320POST 20029PRE 21065PRE 25354ORA320POST 20449ORA321PRE 22992A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 9EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE526102-01-1 N/A DETAILED INSPECTION OF ENTRANCE STAIRS DOORSKIN, EXTERNAL SURFACE44100 FC 44100 FC GROUP 18-1APOST 23288ORGROUP 19-1APOST 23288ORGROUP 19-1BPOST 23288ORA320POST 20062ORA320POST 23288ORA321POST 23288528103-02-2 DELETED FROM ALI DOCUMENT AT ISSUE 10R 528107-01-1 734 744 GENERAL VISUAL INSPECTION OF MLG DOOR FWDFITTING JOINT TO HINGE FITTING, LH/RHNOTE: FOR PRE 24428 OR PRE 24903 AIRCRAFTRETROFITTED, THRESHOLD IS TO BE COUNTED FROMSB 52-1058 OR SB 52-1073 EMBODIMENT49100 FC 2800 FC POST 24428ORPOST 24903531101-01-1 831 841INSULATIONREMOVEDLINING REMOVEDCEILING PANELSREMOVEDDETAILED INSPECTIONOF FWD PASSENGER/CREWDOOR CUTOUT, INTERCOSTALS FITTINGS N°7 BETWEENFR15-16 AND FR20-21, LH/RH36500 FC 3800 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 10EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE531102-01-1 831 841 DETAILED INSPECTION OF FORWARDPASSENGER/CREW DOOR FRAME, UPPER CORNERS,EXTERNAL SURFACE, LH/RH22000 FC 13600 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321531102-01-3 831 841 DETAILED INSPECTION OF FORWARDPASSENGER/CREW DOOR FRAME, UPPER CORNERS,EXTERNAL SURFACE, LH/RH13700 FC 8500 FC GROUP 19-1CR 531103-01-1 831 841STOP FITTING BOLTSREMOVEDINSULATIONREMOVEDLINING REMOVEDCEILING PANELSREMOVEDGALLEYS ANDTOILETS REMOVED(IF INSTALLED)SPECIAL DETAILED INSPECTION (ROTO) OF FWDPASSENGER/CREW DOOR CUTOUT, STOP FITTINGSHOLES ON THEFR20, LH/RH48000 FC 16800 FC A320-200PRE 160000R 531105-01-1 SLIDING WINDOWOPENEDDETAILED INSPECTION OFLATERAL WINDOW FRAMESTIFFENER, UPPER AREA, LH/RHNOTE: THIS TASK IS ANALTERNATIVE INSPECTION TOTASK 531105-02-1.48000 FC 800 FC A320-200PRE 160000R 531105-02-1 SLIDING WINDOWOPENEDSPECIAL DETAILED INSPECTION(HFEC) OF LATERALWINDOW FRAME STIFFENER, UPPER AREA, LH/RHNOTE: THIS TASK IS ANALTERNATIVE INSPECTION TOTASK 531105-01-1.48000 FC 1600 FC A320-200PRE 160000R 531108-01-1 713 714BOLTS REMOVEDSPECIAL DETAILED INSPECTION(ROTO) OF HOLES ATFWD CORNERS OF NLG BAY, FR948000 FCOR96000 FH17200 FCOR34400 FHA320-200PRE 160000A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 11EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE531109-01-1 N/A GENERAL VISUALINSPECTION OF ENTRANCE STAIRSDOOR SURROUND, UPPER AND LOWER CORNERS,EXTERNAL SURFACE, LHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-03-2.3200 FCOR6400 FH3200 FCOR6400 FHGROUP 18-1APOST 23288ORGROUP 19-1APOST 23288ORGROUP 19-1BPOST 23288ORA320POST 20062ORA320POST 23288ORA321POST 23288531109-01-3 N/A GENERAL VISUALINSPECTION OF ENTRANCE STAIRSDOOR SURROUND, UPPER AND LOWER CORNERS,EXTERNAL SURFACE, LHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-03-1.2900 FC 2900 FC GROUP 18-1EORGROUP 19-1C531109-03-1 N/A DETAILED INSPECTION OF ENTRANCE STAIRS DOORSURROUND, UPPER AND LOWER CORNERS, EXTERNALSURFACE, LHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-01-3.5900 FC 5900 FC GROUP 18-1EORGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 12EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE531109-03-2 N/A DETAILED INSPECTION OF ENTRANCE STAIRS DOORSURROUND, UPPER AND LOWER CORNERS, EXTERNALSURFACE, LHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-01-1.6300 FCOR12700 FH6300 FCOR12700 FHGROUP 18-1APOST 23288ORGROUP 19-1APOST 23288ORGROUP 19-1BPOST 23288ORA320POST 20062ORA320POST 23288ORA321POST 23288R 531110-01-1 812 824INSULATIONREMOVEDBOLTS REMOVEDAIR CONDITIONINGDUCTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OFCROSSBEAM SPLICING, FR16 AND FR20, LH/RH38800 FCOR77600 FH28600 FCOR57200 FHA320PRE 20416PRE 21999R 531110-01-2 812 824INSULATIONREMOVEDBOLTS REMOVEDAIR CONDITIONINGDUCTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OFCROSSBEAM SPLICING, FR16 AND FR20, LH/RH38900 FCOR77900 FH14400 FCOR28900 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320POST 20416ORA320POST 21999ORA321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 13EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE531111-01-1 N/A GENERAL VISUAL INSPECTION OF AVIONICSCOMPARTMENT DOORS, SURROUND CORNERS,EXTERNAL SURFACE (4 DOORS)1500 FC 1500 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321531111-01-2 N/A GENERAL VISUAL INSPECTION OF AVIONICSCOMPARTMENT DOORS, SURROUND CORNERS,EXTERNAL SURFACE (4 DOORS)5500 FC 5500 FC GROUP 18-1EORGROUP 19-1C531112-01-1 N/A DETAILED INSPECTION OF FUSELAGE LOWER PANEL ATNLG BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH16300 FCOR32600 FH16300 FCOR32600 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321531112-01-2 N/A DETAILED INSPECTION OF FUSELAGE LOWER PANEL ATNLG BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH15400 FC 15400 FC GROUP 19-1C531113-01-1 N/A GENERAL VISUALINSPECTION OF ATTACHMENT TOSKIN PANEL, FR16, STG 3 LH/RH41400 FC 7400 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 14EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE531114-01-1 N/A DETAILED INSPECTION OF FUSELAGE SKIN ABOVEWINDSHIELD, BETWEEN FR 4 AND FR 12, EXTERNALSURFACE, LH/RH5700 FC 5700 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321531114-01-2 N/A DETAILED INSPECTION OF FUSELAGE SKIN ABOVEWINDSHIELD, BETWEEN FR 4 AND FR 12, EXTERNALSURFACE, LH/RH5700 FC 5700 FC GROUP 19-1C531117-01-1 N/A GENERAL VISUALINSPECTION OF FUSELAGE SIDEPANEL, BELOW COCKPIT SIDEWINDOWS, BETWEEN FR1 AND FR 12, EXTERNAL SURFACE, LH/RH14500 FC 14500 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321531117-01-3 N/A GENERAL VISUALINSPECTION OF FUSELAGE SIDEPANEL, BELOW COCKPIT SIDEWINDOWS, BETWEEN FR1 AND FR 12, EXTERNAL SURFACE, LH/RH14000 FC 14000 FC GROUP 19-1C531118-01-1 N/A GENERAL VISUALINSPECTION OF AREA FORWARD OFWINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR 4,EXTERNAL SURFACE, LH/RH4300 FC 4300 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321531118-01-3 N/A GENERAL VISUALINSPECTION OF AREA FORWARD OFWINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR 4,EXTERNAL SURFACE, LH/RH3700 FC 3700 FC GROUP 18-1EORGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 15EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 531119-01-1 N/A DETAILED INSPECTION OF UPPER SKIN OF LOWERLONGITUDINAL LAP JOINT,BETWEEN FR 9 AND FR 20,EXTERNAL SURFACE, LH/RH41000 FC 12600 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100ORA320-200PRE 30748ORA321PRE 30748R 531119-01-2 N/A DETAILED INSPECTION OF UPPER SKIN OF LOWERLONGITUDINAL LAP JOINT,BETWEEN FR 9 AND FR 20,EXTERNAL SURFACE, LH/RH35300 FC 11700 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 16EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 531124-01-1 824INSULATIONDISPLACEDDETAILED INSPECTION OFFR 20 SPLICE, BETWEENSTRINGER 30 AND STRINGER 32, LH/RH35600 FC 8300 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100PRE 20062ORA320-200PRE 20062PRE 30748ORA321PRE 30748R 531124-01-2 824INSULATIONDISPLACEDDETAILED INSPECTION OFFR 20 SPLICE, BETWEENSTRINGER 30 AND STRINGER 32, LH/RH33600 FC 7900 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748531124-01-3 824INSULATIONDISPLACEDPART OF LEFT ENDSIDE GASKETREMOVEDDETAILED INSPECTION OFFR 20 SPLICE, BETWEENSTRINGER 30 AND STRINGER 32, LH/RH35600 FC 8300 FC A320-100POST 20062ORA320-200POST 20062PRE 30748531126-01-2 LINING REMOVEDINSULATIONREMOVEDAIR CONDITIONINGOUTLET REMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF LATERALSPLICING, FR8, LH/RH25500 FCOR51000 FH4800 FCOR9700 FHMSN 0022-0267A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 17EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE531127-01-1 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF LATERALSPLICING, FR11, LH/RH42400 FC 9900 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321531129-01-1 DELETED FROM ALS PART 2 AT REVISION 01R 531129-02-1 211LW 211MWLH/RH WINDSHIELDSREMOVEDDISPLAY UNIT 4WT1REMOVEDANCHOR NUT SHIMSREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF WINDSHIELDCENTER POST, LOWER ATTACHMENT AREA, INTERNALSIDE36000 FC 10500 FC A320PRE 21999PRE 22058R 531129-02-2 211LW 211MWLH/RH WINDSHIELDSREMOVEDDISPLAY UNIT 4WT1REMOVEDANCHOR NUT SHIMSREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF WINDSHIELDCENTER POST, LOWER ATTACHMENT AREA, INTERNALSIDE36600 FC 9500 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320POST 21999PRE 30748ORA320POST 22058PRE 30748ORA321PRE 30748A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 18EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 531129-02-3 211LW 211MWLH/RH WINDSHIELDSREMOVEDDISPLAY UNIT 4WT1REMOVEDANCHOR NUT SHIMSREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF WINDSHIELDCENTER POST, LOWER ATTACHMENT AREA, INTERNALSIDE34600 FC 9000 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320POST 30748ORA321POST 30748531130-02-1 211NW 211PW212NW212PWSLIDING WINDOWOPENEDSPECIAL DETAILED INSPECTION(HFEC) OF LATERALFORWARD CORNER OF SLIDING WINDOW FRAME ATFR4, LH/RH48000 FC 13800 FC A320-200POST 21657ORA320-200POST 23685531133-01-1 211NW 211PW212NW212PWSLIDING WINDOWOPENEDDETAILED INSPECTION OF WINDSHIELD SIDE POST ATFR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-02-1.26700 FC 2700 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200ORA321531133-01-2 211NW 211PW212NW212PWSLIDING WINDOWOPENEDDETAILED INSPECTION OF WINDSHIELD SIDE POST ATFR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-02-2.25600 FC 1900 FC A320-100A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 19EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE531133-02-1 211NW 211PW212NW212PWSLIDING WINDOWOPENEDSPECIAL DETAILED INSPECTION(HFEC) OF WINDSHIELDSIDE POST AT FR 4, LOWER ATTACHMENT, INTERNALSIDE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-1.26700 FC 5700 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200ORA321531133-02-2 211NW 211PW212NW212PWSLIDING WINDOWOPENEDSPECIAL DETAILED INSPECTION(HFEC) OF WINDSHIELDSIDE POST AT FR 4, LOWER ATTACHMENT, INTERNALSIDE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-2.25600 FC 3900 FC A320-100R 531135-01-1 211BC 211KC 211LC211NW 212BC 212KC212LC 212NWSLIDING WINDOWOPENEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION(ROTO) OF WINDSHIELDSIDE POST AT FR 4, UPPER ATTACHMENT, INTERNALSIDE, LH/RH28800 FC 11500 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100ORA320-200PRE 30748ORA321PRE 30748A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 20EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 531135-01-2 211BC 211KC 211LC211NW 212BC 212KC212LC 212NWSLIDING WINDOWOPENEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION(ROTO) OF WINDSHIELDSIDE POST AT FR 4, UPPER ATTACHMENT, INTERNALSIDE, LH/RH28800 FC 11000 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748531155-02-1 831 841LINING REMOVEDINSULATIONREMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (HFEC AND ROTO) OFDOOR FR 20, AT DOUBLEJOGGLE AREA IN OUTERFLANGE OF FRAME, AT DOOR STOPS NUMBER 1 AND 7LOCATION, LH/RH27700 FC 10300 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321R 531157-01-1 824LADDER REMOVEDFLOOR PANELREMOVEDDETAILED INSPECTION OF CONTINUITY FITTINGBETWEEN FR 20 AND FR 21, AND ANGLE FITTING, BOTHSIDES OF FR 21, AT STRINGER 41 LOCATION, LH/RH24000 FC 7300 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100ORA320-200PRE 30748ORA321PRE 30748A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 21EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 531157-01-2 824LADDER REMOVEDFLOOR PANELREMOVEDDETAILED INSPECTION OF CONTINUITY FITTINGBETWEEN FR 20 AND FR 21, AND ANGLE FITTING, BOTHSIDES OF FR 21, AT STRINGER 41 LOCATION, LH/RH24000 FC 7000 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748R 531170-01-1 LOWER RETAINERSREMOVEDDETAILED INSPECTION OFCOCKPIT WINDSHIELD,LOWER FRONT FITTING AT FR 4, LOWER ATTACHMENT,EXTERNAL SURFACE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-1.36700 FC 5700 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100ORA320-200PRE 30748ORA321PRE 30748R 531170-01-2 LOWER RETAINERSREMOVEDDETAILED INSPECTION OFCOCKPIT WINDSHIELD,LOWER FRONT FITTING AT FR 4, LOWER ATTACHMENT,EXTERNAL SURFACE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-2.36700 FC 5500 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 22EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 531170-02-1 LOWER RETAINERSREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF COCKPITWINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWERATTACHMENT, EXTERNAL SURFACE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-1.36700 FC 15600 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100ORA320-200PRE 30748ORA321PRE 30748R 531170-02-2 LOWER RETAINERSREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF COCKPITWINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWERATTACHMENT, EXTERNAL SURFACE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-2.36700 FC 15000 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748531184-01-1 811INSULATIONREMOVEDDETAILED INSPECTION OF CENTRAL AND ADJACENTVERTICAL POSTS OF FORWARD PRESSURE BULKHEADAND WEB ASSEMBLY, UPPER PORTION32100 FC 14200 FC A320PRE 21521531184-01-2 811INSULATIONREMOVEDDETAILED INSPECTION OF CENTRAL AND ADJACENTVERTICAL POSTS OF FORWARD PRESSURE BULKHEADAND WEB ASSEMBLY, UPPER PORTION34000 FC 13500 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320POST 21521ORA321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 23EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE532104-01-1 825CEILING PANELSREMOVEDLINING REMOVEDINSULATIONDISPLACEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OFATTACHMENT AREA OF FR25 LH TO FR34 LH AND FR29RH TO FR34 RH TO CABIN FLOOR BEAMS, INTERNALSTRUCTURE43400 FCOR86900 FH35600 FCOR71200 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321WFD532132-01-1 825 DETAILED INSPECTION OF FUSELAGE FORWARDCARGO DOOR HINGE FITTING AND EXTERNALATTACHMENT AREA24000 FC 13800 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321532135-01-2 825 GENERAL VISUALINSPECTION OF FORWARD CARGODOOR CUTOUT, VISIBLE PART OF LATERAL FR 24A ANDFR 281200 FCOR2400 FH1200 FCOR2400 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321532135-01-3 825 GENERAL VISUALINSPECTION OF FORWARD CARGODOOR CUTOUT, VISIBLE PART OF LATERAL FR 24A ANDFR 281100 FC 1100 FC GROUP 19-1C532135-01-4 825 GENERAL VISUALINSPECTION OF FORWARD CARGODOOR CUTOUT, VISIBLE PART OF LATERAL FR 24A ANDFR 281700 FC 1700 FC GROUP 18-1EA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 24EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE532137-01-1 825 DETAILED INSPECTION OF FORWARD CARGO DOORCUTOUT PANELS, UPPERAND LOWER CORNERS,EXTERNAL SURFACE9700 FCOR19400 FH9700 FCOR19400 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321532137-01-2 825 DETAILED INSPECTION OF FORWARD CARGO DOORCUTOUT PANELS, UPPERAND LOWER CORNERS,EXTERNAL SURFACE9000 FC 9000 FC GROUP 19-1C532150-01-1 833 DETAILED INSPECTION OF FORWARD EMERGENCY EXITSKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE,LH13500 FCOR35900 FH13500 FCOR35900 FHGROUP 21-1AORGROUP 21-2A532150-01-2 833 DETAILED INSPECTION OF FORWARD EMERGENCY EXITSKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE,LH12600 FCOR33500 FH12600 FCOR33500 FHGROUP 21-1BORGROUP 21-2B532151-01-1 843 DETAILED INSPECTION OF FORWARD EMERGENCY EXITSKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE,RH9500 FCOR25100 FH9500 FCOR25100 FHGROUP 21-1AORGROUP 21-2A532151-01-2 843 DETAILED INSPECTION OF FORWARD EMERGENCY EXITSKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE,RH9200 FCOR24500 FH9200 FCOR24500 FHGROUP 21-1BORGROUP 21-2B532152-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND FORWARD EMERGENCY EXIT SKIN CUT OUTBETWEEN FR 35 AND FR 35.3 AND FROM STRINGER 8 TOSTRINGER 23, EXTERNAL SURFACE, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF ZONAL TASK ZL-200-02-4.20000 FCOR42000 FH20000 FCOR42000 FHA321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 25EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 532155-01-1 825CARGO FLOORPANELS REMOVEDINSULATIONREMOVEDDETAILED INSPECTIONOF FRAME SPLICES ATSTRINGER 35 LH, FROM FR 24 TO FR 3434000 FC 11000 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100ORA320-200PRE 30748ORA321PRE 30748R 532155-01-2 825CARGO FLOORPANELS REMOVEDINSULATIONREMOVEDDETAILED INSPECTIONOF FRAME SPLICES ATSTRINGER 35 LH, FROM FR 24 TO FR 3432400 FC 10500 FC GROUP 18-1AORGROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748532156-01-1 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 35.4 AND FR 35.8 FROMSTRINGER 8 TO STRINGER 14 AND STRINGER 18 TOSTRINGER 23, LH/RH24000 FCOR42000 FH4700 FCOR12600 FHGROUP 21-1AORGROUP 21-2A532156-01-2 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 35.4 AND FR 35.8 FROMSTRINGER 8 TO STRINGER 14 AND STRINGER 18 TOSTRINGER 23, LH/RH24000 FCOR42000 FH4400 FCOR11800 FHGROUP 21-1BORGROUP 21-2B532165-01-1 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREASCOVERED BY BELLY FAIRING5400 FC 5400 FC A320-200A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 26EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE532165-01-2 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREASCOVERED BY BELLY FAIRING5600 FC 5600 FC GROUP 19-1AORGROUP 19-1B532165-01-3 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 24 AND FR 35.8, FROMSTRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPTAREAS COVERED BY BELLY FAIRING3600 FC 3600 FC A321532165-01-4 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREASCOVERED BY BELLY FAIRING4000 FC 4000 FC GROUP 18-1A532165-01-7 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREASCOVERED BY BELLY FAIRING8100 FC 8100 FC GROUP 19-1C532165-01-8 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREASCOVERED BY BELLY FAIRINGNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532165-02-5.1600 FC 1600 FC GROUP 18-1E532165-02-4 DELETED FROM ALS PART 2 AT REVISION 01532165-02-5 N/A DETAILED INSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREASCOVERED BY BELLY FAIRINGNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532165-01-8.5800 FC 5800 FC GROUP 18-1E532166-01-1 LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OFFUSELAGE SKIN AT FR 35AND 10 CM FORWARD, AT LEVEL OF STRINGER 30,INTERNAL SIDE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-1.43400 FCOR86900 FH5400 FCOR10800 FHGROUP 19-1AORGROUP 19-1BORA320A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 27EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE532166-02-1 LINING REMOVEDINSULATIONREMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION(ROTO) OF FUSELAGESKIN AT FR 35 AND 10 CM FORWARD, AT LEVEL OFSTRINGER 30, INTERNAL SIDE, LH/RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-1.43400 FCOR86900 FH18800 FCOR37700 FHGROUP 19-1AORGROUP 19-1BORA320R 532170-01-1 825 GENERAL VISUALINSPECTION OF FORWARD CARGODOOR LOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 25 AND FR 27A, EXTERNAL PORTION (6PLACES)9300 FC 9300 FC GROUP 19-1APRE 30748ORGROUP 19-1BPRE 30748ORA320-100ORA320-200PRE 30748ORA321PRE 30748R 532170-01-2 825 GENERAL VISUALINSPECTION OF FORWARD CARGODOOR LOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 25 AND FR 27A, EXTERNAL PORTION (6PLACES)9100 FC 9100 FC GROUP 19-1APOST 30748ORGROUP 19-1BPOST 30748ORA320-200POST 30748ORA321POST 30748532170-01-3 825 GENERAL VISUALINSPECTION OF FORWARD CARGODOOR LOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 25 AND FR 26A, EXTERNAL PORTION (4PLACES)9100 FC 9100 FC GROUP 18-1A532170-01-6 825 GENERAL VISUALINSPECTION OF FORWARD CARGODOOR LOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 25 AND FR 27A, EXTERNAL PORTION (6PLACES)8400 FC 8400 FC GROUP 18-1EORGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 28EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 532186-01-1 N/A SPECIAL DETAILED INSPECTION (LFEC) OFCIRCUMFERENTIAL JOINT AT FR 35, BETWEENSTRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE48000 FCOR96000 FH13300 FCOR26600 FHA320-200PRE 160000WFD532186-01-2 N/A SPECIAL DETAILED INSPECTION (LFEC) OFCIRCUMFERENTIAL JOINT AT FR 35, BETWEENSTRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE42700 FCOR60000 FH13300 FCOR34400 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA321532187-01-1 N/A SPECIAL DETAILED INSPECTION (LFEC) OFCIRCUMFERENTIAL JOINT AT FR 35.8, BETWEENSTRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE44300 FCOR60000 FH17500 FCOR52500 FHA321R 532190-01-1 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE AROUND WATER DRAIN PANEL CUTOUT,BETWEEN FR 25 AND FR 29 AT STRINGER 43 LH48000 FC 8100 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320PRE 160000ORA321532190-01-2 DELETED FROM ALS PART 2 AT REVISION 01532190-01-3 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE AROUND WATER DRAIN PANEL CUTOUT,BETWEEN FR 25 AND FR 29 AT STRINGER 43 LH12000 FC 1500 FC GROUP 19-1C532195-01-1 DELETED FROM ALS PART 2 AT REVISION 01532195-01-2 DELETED FROM ALS PART 2 AT REVISION 01532195-01-3 131AC 825 GENERAL VISUAL INSPECTION OF FORWARD CARGODOOR ACTUATOR ATTACH BRACKETS, BETWEEN CABINFLOOR BEAMS, FROM FR 25A TO FR 27A11400 FC 11400 FC GROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 29EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE533105-01-1 734 744 DETAILEDINSPECTION OF MLG BAY FUSELAGE SIDEPANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46,INCLUDING SLANTED FRAMESAND SIDE BOX, LH/RH28400 FCOR60000 FH12900 FCOR35400 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100533105-01-2 DELETED FROM ALS PART 2 AT REVISION 01533105-01-4 734 744 DETAILEDINSPECTION OF MLG BAY FUSELAGE SIDEPANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46,INCLUDING SLANTED FRAMESAND SIDE BOX, LH/RH23600 FCOR60000 FH10700 FCOR29400 FHGROUP 21-1BORGROUP 21-2B533105-01-6 734 744 DETAILEDINSPECTION OF MLG BAY FUSELAGE SIDEPANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46,INCLUDING SLANTED FRAMESAND SIDE BOX, LH/RH13100 FCOR56400 FH9000 FCOR38700 FHGROUP 19-1C533105-01-8 734 744 DETAILEDINSPECTION OF MLG BAY FUSELAGE SIDEPANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46,INCLUDING SLANTED FRAMESAND SIDE BOX, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533105-01-2.27100 FCOR60000 FH10700 FCOR29400 FHGROUP 21-1AORGROUP 21-2A533109-01-1 CABIN FLOORPANELS REMOVEDINSULATIONREMOVEDAIR CONDITIONINGDUCT REMOVEDDETAILED INSPECTION OFUPPER SURFACES OFPRESSURE DECK MEMBRANES AND SIDE BOXES,BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONSTO LONGITUDINAL BEAMS AND SUPPORT RIBS, LH/RH20000 FCOR55000 FH12300 FCOR33800 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100533109-01-2 CABIN FLOORPANELS REMOVEDINSULATIONREMOVEDAIR CONDITIONINGDUCT REMOVEDDETAILED INSPECTION OFUPPER SURFACES OFPRESSURE DECK MEMBRANES AND SIDE BOXES,BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONSTO LONGITUDINAL BEAMS AND SUPPORT RIBS, LH/RH20000 FCOR55000 FH10100 FCOR27800 FHA321533109-01-3 CABIN FLOORPANELS REMOVEDINSULATIONREMOVEDAIR CONDITIONINGDUCT REMOVEDDETAILED INSPECTION OFUPPER SURFACES OFPRESSURE DECK MEMBRANES AND SIDE BOXES,BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONSTO LONGITUDINAL BEAMS AND SUPPORT RIBS, LH/RH13100 FCOR56400 FH9000 FCOR38700 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 30EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 533111-01-1 734 744 DETAILEDINSPECTION OF LOWER SURFACE OFPRESSURE DECK MEMBRANES, BETWEEN FR 42 AND FR46, INCLUDING CONNECTIONS TO LONGITUDINALBEAMS, SIDE BOXES, SUPPORT RIBS, REAR SPAR OFCENTER WING BOX AND PRESSURE BULKHEAD, LH/RH24000 FCOR48000 FH8400 FCOR16800 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320PRE 160001533111-01-2 734 744 DETAILEDINSPECTION OF LOWER SURFACE OFPRESSURE DECK MEMBRANES, BETWEEN FR 42 AND FR46, INCLUDING CONNECTIONS TO LONGITUDINALBEAMS, SIDE BOXES, SUPPORT RIBS, REAR SPAR OFCENTER WING BOX AND PRESSURE BULKHEAD, LH/RH22000 FCOR60000 FH8000 FCOR22000 FHA321533122-01-1 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREA AT FR 47,FROM STRINGER 10, LH/RH TO CROWN CENTERLINE,EXTERNAL SURFACE33300 FC 11500 FC A320-100R 533122-01-2 N/A DETAILED INSPECTIONOF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREA AT FR 47,FROM STRINGER 10, LH/RH TO CROWN CENTERLINE,EXTERNAL SURFACE33000 FC 9200 FC A320-200POST 34650ORA320-200POST 152970ORA321533122-01-3 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREA AT FR 47/51,FROM STRINGER 10, LH/RH TO CROWN CENTERLINE,EXTERNAL SURFACE33300 FC 11500 FC GROUP 19-1AORGROUP 19-1B533122-01-4 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREA AT FR 47/54,FROM STRINGER 10, LH/RH TO CROWN CENTERLINE,EXTERNAL SURFACE33300 FC 11500 FC GROUP 18-1A533124-01-1 DELETED FROM ALS PART 2 AT REVISION 01533124-01-2 DELETED FROM ALS PART 2 AT REVISION 01533124-01-3 DELETED FROM ALS PART 2 AT REVISION 01533124-01-4 DELETED FROM ALS PART 2 AT REVISION 01533125-01-1 DELETED FROM ALS PART 2 AT REVISION 01533125-01-2 DELETED FROM ALS PART 2 AT REVISION 01533125-01-3 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 31EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE533125-01-4 DELETED FROM ALS PART 2 AT REVISION 01533126-01-1 DELETED FROM ALS PART 2 AT REVISION 01533126-01-2 DELETED FROM ALS PART 2 AT REVISION 01533126-01-3 DELETED FROM ALS PART 2 AT REVISION 01533126-01-4 DELETED FROM ALS PART 2 AT REVISION 01533126-02-1 DELETED FROM ALS PART 2 AT REVISION 01533126-02-2 DELETED FROM ALS PART 2 AT REVISION 01533126-02-3 DELETED FROM ALS PART 2 AT REVISION 01533126-02-4 DELETED FROM ALS PART 2 AT REVISION 01533127-01-1 DELETED FROM ALS PART 2 AT REVISION 01533127-01-2 DELETED FROM ALS PART 2 AT REVISION 01533127-01-3 DELETED FROM ALS PART 2 AT REVISION 01533127-01-4 DELETED FROM ALS PART 2 AT REVISION 01533128-01-1 833 834 843844DETAILED INSPECTION OF EMERGENCY EXIT SKINCUTOUTS, UPPER AND LOWER CORNERS, LH/RH24000 FCOR48000 FH9800 FCOR24500 FHA320-100R 533128-01-2 833 834 843844DETAILED INSPECTION OF EMERGENCY EXIT SKINCUTOUTS, UPPER AND LOWER CORNERS, LH/RH31100 FCOR62200 FH10900 FCOR21900 FHA320-200PRE 34650PRE 152970PRE 160001533128-01-3 834 844 DETAILEDINSPECTION OF EMERGENCY EXIT SKINCUTOUTS, UPPER AND LOWER CORNERS, LH/RH24000 FCOR60000 FH9800 FCOR24500 FHGROUP 19-1APRE 32208ORGROUP 19-1BPRE 32208533128-01-4 833 834 843844DETAILED INSPECTION OF EMERGENCY EXIT SKINCUTOUTS, UPPER AND LOWER CORNERS, LH/RH24000 FCOR60000 FH9600 FCOR24000 FHGROUP 19-1APOST 32208ORGROUP 19-1BPOST 32208533128-01-5 834 844 DETAILEDINSPECTION OF EMERGENCY EXIT SKINCUTOUTS, UPPER AND LOWER CORNERS, LH/RH24000 FCOR60000 FH7600 FCOR19000 FHGROUP 18-1AR 533128-01-6 833 834 843844DETAILED INSPECTION OF EMERGENCY EXITS SKINCUTOUTS, UPPER AND LOWER CORNERS, LH/ RH24000 FCOR60000 FH8700 FCOR21700 FHA320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 32EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTEN 533128-01-7 833 834 843844DETAILED INSPECTION OF EMERGENCY EXITS SKINCUTOUTS, UPPER AND LOWER CORNERS, LH/ RH28000 FCOR56000 FH10700 FCOR21400 FHA320-200POST 160001533130-01-1 DELETED FROM ALS PART 2 AT REVISION 01533130-01-2 ANTI-COLLISIONLIGHT COVERREMOVEDANTI-COLLISIONLIGHT REMOVEDDETAILED INSPECTION OF SKIN AROUND ANTICOLLISION LIGHT CUTOUT, BETWEEN FR 40 AND FR 41AND BETWEEN STRINGER 1, LH/RH, EXTERNALSURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533130-01-1.30500 FC 17000 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORGROUP 21-1A533130-01-3 ANTI-COLLISIONLIGHT COVERREMOVEDANTI-COLLISIONLIGHT REMOVEDDETAILED INSPECTION OF SKIN AROUND ANTICOLLISION LIGHT CUTOUT, BETWEEN FR 40 AND FR 41AND BETWEEN STRINGER 1, LH/RH, EXTERNALSURFACE27800 FC 13500 FC GROUP 21-2AR 533130-01-4 ANTI-COLLISIONLIGHT COVERREMOVEDANTI-COLLISIONLIGHT REMOVEDDETAILED INSPECTION OF SKIN AROUND ANTICOLLISION LIGHT CUTOUT, BETWEEN FR 40 AND FR 41AND BETWEEN STRINGER 1, LH/RH, EXTERNALSURFACE27800 FC 11500 FC A320-200POST 34650ORA320-200POST 152970ORGROUP 21-1BORGROUP 21-2B533131-01-1 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 33EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 533131-01-5 ANTENNA COVERREMOVEDANTENNA REMOVEDDETAILED INSPECTION OF SKIN AROUND ADF 1ANTENNA CUTOUT, BETWEENFR 44 AND FR 45 ANDBETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK533131-01-1.26300 FC 15700 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA320-200POST 34650ORA320-200POST 152970ORA321D 533132-01-1 DELETED FROM ALS PART 2 AT REVISION 02533132-01-2 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOWFORGINGS AND FUSELAGE SKIN IN WINDOW FORGINGAREA, BETWEEN FR 35.8 AND FR 47, LH/RH, EXTERNALSURFACE36300 FC 9300 FC A321533132-01-3 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOWFORGINGS AND FUSELAGE SKIN IN WINDOW FORGINGAREA, BETWEEN FR 35 AND FR47/51, LH/RH, EXTERNALSURFACE36300 FC 9300 FC GROUP 19-1AORGROUP 19-1B533132-01-4 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOWFORGINGS AND FUSELAGE SKIN IN WINDOW FORGINGAREA, BETWEEN FR 35 AND FR47/54, LH/RH, EXTERNALSURFACE36300 FC 9300 FC GROUP 18-1A533132-01-5 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOWFORGINGS AND FUSELAGE SKIN IN WINDOW FORGINGAREA, BETWEEN FR 35 ANDFR 47, LH/RH, EXTERNALSURFACE36300 FC 9300 FC A320-100R 533138-01-1 LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF LOWER SKIN OFLONGITUDINAL LAP JOINT AT STRINGER 18 LH ANDSTRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNALNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533138-02-1.40000 FCOR80000 FH17400 FCOR34900 FHA320-200PRE 39516A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 34EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE533138-01-2 LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF LOWER SKIN OFLONGITUDINAL LAP JOINT AT STRINGER 18 LH ANDSTRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNALNOTE: THIS TASK IS ANALTERNATIVE INSPECTION TOTASK 533138-02-2.40000 FC 10000 FC GROUP 19-1AORGROUP 19-1BORA320-100ORA321R 533138-02-1 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF LOWER SKINOF LONGITUDINAL LAP JOINT AT STRINGER 18 LH ANDSTRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNALNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533138-01-1.40000 FCOR80000 FH31400 FCOR62800 FHA320-200PRE 39516533138-02-2 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF LOWER SKINOF LONGITUDINAL LAP JOINT AT STRINGER 18 LH ANDSTRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNALNOTE: THIS TASK IS ANALTERNATIVE INSPECTION TOTASK 533138-01-2.40000 FC 12000 FC GROUP 19-1AORGROUP 19-1BORA320-100ORA321R 533139-01-1 LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OFFRAME FLANGES AT FR 38AND 39, AND AT FR 40 AND 41 BETWEEN STRINGER 12AND STRINGER 21, LH/RH,AND LONGITUDINAL BEAMFLANGE AT STRINGER 20A LH AND STRINGER 20A RH,BETWEEN FR 38 AND FR 39 AND BETWEEN FR 40 ANDFR 4127400 FCOR54800 FH7400 FCOR14900 FHA320-200PRE 34650PRE 152970PRE 160001533139-01-2 LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OFFRAME FLANGES AT FR 40AND 41, BETWEEN STRINGER 12 AND STRINGER 21,LH/RH, AND LONGITUDINALBEAM FLANGE AT STRINGER20A LH AND STRINGER 20A RH, BETWEEN FR 40 AND FR4124000 FC 7400 FC GROUP 19-1APRE 32208ORGROUP 19-1BPRE 32208A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 35EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 533139-01-3 LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OFFRAME FLANGES AT FR 38AND FR 39 AND AT FR 40 AND FR 41 BETWEENSTRINGER 12 AND STRINGER 21, LH/RH, ANDLONGITUDINAL BEAM FLANGEAT STRINGER 20A LH ANDSTRINGER 20A RH, BETWEEN FR 38 AND FR 39, ANDBETWEEN FR 40A FR 4124000 FC 7400 FC GROUP 19-1APOST 32208ORGROUP 19-1BPOST 32208ORA320-100ORA320-200POST 34650ORA320-200POST 152970533140-01-1 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47,FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE34500 FC 6900 FC A320-100533140-01-2 DELETED FROM ALS PART 2 AT REVISION 01533140-01-3 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47,FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE40000 FC 17000 FC A321533140-01-4 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47/51,FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE38700 FC 12800 FC GROUP 19-1AORGROUP 19-1B533140-01-5 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47/54,FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE33700 FC 11000 FC GROUP 18-1AR 533140-01-7 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47,FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE31100 FC 5200 FC A320-200POST 34650ORA320-200POST 152970533140-01-8 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47,FROM STRINGER 10, LH/RH, TO CROWN CENTER LINENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 533140-01-2.40300 FCOR80700 FH14800 FCOR29700 FHA320-200PRE 31012WFDA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 36EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE533141-01-1 191BT 191EB 192BT192EBDETAILED INSPECTION OFFUSELAGE SKIN, BETWEENFR 35 AND FR 36 AND BETWEEN STRINGER 25 ANDSTRINGER 30, LH/RH, EXTERNAL SURFACE38600 FCOR77200 FH9800 FCOR19600 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320533141-01-2 191BT 191EB 192BT192EBDETAILED INSPECTION OFFUSELAGE SKIN, BETWEENFR 35.8 AND FR 36 AND BETWEEN STRINGER 25 ANDSTRINGER 30, LH/RH, EXTERNAL SURFACE38600 FCOR60000 FH9800 FCOR19600 FHA321533142-01-1 ALI REPLACED BY SB A320 53-1060 AT ALI DOCUMENTISSUE 6R 533143-01-1 734 744 DETAILED INSPECTION OF SIDE BOX BEAM IN AREAOFATTACHMENT TO FR 46, LH/RH40000 FCOR80000 FH10600 FCOR21200 FHGROUP 19-1AORGROUP 19-1BORA320PRE 31067ORA321R 533144-01-1 LINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OFFRAME ATTACHMENTS TOPRESSURE FLOOR FROM FR 42 TO FR 46, LH/RH33100 FCOR66200 FH12800 FCOR25600 FHGROUP 19-1AORGROUP 19-1BORA321533152-01-1 DELETED FROM ALS PART 2 AT REVISION 01533152-01-3 131NW 131PW132PWINSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDDETAILED INSPECTION OFPRESSURE BULKHEADFORWARD FACE AT FR 35.8 AND PRESSURE DECKUPPER SURFACE, BETWEENFR 35.8 AND FR 36,INCLUDING CONNECTIONS TO CENTER WING BOX ATFR35.8 AND FR 3631000 FC 9100 FC A321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 37EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE533152-01-4 131NW 131PW132PWINSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDDETAILED INSPECTION OFPRESSURE BULKHEADFORWARD FACE AT FR 35 AND PRESSURE DECK UPPERSURFACE, BETWEEN FR 35 AND FR 36, INCLUDINGCONNECTIONS TO CENTER WING BOX AT FR 35 AND FR3631000 FC 9100 FC GROUP 19-1AORGROUP 19-1B533152-01-5 131NW 131PW132PWINSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDDETAILED INSPECTION OFPRESSURE BULKHEADFORWARD FACE AT FR 35 AND PRESSURE DECK UPPERSURFACE, BETWEEN FR 35 AND FR 36, INCLUDINGCONNECTIONS TO CENTER WING BOX AT FR 35 AND FR3631000 FC 9100 FC GROUP 18-1A533152-01-7 DELETED FROM ALS PART 2 AT REVISION 01533152-01-9 131NW 131PW132PW825INSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDDETAILED INSPECTION OFPRESSURE BULKHEADFORWARD FACE AT FR 35 AND PRESSURE DECK UPPERSURFACE, BETWEEN FR 35 AND FR 36, INCLUDINGCONNECTIONS TO CENTER WING BOX AT FR 35 AND FR3631000 FC 9100 FC A320-100R 533152-01-10 131NW 131PW 132PW825INSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDPOTABLE WATERTANK REMOVEDDETAILED INSPECTION OFPRESSURE BULKHEADFORWARD FACE AT FR 35 AND PRESSURE DECK UPPERSURFACE, BETWEEN FR 35 AND FR 36, INCLUDINGCONNECTIONS TO CENTER WING BOX AT FR 35 AND FR3631000 FC 9100 FC A320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 38EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE533154-02-1 ALI SUPERSEDED BY SB A320 53-1195 AND SB A320 53-1196 AT ALS PART 2 REVISION 01NOTE: NTM PROCEDURES REFERENCED IN PREVIOUSESTABLISHED RAS AND REFERRING TO ALI 533154-02-1REMAIN VALID.R 533155-03-1 734 744 SPECIAL DETAILED INSPECTION (HFEC) OF KEELBEAMBOX ELLIPTICAL CUTOUTAT FR 46, LH/RH38400 FCOR60000 FH17500 FCOR39300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA320-200POST 34650ORA320-200POST 152970ORA321R 533180-01-1 CABIN FLOORPANELS REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION (HFEC) OF UPPERSURFACE OF PRESSURE DECK MEMBRANES AND SIDEBOXES, BETWEEN FR42 AND FR 46, AT CONNECTIONS TO LONGITUDINALBEAMS AND SUPPORT RIBS (INCLUDING LATERALOUTER PART OF CONNECTION PLATES) AT Y=+/- 254MM, Y=+/- 765 MM, Y=+/- 1292 MM AND Y=+/- 1650 MM48100 FCOR96200 FH6100 FCOR12200 FHA320-200PRE 160001WFD533181-01-1 734 744CABIN FLOORPANELS REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION (HFEC) OFLONGITUDINAL BEAMS FLANGES AT ATTACHMENT AREATO PRESSURE DECK MEMBRANE BETWEEN FR 42 ANDFR 46 AT Y=+/- 254 MM, Y=+/- 765MM, Y=+/- 1292 MM ANDSIDE BOX FLANGE AT Y=+/- 1650 MM48500 FCOR97000 FH17200 FCOR34400 FHA320-200 WFDA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 39EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 533185-01-1 131NW, 131PW,132PW825INSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (LFEC AND ROTO) OFPRESSURE DECK MEMBRANE UPPER SURFACE TOCENTER WING BOX, UNDER TITANIUM ANGLECONNECTION AND CORNER BRAKETS, AT FR 3648000 FCOR96000 FH31200 FCOR62500 FHA320-200PRE 21003PRE 34650PRE 152970PRE 160001R 533185-01-2 131NW, 131PW,132PW825INSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDPOTABLE WATERTANK REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (LFEC AND ROTO) OFPRESSURE DECK MEMBRANE UPPER SURFACE TOCENTER WING BOX, UNDER TITANIUM ANGLECONNECTION AND CORNER BRAKETS, AT FR 3648000 FCOR96000 FH31200 FCOR62500 FHA320-200POST 21003PRE 34650PRE 152970PRE 160001533186-01-1 131PW 132PWINSULATIONREMOVEDRECIRCULATIONFILTER REMOVEDAIR CONDITIONINGDUCTS REMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FR 35FORWARD FACE TO PRESSURE BULKHEADATTACHMENTS, AROUND RIVETS AND HOLES BETWEENSTR 28 AND STR 31, LH/RH40000 FCOR80000 FH15000 FCOR30000 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321533188-01-1 191BB 191EB 192EB192FBDETAILED INSPECTION OFFR35, PRESSURE BULKHEAD,AFT FACE, LOWER PART OF VERTICAL STRUTS (200 MMFROM BOTTOM) AT Y=+/-765 MM (2 PLACES)30300 FC 8400 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 40EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE533188-01-2 191BB 191EB 192EB192FBDETAILED INSPECTION OF FR 35.8 PRESSUREBULKHEAD, AFT FACE, LOWER PART OF VERTICALSTRUTS (200 MM FROM BOTTOM) AT Y= +/-765 MM (2PLACES)30300 FC 8400 FC A321533189-01-1 191BT 192BTAIR CONDITIONINGDUCTS REMOVEDSPECIAL DETAILED INSPECTION (LFEC) OF ANGLEFITTING FORWARD ATTACHMENT, AT FRAME 36 ATSTRINGER 30, LH/RH26900 FCOR53800 FH21500 FCOR43000 FHGROUP 18-1APRE 150069ORGROUP 19-1APRE 150069ORGROUP 19-1BPRE 150069ORA320PRE 150069R 533189-01-3 191BT 192BTAIR CONDITIONINGDUCTS REMOVEDSPECIAL DETAILED INSPECTION (LFEC) OF ANGLEFITTING FORWARD ATTACHMENT, AT FRAME 36 ATSTRINGER 30, LH/RH50100 FCOR100200 FH32600 FCOR65200 FHA320POST 150069PRE 160001534101-01-1 DELETED FROM ALS PART 2 AT REVISION 01534101-01-2 DELETED FROM ALS PART 2 AT REVISION 01534101-01-3 DELETED FROM ALS PART 2 AT REVISION 01534102-01-1 DELETED FROM ALS PART 2 AT REVISION 01534102-01-2 DELETED FROM ALS PART 2 AT REVISION 01534102-01-3 DELETED FROM ALS PART 2 AT REVISION 01534102-02-1 DELETED FROM ALS PART 2 AT REVISION 01534102-02-2 DELETED FROM ALS PART 2 AT REVISION 01534102-02-3 DELETED FROM ALS PART 2 AT REVISION 01534104-01-1 DELETED FROM ALS PART 2 AT REVISION 01534104-01-2 DELETED FROM ALS PART 2 AT REVISION 01534104-01-3 DELETED FROM ALS PART 2 AT REVISION 01534104-01-4 DELETED FROM ALS PART 2 AT REVISION 01534105-01-1 DELETED FROM ALS PART 2 AT REVISION 01534105-01-2 DELETED FROM ALS PART 2 AT REVISION 01534105-01-3 DELETED FROM ALS PART 2 AT REVISION 01534105-01-4 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 41EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534106-01-1 252HW 252LW 252PWINSULATIONREMOVEDDETAILED INSPECTIONOF FRAME SPLICES ANDADJACENT AREA FROM FR 53 TO FR 56, LOCATEDABOVE STRINGER 18 RH51300 FCOR102700 FH12900 FCOR25800 FHA320-200PRE 34650PRE 152970PRE 160001534106-01-4 252HW 252LW 252PWINSULATIONREMOVEDDETAILED INSPECTIONOF FRAME SPLICES ANDADJACENT AREA FROM FR 53 TO FR 56, LOCATEDABOVE STRINGER 18 RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534106-02-4.12000 FCOR69000 FH4000 FCOR23000 FHGROUP 19-1C534106-02-4 252HW 252LW 252PWINSULATIONREMOVEDSPECIAL DETAILED INSPECTION (US) OF FRAMESPLICES AND ADJACENT AREAFROM FR 53 TO FR 56,LOCATED ABOVE STRINGER 18 RHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534106-01-4.12000 FCOR69000 FH9100 FCOR52500 FHGROUP 19-1C534107-01-1 DELETED FROM ALS PART 2 AT REVISION 01534108-01-2 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 47 AND FR 70, FROM STRINGER23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREACOVERED BY BELLY FAIRING3000 FC 3000 FC A320ORA321534108-01-4 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 47/51 AND FR 70, FROMSTRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPTAREA COVERED BY BELLY FAIRING3000 FC 3000 FC GROUP 19-1AORGROUP 19-1B534108-01-6 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 47/54 AND FR 70, FROMSTRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPTAREA COVERED BY BELLY FAIRING3000 FC 3000 FC GROUP 18-1A534108-01-7 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 47/51 AND FR 70, FROMSTRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPTAREA COVERED BY BELLY FAIRING700 FCOR3200 FH700 FCOR3200 FHGROUP 19-1C534108-01-8 N/A GENERAL VISUALINSPECTION OF FUSELAGE EXTERNALSURFACE, BETWEEN FR 47/54 AND FR 70, FROMSTRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPTAREA COVERED BY BELLY FAIRING1300 FC 1300 FC GROUP 18-1E534111-01-1 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 42EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534111-01-2 ANTENNA COVERREMOVEDANTENNA REMOVEDDETAILED INSPECTION OF SKIN AROUND ADF2ANTENNA CUTOUT, BETWEENFR 47.1 AND FR 47.2BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACENOTE: FOR PRE 20053 AIRCRAFT RETROFITTED,THRESHOLD IS TO BE COUNTED FROM SBEMBODIMENT.28800 FCOR60000 FH16700 FCOR41700 FHA321POST 20053R 534111-01-3 ANTENNA COVERREMOVEDANTENNA REMOVEDDETAILED INSPECTION OF SKIN AROUND ADF2ANTENNA CUTOUT, BETWEENFR 52 AND FR 53,BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACENOTE: FOR PRE 20053 AIRCRAFT RETROFITTED,THRESHOLD IS TO BE COUNTED FROM SBEMBODIMENT.28800 FCOR60000 FH16700 FCOR41700 FHGROUP 19-1APOST 20053ORGROUP 19-1BPOST 20053R 534111-01-4 ANTENNA COVERREMOVEDANTENNA REMOVEDDETAILED INSPECTION OF SKIN AROUND ADF2ANTENNA CUTOUT, BETWEENFR 55 AND FR 56,BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACENOTE: FOR PRE 20053 AIRCRAFT RETROFITTED,THRESHOLD IS TO BE COUNTED FROM SBEMBODIMENT.28800 FCOR60000 FH16700 FCOR41700 FHGROUP 18-1APOST 20053R 534111-01-7 ANTENNA COVERREMOVEDANTENNA REMOVEDDETAILED INSPECTION OF SKIN AROUND ADF2ANTENNA CUTOUT, BETWEENFR 48 AND FR 49BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE28800 FCOR60000 FH16700 FCOR41700 FHA320-100POST 20053ORA320-200POST 34650ORA320-200POST 152970534112-01-1 DELETED FROM ALS PART 2 AT REVISION 01534112-01-3 ANTENNA REMOVED DETAILED INSPECTION OF SKIN AROUND VHF 3ANTENNA CUTOUT, BETWEENFR 56 AND FR 57 ANDBETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE31200 FCOR60000 FH18700 FCOR56100 FHGROUP 19-1AORGROUP 19-1B534112-01-4 ANTENNA REMOVED DETAILED INSPECTION OF SKIN AROUND VHF 3ANTENNA CUTOUT, BETWEENFR 61 AND FR 62 ANDBETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE31200 FCOR60000 FH18700 FCOR56100 FHGROUP 18-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 43EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534112-01-7 ANTENNA REMOVED DETAILEDINSPECTION OF SKIN AROUND VHF 3ANTENNA CUTOUT, BETWEENFR 52 AND FR 53 ANDBETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF 534112-01-1.31200 FCOR60000 FH18700 FCOR56100 FHA320-100ORA320-200POST 34650ORA320-200POST 152970ORA321534113-01-1 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS AT FR 64,FROM STRINGER 10, LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE40000 FC 13500 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100534113-01-2 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS AT FR 64,FROM STRINGER 10, LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE36000 FC 10900 FC A321534113-01-3 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS AT FR 64,FROM STRINGER 10, LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE12500 FCOR56600 FH10500 FCOR47600 FHGROUP 19-1CPRE 31012534114-01-1 DELETED FROM ALS PART 2 AT REVISION 01534114-01-2 DELETED FROM ALS PART 2 AT REVISION 01534114-01-3 DELETED FROM ALS PART 2 AT REVISION 01534114-01-4 DELETED FROM ALS PART 2 AT REVISION 01534115-01-1 DELETED FROM ALS PART 2 AT REVISION 01534115-01-2 DELETED FROM ALS PART 2 AT REVISION 01534115-01-3 DELETED FROM ALS PART 2 AT REVISION 01534115-01-4 DELETED FROM ALS PART 2 AT REVISION 01534116-01-1 DELETED FROM ALS PART 2 AT REVISION 01534116-01-2 DELETED FROM ALS PART 2 AT REVISION 01534116-01-3 DELETED FROM ALS PART 2 AT REVISION 01534116-01-4 DELETED FROM ALS PART 2 AT REVISION 01534116-02-1 DELETED FROM ALS PART 2 AT REVISION 01534116-02-2 DELETED FROM ALS PART 2 AT REVISION 01534116-02-3 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 44EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534116-02-4 DELETED FROM ALS PART 2 AT REVISION 01534117-01-1 DELETED FROM ALS PART 2 AT REVISION 01534117-01-2 DELETED FROM ALS PART 2 AT REVISION 01534117-01-3 DELETED FROM ALS PART 2 AT REVISION 01534117-01-4 DELETED FROM ALS PART 2 AT REVISION 01534121-01-1 DELETED FROM ALS PART 2 AT REVISION 01534121-01-3 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 64,FROM STRINGER 10, LH/RH TO CROWN CENTERLINE12500 FCOR56500 FH10500 FCOR47600 FHGROUP 19-1CPRE 31012534121-01-4 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 64,FROM STRINGER 10, LH/RH TO CROWN CENTERLINE40000 FC 15000 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA321534122-01-1 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGESKIN UNDER THE COMPLETE OUTER RIVET ROW OF THEDOUBLER OF THE SATCOM ANTENNA, IN THE AREA OFFR 58 TO FR 61, STGR 2 LH AND STGR 2 RH, EXCEPTRIVETS AT STRINGER OR FRAME JUNCTIONS36200 FCOR60000 FH8700 FCOR17400 FHGROUP 19-1APOST 26372ORGROUP 19-1APOST 26995ORGROUP 19-1APOST 32856ORGROUP 19-1BPOST 26372ORGROUP 19-1BPOST 26995ORGROUP 19-1BPOST 32856WFDA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 45EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534122-01-3 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGESKIN UNDER THE COMPLETE OUTER RIVET ROW OF THEDOUBLER OF THE SATCOM ANTENNA, IN THE AREA OFFR 58 TO FR 61, STGR 2 LH AND STGR 2 RH, EXCEPTRIVETS AT STRINGER OR FRAME JUNCTIONS41300 FCOR60000 FH7800 FCOR15600 FHA321POST 26995ORA321POST 32856WFDR 534123-01-1 832 842LINING REMOVEDINSULATIONREMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION(ROTO) OF FUSELAGEINTERNAL STRUCTURE, FRAME 66 AND FRAME 68 INNERCAP JOINT TO GUSSETS PLATE FROM STRINGER 10 TOSTRINGER 16, LH/RH41600 FCOR60000 FH6300 FCOR12600 FHGROUP 18-1A534124-01-1 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION (HFEC) OF AFTPASSENGER/CREW DOORCUTOUT, AFT UPPERCORNER BETWEEN STRINGER 8 AND STRINGER 10,FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE,LH/RH22100 FCOR44200 FH5400 FCOR10800 FHGROUP 18-1A534124-01-2 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION (HFEC) OF AFTPASSENGER/CREW DOORCUTOUT, AFT UPPERCORNER BETWEEN STRINGER 8 AND STRINGER 10,FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE,LH/RH28300 FCOR56600 FH6600 FCOR13200 FHGROUP 19-1AORGROUP 19-1B534124-01-3 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION (HFEC) OF AFTPASSENGER/CREW DOORCUTOUT, AFT UPPERCORNER BETWEEN STRINGER 8 AND STRINGER 10,FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE,LH/RH32700 FCOR65400 FH7500 FCOR15000 FHA320-200534124-01-4 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION (HFEC) OF AFTPASSENGER/CREW DOORCUTOUT, AFT UPPERCORNER BETWEEN STRINGER 8 AND STRINGER 10,FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE,LH/RH30900 FCOR60000 FH7200 FCOR14400 FHA321534125-01-1 N/A SPECIAL DETAILEDINSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WATER SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT ANDBELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKINTO REINFORCEMENT JOINT, LH29400 FCOR58800 FH2600 FCOR5200 FHGROUP 18-1A WFDA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 46EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534125-01-2 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WATER SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT ANDBELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKINTO REINFORCEMENT JOINT, LH32100 FCOR60000 FH3000 FCOR6000 FHGROUP 19-1APRE 160055ORGROUP 19-1BPRE160055WFDR 534125-01-3 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WATER SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT ANDBELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKINTO REINFORCEMENT JOINT, LH36100 FCOR72200 FH3200 FCOR6400 FHA320-200PRE 153074PRE 160055PRE 160500WFDR 534125-01-4 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WATER SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT ANDBELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKINTO REINFORCEMENT JOINT, LH41500 FCOR60000 FH3500 FCOR7000 FHA321PRE 160055WFD534126-01-1 N/A SPECIAL DETAILEDINSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WASTE SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOWSTRINGER 33, TWO UPPER RIVET ROWS AT SKIN TOREINFORCEMENT JOINT, RH27800 FCOR55600 FH2000 FCOR4000 FHGROUP 18-1A WFDR 534126-01-2 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WASTE SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOWSTRINGER 33, TWO UPPER RIVET ROWS AT SKIN TOREINFORCEMENT JOINT, RH28700 FCOR57400 FH2200 FCOR4400 FHGROUP 19-1APRE 153073PRE 160055ORGROUP 19-1BPRE 153073PRE160055WFDR 534126-01-3 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WASTE SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOWSTRINGER 33, TWO UPPER RIVET ROWS AT SKIN TOREINFORCEMENT JOINT, RH30900 FCOR61800 FH2300 FCOR4600 FHA320-200PRE 153073PRE 160055PRE 160500WFDR 534126-01-4 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN EXTERNAL SURFACE AT WASTE SERVICE PANELCUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOWSTRINGER 33, TWO UPPER RIVET ROWS AT SKIN TOREINFORCEMENT JOINT, RH34400 FCOR60000 FH2400 FCOR4800 FHA321PRE 160055WFDA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 47EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534127-01-1 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGEINTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TOUPPER FRAME 68 BETWEEN STRINGER 4 ANDSTRINGER 5, LH/RH23500 FCOR47000 FH5000 FCOR10000 FHGROUP 18-1AR 534127-01-2 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGEINTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TOUPPER FRAME 68 BETWEEN STRINGER 4 ANDSTRINGER 5, LH/RH27700 FCOR55400 FH5700 FCOR11400 FHGROUP 19-1AORGROUP 19-1BR 534127-01-3 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGEINTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TOUPPER FRAME 68 BETWEEN STRINGER 4 ANDSTRINGER 5, LH/RH28700 FCOR57400 FH5800 FCOR11600 FHA320-200MSN 0124-9999R 534127-01-4 832 842LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGEINTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TOUPPER FRAME 68 BETWEEN STRINGER 4 ANDSTRINGER 5, LH/RH26400 FCOR52800 FH5600 FCOR11200 FHA321534129-01-1 832 842LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 66 WEB, LH/RH34800 FCOR60000 FH5900 FCOR11800 FHGROUP 18-1A534129-01-2 832 42LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 66 WEB, LH/RH40200 FCOR60000 FH8300 FCOR16600 FHGROUP 19-1AORGROUP 19-1BR 534129-01-3 832 842LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 66 WEB, LH/RH48000 FCOR96000 FH9700 FCOR19400 FHA320-200PRE 160500534129-01-4 832 842LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 66 WEB, LH/RH42300 FCOR60000 FH8800 FCOR17600 FHA321N 534129-01-5 832 842LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 66 WEB, LH/RH45500 FCOR91000 FH7800 FCOR15600 FHA320-200POST 160500534130-01-1 832 842LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 68 WEB, LH/RH30600 FCOR60000 FH5900 FCOR11800 FHGROUP 18-1A534130-01-2 832 42LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 68 WEB, LH/RH34100 FCOR60000 FH8300 FCOR16600 FHGROUP 19-1AORGROUP 19-1BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 48EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534130-01-3 832 842LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 68 WEB, LH/RH40900 FCOR81800 FH9700 FCOR19400 FHA320-200534130-01-4 832 842LINING REMOVEDBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF AFTPASSENGER/CREW DOOR CUTOUT, DOOR STOPFITTINGS HOLES AT FRAME 68 WEB, LH/RH39800 FCOR60000 FH8800 FCOR17600 FHA321534131-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND AFT PASSENGER/CREW DOOR CUTOUTS,BETWEEN FRAME 65 AND FRAME 70 AND FROMSTRINGER 6 TO STRINGER 26, EXTERNAL SURFACE(EXCEPT AREA UNDER SCUFF PLATE), LH/RH23800 FCOR47600 FH23800 FCOR47600 FHA320-200534131-01-3 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND AFT PASSENGER/CREW DOOR CUTOUTS,BETWEEN FRAME 65 AND FRAME 70 AND FROMSTRINGER 6 TO STRINGER 26, EXTERNAL SURFACE(EXCEPT AREA UNDER SCUFF PLATE), LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534131-01-1.23100 FCOR46200 FH23100 FCOR46200 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1B534131-01-4 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND AFT PASSENGER/CREW DOOR CUTOUTS,BETWEEN FRAME 65 AND FRAME 70 AND FROMSTRINGER 6 TO STRINGER 26, EXTERNAL SURFACE(EXCEPT AREA UNDER SCUFF PLATE), LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534131-01-1.23700 FCOR47400 FH23700 FCOR47400 FHA321534131-01-5 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND AFT PASSENGER/CREW DOOR CUTOUTS,BETWEEN FRAME 65 AND FRAME 70 AND FROMSTRINGER 6 TO STRINGER 26, EXTERNAL SURFACE(EXCEPT AREA UNDER SCUFF PLATE), LH/RH28200 FC 28200 FC A320-100534132-01-1 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RH12000 FC 10200 FC A320-100534132-01-2 DELETED FROM ALS PART 2 AT REVISION 01534132-01-3 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 49EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534132-01-4 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534132-01-1.16300 FCOR32600 FH10300 FCOR20600 FHA320-200PRE 160500534132-01-5 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534132-01-2.15900 FCOR31800 FH10000 FCOR20000 FHA321534132-01-6 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RHNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534132-01-3.12400 FCOR24800 FH7700 FCOR15400 FHGROUP 19-1AORGROUP 19-1B534132-01-7 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RH11300 FCOR22600 FH7100 FCOR14200 FHGROUP 18-1A534132-01-8 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RH6200 FCOR26900 FH5200 FCOR22700 FHGROUP 19-1C534132-01-9 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RH6700 FCOR20200 FH5700 FCOR17100 FHGROUP 18-1EN 534132-01-10 832 842 DETAILEDINSPECTION OF AFT PASSENGER/CREWDOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN ANDINTERNALLY THE VISIBLEPORTION OF THE INTERNALDOUBLER, LH/RH11200 FCOR22400 FH6900 FCOR13800 FHA320-200POST 160500A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 50EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534137-01-1 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF INTERNALDOUBLER, FORWARD AND AFT OF WASTE SERVICEPANEL CUTOUT, BETWEEN STRINGER 35 AND STRINGER39, RH57700 FCOR115400 FH24900 FCOR49800 FHA320-200534137-01-2 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF INTERNALDOUBLER, FORWARD AND AFT OF WASTE SERVICEPANEL CUTOUT, BETWEEN STRINGER 35 AND STRINGER39, RH38000 FCOR60000 FH8400 FCOR16800 FHGROUP 18-1A534137-01-3 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF INTERNALDOUBLER, FORWARD AND AFT OF WASTE SERVICEPANEL CUTOUT, BETWEEN STRINGER 35 AND STRINGER39, RH41900 FCOR60000 FH25500 FCOR51000 FHGROUP 19-1AORGROUP 19-1B534140-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME65 AND FRAME 66 AND FROM STRINGER 26 TOSTRINGER 31, RH, EXTERNAL SURFACE25900 FC 8100 FC A320-100R 534140-01-2 N/A GENERAL VISUALINSPECTION OF FUSELAGE SKINAROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME65 AND FRAME 66 AND FROM STRINGER 26 TOSTRINGER 31, RH, EXTERNAL SURFACE31700 FCOR60000 FH3600 FCOR7200 FHGROUP 21-1A534140-01-3 DELETED FROM ALS PART 2 AT REVISION 01534140-01-4 DELETED FROM ALS PART 2 AT REVISION 01R 534140-01-5 N/A GENERAL VISUALINSPECTION OF FUSELAGE SKINAROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME65 AND FRAME 66 AND FROM STRINGER 26 TOSTRINGER 31, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534140-01-7.39600 FCOR60000 FH3500 FCOR7000 FHGROUP 21-2BR 534140-01-6 N/A GENERAL VISUALINSPECTION OF FUSELAGE SKINAROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME65 AND FRAME 66 AND FROM STRINGER 26 TOSTRINGER 31, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534140-01-3.38400 FCOR60000 FH3000 FCOR6000 FHGROUP 19-1AORGROUP 19-1BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 51EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534140-01-7 N/A GENERAL VISUALINSPECTION OF FUSELAGE SKINAROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME65 AND FRAME 66 AND FROM STRINGER 26 TOSTRINGER 31, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534140-01-5.39500 FCOR60000 FH3500 FCOR7000 FHGROUP 21-1BORGROUP 21-2AR 534140-01-8 N/A GENERAL VISUALINSPECTION OF FUSELAGE SKINAROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME65 AND FRAME 66 AND FROM STRINGER 26 TOSTRINGER 31, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK534140-01-1 OR 534140-01-4.35600 FCOR71200 FH3200 FCOR6400 FHA320-200R 534140-01-9 N/A GENERAL VISUALINSPECTION OF FUSELAGE SKINAROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME65 AND FRAME 66 AND FROM STRINGER 26 TOSTRINGER 31, RH, EXTERNAL SURFACE37700 FCOR60000 FH2800 FCOR5600 FHGROUP 18-1A534141-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND WATER SERVICEPANEL CUTOUT, BETWEENFRAME 65 AND FRAME 66 AND FROM STRINGER 37 TOSTRINGER 43, LH, EXTERNAL SURFACE29900 FC 7800 FC A320-100534141-01-2 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 37 TO STRINGER43, LH, EXTERNAL SURFACE32700 FCOR60000 FH11500 FCOR23000 FHGROUP 21-1A534141-01-3 DELETED FROM ALS PART 2 AT REVISION 01534141-01-4 DELETED FROM ALS PART 2 AT REVISION 01R 534141-01-5 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 37 TO STRINGER43, LH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534141-01-1.29600 FCOR59200 FH10700 FCOR21400 FHA320-200PRE 160500A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 52EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534141-01-6 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 37 TO STRINGER43, LH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534141-01-3.29700 FCOR59400 FH10700 FCOR21400 FHGROUP 21-1BORGROUP 21-2A534141-01-7 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 37 TO STRINGER43, LH, EXTERNAL SURFACE30500 FCOR60000 FH10900 FCOR21800 FHGROUP 21-2B534141-01-8 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 37 TO STRINGER43, LH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534141-01-4.25700 FCOR51400 FH9500 FCOR19000 FHGROUP 19-1AORGROUP 19-1B534141-01-9 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 37 TO STRINGER43, LH, EXTERNAL SURFACE21900 FCOR43800 FH8500 FCOR17000 FHGROUP 18-1A534141-01-10 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND WATER SERVICEPANEL CUTOUT, BETWEENFR 65 AND FR 66 AND FROMSTRINGER 37 TO STRINGER43, LH, EXTERNAL SURFACE14700 FCOR63200 FH4700 FCOR20300 FHGROUP 19-1CN 534141-01-11 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWATER SERVICE PANEL CUTOUT, BETWEEN FR 65 ANDFR 66 AND FROM STRINGER 37 TO STRINGER 43, LH,EXTERNAL SURFACE27500 FCOR55000 FH9700 FCOR19400 FHA320-200POST 160500534142-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND WASTE SERVICEPANEL CUTOUT, BETWEENFRAME 65 AND FRAME 66 AND FROM STRINGER 33 TOSTRINGER 40, RH, EXTERNAL SURFACE20900 FCOR47000 FH14400 FCOR32400 FHA320-100A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 53EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534142-01-2 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 33 TO STRINGER40, RH, EXTERNAL SURFACE38000 FCOR60000 FH14500 FCOR29000 FHGROUP 21-1A534142-01-3 DELETED FROM ALS PART 2 AT REVISION 01534142-01-4 DELETED FROM ALS PART 2 AT REVISION 01534142-01-5 DELETED FROM ALS PART 2 AT REVISION 01534142-01-6 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 33 TO STRINGER40, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534142-01-3.35000 FCOR60000 FH13600 FCOR27200 FHGROUP 21-1BORGROUP 21-2A534142-01-7 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 33 TO STRINGER40, RH, EXTERNAL SURFACE35400 FCOR60000 FH13700 FCOR27400 FHGROUP 21-2B534142-01-8 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 33 TO STRINGER40, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534142-01-4.33000 FCOR60000 FH12900 FCOR25800 FHGROUP 19-1AORGROUP 19-1B534142-01-9 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 33 TO STRINGER40, RH, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK534142-01-5 OR 534142-01-1.35400 FCOR70800 FH13700 FCOR27400 FHA320-200534142-01-10 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUNDWASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65AND FRAME 66 AND FROM STRINGER 33 TO STRINGER40, RH, EXTERNAL SURFACE32300 FCOR60000 FH12800 FCOR25600 FHGROUP 18-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 54EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534142-01-11 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND WASTE SERVICEPANEL CUTOUT, BETWEENFR 65 AND FR 66 AND FROMSTRINGER 33 TO STRINGER40, RH, EXTERNAL SURFACE12900 FCOR55800 FH8900 FCOR38300 FHGROUP 19-1C534145-01-1 N/A SPECIAL DETAILEDINSPECTION (LFEC) OF SPLICEPLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47.5,FROM STRINGER 16, LH/RH, TO CROWN CENTER LINE28300 FC 6500 FC A321534149-01-1 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS AT FR 47.5,FROM STRINGER 16, LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE29000 FC 9000 FC A321534152-01-1 DELETED FROM ALS PART 2 AT REVISION 01534152-01-2 DELETED FROM ALS PART 2 AT REVISION 01534152-01-3 DELETED FROM ALS PART 2 AT REVISION 01534152-01-4 DELETED FROM ALS PART 2 AT REVISION 01534153-01-1 DELETED FROM ALS PART 2 AT REVISION 01534153-01-2 DELETED FROM ALS PART 2 AT REVISION 01534153-01-3 DELETED FROM ALS PART 2 AT REVISION 01534154-01-1 252NW 826CEILING PANELREMOVEDLINING REMOVEDBOLTS REMOVEDINSULATIONREMOVEDREAR ACT REMOVED(IF INSTALLED)SPECIAL DETAILED INSPECTION(ROTO) OF FUSELAGESTRUCTURE AT ATTACHMENT AREA UNDER AFT CARGODOOR OUTER HINGE FITTINGS FROM FR 55 TO FR 56BETWEEN STRINGER 22 AND STRINGER 2348000 FCOR96000 FH39000 FCOR78000 FHA320534157-01-3 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 53 AND FR 55A, EXTERNAL PORTION (6PLACES)13100 FC 13100 FC A320-100534157-01-4 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 53 AND FR 55A, EXTERNAL PORTION (6PLACES)14100 FCOR28300 FH14100 FCOR28300 FHA320-200534157-01-5 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 56 AND FR 58A, EXTERNAL PORTION (6PLACES)13100 FC 13100 FC GROUP 19-1AORGROUP 19-1BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 55EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534157-01-6 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 53 AND FR 55A, EXTERNAL PORTION (6PLACES)11400 FC 11400 FC A321534157-01-7 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 56 AND FR 58A, EXTERNAL PORTION (6PLACES)7500 FCOR32300 FH7500 FCOR32300 FHGROUP 19-1CR 534159-01-1 826 DETAILED INSPECTIONOF AFT CARGO DOOR CUTOUT,UPPER AND LOWER CORNERS, EXTERNAL SURFACE13400 FCOR26800 FH13400 FCOR26800 FHA320-200PRE 160001534159-01-2 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT,UPPER AND LOWER CORNERS, EXTERNAL SURFACE12000 FCOR51600 FH12000 FCOR51600 FHGROUP 19-1C534159-01-3 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT,UPPER AND LOWER CORNERS, EXTERNAL SURFACENOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534159-01-1.12000 FC 12000 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA321N 534159-01-4 826 DETAILED INSPECTIONOF AFT CARGO DOOR CUTOUT,UPPER AND LOWER CORNERS, EXTERNAL SURFACE11300 FCOR22600 FH11300 FCOR22600 FHA320-200POST 160001534160-01-3 DELETED FROM ALS PART 2 AT REVISION 01534160-01-4 DELETED FROM ALS PART 2 AT REVISION 01534160-01-5 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORCUTOUT, VISIBLE PART OF LATERAL FR 55A AND FR 591000 FCOR4300 FH1000 FCOR4300 FHGROUP 19-1CR 534160-02-1 826 DETAILED INSPECTIONOF AFT CARGO DOOR CUTOUT,VISIBLE PART OF LATERAL FR 52A AND FR 561400 FCOR2800 FH1400 FCOR2800 FHA320PRE 160001ORA321R 534160-02-2 826 DETAILED INSPECTIONOF AFT CARGO DOOR CUTOUT,VISIBLE PART OF LATERAL FR 55A AND FR 591000 FCOR2100 FH1000 FCOR2100 FHGROUP 19-1AORGROUP 19-1BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 56EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTEN 534160-02-3 826 DETAILED INSPECTIONOF AFT CARGO DOOR CUTOUT,VISIBLE PART OF LATERAL FR 52A AND FR 561100 FCOR2200 FH1100 FCOR2200 FHA320POST 160001534161-01-1 DELETED FROM ALS PART 2 AT REVISION 01534163-01-1 DELETED FROM ALS PART 2 AT REVISION 01534163-01-2 DELETED FROM ALS PART 2 AT REVISION 01534163-01-3 DELETED FROM ALS PART 2 AT REVISION 01534163-01-4 151GCREAR ACT(S)REMOVED (IFINSTALLED)GENERAL VISUAL INSPECTION OF AFT CARGO DOORACTUATOR ATTACH BRACKET, BETWEEN FLOOR BEAMSAT FR 56, FR 57 AND FR 5811400 FC 11400 FC GROUP 19-1C534171-01-1 827 SPECIAL DETAILEDINSPECTION (HFEC) OF FUSELAGESKIN OF BULK CARGO DOOR CUTOUT AT UPPERCORNERS10900 FC 10900 FC A320-100POST 20029ORA320-100POST 20449R 534171-01-2 827 SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN OF BULK CARGO DOOR CUTOUT AT UPPERCORNERSNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534171-01-3.21000 FCOR42100 FH21000 FCOR42100 FHA320-200POST 20449ORA320-200POST 20029PRE 21065PRE 25354PRE 160001ORA321PRE 22992534171-01-3 DELETED FROM ALS PART 2 AT REVISION 01N 534171-01-4 827 SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGESKIN OF BULK CARGO DOOR CUTOUT AT UPPERCORNERS19900 FCOR39800 FH19900 FCOR39800 FHA320-200POST 20029PRE 21065PRE 25354POST 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 57EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 534172-01-2 827 GENERAL VISUAL INSPECTION OF SEALING PROFILE OFBULK CARGO DOOR CUTOUT AT UPPER CORNERS15300 FCOR30600 FH15300 FCOR30600 FHA320-200POST 20449ORA320-200POST 20029PRE 21065PRE 25354ORA321PRE 22992534172-01-3 827 GENERAL VISUALINSPECTION OF SEALING PROFILE OFBULK CARGO DOOR CUTOUT AT UPPER CORNERS5000 FC 5000 FC A320-100POST 20029ORA320-100POST 20449534183-01-1 N/A GENERAL VISUALINSPECTION OF CIRCUMFERENTIALJOINT ABOVE AFT EMERGENCY EXIT DOOR AT FR 47.3FROM STRINGER 6 TO STRINGER 12, EXTERNALSURFACE, LH/RH24000 FC 11900 FC A321534199-02-1 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGESKIN UNDER THE COMPLETE OUTER RIVET ROW OF THEDOUBLER OF THE CABIN SWIFT BROADBAND ANTENNA,IN THE AREA OF FR 57 TO FR59, STGR 2 LH AND STGR 2RH, EXCEPT RIVETS AT STRINGER OR FRAMEJUNCTIONS45600 FCOR60000 FH9900 FCOR19800 FHGROUP 18-1APOST 36590PRE 38068WFD534199-02-2 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGESKIN UNDER THE COMPLETE OUTER RIVET ROW OF THEDOUBLER OF THE CABIN SWIFT BROADBAND ANTENNA,IN THE AREA OF FR 59 TO FR61, STGR 2 LH AND STGR 2RH, EXCEPT RIVETS AT STRINGER OR FRAMEJUNCTIONS33600 FCOR60000 FH7600 FCOR15200 FHGROUP 19-1APOST 36590PRE 38068ORGROUP 19-1BPOST 36590PRE 38068WFD534199-02-4 LINING REMOVEDINSULATIONREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF FUSELAGESKIN UNDER THE COMPLETE OUTER RIVET ROW OF THEDOUBLER OF THE CABIN SWIFT BROADBAND ANTENNA,IN THE AREA OF FR 59 TO FR61, STGR 2 LH AND STGR 2RH, EXCEPT RIVETS AT STRINGER OR FRAMEJUNCTIONS44800 FCOR60000 FH7800 FCOR15600 FHA321POST 36590PRE 38068WFD534252-01-1 DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 58EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE534253-01-1 DELETED FROM ALS PART 2 AT REVISION 01534257-01-2 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 58 AND FR 59A, EXTERNAL PORTION (4PLACES)12200 FC 12200 FC GROUP 18-1A534257-01-3 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORLOCK FITTINGS AND SURROUNDING STRUCTURE,BETWEEN FR 58 AND FR 59A, EXTERNAL PORTION (4PLACES)7500 FCOR22500 FH7500 FCOR22500 FHGROUP 18-1E534260-01-2 DELETED FROM ALS PART 2 AT REVISION 01534260-01-3 826 GENERAL VISUALINSPECTION OF AFT CARGO DOORCUTOUT, VISIBLE PART OF LATERAL FR 57A AND FR 601000 FCOR3000 FH1000 FCOR3000 FHGROUP 18-1E534260-02-1 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT,VISIBLE PART OF LATERAL FR 57A AND FR 60NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 534260-01-2.1400 FCOR2800 FH1400 FCOR2800 FHGROUP 18-1A534261-01-1 DELETED FROM ALS PART 2 AT REVISION 01534261-01-2 DELETED FROM ALS PART 2 AT REVISION 01534261-01-3 DELETED FROM ALS PART 2 AT REVISION 01535103-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND CUTOUT FOR TAILCOMPARTMENT ACCESSDOOR, BETWEEN FR 70 AND FR 73 AND BETWEENSTRINGER 25 RH AND BOTTOM CENTER LINE,EXTERNAL SURFACE17500 FCOR35000 FH17500 FCOR35000 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321535103-01-3 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINAROUND CUTOUT FOR TAILCOMPARTMENT ACCESSDOOR, BETWEEN FR 70 AND FR 73 AND BETWEENSTRINGER 25 RH AND BOTTOM CENTER LINE,EXTERNAL SURFACE8900 FCOR48100 FH8900 FCOR48100 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 59EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE535119-01-1 312AR DETAILED INSPECTION OF SHEAR TIES AND FRAMECLIPS AT FR 72 AND FR 74, BETWEEN STRINGER 3 ANDSTRINGER 9, LH/RH, INTERNAL STRUCTURE33100 FCOR66200 FH9500 FCOR19100 FHGROUP 19-1APRE 30975ORGROUP 19-1BPRE 30975ORA320PRE 30975ORA321PRE 30975WFD535162-01-1 DELETED FROM ALS PART 2 AT REVISION 01535162-01-2 323AL 323AR DETAILEDINSPECTION OF FIN TO FUSELAGE,FORWARD, MID AND AFT ATTACH FITTINGS, OUTSIDEFUSELAGE, LH/RH34100 FC 14400 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA321545101-01-4 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARBOLTS REMOVEDSPECIAL DETAILED INSPECTION (ROTO) OF PYLONFORWARD MOUNT FITTING AND SPIGOT FITTING12000 FCOR51600 FH3000 FCOR13100 FHGROUP 19-1C545102-01-4 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLES12000 FCOR51600 FH5200 FCOR22700 FHGROUP 19-1C545102-01-5 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLES23600 FCOR60000 FH12700 FCOR35000 FHGROUP 18-1APWA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 60EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE545102-01-6 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLES24000 FCOR42000 FH9500 FCOR19000 FHA320-200PRE 22060CFMORA320-200PRE 22061IAE545102-01-7 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLESNOTE: CREDIT CANNOTBE TAKEN FROM PREVIOUSACCOMPLISHMENT OF MRB TASK 545102-01-1.24000 FCOR42000 FH8100 FCOR8100 FHA320-100R 545102-01-8 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLES40200 FCOR60000 FH16000 FCOR37600 FHA321-100CFMORA321-200PRE 34650PRE 152970CFMR 545102-01-9 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLES15200 FCOR35900 FH13600 FCOR31900 FHA321-200POST 34650CFMORA321-200POST 152970CFM545102-01-10 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLESNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 545102-01-6.24000 FCOR42000 FH13500 FCOR27000 FHA320-200POST 22060CFMORA320-200POST 22061IAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 61EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE545102-01-11 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (US) OF PYLONFORWARD MOUNT FITTING, END OF LOWER ARMS, AFTOF RIB 1, FORWARD AND AFT ATTACHMENT, BOLTHOLESNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 545102-01-6.24000 FCOR42000 FH11100 FCOR30700 FHGROUP 19-1ACFMORGROUP 19-1BCFM545103-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 15700 FC 5700 FC A320-100R 545103-01-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 18300 FC 8300 FC GROUP 19-1APRE 34650PRE 152970ORGROUP 19-1BPRE 34650PRE 152970ORA320-200ORA321R 545103-01-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 17400 FC 7400 FC GROUP 19-1APOST 34650ORGROUP 19-1APOST 152970ORGROUP 19-1BPOST 34650ORGROUP 19-1BPOST 152970545103-01-4 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 120000 FC 20000 FC GROUP 18-1ACFMA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 62EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE545103-01-5 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 112000 FC 12000 FC GROUP 18-1APW545103-01-6 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 19400 FCOR40700 FH9400 FCOR40700 FHGROUP 19-1CCFM545103-01-7 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 111800 FCOR50800 FH11800 FCOR50800 FHGROUP 19-1CIAE545103-01-8 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFPYLON FORWARD MOUNTFITTING, FORWARD OF RIB 111900 FCOR35900 FH11900 FCOR35900 FHGROUP 18-1ECFMN 545107-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFENGINE AFT ATTACHMENTBEAM48000 FCOR80000 FH11600 FCOR23200 FHA320-200D 545107-01-4 DELETED FROM ALS PART 2 AT REVISION 02N 545114-01-2 414FR 423FL 471AL472AR 481AL 482ARDETAILED INSPECTION OFPYLON TO WING ATTACHFITTING LUGS AT RIB 448000 FCOR80000 FH13900 FCOR27800 FHA320-200PRE 33844CFMORA320-200PRE 33847IAEN 545114-01-5 471AL 471AR 471BL471BR 481AL 481AR481BL 481BRDETAILED INSPECTION OFPYLON TO WING ATTACHFITTING LUGS AT RIB 448000 FCOR80000 FH13900 FCOR27800 FHA320-200POST 33844CFMORA320-200POST 33847IAED 545114-01-8 DELETED FROM ALS PART 2 AT REVISION 02D 545114-01-9 DELETED FROM ALS PART 2 AT REVISION 02N 545115-01-2 414FR 423FL 471AL472AR 481AL 482AR521BT 621BTDETAILED INSPECTION OFPYLON TO WING FORWARDATTACHMENT SHACKLES AT RIB 4NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-2.48000 FCOR80000 FH5700 FCOR11400 FHA320-200PRE 33844CFMORA320-200PRE 33847IAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 63EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTEN 545115-01-5 471AL 471AR 471BL471BR 481AL 481AR481BL 481BR 521BT621BTDETAILED INSPECTION OFPYLON TO WING FORWARDATTACHMENT SHACKLES AT RIB 4NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-5.48000 FCOR80000 FH5700 FCOR11400 FHA320-200POST 33844CFMORA320-200POST 33847IAED 545115-01-8 DELETED FROM ALS PART 2 AT REVISION 02D 545115-01-9 DELETED FROM ALS PART 2 AT REVISION 02N 545115-02-2 414FR 423FL 471AL472AR 481AL 482AR521BT 621BTSPECIAL DETAILED INSPECTION(US) OF PYLON TOWING FORWARD ATTACHMENT SHACKLES AT RIB 4NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-01-2.48000 FCOR80000 FH10800 FCOR21600 FHA320-200PRE 33844CFMORA320-200PRE 33847IAEN 545115-02-5 471AL 471AR 471BL471BR 481AL 481AR481BL 481BR 521BT621BTSPECIAL DETAILED INSPECTION(US) OF PYLON TOWING FORWARD ATTACHMENT SHACKLES AT RIB 4NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-01-5.48000 FCOR80000 FH10800 FCOR21600 FHA320-200POST 33844CFMORA320-200POST 33847IAED 545115-02-8 DELETED FROM ALS PART 2 AT REVISION 02D 545115-02-9 DELETED FROM ALS PART 2 AT REVISION 02N 545120-01-2 471CL 472BR 475BL476BR 481BL 482CR485BL 486BRDETAILED INSPECTION OFPYLON TO WING ATTACHFITTING LUGS AT RIB 1048000 FCOR80000 FH13600 FCOR27200 FHA320-200PRE 33844CFMORA320-200PRE 33847IAEN 545120-01-5 471CR 471DL 475BL475BR 481CL 481DR485BL 485BRDETAILED INSPECTION OFPYLON TO WING ATTACHFITTING LUGS AT RIB 1048000 FCOR80000 FH13600 FCOR27200 FHA320-200POST 33844CFMORA320-200POST 33847IAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 64EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTED 545120-01-7 DELETED FROM ALS PART 2 AT REVISION 02D 545120-01-8 DELETED FROM ALS PART 2 AT REVISION 02N 545123-01-2 471CL 472BR 475AL475BL 476AR 476BR481BL 482CR 485AL485BL 486AR 486BRSPECIAL DETAILED INSPECTION(US) OF PYLON TOWING AFT ATTACHMENT SHACKLES AT RIB 1048000 FCOR80000 FH13200 FCOR26400 FHA320-200PRE 33844CFMORA320-200PRE 33847IAEN 545123-01-6 471CR 471DL 475AL475AR 475BL 475BR481CL 481DR 485AL485AR 485BL 485BRSPECIAL DETAILED INSPECTION(US) OF PYLON TOWING AFT ATTACHMENT SHACKLES AT RIB 1048000 FCOR80000 FH13200 FCOR26400 FHA320-200POST 33844CFMORA320-200POST 33847IAED 545123-01-9 DELETED FROM ALS PART 2 AT REVISION 02D 545123-01-10 DELETED FROM ALS PART 2 AT REVISION 02R 545130-01-1 415BL 415BR 425BL425BRDETAILED INSPECTION OF PYLON, LATERAL PANELS, ATTHE EDGE OF ACCESS DOORCUTOUTS, BETWEEN RIB 5AND RIB 6, LH/RH20000 FC 20000 FC GROUP 18-1AORGROUP 19-1APRE 34650PRE 152970CFMORGROUP 19-1BPRE 34650PRE 152970CFMORA320-200ORA321CFM545130-01-2DELETED FROM ALS PART 2 AT REVISION 01A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 65EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE545130-01-3 415BL 415BR 425BL425BRDETAILED INSPECTION OF PYLON, LATERAL PANELS, ATTHE EDGE OF ACCESS DOORCUTOUTS, BETWEEN RIB 5AND RIB 6, LH/RH13000 FC 13000 FC GROUP 19-1AIAEORGROUP 19-1BIAEORA321IAE545130-01-4 415BL 415BR 425BL425BRDETAILED INSPECTION OF PYLON, LATERAL PANELS, ATTHE EDGE OF ACCESS DOORCUTOUTS, BETWEEN RIB 5AND RIB 6, LH/RH17000 FC 17000 FC A320-100R 545130-01-5 415BL 415BR 425BL425BRDETAILED INSPECTION OF PYLON, LATERAL PANELS, ATTHE EDGE OF ACCESS DOORCUTOUTS, BETWEEN RIB 5AND RIB 6, LH/RH19100 FC 19100 FC GROUP 19-1APOST 34650CFMORGROUP 19-1APOST 152970CFMORGROUP 19-1BPOST 34650CFMORGROUP 19-1BPOST 152970CFM545130-01-6DELETED FROM ALS PART 2 AT REVISION 01545130-01-7 DELETED FROM ALI DOCUMENT AT ISSUE 10545130-01-8 DELETED FROM ALI DOCUMENT AT ISSUE 10A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 66EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE552007-01-1 N/A SPECIAL DETAILEDINSPECTION (THERMOGRAPHIC) OFELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RHNOTE: THRESHOLD IS 6 YEARS SINCE THE DATE OF THEFIRST FLIGHT AFTER ACCOMPLISHMENT OF SB A320-55-1024, MANDATED BY CN-2001-062(B).NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-3.6 YENOTE6 YE GROUP 19-1APRE 23558ORGROUP 19-1BPRE 23558ORA320PRE 23558ORA321PRE 23558552007-01-2 N/A SPECIAL DETAILEDINSPECTION (THERMOGRAPHIC) OFELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RHNOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OFTHE FIRST FLIGHT.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-4.12 YENOTE6 YE GROUP 18-1APRE 35515ORA319POST 23558PRE 35515ORA320POST 23558PRE 35515ORA321POST 23558PRE 35515552007-01-3 ELEVATOR REMOVED SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OFELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RHNOTE: THRESHOLD IS 6 YEARS SINCE THE DATE OF THEFIRST FLIGHT AFTER ACCOMPLISHMENT OF SB A320-55-1024, MANDATED BY CN-2001-062(B).NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-1.6 YENOTE6 YE GROUP 19-1APRE 23558ORGROUP 19-1BPRE 23558ORA320PRE 23558ORA321PRE 23558A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 67EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE552007-01-4 ELEVATOR REMOVED SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OFELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RHNOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OFTHE FIRST FLIGHT.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-2.12 YENOTE6 YE GROUP 18-1APRE 35515ORA319POST 23558PRE 35515ORA320POST 23558PRE 35515ORA321POST 23558PRE 35515562101-01-1 DELETED FROM ALI DOCUMENT AT ISSUE 7R 571101-02-1 734 744 SPECIAL DETAILEDINSPECTION (HFEC) OF CENTERWING BOX, REAR SPAR,SYSTEM HOLES NEAR MANHOLES37200 FCOR74400 FH20300 FCOR40600 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320PRE 160000571134-01-1 191BB 191CT 191EB191KB 191LB 192CT192EB 192FB 192KB192LB 195AB 196AB734 744DETAILED INSPECTION OF CENTER WING BOX, BOTTOMSKIN LOWER SURFACE, FROM STRINGER 11 TOSTRINGER 15, BETWEEN Y=+/-1292, AS FAR AS VISIBLE32800 FCOR65600 FH7200 FCOR14500 FHA320R 571134-01-6 191BB 191CT 191EB191KB 191LB 192CT192EB 192FB 192KB192LB 195AB 196AB734 744DETAILED INSPECTION OF CENTER WING BOX, BOTTOMSKIN LOWER SURFACE, FROM STRINGER 11 TOSTRINGER 15, BETWEEN Y=+/-1292, AS FAR AS VISIBLE32800 FCOR60000 FH7600 FCOR21100 FHGROUP 19-1APOST 34650ORGROUP 19-1APOST 152970ORGROUP 19-1BPOST 34650ORGROUP 19-1BPOST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 68EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE571135-01-1 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX, BOTTOMSKIN UPPER SURFACE, INCLUDING STRINGERS, FROMSTRINGER 6 TO STRINGER 11, BETWEEN Y=+/-765 ANDFROM STRINGER 11 TO STRINGER 15, BETWEEN Y=+/-129232800 FCOR65600 FH9500 FCOR19000 FHA320R 571135-01-6 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX, BOTTOMSKIN UPPER SURFACE, INCLUDING STRINGERS, FROMSTRINGER 6 TO STRINGER 11, BETWEEN Y=+/-765 ANDFROM STRINGER 11 TO STRINGER 15, BETWEEN Y=+/-129232800 FCOR60000 FH10000 FCOR27600 FHGROUP 19-1APOST 34650ORGROUP 19-1APOST 152970ORGROUP 19-1BPOST 34650ORGROUP 19-1BPOST 152970R 571136-01-1 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION(ROTO) OF CENTERWING BOX, DRAIN HOLES ON STRINGER 13 ANDSTRINGER 14 ON BOTTOMSKIN, UPPER SURFACE (12PLACES)36900 FCOR73900 FH7900 FCOR15800 FHA320-200PRE 160000R 571136-01-2 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION(ROTO) OF CENTERWING BOX, DRAIN HOLES ON STRINGER 13 ANDSTRINGER 14 ON BOTTOMSKIN, UPPER SURFACE (12PLACES)20000 FCOR41700 FH8600 FCOR23700 FHGROUP 18-1AORGROUP 19-1APRE 34650PRE 152970ORGROUP 19-1BPRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 69EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 571136-01-3 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION(ROTO) OF CENTERWING BOX, DRAIN HOLES ON STRINGER 13 ANDSTRINGER 14 ON BOTTOMSKIN, UPPER SURFACE (12PLACES)19900 FCOR36200 FH8100 FCOR22200 FHGROUP 19-1APOST 34650ORGROUP 19-1APOST 152970ORGROUP 19-1BPOST 34650ORGROUP 19-1BPOST 152970R 571136-01-4 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION(ROTO) OF CENTERWING BOX, DRAIN HOLES ON STRINGER 13 ANDSTRINGER 14 ON BOTTOMSKIN, UPPER SURFACE (12PLACES)16500 FCOR71200 FH8800 FCOR38000 FHGROUP 19-1CR 571136-01-5 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION(ROTO) OF CENTERWING BOX, DRAIN HOLES ON STRINGER 13 ANDSTRINGER 14 ON BOTTOMSKIN, UPPER SURFACE (12PLACES)20000 FCOR48000 FH8600 FCOR23600 FHA320-100571164-01-1 CABIN FLOORPANELS REMOVEDLINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF CENTER WING BOX, UPPERPANEL, ENDS OF FLOOR BEAM,AFT FLANGE (6 PLACES)25400 FCOR50800 FH11700 FCOR23500 FHA320-200PRE 21284571164-01-2 CABIN FLOORPANELS REMOVEDLINING REMOVEDINSULATIONREMOVEDDETAILED INSPECTION OF CENTER WING BOX, UPPERPANEL, ENDS OF FLOOR BEAM,AFT FLANGE (6 PLACES)29900 FCOR48000 FH15800 FCOR45100 FHA320-100R 571170-01-1 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH34000 FCOR60000 FH9100 FCOR18200 FHGROUP 18-1AORGROUP 19-1APRE 34650PRE 152970ORGROUP 19-1BPRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 70EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 571170-01-2 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH21000 FCOR42000 FH9100 FCOR18200 FHA320-200PRE 160000R 571170-01-3 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH35000 FCOR60000 FH9100 FCOR18200 FHA321-100ORGROUP 21-2APRE 34650PRE 152970ORGROUP 21-2BR 571170-01-4 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH23900 FCOR42000 FH9100 FCOR18200 FHGROUP 19-1APOST 34650ORGROUP 19-1APOST 152970ORGROUP 19-1BPOST 34650ORGROUP 19-1BPOST 152970571170-01-5 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH10100 FCOR43600 FH4200 FCOR18000 FHGROUP 19-1CR 571170-01-6 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH34100 FCOR60000 FH9100 FCOR18200 FHGROUP 21-2APOST 34650ORGROUP 21-2APOST 152970R 571170-01-7 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH24000 FCOR48000 FH9100 FCOR9100 FHA320-100N 571170-01-8 191DT 191ET 192DT192ETSPECIAL DETAILED INSPECTION (US) OF CENTER WINGBOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVELOF FRAME 42, LH/RH21000 FCOR42000 FH6900 FCOR13800 FHA320-200POST 160000571181-01-1 147AZ 148AZ 734744FASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION(US) OF CWB, UPPERSURFACE OF TRIFORM FITTING (ON FIRST ROW OFFASTENERS FROM RIB 1),BETWEEN STRINGER 8 ANDFR 42, LH/RH29600 FCOR59300 FH29600 FCOR59300 FHA320-200PRE 38481A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 71EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 571181-01-6 147AZ 148AZ 734744FASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION(US) OF CWB, UPPERSURFACE OF TRIFORM FITTING (ON FIRST ROW OFFASTENERS FROM RIB 1),BETWEEN STRINGER 8 ANDFR 42, LH/RH24000 FCOR53800 FH9300 FCOR25500 FHGROUP 19-1APOST 34650PRE 38481ORGROUP 19-1APRE 38481POST 152970ORGROUP 19-1BPOST 34650PRE 38481ORGROUP 19-1BPRE 38481POST 152970ORA320-100571182-01-1 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION(US) OF OUTER WB,UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROWOF FASTENERS FROM RIB1), BETWEEN STRINGER 8AND FR 42, LH/RH29600 FCOR59300 FH14800 FCOR29700 FHA320-200PRE 38481WFDR 571182-01-6 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION(US) OF OUTER WB,UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROWOF FASTENERS FROM RIB1), BETWEEN STRINGER 8AND FR 42, LH/RH24000 FCOR53800 FH9300 FCOR25500 FHGROUP 19-1APOST 34650PRE 38481ORGROUP 19-1APRE 38481POST 152970ORGROUP 19-1BPOST 34650PRE 38481ORGROUP 19-1BPRE 38481POST 152970ORA320-100A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 72EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE571183-01-1 191LB 192LB 734744SPECIAL DETAILED INSPECTION(US) OF CWB, LOWERSPLICE ON LOWER SKIN LOWER SURFACE AT RIB 1 (ATTWO CENTRAL ROWS OF FASTENERS), BETWEENSTRINGER 8 AND FR 42, LH/RH29600 FCOR59300 FH15200 FCOR30400 FHA320-200PRE 38481WFDR 571183-01-5 191LB 192LB 734744SPECIAL DETAILED INSPECTION(US) OF CWB, LOWERSPLICE ON LOWER SKIN LOWER SURFACE AT RIB 1 (ATTWO CENTRAL ROWS OF FASTENERS), BETWEENSTRINGER 8 AND FR 42, LH/RH24000 FCOR37100 FH9300 FCOR25500 FHGROUP 19-1APOST 34650PRE 38481ORGROUP 19-1APRE 38481POST 152970ORGROUP 19-1BPOST 34650PRE 38481ORGROUP 19-1BPRE 38481POST 152970ORA320-100R 571185-01-1 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION (US) OF OUTER WINGBOX (HOLES ON) UPPER HALF OF VERTICAL TEEFITTING AT JUNCTION WITH RIB 1 AND REAR SPAR,LH/RH29000 FCOR60000 FH11200 FCOR33000 FHGROUP 18-1AORGROUP 19-1APRE 34650PRE 152970ORGROUP 19-1BPRE 34650PRE 152970ORA320-100571185-01-2 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION (US) OF OUTER WINGBOX (HOLES ON) UPPER HALF OF VERTICAL TEEFITTING AT JUNCTION WITH RIB 1 AND REAR SPAR,LH/RH34600 FCOR60000 FH10400 FCOR27600 FHGROUP 21-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 73EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 571185-01-3 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION (US) OF OUTER WINGBOX (HOLES ON) UPPER HALF OF VERTICAL TEEFITTING AT JUNCTION WITH RIB 1 AND REAR SPAR,LH/RH20000 FCOR52900 FH5500 FCOR14600 FHGROUP 21-2APRE 34650PRE 152970571185-01-4 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION (US) OF OUTER WINGBOX (HOLES ON) UPPER HALF OF VERTICAL TEEFITTING AT JUNCTION WITH RIB 1 AND REAR SPAR,LH/RH24000 FCOR42000 FH4900 FCOR13200 FHGROUP 21-1BORGROUP 21-2BR 571185-01-5 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION (US) OF OUTER WINGBOX (HOLES ON) UPPER HALF OF VERTICAL TEEFITTING AT JUNCTION WITH RIB 1 AND REAR SPAR,LH/RH24000 FCOR42000 FH10500 FCOR31100 FHGROUP 19-1APOST 34650ORGROUP 19-1APOST 152970ORGROUP 19-1BPOST 34650ORGROUP 19-1BPOST 152970R 571185-01-7 540AB 540AZ 540BZ640AB 640AZ 640BZFASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION (US) OF OUTER WINGBOX (HOLES ON) UPPER HALF OF VERTICAL TEEFITTING AT JUNCTION WITH RIB 1 AND REAR SPAR,LH/RH20000 FCOR57000 FH4700 FCOR14100 FHGROUP 21-2APOST 34650ORGROUP 21-2APOST 152970571189-01-1 147AZ 148AZ 734744DETAILED INSPECTION OFCENTER WING BOX,STRINGER WEB AT JUNCTION WITH STRUT ATTACHFITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 1622900 FCOR48000 FH9500 FCOR27000 FHA320-100POST 20188R 571189-01-3 147AZ 148AZ 734744DETAILED INSPECTION OFCENTER WING BOX,STRINGER WEB AT JUNCTION WITH STRUT ATTACHFITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 1622600 FCOR59900 FH13100 FCOR36000 FHGROUP 18-1AORGROUP 19-1APRE 34650PRE 152970ORGROUP 19-1BPRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 74EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE571189-01-5 147AZ 148AZ 734744DETAILED INSPECTION OFCENTER WING BOX,STRINGER WEB AT JUNCTION WITH STRUT ATTACHFITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 571189-01-1.16900 FCOR33800 FH13500 FCOR27100 FHA320-200PRE 21287R 571189-01-7 147AZ 148AZ 734744DETAILED INSPECTION OFCENTER WING BOX,STRINGER WEB AT JUNCTION WITH STRUT ATTACHFITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 1620200 FCOR53600 FH8700 FCOR24100 FHGROUP 19-1APOST 34650ORGROUP 19-1APOST 152970ORGROUP 19-1BPOST 34650ORGROUP 19-1BPOST 152970571190-01-1 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION(HFEC) OF CENTERWING BOX, FRAME FEET, UPPER FLANGE AT JUNCTIONWITH CROWN FITTING ON FR 37 TO FR 4130300 FCOR60600 FH9700 FCOR19500 FHA320-200PRE 21288571190-01-2 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION(HFEC) OF CENTERWING BOX, FRAME FEET, UPPER FLANGE AT JUNCTIONWITH CROWN FITTING ON FR 37 TO FR 4128900 FCOR48000 FH9100 FCOR25100 FHA320-100571192-01-1 147AZ 148AZ 734744FASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF CENTERWING BOX, REAR SPAR, EDGE OF LOWER FLANGE ATCORNER FITTING, LH/RH21400 FCOR42800 FH10900 FCOR21800 FHA320-200PRE 26228571192-01-2 147AZ 148AZ 734744FASTENER SEALANTREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF CENTERWING BOX, REAR SPAR, EDGE OF LOWER FLANGE ATCORNER FITTING, LH/RH17800 FCOR45400 FH11100 FCOR29600 FHGROUP 19-1APRE 26228ORGROUP 19-1BPRE 26228ORA320-100R 572004-01-1 540AB 540AZ 540BB540CB 640AB 640AZ640BB 640CBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THEAREA INSIDE THE DRY BAY60000 FCOR120000 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 75EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572004-01-2 540AB 540AZ 540BB540CB 640AB 640AZ640BB 640CBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THEAREA INSIDE THE DRY BAY44000 FCOR60000 FH15000 FCOR24800 FHA321R 572004-01-4 540AB 540AZ 540BB540CB 640AB 640AZ640BB 640CBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THEAREA INSIDE THE DRY BAY39800 FCOR60000 FH14700 FCOR24300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA320-200POST 34650ORA320-200POST 152970N 572004-01-5 540AB 540AZ 540BB540CB 640AB 640AZ640BB 640CBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THEAREA INSIDE THE DRY BAY34200 FCOR68400 FH9900 FCOR19800 FHA320-200POST 160058ORA320-200POST 160075ORA320-200POST 160076N 572004-01-6 540AB 540AZ 540BB540CB 640AB 640AZ640BB 640CBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THEAREA INSIDE THE DRY BAY27500 FCOR55000 FH9900 FCOR19800 FHA320-200PRE 160058POST 160001PRE 160075PRE 160076572004-03-1 DELETED FROM ALI DOCUMENT AT ISSUE 10572007-01-1 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE12500 FCOR20500 FH12500 FCOR20500 FHA320-100R 572007-01-2 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE11900 FCOR23800 FH11900 FCOR23800 FHA320-200PRE 34650PRE 152970PRE 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 76EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572007-01-3 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE11200 FCOR18400 FH11200 FCOR18400 FHGROUP 18-1AORGROUP 21-1AR 572007-01-4 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE10800 FCOR17700 FH10800 FCOR17700 FHGROUP 21-1BORGROUP 21-2AR 572007-01-5 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE9600 FCOR15800 FH9600 FCOR15800 FHGROUP 21-2B572007-01-6 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE10600 FCOR45500 FH10600 FCOR45500 FHGROUP 19-1CR 572007-01-8 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE10600 FCOR17400 FH10600 FCOR17400 FHGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970N 572007-01-9 N/A DETAILED INSPECTION OF OUTER WING, REAR SPARAFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5,INCLUDING REAR SPAR ANGLE10500 FCOR21000 FH10500 FCOR21000 FHA320-200POST 160001N 572008-01-4 574AB 574BB 674AB674BBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, REAR SPAR AFT FACE SPAR JOINT PLATEAT RIB 621300 FCOR42600 FH7800 FCOR15600 FHA320-200POST 160001N 572009-01-1 540AB 540BB 540BZ640AB 640BB 640BZSPECIAL DETAILED INSPECTION(US) OF OUTER WING,REAR SPAR FORWARD FACE, AT THE ATTACHMENTHOLES OF GEAR SUPPORT RIB 5, MLG FORWARDPINTLE FITTING AND RETRACTION JACK FITTING48000 FCOR96000 FH12000 FCOR24000 FHA320-200PRE 34650PRE 152970PRE 160001N 572009-01-2 540AB 540BB 540BZ640AB 640BB 640BZSPECIAL DETAILED INSPECTION(US) OF OUTER WING,REAR SPAR FORWARD FACE, AT THE ATTACHMENTHOLES OF GEAR SUPPORT RIB 5, MLG FORWARDPINTLE FITTING AND RETRACTION JACK FITTING32800 FCOR65600 FH9000 FCOR18000 FHA320-200POST 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 77EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572010-01-1 540AB 540BZ 640AB640BZDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, UPPER AND LOWER ROOT JOINTFITTING36200 FCOR48000 FH11400 FCOR23600 FHA320-100R 572010-01-4 540AB 540BZ 640AB640BZDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, UPPER AND LOWER ROOT JOINTFITTING58600 FCOR117200 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001572010-01-5 540AB 540BZ 640AB640BZDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, UPPER AND LOWER ROOT JOINTFITTING36200 FCOR60000 FH11400 FCOR23600 FHGROUP 19-1AORGROUP 19-1B572010-01-6 540AB 540BZ 640AB640BZDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, UPPER AND LOWER ROOT JOINTFITTING34100 FCOR60000 FH11400 FCOR23600 FHGROUP 18-1AR 572010-01-7 540AB 540BZ 640AB640BZDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, UPPER AND LOWER ROOT JOINTFITTING35200 FCOR60000 FH11400 FCOR23600 FHA320-200POST 34650ORA320-200POST 152970N 572010-01-10 540AB 540BZ 640AB640BZDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, UPPER AND LOWER ROOT JOINTFITTING44300 FCOR88600 FH14300 FCOR28600 FHA320-200POST 160001R 572011-01-1 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES32900 FCOR48000 FH9600 FCOR15600 FHA320-100R 572011-01-2 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES32400 FCOR64800 FH9300 FCOR18600 FHA320-200PRE 34650PRE 152970PRE 160001R 572011-01-3 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES30000 FCOR60000 FH10500 FCOR17200 FHGROUP 21-1AR 572011-01-4 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES30000 FCOR60000 FH11600 FCOR19000 FHGROUP 21-1BORA321-200A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 78EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572011-01-5 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES32900 FCOR60000 FH9400 FCOR15300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BR 572011-01-6 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES32400 FCOR53300 FH9100 FCOR15000 FHA320-200POST 34650ORA320-200POST 152970R 572011-01-7 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES9000 FCOR38700 FH9000 FCOR38700 FHGROUP 19-1CN 572011-01-8 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES31500 FCOR63000 FH6200 FCOR12400 FHA320-200POST 160058ORA320-200POST 160075ORA320-200POST 160076N 572011-01-9 540AB 540BB 540BZ540CB 640AB 640BB640BZ 640CBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDINGTHE REGION OF THE JOINT AT RIB 6 AND TOP ANDBOTTOM FLANGES18600 FCOR37200 FH6200 FCOR12400 FHA320-200PRE 160058POST 160001PRE 160075PRE 160076R 572012-01-1 N/A DETAILED INSPECTION OF OUTER WING, TOP SKINUPPER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR, BETWEEN RIB 1 AND RIB 859600 FCOR119200 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970R 572014-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING, TOPSKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS ANDSTRINGERS BETWEEN RIB 1 AND RIB 8 FROM FRONTSPAR TO REAR SPAR48300 FCOR96600FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001572014-01-4 N/A GENERAL VISUALINSPECTION OF OUTER WING, TOPSKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS ANDSTRINGERS BETWEEN RIB 1 AND RIB 8 FROM FRONTSPAR TO REAR SPAR42700 FCOR60000 FH8000 FCOR12600 FHGROUP 18-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 79EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572014-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING, TOPSKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS ANDSTRINGERS BETWEEN RIB 1 AND RIB 8 FROM FRONTSPAR TO REAR SPAR42800 FCOR60000 FH10000 FCOR15900 FHGROUP 21-1BORA321-200R 572020-01-1 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES, STRINGERJOINTS, AND BUTT STRAP, ATSTRINGER 11, EXCLUDINGTHE AREA INSIDE THE DRY BAY33900 FCOR67800 FH11700 FCOR23400 FHA320-200PRE 34650PRE 152970PRE 160001572020-01-3 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP,AT STRINGER 11, EXCLUDING THE AREA INSIDE THEDRY BAY33900 FCOR60000 FH10500 FCOR20400 FHGROUP 19-1AORGROUP 19-1B572020-01-4 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP,AT STRINGER 11, EXCLUDING THE AREA INSIDE THEDRY BAY38400 FCOR60000 FH11900 FCOR23100 FHGROUP 21-1A572020-01-5 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP,AT STRINGER 11, EXCLUDING THE AREA INSIDE THEDRY BAY41800 FCOR60000 FH12000 FCOR23200 FHGROUP 21-2A572020-01-6 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP,AT STRINGER 11, EXCLUDING THE AREA INSIDE THEDRY BAY33000 FCOR60000 FH11800 FCOR22800 FHGROUP 21-1BORGROUP 21-2B572020-01-7 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP,AT STRINGER 11, EXCLUDING THE AREA INSIDE THEDRY BAY32000 FCOR60000 FH10600 FCOR20500 FHGROUP 18-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 80EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572020-01-9 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES, STRINGERJOINTS, AND BUTT STRAP, ATSTRINGER 11, EXCLUDINGTHE AREA INSIDE THE DRY BAY33900 FCOR60000 FH11700 FCOR22600 FHA320-100ORA320-200POST 34650ORA320-200POST 152970N 572020-01-10 540AB 540AZ 540BB540BZ 640AB 640AZ640BB 640BZDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES, STRINGERJOINTS, AND BUTT STRAP, ATSTRINGER 11, EXCLUDINGTHE AREA INSIDE THE DRY BAY36700 FCOR73400 FH36700 FCOR73400 FHA320-200POST 160001572020-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 10572026-01-1DELETED FROM ALS PART 2 AT REVISION 01572026-01-3 540AB 540BB 640AB640BBDETAILED INSPECTION OF OUTER WING, RIB 5, AFT OFBOLTED PANEL28400 FCOR48000 FH10800 FCOR25300 FHA320-100R 572026-01-6 540AB 540BB 640AB640BBDETAILED INSPECTION OF OUTER WING, RIB 5, AFT OFBOLTED PANELNOTE: CREDIT CAN BETAKN FROM PREVIOUSACCOMPLISHMENT OF TASK 572026-01-1.38300 FCOR60000 FH10800 FCOR25300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970R 572032-01-1 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR,BETWEEN RIB 1 AND RIB 8, EXCLUDING AREASCOVERED BY MLG REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING60000 FCOR120000 FH7500 FCOR15000 FHA320-200PRE 34650PRE 152970572032-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR,BETWEEN RIB 1 AND RIB 8, EXCLUDING AREASCOVERED BY MLG REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING24000 FCOR42000 FH6800 FCOR11800 FHA321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 81EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572032-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR,BETWEEN RIB 1 AND RIB 8, EXCLUDING AREASCOVERED BY MLG REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING18000 FCOR31200 FH6500 FCOR11300 FHGROUP 19-1AORGROUP 19-1B572032-01-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR,BETWEEN RIB 1 AND RIB 8, EXCLUDING AREASCOVERED BY MLG REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING16800 FCOR72300 FH4400 FCOR19000 FHGROUP 19-1CR 572032-01-5 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR,BETWEEN RIB 1 AND RIB 8, EXCLUDING AREASCOVERED BY MLG REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING24000 FCOR42000 FH6500 FCOR11300 FHGROUP 18-1AORA320-200POST 34650ORA320-200POST 152970572032-01-6 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR,BETWEEN RIB 1 AND RIB 8, EXCLUDING AREASCOVERED BY MLG REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING24000 FCOR42000 FH6500 FCOR11300 FHA320-100R 572033-01-1 540AB 540BB 640AB640BBSPECIAL DETAILED INSPECTION (X-RAY) OF OUTERWING, BOTTOM SKIN, FORWARD OF REAR SPAR IN AREAMASKED BY MLG REINFORCING PLATE, INCLUDINGATTACHMENT TO REAR SPAR48000 FCOR96000 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970572034-01-1 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE MLG REINFORCINGPLATE31700 FCOR51400 FH10100 FCOR16300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1B572034-01-2 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKINLOWER SURFACE MLG REINFORCINGPLATE32700 FCOR53000 FH10000 FCOR16200 FHGROUP 21-1A572034-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE MLG REINFORCINGPLATE32700 FCOR53000 FH10200 FCOR16600 FHGROUP 21-1BORA321-200A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 82EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572034-01-4 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE MLG REINFORCINGPLATE27500 FCOR44700 FH9600 FCOR15500 FHA320-100D 572034-01-5 DELETED FROM ALS PART 2 AT REVISION 02572034-01-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE MLG REINFORCINGPLATE15400 FCOR66300 FH5300 FCOR23000 FHGROUP 19-1CR 572034-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE MLG REINFORCINGPLATE25000 FCOR40500 FH8300 FCOR13300 FHA320-200POST 34650ORA320-200POST 152970572036-01-1 531AB 531BB 531CB631AB 631BB 631CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, FORWARDOF REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRINGS, INCLUDINGATTACHMENT TO REAR SPAR41500 FCOR48000 FH12500 FCOR21700 FHA320-100R 572036-01-2 531AB 531BB 531CB631AB 631BB 631CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, FORWARDOF REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRINGS, INCLUDINGATTACHMENT TO REAR SPAR60000 FCOR120000 FH10700 FCOR21400 FHA320-200PRE 34650PRE 152970572036-01-3 531CB 531EB 631CB631EBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, FORWARDOF REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRINGS, INCLUDINGATTACHMENT TO REAR SPAR35800 FCOR60000 FH10600 FCOR18400 FHGROUP 21-1BORA321-200572036-01-4 531CB 531EB 631CB631EBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, FORWARDOF REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRINGS, INCLUDINGATTACHMENT TO REAR SPAR28700 FCOR49800 FH10600 FCOR18400 FHGROUP 21-1A572036-01-5 531AB 531BB 531CB631AB 631BB 631CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, FORWARDOF REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRINGS, INCLUDINGATTACHMENT TO REAR SPAR36500 FCOR60000 FH10200 FCOR17700 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BR 572036-01-7 531AB 531BB 531CB631AB 631BB 631CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, FORWARDOF REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRINGS, INCLUDINGATTACHMENT TO REAR SPAR35800 FCOR60000 FH10700 FCOR18600 FHA320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 83EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572038-01-1 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUTS OF STRINGER 2 (RIBBAY 5-6), STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER10 (RIB BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4)AND STRINGER 15 (RIB BAY 2-3)54600 FCOR109200 FH5600 FCOR11200 FHA320-200PRE 34650PRE 152970572038-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUTS OF STRINGER 2 (RIBBAY 5-6), STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER10 (RIB BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4)AND STRINGER 15 (RIB BAY 2-3)24000 FCOR41700 FH4100 FCOR7200 FHA321572040-03-1 540AB 540BB 640AB640BBSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, BOTTOM SKIN, UPPER AND LOWER SURFACES,AROUND ACCESS DOOR CUTOUTS IN RIB BAY 2-3 ANDRIB BAY 6-741600 FCOR60000 FH15000 FCOR27100 FHGROUP 21-1AR 572040-03-4 540AB 540BB 640AB640BBSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, BOTTOM SKIN, UPPER AND LOWER SURFACES,AROUND ACCESS DOOR CUTOUTS IN RIB BAY 2-3 ANDRIB BAY 6-751900 FCOR103800 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970R 572041-02-4 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKIN,LOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS (EXCLUDING STRINGERS 8 AND 11)BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY FAIRINGS ANDREINFORCING PLATES31200 FCOR62400 FH4900 FCOR9800 FHA320-200PRE 34650PRE 152970PRE 160001R 572041-02-5 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKIN,LOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS (EXCLUDING STRINGERS 8 AND 11)BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY FAIRINGS ANDREINFORCING PLATES31200 FCOR50700 FH4900 FCOR7900 FHA320-200POST 34650ORA320-200POST 152970572041-02-6 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKIN,LOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS (EXCLUDING STRINGERS 8 AND 11)BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY FAIRINGS ANDREINFORCING PLATES42800 FCOR60000 FH4900 FCOR7900 FHGROUP 18-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 84EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572041-02-7 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKIN,LOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS (EXCLUDING STRINGERS 8 AND 11)BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY FAIRINGS ANDREINFORCING PLATES37600 FCOR60000 FH4900 FCOR7900 FHGROUP 19-1AORGROUP 19-1B572041-02-8 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKIN,LOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS (EXCLUDING STRINGERS 8 AND 11)BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY FAIRINGS ANDREINFORCING PLATES36200 FCOR58800 FH4900 FCOR7900 FHGROUP 21-1A572041-02-9 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKIN,LOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS (EXCLUDING STRINGERS 8 AND 11)BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY FAIRINGS ANDREINFORCING PLATES42400 FCOR60000 FH4900 FCOR7900 FHGROUP 21-1BORGROUP 21-2A572041-02-10 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN,LOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS (EXCLUDING STRINGERS 8 AND 11)BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY FAIRINGS ANDREINFORCING PLATES39600 FCOR60000 FH4900 FCOR7900 FHGROUP 21-2B572042-01-1 PYLON FAIRINGSREMOVEDGENERAL VISUAL INSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, INAREA COVERED BY PYLONFAIRING24000 FCOR42000 FH5100 FCOR8300 FHA320-100R 572042-01-2 PYLON FAIRINGSREMOVEDGENERAL VISUAL INSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, INAREA COVERED BY PYLONFAIRING37300 FCOR74600 FH5300 FCOR10600 FHA320-200PRE 34650PRE 152970PRE 160001572042-01-3 PYLON FAIRINGSREMOVEDGENERAL VISUAL INSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, INAREA COVERED BY PYLONFAIRING22500 FCOR36600 FH4000 FCOR6500 FHGROUP 21-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 85EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572042-01-4 PYLON FAIRINGSREMOVEDGENERAL VISUAL INSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, INAREA COVERED BY PYLONFAIRING24000 FCOR42000 FH4000 FCOR6500 FHGROUP 21-1BORA321-200572042-01-6 PYLON FAIRINGSREMOVEDGENERAL VISUAL INSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, INAREA COVERED BY PYLONFAIRING14700 FCOR63400 FH3800 FCOR16300 FHGROUP 19-1CR 572042-01-7 PYLON FAIRINGSREMOVEDGENERAL VISUAL INSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, INAREA COVERED BY PYLONFAIRINGNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572042-01-2.24000 FCOR42000 FH3800 FCOR6200 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970572044-01-1 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTSAT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREASCOVERED BY REINFORCINGPLATES AND FAIRINGS29000 FCOR47100 FH5100 FCOR8300 FHA320-100R 572044-01-2 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTSAT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREASCOVERED BY REINFORCINGPLATES AND FAIRINGS38000 FCOR76000 FH5800 FCOR11600 FHA320-200PRE 34650PRE 152970PRE 160001572044-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTSAT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREASCOVERED BY REINFORCINGPLATES AND FAIRINGS26300 FCOR42800 FH3800 FCOR6200 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1B572044-01-4 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTSAT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREASCOVERED BY REINFORCINGPLATES AND FAIRINGS19100 FCOR31000 FH4600 FCOR7500 FHGROUP 21-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 86EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572044-01-5 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTSAT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREASCOVERED BY REINFORCINGPLATES AND FAIRINGS29000 FCOR47100 FH4600 FCOR7500 FHGROUP 21-1BORA321-200572044-01-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTSAT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREASCOVERED BY REINFORCINGPLATES AND FAIRINGS12700 FCOR54600 FH3800 FCOR16300 FHGROUP 19-1CR 572044-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTSAT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 ANDRIB 8, EXCLUDING AREASCOVERED BY REINFORCINGPLATES AND FAIRINGS22600 FCOR36800 FH3800 FCOR6200 FHA320-200POST 34650ORA320-200POST 152970572047-01-2 PYLON FAIRINGSREMOVEDSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, BOTTOM SKIN LOWER SURFACE AROUND AFTPYLON ATTACHMENT FITTING CUTOUT42500 FCOR60000 FH14000 FCOR21000 FHGROUP 21-1A572049-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 9572049-02-2 DELETED FROM ALI DOCUMENT AT ISSUE 9572049-02-3 DELETED FROM ALI DOCUMENT AT ISSUE 9572049-02-4 DELETED FROM ALI DOCUMENT AT ISSUE 9572049-02-5 DELETED FROM ALI DOCUMENT AT ISSUE 10572050-01-1 540AB 540BB 540CZ540DZ 640AB 640BB640CZ 640DZDETAILED INSPECTION OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-1.25000 FCOR44800 FH10600 FCOR20500 FHGROUP 18-1APRE 37331ORGROUP 19-1APRE 37331ORGROUP 19-1APOST 37332ORGROUP 19-1BPRE 37331ORGROUP 19-1BPOST 37332A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 87EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572050-01-2 540AB 540BB 540CZ540DZ 640AB 640BB640CZ 640DZDETAILED INSPECTION OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-2.12700 FCOR54600 FH5700 FCOR24300 FHGROUP 19-1CPRE 37331ORGROUP 19-1CPOST 37332572050-01-3 540AB 540BB 540CZ540DZ 640AB 640BB640CZ 640DZDETAILED INSPECTION OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-3.28100 FCOR48000 FH11700 FCOR21100 FHA320-100PRE 20154ORA320-100POST 20167R 572050-01-4 540AB 540BB 540CZ540DZ 640AB 640BB640CZ 640DZDETAILED INSPECTION OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-4.29800 FCOR59600 FH15000 FCOR30000 FHA320-200PRE 34650PRE 37331PRE 152970PRE 160001ORA320-200PRE 34650POST 37332PRE 152970PRE 160001572050-01-5 540AB 540BB 540CZ540DZ 640AB 640BB640CZ 640DZDETAILED INSPECTION OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-5.28700 FCOR51400 FH12000 FCOR22000 FHGROUP 21-1APRE 38616ORGROUP 21-1APOST 38617ORGROUP 21-2APRE 38616ORGROUP 21-2APOST 38617A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 88EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572050-01-6 540AB 540BB 540CZ540DZ 640AB 640BB640CZ 640DZDETAILED INSPECTION OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-6.28700 FCOR51400 FH11800 FCOR22000 FHGROUP 21-1BPRE 38616ORGROUP 21-1BPOST 38617ORGROUP 21-2BPRE 38616ORGROUP 21-2BPOST 38617572050-01-7 540AB 540BB 540CZ DETAILEDINSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-7.28100 FCOR48000 FH11700 FCOR21100 FHA320-100POST 20154PRE 20167R 572050-01-8 540AB 540BB 540CZ540DZ 640AB 640BB640CZ 640DZDETAILED INSPECTION OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-8.25000 FCOR44800 FH11700 FCOR21100 FHA320-200POST 34650PRE 37331ORA320-200POST 34650POST 37332ORA320-200PRE 37331POST 152970ORA320-200POST 37332POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 89EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572050-02-1 521AZ 521BZ 521EB621AZ 621BZ 621EBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-1.25000 FCOR44800 FH10600 FCOR20500 FHGROUP 18-1APRE 37331ORGROUP 19-1APRE 37331ORGROUP 19-1APOST 37332ORGROUP 19-1BPRE 37331ORGROUP 19-1BPOST 37332572050-02-2 521AZ 521BZ 521EB621AZ 621BZ 621EBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-2.12700 FCOR54600 FH5700 FCOR24300 FHGROUP 19-1CPRE 37331ORGROUP 19-1CPOST 37332572050-02-3 521AZ 521BZ 521EB621AZ 621BZ 621EBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-3.28100 FCOR48000 FH11700 FCOR21100 FHA320-100PRE 20154ORA320-100POST 20167R 572050-02-4 521AZ 521BZ 521EB621AZ 621BZ 621EBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-4.29800 FCOR59600 FH15000 FCOR30000 FHA320-200PRE 34650PRE 37331PRE 152970PRE 160001ORA320-200PRE 34650POST 37332PRE 152970PRE 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 90EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572050-02-5 521AZ 521BZ 521EB621AZ 621BZ 621EBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-5.28700 FCOR51400 FH12000 FCOR22000 FHGROUP 21-1APRE 38616ORGROUP 21-1APOST 38617ORGROUP 21-2APRE 38616ORGROUP 21-2APOST 38617572050-02-6 521AZ 521BZ 521EB621AZ 621BZ 621EBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-6.28700 FCOR51400 FH11800 FCOR22000 FHGROUP 21-1BPRE 38616ORGROUP 21-1BPOST 38617ORGROUP 21-2BPRE 38616ORGROUP 21-2BPOST 38617572050-02-7 521AZ 521EB SPECIAL DETAILED INSPECTION(ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-7.28100 FCOR48000 FH11700 FCOR21100 FHA320-100POST 20154PRE 20167A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 91EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572050-02-8 521AZ 521BZ 521EB621AZ 621BZ 621EBSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFOUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-8.25000 FCOR44800 FH11700 FCOR21100 FHA320-200POST 34650PRE 37331ORA320-200POST 34650POST 37332ORA320-200PRE 37331POST 152970ORA320-200POST 37332POST 152970572053-01-1 540AB 540AZ 540BB540BZ 540CB 640AB640AZ 640BB 640BZ640CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGDRAIN HOLES IN STRINGERS AND BUTT STRAP ATSTRINGER 8 AND STRINGER 11, EXCLUDING THE AREAINSIDE THE DRY BAY28100 FCOR48000 FH11800 FCOR21100 FHA320-100R 572053-01-2 540AB 540AZ 540BB540BZ 540CB 640AB640AZ 640BB 640BZ640CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGDRAIN HOLES IN STRINGERS AND BUTT STRAP ATSTRINGER 8 AND STRINGER 11, EXCLUDING THE AREAINSIDE THE DRY BAY37300 FCOR74600 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001572053-01-3 540AB 540AZ 540BB540BZ 540CB 640AB640AZ 640BB 640BZ640CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGDRAIN HOLES IN STRINGERS AND BUTT STRAP ATSTRINGER 8 AND STRINGER 11, EXCLUDING THE AREAINSIDE THE DRY BAY28700 FCOR51400 FH12300 FCOR22000 FHA321572053-01-4 540AB 540AZ 540BB540BZ 540CB 640AB640AZ 640BB 640BZ640CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGDRAIN HOLES IN STRINGERS AND BUTT STRAP ATSTRINGER 8 AND STRINGER 11, EXCLUDING THE AREAINSIDE THE DRY BAY12700 FCOR54600 FH11800 FCOR50900 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 92EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572053-01-5 540AB 540AZ 540BB540BZ 540CB 640AB640AZ 640BB 640BZ640CBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDINGDRAIN HOLES IN STRINGERS AND BUTT STRAP ATSTRINGER 8 AND STRINGER 11, EXCLUDING THE AREAINSIDE THE DRY BAYNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572053-01-2.25000 FCOR44800 FH11800 FCOR21100 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970572053-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 10R 572054-01-1 FUEL PUMPREMOVEDDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT FUELPUMP APERTURES BETWEENRIB 1 AND RIB 249700 FCOR99400 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001N 572054-01-8 FUEL PUMPREMOVEDDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT FUELPUMP APERTURES BETWEENRIB 1 AND RIB 224700 FCOR49400 FH7500 FCOR15000 FHA320-200POST 160001R 572101-01-1 522AB 522CB 522EB522FB 522HB 522JB522KB 522LB 522NB522QB 622AB 622CB622EB 622FB 622HB622JB 622KB 622LB622NB 622QBDETAILED INSPECTION OFOUTER WING, FRONT SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 22,INCLUDING ALL CUTOUTS43000 FCOR86000 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001R 572101-01-7 522AB 522CB 522EB522FB 522HB 522JB522KB 522LB 522NB522QB 622AB 622CB622EB 622FB 622HB622JB 622KB 622LB622NB 622QBDETAILED INSPECTION OFOUTER WING, FRONT SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 22,INCLUDING ALL CUTOUTSNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572101-01-1.33300 FCOR55100 FH11600 FCOR19100 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 93EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTEN 572101-01-8 522AB 522CB 522EB522FB 522HB 522JB522KB 522LB 522NB522QB 622AB 622CB622EB 622FB 622HB622JB 622KB 622LB622NB 622QBDETAILED INSPECTION OFOUTER WING, FRONT SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 22,INCLUDING ALL CUTOUTS30500 FCOR61000 FH4700 FCOR9400 FHA320-200POST 160001572108-01-1 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2233100 FCOR48000 FH10500 FCOR23200 FHA320-100R 572108-01-2 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2235700 FCOR71400 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001572108-01-4 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2231000 FCOR51200 FH8800 FCOR14500 FHGROUP 19-1AORGROUP 19-1BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 94EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572108-01-5 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2227100 FCOR44700 FH7800 FCOR13000 FHA320-200POST 34650ORA320-200POST 152970572108-01-6 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2229500 FCOR48700 FH8000 FCOR13100 FHGROUP 18-1A572108-01-7 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2217100 FCOR73800 FH5000 FCOR21500 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 95EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTEN 572108-01-8 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2230300 FCOR60600 FH8300 FCOR16600 FHA320-200POST 160058ORA320-200POST 160075ORA320-200POST 160076N 572108-01-9 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 640CB640DB 640EB 640FB640GB 640HB 640JB640KB 640LB 640MB640NB 640PB 640QB640RBDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 8 AND RIB 2224200 FCOR48400 FH8300 FCOR16600 FHA320-200PRE 160058POST 160001PRE 160075PRE 160076N 572109-01-5 550AB 550BB 550CB550DB 650AB 650BB650CB 650DB 560AB660ABDETAILED INSPECTION OFOUTER WING, FRONT SPARAFT FACE, BETWEEN RIB 22 AND RIB 2733900 FCOR67800 FH3100 FCOR6200 FHA320-200POST 160001572111-01-1DELETED FROM ALS PART 2 AT REVISION 01572111-01-2 573CB 573EB 573FB575AB 673CB 673EB673FB 675ABDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, FROM RIB 8 TO RIB 1121800 FCOR35800 FH11600 FCOR19000 FHGROUP 18-1AORGROUP 19-1AORGROUP 21-1A572111-01-3 573CB 573EB 573FB575AB 673CB 673EB673FB 675ABDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, FROM RIB 8 TO RIB 1124000 FCOR42000 FH14000 FCOR23000 FHGROUP 21-1BORA321-200572111-01-4 573CB 573EB 573FB575AB 673CB 673EB673FB 675ABDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, FROM RIB 8 TO RIB 1115900 FCOR68300 FH9600 FCOR41400 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 96EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572111-01-6 573CB 573EB 573FB575AB 673CB 673EB673FB 675ABDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, FROM RIB 8 TO RIB 11NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572111-01-1.21800 FCOR35800 FH11200 FCOR18400 FHGROUP 19-1BORA320-100ORA320-200POST 34650ORA320-200POST 152970R 572112-01-1 575BB 575CB 575DB575EB 575FB 575GB575HB 575KB 575LB575MB 675BB 675CB675DB 675EB 675FB675GB 675HB 675KB675LB 675MBDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDINGJOINT PLATE AT RIB 2221000 FCOR42000 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001572112-01-2 575BB 575CB 575DB575EB 575FB 575GB575HB 575KB 575LB575MB 675BB 675CB675DB 675EB 675FB675GB 675HB 675KB675LB 675MBDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDINGJOINT PLATE AT RIB 2222800 FCOR40300 FH12500 FCOR22100 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORGROUP 21-1A572112-01-3 575BB 575CB 575DB575EB 575FB 575GB575HB 575KB 575LB575MB 675BB 675CB675DB 675EB 675FB675GB 675HB 675KB675LB 675MBDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDINGJOINT PLATE AT RIB 2224000 FCOR42000 FH15100 FCOR26700 FHGROUP 21-1BORA321-200572112-01-4 DELETED FROM ALI DOCUMENT AT ISSUE 10R 572112-01-6 575BB 575CB 575DB575EB 575FB 575GB575HB 575KB 575LB575MB 675BB 675CB675DB 675EB 675FB675GB 675HB 675KB675LB 675MBDETAILED INSPECTION OFOUTER WING, REAR SPARAFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDINGJOINT PLATE AT RIB 2221000 FCOR37200 FH11900 FCOR21000 FHA320-100ORA320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 97EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572114-01-1 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES32900 FCOR48000 FH9600 FCOR15600 FHA320-100572114-01-2 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES37100 FCOR60000 FH10500 FCOR17200 FHGROUP 21-1A572114-01-3 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES30100 FCOR49400 FH9400 FCOR15300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BR 572114-01-4 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES30100 FCOR60200 FH10100 FCOR20200 FHA320-200PRE 34650PRE 152970PRE 160001572114-01-5 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES38900 FCOR60000 FH11600 FCOR19000 FHGROUP 21-1BORA321-200R 572114-01-6 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES30100 FCOR49400 FH8500 FCOR13900 FHA320-200POST 34650ORA320-200POST 152970N 572114-01-8 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES32500 FCOR65000 FH7100 FCOR14200 FHA320-200POST 160058ORA320-200POST 160075ORA320-200POST 160076N 572114-01-9 540CB 540DB 540EB640CB 640DB 640EBDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 8 AND RIB 11,INCLUDING TOP AND BOTTOM FLANGES21100 FCOR42200 FH7100 FCOR14200 FHA320-200PRE 160058POST 160001PRE 160075PRE 160076A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 98EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572115-01-2 540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 550AB550BB 550CB 550DB560AB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QB 640RB650AB 650BB 650CB650DB 660ABDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 11 AND RIB 27,INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOMFLANGES43200 FCOR86400 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001572115-01-3 540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 550AB550BB 550CB 550DB560AB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QB 640RB650AB 650BB 650CB650DB 660ABDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 11 AND RIB 27,INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOMFLANGES35600 FCOR58100 FH12400 FCOR20200 FHGROUP 21-1BORA321-200572115-01-4 540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 550AB550BB 550CB 550DB560AB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QB 640RB650AB 650BB 650CB650DB 660ABDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 11 AND RIB 27,INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOMFLANGES34600 FCOR56400 FH12400 FCOR20200 FHGROUP 21-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 99EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572115-01-6 540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 550AB550BB 550CB 550DB560AB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QB 640RB650AB 650BB 650CB650DB 660ABDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 11 AND RIB 27,INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOMFLANGES24600 FCOR40100 FH15800 FCOR25700 FHA320-200POST 34650ORA320-200POST 152970N 572115-01-8 540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 550AB550BB 550CB 550DB560AB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QB 640RB650AB 650BB 650CB650DB 660ABDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 11 AND RIB 27,INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOMFLANGES11100 FCOR22200 FH6800 FCOR13600 FHA320-200PRE 160058POST 160001PRE 160075PRE 160076N 572115-01-9 540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 540RB 550AB550BB 550CB 550DB560AB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QB 640RB650AB 650BB 650CB650DB 660ABDETAILED INSPECTION OFOUTER WING, REAR SPARFORWARD FACE, BETWEEN RIB 11 AND RIB 27,INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOMFLANGES33500 FCOR67000 FH6800 FCOR13600 FHA320-200POST 160058ORA320-200POST 160075ORA320-200POST 160076R 572116-02-1 N/A DETAILED INSPECTION OF OUTER WING, TOP SKIN,UPPER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR BETWEEN RIB 8 AND RIB 2258800 FCOR117600 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 100EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572120-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING, TOPSKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS ANDSTRINGERS BETWEEN RIB 8 AND RIB 27 FROM FRONTSPAR TO REAR SPAR51700 FCOR103400 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001R 572123-01-1 540CB 540DB 540EB540FB 540GB 640CB640DB 640EB 640FB640GBDETAILED INSPECTION OF OUTER WING, TOP SKIN,STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES, STRINGERSJOINT BETWEEN RIB 8 AND RIB 9 AND BUTT STRAP ATSTRINGER 1153200 FCOR106400 FH20000 FCOR40000 FHA320-200PRE 34650PRE 152970PRE 160001N 572123-01-4 540CB 540DB 540EB540FB 540GB 640CB640DB 640EB 640FB640GBDETAILED INSPECTION OF OUTER WING, TOP SKIN,STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDINGRUNOUTS AND AIR TRANSFER HOLES, STRINGERSJOINT BETWEEN RIB 8 AND RIB 9 AND BUTT STRAP ATSTRINGER 1137500 FCOR75000 FH29400 FCOR58800 FHA320-200POST 160001572124-01-1 540HB 540JB 540KB540LB 540MB 540NB540PB 540QB 540RB550AB 550BB 550CB550DB 560AB 640HB640JB 640KB 640LB640MB 640NB 640PB640QB 640RB 650AB650BB 650CB 650DB660ABDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDINGRUNOUTS, AIR TRANSFERHOLES AND BUTT STRAP ATSTRINGER 11, INCLUDING RUNOUT AT FRONT SPAR ATRIB 1839900 FCOR48000 FH17300 FCOR30500 FHA320-100R 572124-01-3 540HB 540JB 540KB540LB 540MB 540NB540PB 540QB 540RB550AB 550BB 550CB550DB 560AB 640HB640JB 640KB 640LB640MB 640NB 640PB640QB 640RB 650AB650BB 650CB 650DB660ABDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDINGRUNOUTS, AIR TRANSFERHOLES AND BUTT STRAP ATSTRINGER 11, INCLUDING RUNOUT AT FRONT SPAR ATRIB 1853300 FCOR106600 FH17300 FCOR34600 FHA320-200PRE 34650PRE 152970PRE 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 101EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572124-01-4 540HB 540JB 540KB540LB 540MB 540NB540PB 540QB 540RB550AB 550BB 550CB550DB 560AB 640HB640JB 640KB 640LB640MB 640NB 640PB640QB 640RB 650AB650BB 650CB 650DB660ABDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDINGRUNOUTS, AIR TRANSFERHOLES AND BUTT STRAP ATSTRINGER 11, INCLUDING RUNOUT AT FRONT SPAR ATRIB 1844700 FCOR60000 FH17300 FCOR30500 FHGROUP 19-1AORGROUP 19-1B572124-01-5 540HB 540JB 540KB540LB 540MB 540NB540PB 540QB 540RB550AB 550BB 550CB550DB 560AB 640HB640JB 640KB 640LB640MB 640NB 640PB640QB 640RB 650AB650BB 650CB 650DB660ABDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDINGRUNOUTS, AIR TRANSFERHOLES AND BUTT STRAP ATSTRINGER 11, INCLUDING RUNOUT AT FRONT SPAR ATRIB 1842900 FCOR60000 FH17300 FCOR30500 FHGROUP 18-1A572124-01-6 540HB 540JB 540KB540LB 540MB 540NB540PB 540QB 540RB550AB 550BB 550CB550DB 560AB 640HB640JB 640KB 640LB640MB 640NB 640PB640QB 640RB 650AB650BB 650CB 650DB660ABDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDINGRUNOUTS, AIR TRANSFERHOLES AND BUTT STRAP ATSTRINGER 11, INCLUDING RUNOUT AT FRONT SPAR ATRIB 1817800 FCOR76600 FH14400 FCOR62100 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 102EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572124-01-7 540HB 540JB 540KB540LB 540MB 540NB540PB 540QB 540RB550AB 550BB 550CB550DB 560AB 640HB640JB 640KB 640LB640MB 640NB 640PB640QB 640RB 650AB650BB 650CB 650DB660ABDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDINGRUNOUTS, AIR TRANSFERHOLES AND BUTT STRAP ATSTRINGER 11, INCLUDING RUNOUT AT FRONT SPAR ATRIB 1843000 FCOR60000 FH17300 FCOR30500 FHA320-200POST 34650ORA320-200POST 152970N 572124-01-8 540HB 540JB 540KB540LB 540MB 540NB540PB 540QB 540RB550AB 550BB 550CB550DB 560AB 640HB640JB 640KB 640LB640MB 640NB 640PB640QB 640RB 650AB650BB 650CB 650DB660ABDETAILED INSPECTION OF OUTER WING, TOP SKINSTRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDINGRUNOUTS, AIR TRANSFERHOLES AND BUTT STRAP ATSTRINGER 11, INCLUDING RUNOUT AT FRONT SPAR ATRIB 1840300 FCOR80600 FH29400 FCOR58800 FHA320-200POST 160001572129-01-1 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENTS TO FRONT SPARAND REAR SPAR, BETWEEN RIB 8 AND RIB 15,EXCLUDING AREAS COVERED BY PYLON REINFORCING,PYLON FAIRING AND FLAP TRACK 3 FAIRING28900 FCOR50200 FH6300 FCOR10900 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100572129-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENTS TO FRONT SPARAND REAR SPAR, BETWEEN RIB 8 AND RIB 15,EXCLUDING AREAS COVERED BY PYLON REINFORCING,PYLON FAIRING AND FLAP TRACK 3 FAIRING38000 FCOR60000 FH6500 FCOR11300 FHGROUP 21-1AORGROUP 21-2A572129-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENTS, TO FRONT SPARAND REAR SPAR, BETWEEN RIB 8 AND RIB 15,EXCLUDING AREAS COVERED BY PYLON REINFORCING,PYLON FAIRING AND FLAP TRACK 3 FAIRING32400 FCOR56300 FH4900 FCOR8500 FHGROUP 21-1BORGROUP 21-2BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 103EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572129-01-4 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENTS TO FRONT SPARAND REAR SPAR, BETWEEN RIB 8 AND RIB 15,EXCLUDING AREAS COVERED BY PYLON REINFORCING,PYLON FAIRING AND FLAP TRACK 3 FAIRING45700 FCOR91400 FH7300 FCOR14600 FHA320-200PRE 34650PRE 152970PRE 160001572129-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENTS TO FRONT SPARAND REAR SPAR, BETWEEN RIB 8 AND RIB 15,EXCLUDING AREAS COVERED BY PYLON REINFORCING,PYLON FAIRING AND FLAP TRACK 3 FAIRING14800 FCOR63600 FH6300 FCOR27000 FHGROUP 19-1CR 572129-01-6 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENTS TO FRONT SPARAND REAR SPAR, BETWEEN RIB 8 AND RIB 15,EXCLUDING AREAS COVERED BY PYLON REINFORCING,PYLON FAIRING AND FLAP TRACK 3 FAIRING41400 FCOR60000 FH7300 FCOR12700 FHA320-200POST 34650ORA320-200POST 152970572130-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR, BETWEEN RIB 15 AND RIB 22,EXCLUDING AREA COVERED BYFLAP TRACK 4 FAIRING35600 FCOR60000 FH6500 FCOR11300 FHGROUP 21-1A572130-01-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR, BETWEEN RIB 15 AND RIB 22,EXCLUDING AREA COVERED BYFLAP TRACK 4 FAIRING38000 FCOR60000 FH6500 FCOR11300 FHGROUP 21-2A572130-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR, BETWEEN RIB 15 AND RIB 22,EXCLUDING AREA COVERED BYFLAP TRACK 4 FAIRING36700 FCOR60000 FH6500 FCOR11300 FHGROUP 21-1BORGROUP 21-2BR 572130-01-6 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR, BETWEEN RIB 15 AND RIB 22,EXCLUDING AREA COVERED BYFLAP TRACK 4 FAIRING46000 FCOR60000 FH14100 FCOR24600 FHA320-200POST 34650ORA320-200POST 152970R 572130-01-7 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARAND REAR SPAR, BETWEEN RIB 15 AND RIB 22,EXCLUDING AREA COVERED BYFLAP TRACK 4 FAIRING46000 FCOR92000 FH14100 FCOR28200 FHA320-200PRE 34650PRE 152970PRE 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 104EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572134-01-1 540FB 540GB 540NB540PB 640FB 640GB640NB 640PBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE IN AREASOF FLAP TRACK 3 AND 4FORWARD AND AFT PICK UP FITTINGS, INCLUDINGATTACHMENT TO REAR SPAR35500 FCOR48000 FH12700 FCOR28900 FHA320-100R 572134-01-2 540FB 540GB 540NB540PB 640FB 640GB640NB 640PBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE IN AREASOF FLAP TRACK 3 AND 4FORWARD AND AFT PICK UP FITTINGS, INCLUDINGATTACHMENT TO REAR SPAR53500 FCOR107000 FH8800 FCOR17600 FHA320-200PRE 34650PRE 152970572134-01-4 540FB 540GB 540NB540PB 640FB 640GB640NB 640PBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE IN AREASOF FLAP TRACK 3 AND 4FORWARD AND AFT PICK UP FITTINGS, INCLUDINGATTACHMENT TO REAR SPAR32000 FCOR60000 FH10600 FCOR24200 FHGROUP 19-1AORGROUP 19-1B572134-01-5 540FB 540GB 540NB540PB 640FB 640GB640NB 640PBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE IN AREASOF FLAP TRACK 3 AND 4FORWARD AND AFT PICK UP FITTINGS, INCLUDINGATTACHMENT TO REAR SPAR28300 FCOR60000 FH10600 FCOR24200 FHGROUP 18-1A572134-01-6 540FB 540GB 540NB540PB 640FB 640GB640NB 640PBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE IN AREASOF FLAP TRACK 3 AND 4FORWARD AND AFT PICK UP FITTINGS, INCLUDINGATTACHMENT TO REAR SPAR16400 FCOR70500 FH8400 FCOR36200 FHGROUP 19-1CR 572134-01-7 540FB 540GB 540NB540PB 640FB 640GB640NB 640PBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE IN AREASOF FLAP TRACK 3 AND 4FORWARD AND AFT PICK UP FITTINGS, INCLUDINGATTACHMENT TO REAR SPAR29300 FCOR60000 FH7900 FCOR18100 FHA320-200POST 34650ORA320-200POST 152970572137-01-1 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)24000 FCOR42000 FH6200 FCOR10400 FHA320-100R 572137-01-2 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)58200 FCOR116400 FH5500 FCOR11000 FHA320-200PRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 105EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572137-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)24000 FCOR42000 FH4900 FCOR8200 FHGROUP 21-1AORGROUP 21-2A572137-01-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)24000 FCOR42000 FH5000 FCOR8400 FHGROUP 19-1AORGROUP 19-1B572137-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)24000 FCOR42000 FH4500 FCOR7600 FHGROUP 21-1BORGROUP 21-2BR 572137-01-6 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)19700 FCOR33400 FH4700 FCOR7900 FHA320-200POST 34650ORA320-200POST 152970572137-01-7 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)10500 FCOR45100 FH4200 FCOR18000 FHGROUP 19-1C572137-01-8 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY10-11), STRINGER 5 (RIB BAY13-14), STRINGER 13 (RIBBAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIBBAY 19-20) AND STRINGER 12 (RIB BAY 17-18)24000 FCOR42000 FH4700 FCOR7900 FHGROUP 18-1AR 572139-02-1 540CB 540DB 540EB540FB 540GB 640CB640DB 640EB 640FB640GBSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, BOTTOM SKIN, UPPER AND LOWER SURFACESAROUND ACCESS DOOR CUTOUTSIN RIB BAYS 8-9, 9-10,10-11, 11-12 AND 12-1352800 FCOR105600 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970572140-02-2DELETED FROM ALS PART 2 AT REVISION 01572140-02-3 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACES, AROUND ACCESSDOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB2740900 FCOR60000 FH3400 FCOR6000 FHGROUP 21-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 106EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572140-02-4 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACES, AROUND ACCESSDOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB2742900 FCOR85800 FH3300 FCOR6600 FHA320-200PRE 34650PRE 152970PRE 160001R 572140-02-5 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACES, AROUND ACCESSDOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB2734200 FCOR60000 FH3200 FCOR5700 FHA320-200POST 34650ORA320-200POST 152970572140-02-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACES, AROUND ACCESSDOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB279000 FCOR38700 FH2600 FCOR11100 FHGROUP 19-1C572142-01-1 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15,FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREASCOVERED BY PYLON FAIRING AND FLAP TRACK 3FAIRING24000 FCOR42000 FH4400 FCOR7400 FHA320-100R 572142-01-2 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15,FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREASCOVERED BY PYLON FAIRING AND FLAP TRACK 3FAIRING48300 FCOR96600 FH5600 FCOR11200 FHA320-200PRE 34650PRE 152970PRE 160001572142-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15,FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREASCOVERED BY PYLON FAIRING AND FLAP TRACK 3FAIRING24000 FCOR42000 FH4000 FCOR6800 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORGROUP 21-1BORGROUP 21-2AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 107EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572142-01-4 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15,FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREASCOVERED BY PYLONFAIRING AND FLAP TRACK 3FAIRING19900 FCOR33900 FH4000 FCOR6800 FHGROUP 21-1A572142-01-5 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15,FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREASCOVERED BY PYLONFAIRING AND FLAP TRACK 3FAIRING42700 FCOR60000 FH4000 FCOR6800 FHGROUP 21-2B572142-01-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15,FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREASCOVERED BY PYLON FAIRING AND FLAP TRACK 3FAIRING12400 FCOR53300 FH4000 FCOR17200 FHGROUP 19-1CR 572142-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15,FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREASCOVERED BY PYLON FAIRING AND FLAP TRACK 3FAIRING24000 FCOR42000 FH3800 FCOR6400 FHA320-200POST 34650ORA320-200POST 152970572143-01-1 532AB 532BB 532CB532DB 533AB 533BB533CB 533DB 632AB632BB 632CB 632DB633AB 633BB 633CB633DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS IN AREA COVERED BY FLAP TRACK 3FAIRING AND FLAP TRACK 4 FAIRING35800 FCOR48000 FH12100 FCOR20600 FHA320-100R 572143-01-2 532AB 532BB 532CB532DB 533AB 533BB533CB 533DB 632AB632BB 632CB 632DB633AB 633BB 633CB633DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS IN AREA COVERED BY FLAP TRACK 3FAIRING AND FLAP TRACK 4 FAIRING53500 FCOR107000 FH10900 FCOR21800 FHA320-200PRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 108EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572143-01-3 532CB 532EB 533CB533EB 632CB 632EB633CB 633EBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS IN AREA COVERED BY FLAP TRACK 3FAIRING AND FLAP TRACK 4 FAIRING39200 FCOR60000 FH9800 FCOR16600 FHA321572143-01-4 532AB 532BB 532CB532DB 533AB 533BB533CB 533DB 632AB632BB 632CB 632DB633AB 633BB 633CB633DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS IN AREA COVERED BY FLAP TRACK 3FAIRING AND FLAP TRACK 4 FAIRING17800 FCOR76500 FH9400 FCOR40400 FHGROUP 19-1CR 572143-01-5 532AB 532BB 532CB532DB 533AB 533BB533CB 533DB 632AB632BB 632CB 632DB633AB 633BB 633CB633DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO RIBS ANDSTRINGERS IN AREA COVERED BY FLAP TRACK 3FAIRING AND FLAP TRACK 4 FAIRINGNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572143-01-2.31700 FCOR54000 FH9400 FCOR16000 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970R 572144-01-5 N/A GENERAL VISUALINSPECTION OF OUTER WING ,BOTTOM SKIN, LOWER SURFACE AT ATTACHMENT TORIBS AND STRINGERS BETWEEN RIB 15 AND RIB 27FROM FRONT SPAR TO REAR SPAR EXCLUDING AREACOVERED BY FLAP TRACK 4 FAIRING.50800 FCOR101600 FH6700 FCOR13400 FHA320-200PRE 34650PRE 152970PRE 160001572148-01-1 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING24000 FCOR42000 FH4400 FCOR7100 FHA320-100R 572148-01-2 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING48300 FCOR96600 FH6000 FCOR12000 FHA320-200PRE 34650PRE 152970PRE 160001A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 109EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572148-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING24000 FCOR40400 FH3800 FCOR6100 FHGROUP 19-1AORGROUP 19-1B572148-01-4 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING19900 FCOR32300 FH4500 FCOR7300 FHGROUP 21-1A572148-01-5 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING24000 FCOR39000 FH4500 FCOR7300 FHGROUP 21-2A572148-01-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING24000 FCOR39000 FH3700 FCOR6100 FHGROUP 21-1BORGROUP 21-2B572148-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING24000 FCOR42000 FH3500 FCOR5700 FHGROUP 18-1A572148-01-8 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING12100 FCOR52300 FH3800 FCOR16300 FHGROUP 19-1CR 572148-01-9 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 8 AND RIB 18, EXCLUDING AREAS COVERED BYPYLON FAIRING AND BYFLAP TRACK 3 FAIRING21700 FCOR35300 FH3800 FCOR6100 FHA320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 110EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572149-01-1 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING40000 FCOR48000 FH5800 FCOR9400 FHA320-100R 572149-01-2 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING56500 FCOR113000 FH6000 FCOR12000 FHA320-200PRE 34650PRE 152970PRE 160001572149-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING25800 FCOR42000 FH5100 FCOR8300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1B572149-01-4 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING27000 FCOR43900 FH5300 FCOR8600 FHGROUP 21-1AR 572149-01-5 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING32200 FCOR52300 FH5300 FCOR8600 FHGROUP 21-2A572149-01-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING32200 FCOR53300 FH3700 FCOR6100 FHGROUP 21-1BORGROUP 21-2BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 111EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572149-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING12600 FCOR54400 FH3900 FCOR16800 FHGROUP 19-1CR 572149-01-8 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, SPANWISE SKINJOINTS AT STRINGER 8 AND STRINGER 11, BETWEENRIB 18 AND RIB 21, ADJACENT TO FRONT SPAR ANDREAR SPAR, EXCLUDINGAREA COVERED BY FLAPTRACK 4 FAIRING22600 FCOR36700 FH5100 FCOR8300 FHA320-200POST 34650ORA320-200POST 152970572150-01-1 532AB 532BB 532CB532DB 632AB 632BB632CB 632DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 11 ANDRIB 13 IN AREA COVEREDBY FLAP TRACK 3 FAIRING29500 FCOR48000 FH10100 FCOR17200 FHA320-100R 572150-01-2 532AB 532BB 532CB532DB 632AB 632BB632CB 632DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 11 ANDRIB 13 IN AREAS COVEREDBY FLAP TRACK 3 FAIRING53500 FCOR107000 FH7800 FCOR15600 FHA320-200PRE 34650PRE 152970572150-01-3 532AB 532BB 532CB532DB 632AB 632BB632CB 632DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 11 ANDRIB 13 IN AREA COVEREDBY FLAP TRACK 3 FAIRING24000 FCOR42000 FH9400 FCOR16000 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1B572150-01-4 532CB 532EB 632CB632EBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 11 ANDRIB 13 IN AREA COVEREDBY FLAP TRACK 3 FAIRING24000 FCOR42000 FH9400 FCOR16000 FHGROUP 21-1AORGROUP 21-2A572150-01-5 532CB 532EB 632CB632EBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 11 ANDRIB 13 IN AREAS COVEREDBY FLAP TRACK 3 FAIRING24000 FCOR40700 FH4800 FCOR8300 FHGROUP 21-1BORGROUP 21-2B572150-01-6 532AB 532BB 532CB532DB 632AB 632BB632CB 632DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 11 ANDRIB 13 IN AREA COVEREDBY FLAP TRACK 3 FAIRING12500 FCOR53700 FH6200 FCOR26800 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 112EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572150-01-7 532AB 532BB 532CB532DB 632AB 632BB632CB 632DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 11 ANDRIB 13 IN AREAS COVEREDBY FLAP TRACK 3 FAIRING24000 FCOR42000 FH9400 FCOR16000 FHA320-200POST 34650ORA320-200POST 152970R 572151-01-2 533AB 533BB 533CB533DB 633AB 633BB633CB 633DBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, SPANWISE SKIN JOINTS ATSTRINGER 8 AND STRINGER 11, BETWEEN RIB 18 ANDRIB 20 IN AREA COVEREDBY FLAP TRACK 4 FAIRING56500 FCOR113000 FH10900 FCOR21800 FHA320-200PRE 34650PRE 152970R 572155-01-1 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE BUTT STRAPS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 2148300 FCOR96600 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970572155-01-2 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE BUTT STRAPS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 2122500 FCOR42800 FH11700 FCOR22200 FHGROUP 21-1AR 572155-01-3 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE BUTT STRAPS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 2130500 FCOR58100 FH15500 FCOR29600 FHGROUP 21-2APRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 113EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572155-01-4 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE BUTT STRAPS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 2122800 FCOR42000 FH9900 FCOR18800 FHGROUP 21-1BORGROUP 21-2BR 572155-01-5 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE BUTT STRAPS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 2130500 FCOR58100 FH9600 FCOR18300 FHGROUP 21-2APOST 34650ORGROUP 21-2APOST 152970572155-01-6 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE BUTT STRAPS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 2116000 FCOR68800 FH11200 FCOR48100 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 114EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572155-01-7 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 540NB 540PB540QB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MB 640NB640PB 640QBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINUPPER SURFACE BUTT STRAPS AT STRINGER 8 ANDSTRINGER 11, BETWEEN RIB 8 AND RIB 21NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572155-01-1.28700 FCOR54600 FH11200 FCOR21300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA320-200POST 34650ORA320-200POST 152970572158-01-1 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1329900 FCOR48000 FH12400 FCOR25000 FHA320-100R 572158-01-2 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1348300 FCOR96600 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970PRE 160001572158-01-3 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1324000 FCOR42000 FH11900 FCOR24000 FHGROUP 21-1AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 115EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE572158-01-4 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1324000 FCOR42000 FH9800 FCOR19800 FHGROUP 21-1BORGROUP 21-2B572158-01-5 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1329900 FCOR60000 FH11400 FCOR23000 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BR 572158-01-6 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1328600 FCOR57900 FH9600 FCOR19500 FHGROUP 21-2APOST 34650ORGROUP 21-2APOST 152970572158-01-7 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1315600 FCOR67000 FH10600 FCOR45500 FHGROUP 19-1CR 572158-01-8 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 13NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572158-01-4.28600 FCOR57900 FH21800 FCOR44100 FHGROUP 21-2APRE 34650PRE 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 116EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572158-01-9 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1328000 FCOR56500 FH11400 FCOR23000 FHA320-200POST 34650ORA320-200POST 152970N 572158-01-10 540CB 540DB 540EB540FB 540GB 540HB540JB 540KB 540LB540MB 640CB 640DB640EB 640FB 640GB640HB 640JB 640KB640LB 640MBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12AND 1342000 FCOR84000 FH10400 FCOR20800 FHA320-200POST 160001572160-01-1 540NB 540PB 540QB540RB 550AB 550BB550CB 550DB 560AB640NB 640PB 640QB640RB 650AB 650BB650CB 650DB 660ABDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISINGSTRINGERS 7, 8 AND 1136800 FCOR48000 FH17200 FCOR29700 FHA320-100572160-01-2DELETED FROM ALS PART 2 AT REVISION 01572160-01-3 540NB 540PB 540QB540RB 550AB 550BB550CB 550DB 560AB640NB 640PB 640QB640RB 650AB 650BB650CB 650DB 660ABDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISINGSTRINGERS 7, 8 AND 1124000 FCOR42000 FH16100 FCOR27800 FHA321572160-01-4 540NB 540PB 540QB540RB 550AB 550BB550CB 550DB 560AB640NB 640PB 640QB640RB 650AB 650BB650CB 650DB 660ABDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISINGSTRINGERS 7, 8 AND 1112700 FCOR54600 FH12700 FCOR54600 FHGROUP 19-1CA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 117EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 572160-01-5 540NB 540PB 540QB540RB 550AB 550BB550CB 550DB 560AB640NB 640PB 640QB640RB 650AB 650BB650CB 650DB 660ABDETAILED INSPECTION OF OUTER WING, BOTTOM SKINSTRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISINGSTRINGERS 7, 8 AND 11NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 572160-01-2.34000 FCOR58700 FH15500 FCOR26800 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970572164-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 9572164-02-2 DELETED FROM ALI DOCUMENT AT ISSUE 9572164-02-3 DELETED FROM ALI DOCUMENT AT ISSUE 9572164-02-4 DELETED FROM ALI DOCUMENT AT ISSUE 9572164-02-5 DELETED FROM ALI DOCUMENT AT ISSUE 10R 572164-02-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE AT FUEL TANK WATERDRAIN HOLES BETWEEN RIB 15-16 AND RIB 22-2348000 FCOR96000 FH8300 FCOR16600 FHA320-200PRE 34650PRE 152970PRE 160001R 573101-01-1 N/A DETAILED INSPECTION OF WING TIP, BOTTOM SKINLOWER SURFACE JOINT, OUTBOARD OF RIB 2760000 FCOR120000 FH15000 FCOR30000 FHA320-200PRE 34650PRE 152970573101-01-3 N/A DETAILED INSPECTION OF WING TIP, BOTTOM SKINLOWER SURFACE JOINT, OUTBOARD OF RIB 2715600 FCOR67100 FH12400 FCOR53300 FHGROUP 19-1CR 573101-01-4 N/A DETAILED INSPECTION OF WING TIP, BOTTOM SKINLOWER SURFACE JOINT, OUTBOARD OF RIB 27NOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 573101-01-1.27900 FCOR39000 FH12400 FCOR17300 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 118EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE574101-01-3 521AB 521CB 521EB522AB 522CB 522FB522KB 522LB 522NB522QB 522SB 522UB621AB 621CB 621EB622AB 622CB 622FB622KB 622LB 622NB622QB 622SB 622UBDETAILED INSPECTION OF OUTER WING, FIXED LEADINGEDGE, ROLLER PIN HOLES AND OTHER CUTOUTS INTRACK RIB 1 TO 1252200 FCOR104400 FH20600 FCOR41200 FHA320-200N 574106-01-8 521AB 521CB 521EB522AB 522CB 522FB522KB 522LB 522NB522QB 522SB 522UB621AB 621CB 621EB622AB 622CB 622FB622KB 622LB 622NB622QB 622SB 622UBDETAILED INSPECTION OF OUTER WING, FIXED LEADINGEDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TORIB 1236900 FCOR73800 FH12700 FCOR25400 FHA320-200POST 160001N 574112-02-3 521AB 521CB 521EB522AB 522CB 522FB522KB 522LB 522NB522QB 522SB 522UB621AB 621CB 621EB622AB 622CB 622FB622KB 622LB 622NB622QB 622SB 622UBGENERAL VISUAL INSPECTIONOF OUTER WING, FIXEDLEADING EDGE, BOTTOM WING SKIN, UPPER ANDLOWER SURFACES, FORWARD OF FRONT SPAR, FROMRIB 1 TO RIB 27, INCLUDING SIGHTING ROD HOLES INRIB BAY 8-9 AND RIB BAY 26-27, LIFTING BEAM HOLESAND RAIN HOLES31200 FCOR62400 FH6600 FCOR13200 FHA320-200POST 160001574114-01-1 521CB 521EB 522AB522CB 522FB 522KB522LB 522NB 522QB522SB 522UB 621CB621EB 622AB 622CB622FB 622KB 622LB622NB 622QB 622SB622UBSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, FIXED LEADING EDGE PINION FITTING BOLTINGAND ACTUATOR BOLTING LOWER BOLT HOLES ON RIBS2, 3, 5, 6, 7, 8, 9, 10, 11 AND 1236900 FCOR51600 FH12300 FCOR17100 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 119EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 574114-01-3 521CB 521EB 522AB522CB 522FB 522KB522LB 522NB 522QB522SB 522UB 621CB621EB 622AB 622CB622FB 622KB 622LB622NB 622QB 622SB622UBSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, FIXED LEADING EDGE PINION FITTING BOLTINGAND ACTUATOR BOLTING LOWER BOLT HOLES ON RIBS2, 3, 5, 6, 7, 8, 9, 10, 11 AND 1233200 FCOR46500 FH12300 FCOR17100 FHA320-200POST 34650ORA320-200POST 152970N 575151-01-6 573AB 573BB 573CB574AB 574BB 673AB673BB 673CB 674AB674BBDETAILED INSPECTION OFOUTER WING, TRAILINGEDGE FALSE REAR SPAR, FORWARD AND AFT FACES28900 FCOR57800 FH2400 FCOR4800 FHA320-200POST 160001R 575155-01-4 N/A GENERAL VISUALINSPECTION OF OUTER WING,TRAILING EDGE, TOP SKIN UPPER SURFACE, AFT OFREAR SPAR BETWEEN RIB 1 AND RIB 955800 FCOR111600 FH10200 FCOR20400 FHA320-200PRE 34650PRE 152970N 575156-01-1 571AB 671ABFLAPS EXTENDEDDETAILED INSPECTION OFOUTER WING, FIXEDTRAILING EDGE, SHROUD BOX AND FITTINGS35100 FCOR70200 FH15000 FCOR30000 FHA320-200POST 160001575158-01-1 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9, EXCLUDING AREASCOVERED BY FLAP TRACK 2 FAIRINGS AND PYLONFAIRINGS24000 FCOR42000 FH5200 FCOR8800 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-100ORA321575158-01-2 DELETED FROM ALI DOCUMENT AT ISSUE 7R 575158-01-5 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9, EXCLUDING AREASCOVERED BY FLAP TRACK 2 FAIRINGS AND PYLONFAIRINGS25400 FCOR50800 FH13600 FCOR27200 FHA320-200PRE 34650PRE 152970PRE 160001R 575158-01-6 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9, EXCLUDING AREASCOVERED BY FLAP TRACK 2 FAIRINGS AND PYLONFAIRINGS25400 FCOR42900 FH4900 FCOR8300 FHA320-200POST 34650ORA320-200POST 152970A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 120EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE575158-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING,BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9, EXCLUDING AREASCOVERED BY FLAP TRACK 2 FAIRINGS AND PYLONFAIRINGS24000 FCOR42000 FH5200 FCOR8800 FHA320-100575159-01-1DELETED FROM ALS PART 2 AT REVISION 01575159-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, CURVED SKIN EDGE AFT OF REARSPAR JUST INBOARD OF MLG SUPPORT RIB 521800 FCOR34900 FH7800 FCOR12500 FHA321575159-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, CURVED SKIN EDGE AFT OF REARSPAR JUST INBOARD OF MLG SUPPORT RIB 532700 FCOR48000 FH7500 FCOR12000 FHA320-100R 575159-01-5 N/A DETAILED INSPECTIONOF OUTER WING, BOTTOM SKINLOWER SURFACE, CURVED SKIN EDGE AFT OF REARSPAR JUST INBOARD OF MLG SUPPORT RIB 541200 FCOR60000 FH7500 FCOR12000 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320-200POST 34650ORA320-200POST 152970575160-01-1 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING24000 FCOR38400 FH11800 FCOR18900 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1B575160-01-2 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING24000 FCOR42000 FH12300 FCOR19700 FHGROUP 21-1A575160-01-3 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING24000 FCOR42000 FH11900 FCOR19100 FHGROUP 21-2AA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 121EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE575160-01-4 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING24000 FCOR42000 FH10600 FCOR16900 FHGROUP 21-1BORGROUP 21-2BR 575160-01-5 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING60000 FCOR120000 FH11800 FCOR23600 FHA320-200PRE 34650PRE 152970575160-01-6 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING13400 FCOR57600 FH8600 FCOR37300 FHGROUP 19-1CR 575160-01-7 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING23100 FCOR37000 FH13400 FCOR21500 FHA320-200POST 34650ORA320-200POST 152970575160-01-8 574AB 674ABMLG SECONDARYHINGED FAIRINGREMOVEDSPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OFOUTER WING, TRAILING EDGE BOTTOM SKIN AFT OFREAR SPAR, ABOVE MLG REINFORCING24000 FCOR38400 FH11800 FCOR18900 FHA320-100575161-01-1 N/A GENERAL VISUALINSPECTION OF OUTER WING,TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFTOF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDINGJACKING FITTING HOLE AT RIB 9 AND SIGHTING RODHOLE AT RIB 1024000 FCOR42000 FH3800 FCOR6400 FHGROUP 18-1AORGROUP 19-1AORGROUP 19-1B575161-01-2 N/A GENERAL VISUALINSPECTION OF OUTER WING,TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFTOF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDINGJACKING FITTING HOLE AT RIB 9 AND SIGHTING RODHOLE AT RIB 1024000 FCOR42000 FH4000 FCOR6700 FHGROUP 21-1AORGROUP 21-2A575161-01-3 N/A GENERAL VISUALINSPECTION OF OUTER WING,TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFTOF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDINGJACKING FITTING HOLE AT RIB 9 AND SIGHTING RODHOLE AT RIB 1024000 FCOR42000 FH3600 FCOR6100 FHGROUP 21-1BORGROUP 21-2BA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 122EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTER 575161-01-5 N/A GENERAL VISUALINSPECTION OF OUTER WING,TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFTOF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDINGJACKING FITTING HOLE AT RIB 9 AND SIGHTING RODHOLE AT RIB 1040400 FCOR60000 FH4500 FCOR7600 FHA320-200POST 34650ORA320-200POST 152970575161-01-7 N/A GENERAL VISUALINSPECTION OF OUTER WING,TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFTOF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDINGJACKING FITTING HOLE AT RIB 9 AND SIGHTING RODHOLE AT RIB 1024000 FCOR42000 FH3800 FCOR6400 FHA320-100R 575163-01-2 PYLON FAIRINGSREMOVEDSPECIAL DETAILED INSPECTION (LFEC) OF OUTERWING, BOTTOM SKIN LOWERSURFACE, AFT OF REARSPAR, UNDER PYLON FAIRING48000 FCOR96000 FH13200 FCOR26400 FHA320-200PRE 34650PRE 152970575163-01-3 PYLON FAIRINGSREMOVEDSPECIAL DETAILED INSPECTION (LFEC) OF OUTERWING, BOTTOM SKIN LOWERSURFACE, AFT OF REARSPAR, UNDER PYLON FAIRING41500 FCOR60000 FH3600 FCOR5500 FHA321R 575163-01-5 PYLON FAIRINGSREMOVEDSPECIAL DETAILED INSPECTION (LFEC) OF OUTERWING, BOTTOM SKIN LOWERSURFACE, AFT OF REARSPAR, UNDER PYLON FAIRING48000 FCOR60000 FH12100 FCOR18800 FHA320-200POST 34650ORA320-200POST 152970575164-01-3 531CB 531EB 631CB631EBSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, BOTTOM SKIN LOWERSURFACE, AFT OF REARSPAR, AROUND FLAP TRACK 2 FORWARD FITTINGS21400 FCOR35500 FH3900 FCOR6400 FHGROUP 21-1A575164-01-4 531CB 531EB 631CB631EBSPECIAL DETAILED INSPECTION (HFEC) OF OUTERWING, BOTTOM SKIN LOWERSURFACE, AFT OF REARSPAR, AROUND FLAP TRACK 2 FORWARD FITTINGS24000 FCOR42000 FH3900 FCOR6400 FHGROUP 21-1BORA321-200R 575165-01-2 531EB 535AB 535BB631EB 635AB 635BBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, AFT OF REAR SPAR, UNDER FLAPTRACK 2 FAIRING AND FLAP TAB DRIVE 1A FAIRING35400 FCOR58800 FH12700 FCOR21100 FHGROUP 21-1BORA321-200575165-01-3 DELETED FROM ALI DOCUMENT AT ISSUE 7R 575165-01-4 531EB 535AB 535BB631EB 635AB 635BBDETAILED INSPECTION OF OUTER WING, BOTTOM SKINLOWER SURFACE, AFT OF REAR SPAR, UNDER FLAPTRACK 2 FAIRING AND FLAP TAB DRIVE 1A FAIRING29000 FCOR48200 FH12700 FCOR21100 FHGROUP 21-1A575221-01-1 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF INBOARD DOUBLESLOTTED FLAP, EXTERNAL SURFACE OF UPPER ANDLOWER SKIN, LH/RH4800 FC 4800 FC A321A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 123EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE575321-01-2 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF OUTBOARD DOUBLESLOTTED FLAP, INCLUDING TAB, EXTERNAL SURFACEOF UPPER AND LOWER SKIN, LH/RH8500 FC 8500 FC A321576103-01-1 575AT 575KB 575LB575MB 675AT 675KB675LB 675MBDETAILED INSPECTION OF AILERON, HINGE FITTINGSAND ACTUATOR ATTACHMENT FITTINGS38700 FC 15800 FC GROUP 18-1AORGROUP 19-1AORGROUP 19-1BORA320ORA321711300-01-1 437AL 438AR 447AL448ARGENERAL VISUAL INSPECTION OF FAN COWL DOORHINGE FITTINGS7500 FC 7500 FC CFM711300-01-3 DELETED FROM ALI DOCUMENT AT ISSUE 10711300-01-5 DELETED FROM ALI DOCUMENT AT ISSUE 10711300-03-1 437AL 438AR 447AL448ARGENERAL VISUAL INSPECTION OF FAN COWL DOORHINGE FITTINGSNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 711300-01-3.3000 FC 3000 FC IAE711300-03-2 DELETED FROM ALI DOCUMENT AT ISSUE 10711301-01-1 437AL 438AR 447AL448ARDETAILED INSPECTION OFTHE FAN COWL DOORSHINGES AND SURROUNDING STRUCTURE7500 FC 7500 FC PW711302-01-1 437AL 438AR 447AL448ARDETAILED INSPECTION OFTHE FAN COWL DOORSLATCHES AND SURROUNDING STRUCTURE7500 FC 7500 FC PW712102-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTAND SECONDARY LOAD PATH CLEARANCE7500 FCOR9300 FH7500 FCOR9300 FHPW712102-02-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (TC) OF FORWARDENGINE MOUNT BOLTS7500 FCOR9300 FH7500 FCOR9300 FHPWA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 124EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE712111-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTINSTALLATION7500 FCOR15000 FH7500 FCOR15000 FHGROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321-100CFM712111-01-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTINSTALLATION3500 FCOR7000 FH3500 FCOR7000 FHA321-200CFM712111-01-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTINSTALLATION2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CCFM712111-01-4 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTINSTALLATION6900 FCOR20700 FH6900 FCOR20700 FHGROUP 18-1ECFM712111-03-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTINSTALLATION7500 FCOR15000 FH7500 FCOR15000 FHGROUP 19-1AIAEORGROUP 19-1BIAEORA320IAEORA321-100IAE712111-03-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTINSTALLATION4500 FCOR9000 FH4500 FCOR9000 FHA321-200IAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 125EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE712111-03-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFFORWARD ENGINE MOUNTINSTALLATION2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CIAE712111-05-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (TC) OF FORWARDENGINE MOUNT PYLON BOLTS2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CCFM712111-05-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (TC) OF FORWARDENGINE MOUNT PYLON BOLTS6900 FCOR20700 FH6900 FCOR20700 FHGROUP 18-1ECFM712111-05-4 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (TC) OF FORWARDENGINE MOUNT PYLON BOLTS7500 FCOR15000 FH7500 FCOR15000 FHGROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM712111-06-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (TC) OF FWD ENGINEMOUNT PYLON BOLTS.7500 FCOR15000 FH7500 FCOR15000 FHGROUP 19-1AIAEORGROUP 19-1BIAEORA320IAEORA321IAE712111-06-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (TC) OF FWD ENGINEMOUNT PYLON BOLTS.2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CIAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 126EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE712112-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFFORWARD ENGINE MOUNT LINK LUGS7500 FCOR15000 FH7500 FCOR15000 FHGROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM712112-01-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFFORWARD ENGINE MOUNT LINK LUGS2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CCFM712112-01-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFFORWARD ENGINE MOUNT LINK LUGS6900 FCOR20700 FH6900 FCOR20700 FHGROUP 18-1ECFM712112-02-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFFORWARD ENGINE MOUNT LINK LUGS7500 FCOR15000 FH7500 FCOR15000 FHGROUP 19-1AIAEORGROUP 19-1BIAEORA320IAEORA321IAE712112-02-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION (ENDOSCOPE) OFFORWARD ENGINE MOUNT LINK LUGS2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CIAE712202-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFAFT ENGINE MOUNT ANDSECONDARY LOAD PATH CLEARANCE7500 FCOR9300 FH7500 FCOR9300 FHPWA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 127EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE712202-02-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(TC) OF AFT ENGINEMOUNT BOLTS7500 FCOR9300 FH7500 FCOR9300 FHPW712211-03-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFAFT ENGINE MOUNTINSTALLATION7500 FCOR15000 FH7500 FCOR15000 FHGROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM712211-03-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFAFT ENGINE MOUNTINSTALLATION2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CCFM712211-03-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFAFT ENGINE MOUNTINSTALLATION6900 FCOR20700 FH6900 FCOR20700 FHGROUP 18-1ECFM712211-04-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFAFT ENGINE MOUNTINSTALLATION7500 FCOR15000 FH7500 FCOR15000 FHGROUP 19-1AIAEORGROUP 19-1BIAEORA320IAEORA321IAE712211-04-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFAFT ENGINE MOUNTINSTALLATION2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CIAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 128EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE712211-05-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(TC) OF AFT ENGINEMOUNT PYLON BOLTS7500 FCOR15000 FH7500 FCOR15000 FHGROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM712211-05-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(TC) OF AFT ENGINEMOUNT PYLON BOLTS2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CCFM712211-05-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(TC) OF AFT ENGINEMOUNT PYLON BOLTS6900 FCOR20700 FH6900 FCOR20700 FHGROUP 18-1ECFM712211-06-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(TC) OF AFT ENGINEMOUNT PYLON BOLTS7500 FCOR15000 FH7500 FCOR15000 FHGROUP 19-1AIAEORGROUP 19-1BIAEORA320IAEORA321IAE712211-06-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(TC) OF AFT ENGINEMOUNT PYLON BOLTS2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CIAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 129EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE712212-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(ENDOSCOPE) OF AFTENGINE MOUNT LINK LUGS7500 FCOR15000 FH7500 FCOR15000 FHGROUP 18-1ACFMORGROUP 19-1ACFMGROUP 19-1BCFMA320CFMORA321CFM712212-01-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(ENDOSCOPE) OF AFTENGINE MOUNT LINK LUGS2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CCFM712212-01-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(ENDOSCOPE) OF AFTENGINE MOUNT LINK LUGS6900 FCOR20700 FH6900 FCOR20700 FHGROUP 18-1ECFM712212-02-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(ENDOSCOPE) OF AFTENGINE MOUNT LINK LUGS7500 FCOR15000 FH7500 FCOR15000 FHGROUP 19-1AIAEORGROUP 19-1BIAEA320IAEORA321IAE712212-02-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARSPECIAL DETAILED INSPECTION(ENDOSCOPE) OF AFTENGINE MOUNT LINK LUGS2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CIAEA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 130EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE712213-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OF AFTENGINE MOUNT PINS 7500 FCOR15000 FH7500 FCOR15000 FHGROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM712213-01-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OF AFTENGINE MOUNT PINS 2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CCFM712213-01-3 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OF AFTENGINE MOUNT PINS 6900 FCOR20700 FH6900 FCOR20700 FHGROUP 18-1ECFM712213-02-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OF AFTENGINE MOUNT PINS 7500 FCOR15000 FH7500 FCOR15000 FHGROUP 19-1AIAEORGROUP 19-1BIAEORA320IAEORA321IAE712213-02-2 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OF AFTENGINE MOUNT PINS 2800 FCOR12000 FH2800 FCOR12000 FHGROUP 19-1CIAE725403-01-1 DELETED FROM ALI DOCUMENT AT ISSUE 11725403-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 11781102-02-1 451AL 452AR 461AL462ARDETAILED INSPECTION OFTHE COMMON NOZZLEASSEMBLY V-GROOVE (J-RING)7500 FC 7500 FC PWA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 131EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE783001-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARTHRUST REVERSERSREMOVEDHEAT SHIELDSREMOVEDDETAILED INSPECTIONOF THRUST REVERSER 12O'CLOCK BEAM JUNCTION WITH THE FORWARD FRAME24000 FC 12000 FC GROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM783002-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARCUT CORNERSREMOVEDDETAILED INSPECTIONOF THRUST REVERSERFORWARD FRAME TO 6O'CLOCK BEAM JOINT24000 FC 12000 FC GROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFMA318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 132EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE783003-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARBRACKETS REMOVEDPIPES REMOVEDHEAT SHIELDSREMOVEDDETAILED INSPECTIONOF THRUST REVERSERFORWARD FRAME TO 3/9 O'CLOCK BEAM JOINT24000 FC 12000 FC GROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM783004-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARACTUATORSREMOVEDSPECIAL DETAILED INSPECTION(HFEC) OF THRUSTREVERSER FORWARD FRAME AT ACTUATORATTACHMENT24000 FC 12000 FC GROUP 18-1ACFMORGROUP 19-1ACFMORGROUP 19-1BCFMORA320CFMORA321CFM783200-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARUPPER HINGEACCESS FAIRINGOPENEDGENERAL VISUAL INSPECTION OF "C" DUCT HINGEFITTINGS7500 FC 7500 FC CFM783200-01-3 DELETED FROM ALI DOCUMENT AT ISSUE 10783200-01-5 DELETED FROM ALI DOCUMENT AT ISSUE 10A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2 PAGE: 133EASA APPROVED©AIRBUS SAS 2013. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYNOTE783200-03-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARGENERAL VISUAL INSPECTION OF "C" DUCT HINGEFITTINGSNOTE: CREDIT CAN BE TAKEN FROM PREVIOUSACCOMPLISHMENT OF TASK 783200-01-3.3000 FC 3000 FC IAE783200-03-2 DELETED FROM ALI DOCUMENT AT ISSUE 10783201-01-1 437AL 438AR 447AL448AR 451BL 451CL451DL 451EL 452BR452CR 452DR 452ER461BL 461CL 461DL461EL 462BR 462CR462DR 462ERDETAILED INSPECTION OFTHE THRUST REVERSERHINGE FITTINGS AND ADJACENT STRUCTURE7500 FC 7500 FC PW783202-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFTHE THRUST REVERSERLATCH ASSEMBLY ON TWO HALVES AND SURROUNDINGSTRUCTURE OF LATCHES (15 CM AROUND)7500 FC 7500 FC PW783206-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFTHE THRUST REVERSER FWDV-BLADE (J-RING)7500 FC 7500 FC PW783207-01-1 437AL 438AR 447AL448AR 451AL 452AR461AL 462ARDETAILED INSPECTION OFTHE THRUST REVERSER AFTV-BLADE7500 FC 7500 FC PW783208-01-1 451LL 451ML 452LR452MR 461LL 461ML462LR 462MRPIVOTING DOORSOPENEDDETAILED INSPECTION OFTHE ACTUATOR FITTINGSAND SURROUNDING STRUCTURE19200 FC 19200 FC PWA318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTIONREV: 02 ALS PART 2PAGE: 1EASA APPROVED©AIRBUS SAS 2013. Allrights reserved.SECTION 3 CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS3.1 EXPLANATION OF CDCCL REQUIREMENTSCDCCLs include reference to any information necessary to maintain those design features that have been defined in the Type Design asneeded to preclude development of an unsafe condition. This information is essential to ensure that installation, modification,maintenance,repairs, or alterations do not unintentionally violate the integrity of the type design.Operators are responsible for ensuring that their internal documentation is amended to reflect the data contained within this section and provideappropriate text to highlight the existence of each CDCCL. Suchidentification is necessary in the instructions used by the person performing aninstallation, alteration, repair or modification so as to minimize the risk that the work performed compromises the original design criteria.Regulatory oversight of the operator’s compliance with thismandatory requirement is based on the appropriate identification ofthe CDCCL inthe accomplishment instructions associated with the installation, alteration, repair or modification.3.2 CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONSRef. CDCCL RequirementReferences Applicability1 ElevatorweightTo ensure that the elevatorweight remains within the published limits following anymaintenance action that might affect its weight such as, but not limited to, repair or painting.AMM27-34-41, PB 40151-75-00, PB 00155-20-00, PB 70111-25-55, PB 201CMM55-21-15, PB 5000SRM55-20-00, PB 101All elevators

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 1- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. 

# The following table summarizes the changes in the A318/A319/A320/A321 ALS Part 2.

REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 528107-01-1 Applicability changed from "POST 24428" to "POST 24428 OR POST 24903"

Description note changed to add "PRE 24903"

R 531103-01-1 Access added "STOP FITTING " and "GALLEYS AND TOILETS REMOVED (IF

INSTALLED)"

Applicability changed from "A320-200" to "A320-200 PRE 160000"

R 531105-01-1 Applicability changed from "A320-200" to "A320-200 PRE 160000"

R 531105-02-1 Applicability changed from "A320-200" to "A320-200 PRE 160000"

R 531108-01-1 Applicability changed from "A320-200" to "A320-200 PRE 160000"

R 531110-01-1 Access added "Air conditioning ducts removed"

R 531110-01-2 Access added "Air conditioning ducts removed"

R 531119-01-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 OR A320-200 PR E 30748 OR A321-100 OR A321-200 PRE

30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 30748 OR A320-100

OR A320-200 PRE 30748 OR A321 PRE 30748"

R 531119-01-2 Applicability changed from "GROUP 18-1A OR GROUP 19-1A POST 30748 OR

GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321-200 POST 30748"

to "GROUP 18-1A OR GROUP 19-1A POST 30748 OR GROUP 19-1B POST 30748

OR A320-200 POST 30748 OR A321 POST 30748"

R 531124-01-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 PRE 20062 OR A320-200 PRE 20062 PRE 30748 OR A321-100

OR A321-200 PRE 30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 PRE 20062 OR A320-200 PRE 20062PRE 30748 OR A321 PRE

30748"

R 531124-01-2 Applicability changed from "GROUP 18-1A OR GROUP 19-1A POST 30748 OR

GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321-200 POST 30748"

to "GROUP 18-1A OR GROUP 19-1A POST 30748 OR GROUP 19-1B POST 30748

OR A320-200 POST 30748 OR A321 POST 30748"

R 531129-02-1 Access "LH/RH WINDSHIELD S REMOVED, DISPLAY UNIT 4WT1 REMOVED,

ANCHOR NUT SHIMS REMOVED"added to be in line with SB 53-1245

R 531129-02-2 Access "LH/RH WINDSHIELD S REMOVED, DISPLAY UNIT 4WT1 REMOVED,

ANCHOR NUT SHIMS REMOVED"added to be in line with SB 53-1245

NOTE: FOR AIRCRAFT ALREADY INSPECTED ACCORDING TO SB A320-53-1245,

FIRST INSPECTION DUE ACCORDING TO THE ALI IS THE INTERVAL FROM

DATE OF SB ACCOMPLISHMENT

R 531129-02-3 Access "LH/RH WINDSHIELD S REMOVED, DISPLAY UNIT 4WT1 REMOVED,

ANCHOR NUT SHIMS REMOVED"added to be in line with SB 53-1245

NOTE: FOR AIRCRAFT ALREADY INSPECTED ACCORDING TO SB A320-53-1245,

FIRST INSPECTION DUE ACCORDING TO THE ALI IS THE INTERVAL FROM

DATE OF SB ACCOMPLISHMENT

R 531135-01-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 OR A320-200 PR E 30748 OR A321-100 OR A321-200 PRE

30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 30748 OR A320-100

OR A320-200 PRE 30748 OR A321 PRE 30748"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 2- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 531135-01-2 Applicability changed from "GROUP 18-1A OR GROUP 19-1A POST 30748 OR

GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321-200 POST 30748"

to "GROUP 18-1A OR GROUP 19-1A POST 30748 OR GROUP 19-1B POST 30748

OR A320-200 POST 30748 OR A321 POST 30748"

R 531157-01-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 OR A320-200 PR E 30748 OR A321-100 OR A321-200 PRE

30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 30748 OR A320-100

OR A320-200 PRE 30748 OR A321 PRE 30748"

R 531157-01-2 Applicability changed from "GROUP 18-1A OR GROUP 19-1A POST 30748 OR

GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321-200 POST 30748"

to "GROUP 18-1A OR GROUP 19-1A POST 30748 OR GROUP 19-1B POST 30748

OR A320-200 POST 30748 OR A321 POST 30748"

R 531170-01-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 OR A320-200 PR E 30748 OR A321-100 OR A321-200 PRE

30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 30748 OR A320-100

OR A320-200 PRE 30748 OR A321 PRE 30748"

R 531170-01-2 Applicability changed from "GROUP 18-1A OR GROUP 19-1A POST 30748 OR

GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321-200 POST 30748"

to "GROUP 18-1A OR GROUP 19-1A POST 30748 OR GROUP 19-1B POST 30748

OR A320-200 POST 30748 OR A321 POST 30748"

R 531170-02-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 OR A320-200 PR E 30748 OR A321-100 OR A321-200 PRE

30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 30748 OR A320-100

OR A320-200 PRE 30748 OR A321 PRE 30748"

R 531170-02-2 Applicability changed from "GROUP 18-1A OR GROUP 19-1A POST 30748 OR

GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321-200 POST 30748"

to "GROUP 18-1A OR GROUP 19-1A POST 30748 OR GROUP 19-1B POST 30748

OR A320-200 POST 30748 OR A321 POST 30748"

R 532155-01-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 OR A320-200 PR E 30748 OR A321-100 OR A321-200 PRE

30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 30748 OR A320-100

OR A320-200 PRE 30748 OR A321 PRE 30748"

R 532155-01-2 Applicability changed from "GROUP 18-1A OR GROUP 19-1A POST 30748 OR

GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321-200 POST 30748"

to "GROUP 18-1A OR GROUP 19-1A POST 30748 OR GROUP 19-1B POST 30748

OR A320-200 POST 30748 OR A321 POST 30748"

R 532170-01-1 Applicability changed from "GRO UP 19-1A PRE 30748 OR GROUP 19-1B PRE

30748 OR A320-100 OR A320-200 PR E 30748 OR A321-100 OR A321-200 PRE

30748" to "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 30748 OR A320-100

OR A320-200 PRE 30748 OR A321 PRE 30748"

R 532170-01-2 Applicability changed from "GROUP 19-1A POST 30748 OR GROUP 19-1B POST

30748 OR A320-200 POST 30748 OR A321-200 POST 30748" to "GROUP 19-1A

POST 30748 OR GROUP 19-1B POST 30748 OR A320-200 POST 30748 OR A321

POST 30748"

R 532186-01-1 Applicability changed from "A320-200" to "A320-200 PRE 160000"

R 532190-01-1 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 OR A321" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 PRE 160000 OR A321"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 3- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 533111-01-1 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR A320 PRE

160001"

R 533122-01-2 Threshold changed from 30000 FC to 33000 FC

Applicability changed from "A320-200 POST 34650 OR A321" to "A320-200 POST

34650 OR A320-200 POST 152970 OR A321"

R 533128-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 533128-01-6 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

N 533128-01-7 New Task for A320-200 POST 160001

R 533130-01-4 Applicability changed from "A320-200 POST 34650 OR GROUP 21-1B OR GROUP

21-2B" to "A320-200 POST 34650 OR A320-200 POST 152970 OR GROUP 21-1B

OR GROUP 21-2B"

R 533131-01-5 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-100 OR A320-200 POST 34650 OR A321" to "GROUP 18-1A OR GROUP 19-

1A OR GROUP 19-1B OR A320-100 OR A320-200 POST 34650 OR A320-200 POST

152970 OR A321"

D 533132-01-1 Task deleted for A320-200

R 533138-01-1 Applicability changed from "A320-200" to " A320-200 PRE 39516"

R 533138-02-1 Applicability changed from "A320-200" to " A320-200 PRE 39516"

R 533139-01-1 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 533139-01-3 Applicability changed from "GROUP 19-1A POST 32208 OR GROUP 19-1B POST

32208 OR A320-100 OR A320-200 POST 34650" to "GROUP 19-1A POST 32208 OR

GROUP 19-1B POST 32208 OR A320-100 OR A320-200 POST 34650 OR A320-200

POST 152970"

R 533140-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 533143-01-1 Applicability changed from "GROUP 19 -1A OR GROUP 19-1B OR A320 OR A321" to

"GROUP 19-1A OR GROUP 19-1B OR A320 PRE 31067 OR A321"

R 533144-01-1 Applicability changed from "GROUP 19-1A POST 20941 OR GROUP 19-1B POST

20941 OR A320 POST 20941 OR A321 POST 20941" to "GROUP 19-1A OR GROUP

19-1B OR A321".

R 533152-01-10 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 533155-03-1 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-100 OR A320-200 POST 34650 OR A321" to "GROUP 18-1A OR GROUP 19-

1A OR GROUP 19-1B OR A320-100 OR A320-200 POST 34650 OR A320-200 POST

152970 OR A321"

R 533180-01-1 Interval changed from "10800 FC or 21600 FH" to "6100 FC or 12200 FH"

Applicability changed from "A320-200" to "A320-200 PRE 160001"

R 533185-01-1 Applicability changed from "A 320-200 PRE 21003 PRE 34650" to A320-200 PRE

21003 PRE 34650 PRE 152970 PRE 160001"

R 533185-01-2 Applicability changed from "A320-200 POST 21003 PRE 34650" to "A320-200 POST

21003 PRE 34650 PRE 152970PRE 160001"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 4- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 533189-01-3 Applicability changed from "A320 POST 150069" to "A320 POST 150069 PRE

160001"

Interval changed from "32700 FC OR 65400 FH" to "32600 FC OR 65200 FH"

R 534106-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970 PRE 160001"

Interval changed from "12800 FC or 25700 FH" to "12900 FC or 25800 FH"

R 534111-01-2 Description note added

R 534111-01-3 Description note added

R 534111-01-4 Description note added

R 534111-01-7 Applicability changed from "A320-100 POST 20053 OR A320-200 POST 34650" to

"A320-100 POST 20053 OR A320-200 POST 34650 OR A320-200 POST 152970"

R 534112-01-7 Applicability changed from "A320-100 OR A320-200 POST 34650 OR A321" to "A320-

100 POST 20053 OR A320-200 POST 34650 OR A320-200 POST 152970 OR A321"

R 534123-01-1 Description changed from "EXC LUDING THE LOCATION AT FRAME 68 AND

STRINGER 18, STRINGER 20 AND STRINGER 22" to "FROM STRINGER 10 TO

STRINGER 16"

R 534125-01-2 Applicability changed from "GROUP 19-1A OR GROUP 19-1B" to "GROUP 19-1A

PRE 160055 OR GROUP 19-1B PRE 160055"

Threshold changed from "33800 FC" to "32100 FC"

Interval changed from "3100 FC or 6200 FH" to "3000 FC or 6000 FH"

R 534125-01-3 Applicability changed from "A320- 200" to "A320-200 PRE 153074 PRE 160055 PRE

160500"

R 534125-01-4 Applicability changed from "A321" to "A321 PRE 160055"

Interval changed from "3600 FC or 7200 FH" to "3500 FC or 7000 FH"

R 534126-01-2 Applicability changed from "GROUP 19-1A OR GROUP 19-1B" to "GROUP 19-1A

PRE 153073 PRE 160055 OR GROUP 19-1B PRE 153073 PRE 160055"

Threshold changed from "30200 FC or 60000 FH" to "28700 FC or 57400 FH"

R 534126-01-3 Applicability changed from "A320- 200" to "A320-200 PRE 153073 PRE 160055 PRE

160500"

R 534126-01-4 Applicability changed from "A321" to "A321 PRE 160055"

Interval changed from "2500 FC or 5000 FH" to "2400 FC or 4800 FH"

R 534127-01-1 Access changed from "N/A" to 832 842 LINING REMOVE INSULATION REMOVED"

R 534127-01-2 Access changed from "N/A" to 832 842 LINING REMOVE INSULATION REMOVED"

R 534127-01-3 Access changed from "N/A" to 832 842 LINING REMOVE INSULATION REMOVED"

Appliability changed from "A320-200 POST 21781" to "A320-200 MSN 0124-9999"

R 534127-01-4 Access changed from "N/A" to 832 842 LINING REMOVE INSULATION REMOVED"

R 534129-01-3 Applicability changed from "A320-200" to "A320-200 PRE 160500"

N 534129-01-5 New task for A320-200 POST 160500

R 534132-01-4 Applicability changed from "A320-200" to "A320-200 PRE 160500"

N 534132-01-10 New task for A320-200 POST 160500

R 534140-01-2 Threshold changed from "19000 FC or 38000 FH" to "31700 or 60000 FH"

R 534140-01-5 Threshold changed from "23700 FC or 47400 FH" to "39600 FC or 60000 FH"

R 534140-01-6 Threshold changed from "23000 FC or 46000 FH" to "38400 FC or 60000 FH"

R 534140-01-7 Threshold changed from "23700 FC or 47400 FH" to "39500 FC or 60000 FH"

R 534140-01-8 Threshold changed from "21300 FC or 42600 FH" to "35600 FC or 71200 FH"

Description Note typo in task reference "534140-01-4" amended

R 534140-01-9 Threshold changed from "22600 FC or 45200 FH" to "37700 FC or 60000 FH"

R 534141-01-5 Applicability changed from "A320-200" to "A320-200 PRE 160500"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 5- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

N 534141-01-11 New task for A320-200 POST 160500

R 534159-01-1 Applicability changed from "A320-200" to "A320-200 PRE 160001"

N 534159-01-4 New Task for A320-200 POST 160001

R 534160-02-1 Applicability changed from "A320 or A321" to "A320 PRE 160001 or A321"

Credit note removed from Task Description

R 534160-02-2 Credit note removed from Task Description

N 534160-02-3 New Task for A320 POST 160001

R 534171-01-2 Applicability changed from "A320-200 POST 20029 PRE 21065 PRE 25354 OR A321

PRE 22992" to "A320-200 POST 20449 OR A320-200 POST 20029 PRE 21065 PRE

25354 PRE 160001 OR A321 PRE 22992"

N 534171-01-4 New task for A320-200 POST 20029 PRE 21065 PRE 25354 POST 160001

R 534172-01-2 Applicability changed from "A320-200 POST 20029 PRE 21065 PRE 25354 OR A321

PRE 22992" to "A320-200 POST 20449 OR A320-200 POST 20029 PRE 21065 PRE

25354 PRE 160001 OR A321 PRE 22992"

Threshold/Interval changed from "15500 FC or 31100 FH" to "15300 FC or 30600 FH".

R 545102-01-8 Applicability changed from "A321-100 CFM OR A321-200 PRE 34650 CFM" to "A321-

100 CFM OR A321-200 PRE 34650 PRE 152970 CFM"

R 545102-01-9 Applicability changed from "A321-200 POST 34650 CFM" to "A321-200 POST 34650

CFM OR A321-200 POST 152970 CFM"

R 545103-01-2 Applicability changed from "GRO UP 19-1A PRE 34650 OR GROUP 19-1B PRE

34650 OR A320-200 OR A321" to "GROUP 19-1A PRE 34650 PRE 152970 OR

GROUP 19-1B PRE 34650 PRE 152970 OR A320-200 OR A321"

R 545103-01-3 Applicability changed from "GROUP 19-1A POST 34650 OR GROUP 19-1B POST

34650" to "GROUP 19-1A POST 34650 OR GROUP 19-1A POST 152970 OR

GROUP 19-1B POST 34650 OR GROUP 19-1B POST 152970"

N 545107-01-1 New task for A320-200

D 545107-01-4 Task deleted for A320-200

N 545114-01-2 New task for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

N 545114-01-5 New task for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

D 545114-01-8 Task deleted for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

D 545114-01-9 Task deleted for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

N 545115-01-2 New task for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

N 545115-01-5 New task for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

D 545115-01-8 Task deleted for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

D 545115-01-9 Task deleted for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

N 545115-02-2 New task for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

N 545115-02-5 New task for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

D 545115-02-8 Task deleted for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

D 545115-02-9 Task deleted for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

N 545120-01-2 New task for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

N 545120-01-5 New task for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

D 545120-01-7 Task deleted for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

D 545120-01-8 Task deleted for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

N 545123-01-2 New task for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

N 545123-01-6 New task for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

D 545123-01-9 Task deleted for A320-200 PRE 33844 CFM OR A320-200 PRE 33847 IAE

D 545123-01-10 Task deleted for A320-200 POST 33844 CFM OR A320-200 POST 33847 IAE

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 6- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 545130-01-1 Applicability changed from "GROUP 18-1A OR GROUP 19-1A PRE 34650 CFM OR

GROUP 19-1B PRE 34650 CFM OR A320-200 OR A321 CFM" to "GROUP 18-1A OR

GROUP 19-1A PRE 34650 PRE 152970 CFM OR GROUP 19-1B PRE 34650 PRE

152970 CFM OR A320-200 OR A321 CFM"

R 545130-01-5 Applicability changed from "GRO UP 19-1A POST 34650 CFM OR GROUP 19-1B

POST 34650 CFM" to "GROUP 19-1A POST 34650 CFM OR GROUP 19-1A POST

152970 CFM OR GROUP 19-1B POST 34650 CFM OR GROUP 19-1B POST 152970

CFM"

R 571101-02-1 Threshold changed from "43600 FC or 87200 FH" to "37200 FC or 74400 FH"

Interval changed from "14200 FC or 28400 FH" to "20300 FC or 40600 FH"

Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR A320 PRE

160000"

R 571134-01-6 Applicability changed from "GROUP 19-1A POST 34650 OR GROUP 19-1B POST

34650" to "GROUP 19-1A POST 34650 OR GROUP 19-1A POST 152970 OR

GROUP 19-1B POST 34650 OR GROUP 19-1B POST 152970"

R 571135-01-6 Applicability changed from "GROUP 19-1A POST 34650 OR GROUP 19-1B POST

34650" to "GROUP 19-1A POST 34650 OR GROUP 19-1A POST 152970 OR

GROUP 19-1B POST 34650 OR GROUP 19-1B POST 152970"

R 571136-01-1 Applicability changed from "A320-200" to "A320-200 PRE 160000"

Access "BOLTS REMOVED" deleted

R 571136-01-2 Access "BOLTS REMOVED" deleted

Applicability changed from "GROUP 18-1A OR GROUP 19-1A PRE 34650 OR

GROUP 19-1B PRE 34650" to "GROUP 18-1A OR GROUP 19-1A PRE 34650 PRE

152970 OR GROUP 19-1B PRE 34650 PRE 152970"

R 571136-01-3 Access "BOLTS REMOVED" deleted

Applicability changed from "GROUP 19-1A POST 34650 OR GROUP 19-1B POST

34650" to "GROUP 19-1A POST 34650 OR GROUP 19-1A POST 152970 OR

GROUP 19-1B POST 34650 OR GROUP 19-1B POST 152970"

R 571136-01-4 Access "BOLTS REMOVED" deleted

R 571136-01-5 Access "BOLTS REMOVED" deleted

R 571170-01-1 Interval changed from "20000 FC or 45900 FH" to "9100 FC or 18200 FH"

Applicability changed from "GROUP 18-1A OR GROUP 19-1A PRE 34650 OR

GROUP 19-1B PRE 34650" to "GROUP 18-1A OR GROUP 19-1A PRE 34650 PRE

152970 OR GROUP 19-1B PRE 34650 PRE 152970"

R 571170-01-2 Interval changed from "18700 FC or 37500 FH" to "9100 FC or 18200 FH"

Applicability changed from "A320-200" to "A320-200 PRE 160000"

R 571170-01-3 Interval changed from "19600 FC or 46100 FH" to "9100 FC or 18200 FH"

Applicability changed from "A321-100 OR GROUP 21-2A PRE 34650 OR GROUP 21-

2B" to "A321-100 OR GROUP 21-2A PRE 34650 PRE 152970 OR GROUP 21-2B"

R 571170-01-4 Interval changed from "13400 FC or 36800 FH" to "9100 FC or 18200 FH"

Applicability changed from "GROUP 19-1A POST 34650 OR GROUP 19-1B POST

34650" to "GROUP 19-1A POST 34650 OR GROUP 19-1A POST 152970 OR

GROUP 19-1B POST 34650 OR GROUP 19-1B POST 152970"

R 571170-01-6 Interval changed from "18500 FC or 43500 FH" to "9100 FC or 18200 FH"

Applicability changed from "GROUP 21-2A POST 34650" to "GROUP 21-2A POST

34650 OR GROUP 21-2A POST 152970"

R 571170-01-7 Interval changed from "15600 FC or 40000 FH" to "9100 FC or 9100 FH"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 7- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

N 571170-01-8 New task for A320-200 POST 160000

R 571181-01-6 Applicability changed from "GROUP 19-1A POST 34650 PRE 38481 OR GROUP 19-

1B POST 34650 PRE 38481 OR A320-100" to "GROUP 19-1A POST 34650 PRE

38481 OR GROUP 19-1A PRE 38481 POST 152970 OR GROUP 19-1B POST 34650

PRE 38481 OR GROUP 19-B PRE 38481 POST 152970 OR A320-100"

R 571182-01-6 Applicability changed from "GROUP 19-1A POST 34650 PRE 38481 OR GROUP 19-

1B POST 34650 PRE 38481 OR A320-100" to "GROUP 19-1A POST 34650 PRE

38481 OR GROUP 19-1A PRE 38481 POST 152970 OR GROUP 19-1B POST 34650

PRE 38481 OR GROUP 19-B PRE 38481 POST 152970 OR A320-100"

R 571183-01-5 Applicability changed from "GROUP 19-1A POST 34650 PRE 38481 OR GROUP 19-

1B POST 34650 PRE 38481 OR A320-100" to "GROUP 19-1A POST 34650 PRE

38481 OR GROUP 19-1A PRE 38481 POST 152970 OR GROUP 19-1B POST 34650

PRE 38481 OR GROUP 19-B PRE 38481 POST 152970 OR A320-100"

R 571185-01-1 Applicability changed from "GRO UP 18-1A OR GROUP 19-1A PRE 34650 OR

GROUP 19-1B PRE 34650 OR A320-100" to "GROUP 18-1A OR GROUP 19-1A PRE

34650 PRE 152970 OR GROUP 19-1B PRE 34650 PRE 152970 OR A320-100"

R 571185-01-3 Applicability changed from "GROUP 21-2A PRE 34650" to "GROUP 21-2A PRE

34650 PRE 152970"

R 571185-01-5 Applicability changed from "GROUP 19-1A POST 34650 OR GROUP 19-1B POST

34650" to "GROUP 19-1A POST 34650 OR GROUP 19-1A POST 152970 OR

GROUP 19-1B POST 34650 OR GROUP 19-1B POST 152970"

R 571185-01-7 Applicability changed from "GROUP 21-2A POST 34650" to "GROUP 21-2A POST

34650 OR GROUP 21-2A POST 152970"

R 571189-01-3 Applicability changed from "GRO UP 18-1A OR GROUP 19-1A PRE 34650 OR

GROUP 19-1B PRE 34650" to "GROUP 18-1A OR GROUP 19-1A PRE 34650 PRE

152970 OR GROUP 19-1B PRE 34650 PRE 152970"

R 571189-01-7 Applicability changed from "GROUP 19-1A POST 34650 OR GROUP 19-1B POST

34650" to "GROUP 19-1A POST 34650 OR GROUP 19-1A POST 152970 OR

GROUP 19-1B POST 34650 OR GROUP 19-1B POST 152970"

R 572004-01-1 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572004-01-4 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-100 OR A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR

GROUP 19-1B OR A320-100 OR A320-200 POST 34650 OR A320-200 POST

152970"

N 572004-01-5 New task for A320-200 POST 160058 OR A320-200 POST 160075 OR A320-200

POST 16076

N 572004-01-6 New task for A320-200 PRE 160058 POST 160001 PRE 160075 PRE 160076

R 572007-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970 PRE 160001"

Threshold and interval changed from "16000 FC or 32000 FH" to "11900 FC or 23800

FH"

R 572007-01-4 Applicability changed from "GROUP 21-2A" to "GROUP 21-1B OR GROUP 21-2A"

R 572007-01-5 Applicability changed from "GROUP 21-1B OR GROUP 21-2B" to "GROUP 21-2B"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 8- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 572007-01-8 Credit note removed from Task Description

CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572007-

01-2 AND 572007-01-3

Applicability changed from "GROUP 19-1A OR GROUP 19-1B OR A320-200 POST

34650" to "GROUP 19-1A OR GROUP 19-1B OR A320-200 POST 34650 OR A320-

200 POST 152970"

N 572007-01-9 New task for A320-200 POST 160001

N 572008-01-4 New task for A320-200 POST 160001

N 572009-01-1 New task for A320-200 PRE 34650 PRE 152970 PRE 160001

N 572009-01-2 New task for A320-200 POST 160001

R 572010-01-4 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572010-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

N 572010-01-10 New task for A320-200 POST 160001

R 572011-01-1 Description changed to in clude "AND TOP AND BOTTOM FLANGES"

R 572011-01-2 Description changed to in clude "AND TOP AND BOTTOM FLANGES"

Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572011-01-3 Description changed to in clude "AND TOP AND BOTTOM FLANGES"

R 572011-01-4 Description changed to in clude "AND TOP AND BOTTOM FLANGES"

R 572011-01-5 Description changed to in clude "AND TOP AND BOTTOM FLANGES"

R 572011-01-6 Description changed to in clude "AND TOP AND BOTTOM FLANGES"

Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572011-01-7 Description changed to in clude "AND TOP AND BOTTOM FLANGES"

N 572011-01-8 New task for A320-200 POST 160058 OR A320-200 POST 160075 OR A320-200

POST 16076

N 572011-01-9 New task for A320-200 PRE 160058 POST 160001 PRE 160075 PRE 160076

R 572012-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572014-01-3 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572020-01-1 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572020-01-9 Applicability changed from "A320-100 OR A320-200 POST 34650" to "A320-100

POST 20053 OR A320-200 POST 34650 OR A320-200 POST 152970"

N 572020-01-10 New task for A320-200 POST 160001

R 572026-01-6 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650 OR A320-200 POST 152970"

R 572032-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572032-01-5 Applicability changed from "GROUP 18-1A OR A320-200 POST 34650" to "GROUP

18-1A OR A320-200 POST 34650 OR A320-200 POST 152970"

R 572033-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

D 572034-01-5 Task deleted for A320-200 PRE 34650

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 9- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 572034-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572036-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572036-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572038-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572040-03-4 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572041-02-4 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572041-02-5 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572042-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572042-01-7 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650 OR A320-200 POST 152970"

R 572044-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572044-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572050-01-4 Applicability changed from "A 320-200 PRE 34650 PRE 37331 OR A320-200 PRE

34650 POST 37332" to "A320-200 PRE 34650 PRE 37331 PRE 152970 PRE 160001

OR A320-200 PRE 34650 POST 37332 PRE 152970 PRE 160001"

R 572050-01-8 Applicability changed from "A320-200 POST 34650 PRE 37331 OR A320-200 POST

34650 POST 37332" to "A320-200 POST 34650 PRE 37331 OR A320-200 POST

34650 POST 37332 OR A320-200 PRE 37331 POST 152970 OR A320-200 POST

37332 POST 152970"

R 572050-02-4 Applicability changed from "A 320-200 PRE 34650 PRE 37331 OR A320-200 PRE

34650 POST 37332" to "A320-200 PRE 34650 PRE 37331 PRE 152970 PRE 160001

OR A320-200 PRE 34650 POST 37332 PRE 152970 PRE 160001"

R 572050-02-8 Applicability changed from "A320-200 POST 34650 PRE 37331 OR A320-200 POST

34650 POST 37332" to "A320-200 POST 34650 PRE 37331 OR A320-200 POST

34650 POST 37332 OR A320-200 PRE 37331 POST 152970 OR A320-200 POST

37332 POST 152970"

R 572053-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572053-01-5 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650 OR A320-200 POST 152970"

R 572054-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970 PRE 160001"

Description changed " MAGNETIC LEVEL INDICATOR HOLE ADJACENT TO FUEL

PUMP APERTURES BETWEEN RIB 1 A ND RIB 2; WATER DRAIN HOLE

ADJACENT TO FUEL PUMP APERTURES BETWEEN RIB 1 AND RIB 2" removed

N 572054-01-8 New task for A320-200 POST 160001

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 10- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 572101-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970 PRE 160001"

Threshold changed from "39600 FC or 79200 FH" to "43000 FC or 86000 FH"

R 572101-01-7 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-100 OR A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR

GROUP 19-1B OR A320-100 OR A320-200 POST 34650 OR A320-200 POST

152970"

N 572101-01-8 New task for A320-200 POST 160001

R 572108-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572108-01-5 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

N 572108-01-8 New task for A320-200 POST 160058 OR A320-200 POST 160075 OR A320-200

POST 16076

N 572108-01-9 New task for A320-200 PRE 160058 POST 160001 PRE 160075 PRE 160076

N 572109-01-5 New task for A320-200 POST 160001

R 572111-01-6 Applicability changed from "GROUP 19-1B OR A320-100 OR A320-200 POST 34650"

to "GROUP 19-1B OR A320-100 OR A320-200 POST 34650 OR A320-200 POST

152970"

R 572112-01-1 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572112-01-6 Applicability changed from "A320-100 OR A320-200 POST 34650" to "A320-100

POST 20053 OR A320-200 POST 34650 OR A320-200 POST 152970"

R 572114-01-4 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572114-01-6 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

N 572114-01-8 New task for A320-200 POST 160058 OR A320-200 POST 160075 OR A320-200

POST 16076

N 572114-01-9 New task for A320-200 PRE 160058 POST 160001 PRE 160075 PRE 160076

R 572115-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572115-01-6 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

N 572115-01-8 New task for A320-200 PRE 160058 POST 160001 PRE 160075 PRE 160076

N 572115-01-9 New task for A320-200 POST 160058 OR A320-200 POST 160075 OR A320-200

POST 16076

R 572116-02-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572120-01-3 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572123-01-1 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

N 572123-01-4 New task for A320-200 POST 160001

R 572124-01-3 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572124-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 11- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

N 572124-01-8 New task for A320-200 POST 160001

R 572129-01-4 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572129-01-6 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572130-01-6 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572130-01-7 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572134-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572134-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572137-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572137-01-6 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572139-02-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572140-02-4 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572140-02-5 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572142-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572142-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572143-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572143-01-5 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650 OR A320-200 POST 152970"

R 572144-01-5 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572148-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572148-01-9 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572149-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572149-01-5 Interval changed from "53300 FH" to "52300 FH"

R 572149-01-8 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 572150-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572150-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 12- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 572151-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572155-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 572155-01-3 Applicability changed from "GROUP 21-2A PRE 34650" to "GROUP 21-2A PRE

34650 PRE 152970"

R 572155-01-5 Applicability changed from "GROUP 21-2A POST 34650" to "GROUP 21-2A POST

34650 OR A320-200 POST 152970"

R 572155-01-7 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-100 OR A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR

GROUP 19-1B OR A320-100 OR A320-200 POST 34650 OR A320-200 POST

152970"

R 572158-01-2 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 572158-01-6 Applicability changed from "GROUP 21-2A POST 34650" to "GROUP 21-2A POST

34650 OR A320-200 POST 152970"

R 572158-01-8 Applicability changed from "GROUP 21-2A PRE 34650" to "GROUP 21-2A PRE

34650 PRE 152970"

R 572158-01-9 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

N 572158-01-10 New task for A320-200 POST 160001

R 572160-01-5 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650 OR A320-200 POST 152970"

R 572164-02-6 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 573101-01-1 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 573101-01-4 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650 OR A320-200 POST 152970"

N 574106-01-8 New task for A320-200 POST 160001

N 574112-02-3 New task for A320-200 POST 160001

R 574114-01-3 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

N 575151-01-6 New task for A320-200 POST 160001

R 575155-01-4 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

N 575156-01-1 New task for A320-200 POST 160001

R 575158-01-5 Applicability changed from "A320- 200 PRE 34650" to " A320-200 PRE 34650 PRE

152970 PRE 160001"

R 575158-01-6 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 575159-01-5 Applicability changed from "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650" to "GROUP 18-1A OR GROUP 19-1A OR GROUP 19-1B OR

A320-200 POST 34650 OR A320-200 POST 152970"

R 575160-01-5 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

REV: 02 ALS PART 2 PAGE: 13- APXA

SUMMARY OF CHANGES

© AIRBUS SAS 2013. All rights reserved. REV

CODE TASK

REFERENCE SOC A318/A319/A320/A321 ALS PART 2 REVISION 02 COMPARED WITH

REVISION 01

R 575160-01-7 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 575161-01-5 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 575163-01-2 Applicability changed from "A320-200 PRE 34650" to "A320-200 PRE 34650 PRE

152970"

R 575163-01-5 Applicability changed from "A320-200 POST 34650" to "A320-200 POST 34650 OR

A320-200 POST 152970"

R 575165-01-2 Access changed from "531CB 631 CB" to "535BB 635BB"

R 575165-01-4 Access changed from "531CB 631 CB" to "535BB 635BB"

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX B – ABBREVIATIONS

REV: 02 ALS PART 2 PAGE: 1- APXB

ABBREVIATIONS

© AIRBUS SAS 2013. All rights reserved.

ABBREVIATION MEANING

AD Airworthiness Directive

ALI Airworthiness Limitation Item

ALS Airworthiness Limitations Section

AMC Acceptable Means of Compliance

AMM Aircraft Maintenance Manual

APX Appendix

ATA Air Transport Association

CFM CFMI engines

CPCP Corrosion Prevention and Control Program

CG Centre of Gravity

CJ Corporate Jet

D Deleted

DT Damage Tolerant

EASA European Aviation Safety Agency

FAR Federal Aviation Regulations

FC Flight Cycle

FH Flight Hour

FR Frame

FT Feet

HFEC High Frequency Eddy Current (NDT inspection method)

HTP Horizontal Tail Plane

IAE IAE engines

JAR Joint Aviation Requirements

LEP List of Effective Pages

LOV Limit Of Validity

M Meter

MLG Main Landing Gear

MLW Maximum Landing Weight

MOD Modification

MPD Maintenance Planning Document

MRBR Maintenance Review Board Report

MSN Manufacturer Serial Number

MTOW Maximum Take Off Weight

MZFW Maximum Zero Fuel Weight

N New

N/A Not Applicable

NDT Non Destructive Test

NLG Nose Landing Gear

NTM Non Destructive Test Manual

PAX Passenger

PW Pratt & Whitney engines

R Revised

RAS Repair Approval Sheet

ROR Record Of Revisions

SB Service Bulletin

SRM Structural Repair Manual

SSI Structural Significant Item

STC Supplemental Type Certificate

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX B – ABBREVIATIONS

REV: 02 ALS PART 2 PAGE: 2- APXB

ABBREVIATIONS

© AIRBUS SAS 2013. All rights reserved.

ABBREVIATION MEANING

STR Stringer

T Ton

TC Type Certificate

TC Torque Check (NDT Inspection method)

THS Trimmable Horizontal Stabilizer

TPS Temporary Protection System

TOC Table Of Contents

US UltraSonic (NDT inspection method)

VTP Vertical Tail Plane

WFD Widespread Fatigue Damage

WV Weight Variant

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX C – TERMS AND DEFINITIONS

REV: 02 ALS PART 2 PAGE: 1- APXC

TERMS AND DEFINITIONS

© AIRBUS SAS 2013. All rights reserved. TERM DEFINITION

AIRCRAFT

STRUCTURE Consists of all load-carrying members in cluding wings, fuselage, empennage, engine

mountings, landing gear, flight control surfaces, and related points of attachment. The

actuating portions of items such as landing gear, flight controls, doors, etc. are treated as

systems components. Attachment of the actuators to the airfra me is treated as structure.

CALENDAR TIME In Years (YE), in Months (MO), etc... shall be counted from the date of initial entry into

service, unless otherwise stat ed. Storage, maintenance, etc... do not freeze calendar time

accumulation.

CONTINUED

AIRWORTHINESS Is the process of ensuring that the level of ai rworthiness guaranteed by TC is maintained for

each individual aircraft at the time of its ent ry into service and during all its service life.

DAMAGE

TOLERANCE

CONCEPT The damage-tolerance evaluation of structure is intended to ensure that should serious

fatigue, corrosion, or accidental damage occur within the operational life of the aircraft, the

remaining structure can withstand reasonable loads without failure or excessive structural

deformation until the damage is detected. Damage -tolerance design is required, unless it

entails such complications that an effective damage-tolerant structure cannot be achieved

within the limitations of geometry, inspec tability, or good design practice. Under these

circumstances, a design that complies with t he fatigue evaluation (safe life) requirements is

used.

DAMAGETOLERANT

AIRWORTHINESS

LIMITATION

ITEMS They are all those parts of the structure whose failu re could result in catastrophic failure of the

airplane and that are designed to fatigue and damage-tolerance concept.

DESIGN

SERVICE GOAL Is a reference figure selected for the de sign and certification of the aircraft.

EXTENDED

SERVICE GOAL Is an extension of the Design Service Goal.

FLIGHT CYCLE A complete take-off and landing sequence

FLIGHT HOUR The accumulated time intervals between ‘wheels-off’ and ‘wheels-on’.

INTERVAL The maximum period expressed in usage param eters between the completion of a task and

its next due accomplishment.

LIMIT OF

VALIDITY It is the period of time, expressed in appropriate units (e.g. flight cycles) for which it has been

shown that the established insp ections and replacement times w ill be sufficient to allow safe

operation and in particular to preclude development of widespread fatigue damage.

THRESHOLD The maximum period of time expressed in usage parameters between the first flight of the

aircraft, and the first due completion of the ta sk. Subsequent accomplis hment deadlines are

obtained by adding the repeat interval and its multiples to the threshold.

TOUCH AND GO A ‘Touch and go’ is a landing in which an airc raft touches the runway and does not come to a

full stop prior to commencing an additional flight.

WIDESPREAD

FATIGUE

DAMAGE The simultaneous presence of cracks at multiple st ructural locations that are of sufficient size

and density that the structure will no longer meet the residual strength requirements of §

25.571(b).

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX D – MODIFICATION LIST

REV: 02 ALS PART 2 PAGE: 1- APXD

MODIFICATION LIST

© AIRBUS SAS 2013. All rights reserved. REV.

CODE MOD

NUMBER MODIFICATION DESCRIPTION SERVICE BULLETIN(S)

20029 DOORS - BULK CARGO COMPARTMENT - INSTALL

AN ADDITIONAL DOOR AT FR 60/62

20053 NAVIGATION - ADF - INSTALL FULL PROVISION

FOR SECOND SYSTEM (CUTOUT ON FUSELAGE

SKIN) 34-1493 34-1363 34-1514 34-1063

34-1492

20062 DOORS - INSTALL ENTRANCE STAIRS AT FWD PAX

DOOR (RETRO OF MOD 23288 ON A320-100) 52-1006

20139 INTRODUCE BOGIE ON MAIN LANDING GEAR

20154 WINGS - DELETE PROVISIONS FOR IAE V2500 DRY

BAY (A320-100 HALF DRY BAY DELETION ON LH

SIDE)

20167 STRUCTURE - REINFORCE STRUCTURE TO

ALLOW MTOW 72T - MLW 63T -MZFW 59T DESIGN

WEIGHTS

20188 WINGS - CENTER WING - MODIFY UPPER SKIN

PANEL STIFFENERS

20416 FUSELAGE - FLOOR STRUCTURE - INTRODUCE

MINOR IMPROVEMENTS

20449 DOORS - 2ND AFT C/C DOOR - RETROFIT

ADDITIONAL DOOR ON A320-100 52-1040

21003 WATER/WASTE - RELOCATE POTABLE WATER

TANK FROM FR 66 TO FR 36

21065 FUSELAGE - REAR FUSELAGE - REPLACE

ADDITIONAL BULK DOOR BY FRAME SHELL AND

ADAPT SYSTEM (ANTI-MOD 20029)

21284 WINGS-CENTER BOX-REINFORCE STRUCTURAL

BEAMS

21287 WINGS-CENTER FU SELAGE-REINFORCE UPPER

STRINGLERS

21288 WINGS-CENTER FU SELAGE-REINFORCE LOWER

SECTION (FR 37 TO 41) 57-1018

21521 FUSELAGE - REINFORCE THE

WINDSHIELD/LOWER FAIRING ATTACHMENT

21657 FUSELAGE - NOSE FUSE LAGE - INTRODUCE COLD

WORKING OF HOLES WINDSHIELD LOWER

LATERAL JUNCTION

21999 GENERAL - CONSOLIDATION MOD FROM A320

MODS BASIC FOR A321

22058 FUSELAGE - WINDSHIELD - REPLACE FRAME

LOWER MEMBER

22060 NACELLES/PYLONS - DEFINE COMMON CFM

PYLON

22061 NACELLES/PYLONS - DEFINE COMMON IAE

A320/A321/A319 PYLON

22129 MLG - REPLACE FO UR WHEELS (BOGIE MLG) BY

TWO WHEELS (TWIN MLG)

22992 FUSELAGE - REAR FUSELAGE - REMOVE BULK

CARGO DOOR ON A321

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX D – MODIFICATION LIST

REV: 02 ALS PART 2 PAGE: 2- APXD

MODIFICATION LIST

© AIRBUS SAS 2013. All rights reserved. REV.

CODE MOD

NUMBER MODIFICATION DESCRIPTION SERVICE BULLETIN(S)

23002 STABILIZERS - TRIMMABLE HORIZONTAL

STABILIZER - INTRODUCE ALUMINIUM CENTRAL

JOINT

23288 DOORS - ENTRANCE STAIRS – INSTALL

COMPLETE PROVISION FOR AIRSTAIRS

23558 STABILIZERS-ELEVATORS-ADD ADDITIONAL

ADHESIVE TO OUTER SURFACE SKIN

23685 FUSELAGE-MAIN STRUCTURE-WINDSCREENREINFORCE ATTACHMENT OF FRONT/LATERAL

LOWER FRAMEWORK (RETROFIT SOLUTION) 53-1044

24428 DOORS - MAIN G EAR DOORS - INTRODUCE

REINFORCED FWD HINGE FITTINGS. 52-1058

24596 STABILIZERS -THS-INTRODUCE TITANIUM FITTING

(ANTI MOD 23002)

24603 DOORS - FWD AND AFT CARGO COMPARTMENT

DOORS -INTRODUCE SOLID SHIM MATERIAL

24903 DOORS-MAIN GEAR DOOR-MODIFY ACTUATOR

FITTING 52-1073

25354 FUSELAGE-REAR FUSELAGE-REMOVE BULK

CARGO DOOR ON A320 A/C (ANTI-MOD 20029)

25714 FUEL TANKS - INSTALL 1ST ACT IN AFT CARGO

COMPARTMENT (A320-200) 28-1146 28-1081 28-1119 28-1136

28-1206

26228 WINGS-CENTER-WINGS MODIFY REAR SPAR OF

SECTION 21

26372 COMMUNICATIONS - SATCOM - INSTALL SATCOM

SYSTEM IN AFT SECTION OF AIRCRAFT

26925 LANDING GEAR - INTRODUCE MODIFIED

ALTERNATE BRAKING SYSTEM

26995 COMMUNICATIO NS-SATCOM-INSTALL

PROVISIONS FOR A TOP-MOUNTED SATCOM

ANTENNA

28162 EXTEND FLIGHT ENVELOPE UP TO 41000 FT (A319

CJ)

28238 FUEL TANKS - A319 CORPORATE JET - ACT

FLEXIBILITY CONCEPT (0 TO 6) 28-1185 28-1080

28342 A319 CORPORATE JET MODIFY

CHARACTERISTICS GROUND/FLIGHT CG LIMIT (TO

FWD) AND ADAPT GREEN BAND ON PITCH TRIM

WHEEL

28653 INSTALLATION OF 2ND ACT ON A321-200 28-1090 28-1115

30748 GENERAL - FLIGHT ENVIRONMENTAL ENVELOPE -

EXTENSION TO 12100 M (39800 FT) FROM 11850 M

(39000 FT) 00-1156

30975 FUSELAGE - CONE/R EAR FUSELAGE - INTRODUCE

MODIFIED SECTION 19 IN A319/A320/A321

31012 FUSELAGE-REAR FUSELAGE- INTRODUCE

MODIFIED BUTT JOINTS FRAME 47 AND 64 IN

A319/320/A321

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX D – MODIFICATION LIST

REV: 02 ALS PART 2 PAGE: 3- APXD

MODIFICATION LIST

© AIRBUS SAS 2013. All rights reserved. REV.

CODE MOD

NUMBER MODIFICATION DESCRIPTION SERVICE BULLETIN(S)

N 31067 INTRODUCE MODIFIED FUSELAGE SECTION 15 IN

A319 AND A320 AIRCRAFT

32208 FUSELAGE - GENERAL - CENTER FUSELAGE

INSTALL A SECOND EMERGENCY EXIT ON A319 AT

CENTER TO INCREASE PASSENGER CAPACITY

32856 COMMUNICATIONS - SATCOM - INSTALL

PROVISIONS FOR A TOP-MOUNTED ANTENNA AND

D/LNA CANADIAN MARCONI

33844 NACELLES / PYLONS - PYLONS - IMPROVE

AERODYNAMIC SHAPE OF CFM PYLON

33847 NACELLES / PYLONS - PYLONS - IMPROVE

AERODYNAMIC SHAPE OF IAE PYLON

34650 LANDING GEAR - NO SE GEAR - MODIFIED SPRING

CURVE 32-1308

35515 STABILIZERS - HORIZONTAL STABILIZER -

ELEVATOR - REPLACE LIGHTNING STRAPS

PROTECTION WITH BRON ZE MESH AND REMOVE

INSERTS AT ELEVATOR TRAILING EDGE

N 36590 FUSELAGE - REAR FUSELAGE - INSTALL

STRUCTURAL PROVISION FOR CABIN SWIFT

BROADBAND ANTENNA

37331 WINGS - FIXED PAR TITION - INTRODUCE A

STANDARD OF BOX WITHOUT DRY BAY ON A318,

A319 AND A320-200

37332 WINGS - FIXED PAR TITION - INTRODUCE A

VERSION OF WING BOX WI TH A DRY BAY ON A318,

A319 AND A320-200 (ANTI-MOD 37331)

37734 A320 FAMILY LOV EXTENSION UP TO 37500 FC OR

80000 FH 00-1198

38068 FUSELAGE - REAR FU SELAGE - REINFORCE SKIN

PANEL FOR INSTALLATION OF GSM ANTENNA

38481 WING - CENTER WING – REPLACE TRANSITION FIT

BY HIGH INTERFERENCE FIT FOR HI-LITE

INSTALLATION

38616 WINGS - FIXED PAR TITION - INTRODUCE A

STANDARD OF WING BOX WITHOUT DRY BAY ON

A321

38617 WINGS - FIXED PAR TITION - INTRODUCE A

VERSION OF WING BOX WITH A DRY BAY ON A321

AIRCRAFT (ANTI-MOD OF 38616)

39020 GENERAL - A320 FAMILY SYSTEM LIFETIME

EXTENSION - CERTIFY EXTENDED SERVICE GOAL

(ESG1)

39195 CERTIFICATION DOCUMENTS - GENERAL -

CERTIFY THE MAXIMUM FLIGHT OPERATING

LEVEL AT 41000 FEET FOR A318 ELITE 00-1219

N 39516 MODIFY AREA OF EMERGENCY EXITS BETWEEN

FR37 AND FR42 ON A320

# A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION

ALS PART 2

DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS

APPENDIX D – MODIFICATION LIST

REV: 02 ALS PART 2 PAGE: 4- APXD

MODIFICATION LIST

© AIRBUS SAS 2013. All rights reserved. REV.

CODE MOD

NUMBER MODIFICATION DESCRIPTION SERVICE BULLETIN(S)

N 150069 WINGS - CENTER WING - IMPROVE FORWARD

ANGLE FITTING MACHINING

N 152970 NOSE GEAR - INSTALL SPRING CURVE FOR

OPERATION IN CIS (CUSTOMISATION FOR

RUSSIAN AUTHORITIES CERTIFICATION)

N 153073 APPLY COLD WORKING AND REPLACE RIVETS IN

THE WASTE WATER SERVICE PANEL AREA AT S18

(SB) 53-1267

N 153074 APPLY COLD WORKING AND REPLACE RIVETS IN

THE POTABLE WATER SERVICE PANEL AREA AT

S18 (SB) 53-1272

N 160000 INTRODUCE STRUCTURE PROVISION FOR

SHARKLET PROJECT IN SECTION 21 FOR A320,

A319, A318

N 160001 DEFINE AND CERTIFY WING STRUCTURAL

PROVISIONS FOR SHARKLET FOR A320/A319/A318.

N 160055 APPLY COLD WORKING AND REPLACE RIVETS IN

THE WASTE AND POTABLE WATER SERVICE

PANELS AREAS AT S18

N 160055 APPLY COLD WORKING AND REPLACE RIVETS IN

S18 FR 66 AND FR 68 INNER CAP JOINT TO

GUSSETS

N 160056 APPLY COLD WORKING AND REPLACE RIVETS IN

WATER SERVICE PANELS AREA AND INNER CAP

JOINT - ADAPTATION SOLUTION

N 160058 IMPROVE FATIGUE LIFE ON WING SPARS FOR

SHARKLET

N 160075 IMPROVE FATIGUE LIFE ON WING SPARS FOR

SHARKLET MSN 5182

N 160076 IMPROVE FATIGUE LIFE ON WING SPARS FOR

SHARKLET MSN 5098

N 160500 CERTIFY SHARKLET INSTALLATION FOR

A320/A319/A318