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 

REV: 02 ALS PART 2 PAGE: 1 

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 

REV: 02 ALS PART 2 PAGE: 2 

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 

ACTs)

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 

REV: 02 ALS PART 2 PAGE: 3 

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 usage 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 inspection 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 catastrophic 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 inspection 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 identified 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, such 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 responsible 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 SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©AIRBUS SAS 2013. All rights reserved. SECTION 2 - DAMAGE-TOLERANT AIRWORTHINESS LIMITATION ITEMS LIST

2.1 EXPLANATION OF SECTION 2.2 TABLE FORMAT

Detailed information is given below concerning the section 2 table format of the DT ALI requirements prov

REV. 

CODE TASK REFERENCE ACCESS TASK DESCRIPTION THRESHOLD INTERVAL A

 “REV CODE” 

This column indicates the revision code “status” of the DT ALI task requirement compared to previou<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 XXXXXX-YY-ZZ  Z = Applicability index  Y = Sequence number  X = SSI number 

The SSI number is composed of six digits, e.g. 531109-01-1. The first set of two digits, e.g. 5311

A318/A319/A320/A321 ATA 100 breakdown, showing the major section where the DT ALI is locateof two digits, e.g. 531109-01-1, is also in accordance with the ATA 100 breakdown, showing the 

located, e.g. 53-11 Fwd Fuselage. The third set of two digits, e.g. 521109-01-1, is a sequential numb

up to 99. 
A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©AIRBUS SAS 2013. All rights reserved. 

The Sequence number is composed of two digits, e.g. 531109-01-1. It follows the SSI number and 

different inspection level e.g. Detailed or Special Detailed. These two digits are also changed when 

different (e.g. Rib 8 or Rib 9) or when the inspections have a major difference in access (e.g. actuatoThe Applicability index is composed of one or two digits, e.g. 531109-01-1. It follows the Sequence n

It identifies the different applicability e.g. aircraft series, mod status, group, etc. This digit is also u

access differences e.g. different panel numbers. 

 “ACCESS” 

This column indicates the access requirements to adequately perform the inspection, i.e. all items (hinged panels/doors) unless otherwise stated (e.g. insulation to be displaced). For each DT ALsufficient to perform the task. 

“TASK DESCRIPTION” 

This column describes the task to be performed. It includes the inspection level, the description and inspected. All items within this boundary are to be inspected e.g. fasteners, cutouts, attachments, information may be added to clarify the inspection area. For Special Detailed Inspections the NDbrackets. Where applicable, Notes providing details such as alternative tasks, specific grace periods or tasks 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 time
A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©AIRBUS SAS 2013. All rights reserved. 

 “APPLICABILITY” 

This column indicates the applicability of the task and lists the aircraft type, series, model, weight vawhich the DT ALI requirement is applicable. Some examples are given below. Details of modification

in Appendix E. 

Applicability Task applicable to 

ALL All A318/A319/A320/A321 series aircraft A320 All A320 series aircraft A321-100 A321-100 series aircraft only A320 PRE 25044 OR A321 PRE 25044 

All A320 and A321 series aircraft on which modification no. 25044 has not be

A320 POST 21003 

All A320 series aircraft on which modification no. 21003 has been embodied 

A320-200 POST 20062 PRE 30748 

A320-200 series aircraft only on which modification no. 20062 has been emhas not been embodied 

GROUP 19-1A A319-100 series aircraft for Weight Variants 000, 001 or 003 IAE 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 SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

2.2 INSPECTION REQUIREMENTS

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 521101-02-1 DELETED FROM ALS PART 2 AT REVISION 01  521103-01-1 N/A GENERAL VISUAL INSPECTION OF FORWARD 

PASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE, LH/RH 

14800 F

 521103-01-3 N/A GENERAL VISUAL INSPECTION OF FORWARD 

PASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE, LH/RH 

10800 F

 521301-02-1 DELETED FROM ALS PART 2 AT REVISION 01  521303-01-1 N/A GENERAL VISUAL INSPECTION OF AFT 

PASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE, LH/RH 

14800 F

 521303-01-3 N/A GENERAL VISUAL INSPECTION OF AFT 

PASSENGER/CREW DOOR SKIN, EXTERNAL SURFACE, LH/RH 

10800 F

 522102-01-1 833 834 843 

844 LINING REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH 

39300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 522102-01-2 834 844 

LINING REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH 

39300 F

 522201-01-1 N/A GENERAL VISUAL INSPECTION OF FORWARD 

EMERGENCY EXITS, EXTERNAL SURFACE, LH/RH 

4500 FC 

 522203-01-1 833 843 GENERAL VISUAL INSPECTION OF DOOR STOP 

ASSEMBLIES AND LOCKING HOOK ON FORWARD EMERGENCY EXIT DOORS, LH/RH 

24000 F

 522204-01-1 N/A GENERAL VISUAL INSPECTION OF AFT EMERGENCY 

EXITS, EXTERNAL SURFACE, LH/RH 

4500 FC 

 522206-01-1 834 844 GENERAL VISUAL INSPECTION OF DOOR STOP 

ASSEMBLIES AND LOCKING HOOK ON AFT EMERGENCY EXIT DOORS, LH/RH 

24000 F

 523101-01-1 N/A GENERAL VISUAL INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

12500 FOR 25000 F

 523101-01-3 N/A GENERAL VISUAL INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

3000 FC OR 14300 F

 523105-01-3 DELETED FROM ALS PART 2 AT REVISION 01  523105-01-4 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR, ACTUATOR ATTACH FITTINGS 

10000 FOR 43000 F

 523106-01-1 825 

LINING REMOVED INSULATION REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF FORWARD CARGO COMPARTMENT DOOR SKIN, UNDERNEATH HINGE FITTINGS AT SELECTED BOLT HOLES 

40000 FOR 80000 F

 523107-01-1 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 523108-01-1 825 DETAILED INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL 

51200 FOR 102400 F

 523109-02-1 825 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND 

LONGERON 5 (6 PLACES) 

10300 FOR 20700 F

 523109-02-2 825 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND 

LONGERON 5 (6 PLACES) 

10000 FOR 45300 F

 523111-01-1 N/A GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

12500 FOR 25000 F

 523115-01-3 DELETED FROM ALS PART 2 AT REVISION 01  523116-01-1 826 

LINING REMOVED INSULATION REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT CARGO COMPARTMENT DOOR SKIN UNDERNEATH HINGE FITTINGS AT SELECTED BOLT HOLES 

40000 FOR 80000 F

 523117-01-1 DELETED FROM ALS PART 2 AT REVISION 01  523117-01-2 DELETED FROM ALS PART 2 AT REVISION 01  523118-01-1 DELETED FROM ALS PART 2 AT REVISION 01  523118-01-2 826 DETAILED INSPECTION OF AFT CARGO COMPARTMENT 

DOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL 

51200 FOR 102400 F

 523119-02-1 826 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES) 

10300 FOR 20700 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 523119-02-2 826 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES) 

10300 FOR 20700 F

 523121-01-1 N/A GENERAL VISUAL INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

4500 FC 

 523121-01-2 N/A GENERAL VISUAL INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

4500 FC OR 13500 F

 523125-01-1 DELETED FROM ALS PART 2 AT REVISION 01  523127-01-1 825 

LINING REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR, HINGE FITTINGS ATTACHMENT AREA, INTERNAL 

36500 F

 523128-01-1 825 DETAILED INSPECTION OF FORWARD CARGO 

COMPARTMENTDOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL 

36500 F

 523129-02-1 825 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND 

LONGERON 5 (4 PLACES) 

13100 F

 523211-01-1 N/A GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

4500 FC 

 523211-01-3 N/A GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

3000 FC OR 14300 F

 523215-01-1 DELETED FROM ALS PART 2 AT REVISION 01  523215-01-2 826 GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR, ACTUATOR ATTACH FITTINGS 

10000 FOR 43000 F

 523217-01-1 826 

LINING REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, HINGE FITTINGS ATTACHMENT AREA, INTERNAL 

35200 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 523218-01-1 826 DETAILED INSPECTION OF AFT CARGO COMPARTMENT 

DOOR HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL 

48000 FOR 60000 F

 523219-02-1 826 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES) 

10300 FOR 20700 F

 523219-02-2 826 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES) 

10000 FOR 45300 F

 523221-01-1 N/A GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

4500 FC 

 523221-01-2 N/A GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

4500 FC OR 13500 F

 523225-01-1 DELETED FROM ALS PART 2 AT REVISION 01  523227-01-1 826 

LINING REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, HINGE FITTINGS ATTACHMENT AREA, INTERNAL 

35200 F

 523228-01-1 826 DETAILED INSPECTION OF AFT CARGO COMPARTMENT 

DOOR HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL 

35200 F

 523229-02-1 826 GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND 

FORK FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (4 PLACES) 

12200 F

 523301-01-1 N/A GENERAL VISUAL INSPECTION OF BULK CARGO 

COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 

7500 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 526102-01-1 N/A DETAILED INSPECTION OF ENTRANCE STAIRS DOOR 

SKIN, EXTERNAL SURFACE 

44100 F

 528103-02-2 DELETED FROM ALI DOCUMENT AT ISSUE 10 

R 528107-01-1 734 744 GENERAL VISUAL INSPECTION OF MLG DOOR FWD 

FITTING JOINT TO HINGE FITTING, LH/RH NOTE: FOR PRE 24428 OR PRE 24903 AIRCRAFT RETROFITTED, THRESHOLD IS TO BE COUNTED FROM SB 52-1058 OR SB 52-1073 EMBODIMENT 

49100 F

 531101-01-1 831 841 

INSULATION REMOVED LINING REMOVED CEILING PANELS REMOVED 

DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUTOUT, INTERCOSTALS FITTINGS N°7 BETWEEN FR15-16 AND FR20-21, LH/RH 

36500 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 531102-01-1 831 841 DETAILED INSPECTION OF FORWARD 

PASSENGER/CREW DOOR FRAME, UPPER CORNERS, EXTERNAL SURFACE, LH/RH 

22000 F

 531102-01-3 831 841 DETAILED INSPECTION OF FORWARD 

PASSENGER/CREW DOOR FRAME, UPPER CORNERS, EXTERNAL SURFACE, LH/RH 

13700 F

R 531103-01-1 831 841 

STOP FITTING BOLTS REMOVED INSULATION REMOVED LINING REMOVED CEILING PANELS REMOVED GALLEYS AND TOILETS REMOVED (IF INSTALLED) 

SPECIAL DETAILED INSPECTION (ROTO) OF FWD PASSENGER/CREW DOOR CUTOUT, STOP FITTINGS 

HOLES ON THE FR20, LH/RH 

48000 F

R 531105-01-1 SLIDING WINDOW 

OPENED 

DETAILED INSPECTION OF LATERAL WINDOW FRAME STIFFENER, UPPER AREA, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 531105-02-1. 

48000 F

R 531105-02-1 SLIDING WINDOW 

OPENED 

SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL WINDOW FRAME STIFFENER, UPPER AREA, LH/RH 

NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 531105-01-1. 

48000 F

R 531108-01-1 713 714 

BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF HOLES AT FWD CORNERS OF NLG BAY, FR9 

48000 FOR 96000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 531109-01-1 N/A GENERAL VISUAL INSPECTION OF ENTRANCE STAIRS 

DOOR SURROUND, UPPER AND LOWER CORNERS, EXTERNAL SURFACE, LH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-03-2. 

3200 FC OR 6400 FH 

 531109-01-3 N/A GENERAL VISUAL INSPECTION OF ENTRANCE STAIRS 

DOOR SURROUND, UPPER AND LOWER CORNERS, EXTERNAL SURFACE, LH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-03-1. 

2900 FC 

 531109-03-1 N/A DETAILED INSPECTION OF ENTRANCE STAIRS DOOR 

SURROUND, UPPER AND LOWER CORNERS, EXTERNAL SURFACE, LH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-01-3. 

5900 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 531109-03-2 N/A DETAILED INSPECTION OF ENTRANCE STAIRS DOOR 

SURROUND, UPPER AND LOWER CORNERS, EXTERNAL SURFACE, LH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531109-01-1. 

6300 FC OR 12700 F

R 531110-01-1 812 824 

INSULATION REMOVED BOLTS REMOVED AIR CONDITIONING DUCTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF 

CROSSBEAM SPLICING, FR16 AND FR20, LH/RH 

38800 FOR 77600 F

R 531110-01-2 812 824 

INSULATION REMOVED BOLTS REMOVED AIR CONDITIONING DUCTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF 

CROSSBEAM SPLICING, FR16 AND FR20, LH/RH 

38900 FOR 77900 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 531111-01-1 N/A GENERAL VISUAL INSPECTION OF AVIONICS 

COMPARTMENT DOORS, SURROUND CORNERS, EXTERNAL SURFACE (4 DOORS) 

1500 FC 

 531111-01-2 N/A GENERAL VISUAL INSPECTION OF AVIONICS 

COMPARTMENT DOORS, SURROUND CORNERS, EXTERNAL SURFACE (4 DOORS) 

5500 FC 

 531112-01-1 N/A DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT 

NLG BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH 

16300 FOR 32600 F

 531112-01-2 N/A DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT 

NLG BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH 

15400 F

 531113-01-1 N/A GENERAL VISUAL INSPECTION OF ATTACHMENT TO 

SKIN PANEL, FR16, STG 3 LH/RH 

41400 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 531114-01-1 N/A DETAILED INSPECTION OF FUSELAGE SKIN ABOVE 

WINDSHIELD, BETWEEN FR 4 AND FR 12, EXTERNAL SURFACE, LH/RH 

5700 FC 

 531114-01-2 N/A DETAILED INSPECTION OF FUSELAGE SKIN ABOVE 

WINDSHIELD, BETWEEN FR 4 AND FR 12, EXTERNAL SURFACE, LH/RH 

5700 FC 

 531117-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SIDE 

PANEL, BELOW COCKPIT SIDE WINDOWS, BETWEEN FR 1 AND FR 12, EXTERNAL SURFACE, LH/RH 

14500 F

 531117-01-3 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SIDE 

PANEL, BELOW COCKPIT SIDE WINDOWS, BETWEEN FR 1 AND FR 12, EXTERNAL SURFACE, LH/RH 

14000 F

 531118-01-1 N/A GENERAL VISUAL INSPECTION OF AREA FORWARD OF 

WINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR 4, 

EXTERNAL SURFACE, LH/RH 

4300 FC 

 531118-01-3 N/A GENERAL VISUAL INSPECTION OF AREA FORWARD OF 

WINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR 4, 

EXTERNAL SURFACE, LH/RH 

3700 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 531119-01-1 N/A DETAILED INSPECTION OF UPPER SKIN OF LOWER 

LONGITUDINAL LAP JOINT, BETWEEN FR 9 AND FR 20, EXTERNAL SURFACE, LH/RH 

41000 F

R 531119-01-2 N/A DETAILED INSPECTION OF UPPER SKIN OF LOWER 

LONGITUDINAL LAP JOINT, BETWEEN FR 9 AND FR 20, EXTERNAL SURFACE, LH/RH 

35300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 531124-01-1 824 

INSULATION DISPLACED 

DETAILED INSPECTION OF FR 20 SPLICE, BETWEEN STRINGER 30 AND STRINGER 32, LH/RH 

35600 F

R 531124-01-2 824 

INSULATION DISPLACED 

DETAILED INSPECTION OF FR 20 SPLICE, BETWEEN STRINGER 30 AND STRINGER 32, LH/RH 

33600 F

 531124-01-3 824 

INSULATION DISPLACED PART OF LEFT END SIDE GASKET REMOVED 

DETAILED INSPECTION OF FR 20 SPLICE, BETWEEN STRINGER 30 AND STRINGER 32, LH/RH 

35600 F

 531126-01-2 LINING REMOVED 

INSULATION REMOVED AIR CONDITIONING OUTLET REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL SPLICING, FR8, LH/RH 

25500 FOR 51000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 531127-01-1 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL SPLICING, FR11, LH/RH 

42400 F

 531129-01-1 DELETED FROM ALS PART 2 AT REVISION 01 

R 531129-02-1 211LW 211MW 

LH/RH WINDSHIELDS REMOVED DISPLAY UNIT 4WT1 REMOVED ANCHOR NUT SHIMS REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD CENTER POST, LOWER ATTACHMENT AREA, INTERNAL SIDE 

36000 F

R 531129-02-2 211LW 211MW 

LH/RH WINDSHIELDS REMOVED DISPLAY UNIT 4WT1 REMOVED ANCHOR NUT SHIMS REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD CENTER POST, LOWER ATTACHMENT AREA, INTERNAL SIDE 

36600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 531129-02-3 211LW 211MW 

LH/RH WINDSHIELDS REMOVED DISPLAY UNIT 4WT1 REMOVED ANCHOR NUT SHIMS REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD CENTER POST, LOWER ATTACHMENT AREA, INTERNAL SIDE 

34600 F

 531130-02-1 211NW 211PW 

212NW 212PW SLIDING WINDOW OPENED 

SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL FORWARD CORNER OF SLIDING WINDOW FRAME AT FR4, LH/RH 

48000 F

 531133-01-1 211NW 211PW 

212NW 212PW SLIDING WINDOW OPENED 

DETAILED INSPECTION OF WINDSHIELD SIDE POST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-02-1. 

26700 F

 531133-01-2 211NW 211PW 

212NW 212PW SLIDING WINDOW OPENED 

DETAILED INSPECTION OF WINDSHIELD SIDE POST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-02-2. 

25600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 531133-02-1 211NW 211PW 

212NW 212PW SLIDING WINDOW OPENED 

SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD SIDE POST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-1. 

26700 F

 531133-02-2 211NW 211PW 

212NW 212PW SLIDING WINDOW OPENED 

SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD SIDE POST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-2. 

25600 F

R 531135-01-1 211BC 211KC 211LC 

211NW 212BC 212KC212LC 212NW SLIDING WINDOW OPENED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF WINDSHIELD SIDE POST AT FR 4, UPPER ATTACHMENT, INTERNAL 

SIDE, LH/RH 

28800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 531135-01-2 211BC 211KC 211LC 

211NW 212BC 212KC212LC 212NW SLIDING WINDOW OPENED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF WINDSHIELD SIDE POST AT FR 4, UPPER ATTACHMENT, INTERNAL 

SIDE, LH/RH 

28800 F

 531155-02-1 831 841 

LINING REMOVED INSULATION REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (HFEC AND ROTO) OF DOOR FR 20, AT DOUBLE JOGGLE AREA IN OUTER FLANGE OF FRAME, AT DOOR STOPS NUMBER 1 AND 7 LOCATION, LH/RH 

27700 F

R 531157-01-1 824 

LADDER REMOVED FLOOR PANEL REMOVED 

DETAILED INSPECTION OF CONTINUITY FITTING BETWEEN FR 20 AND FR 21, AND ANGLE FITTING, BOTH SIDES OF FR 21, AT STRINGER 41 LOCATION, LH/RH 

24000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 531157-01-2 824 

LADDER REMOVED FLOOR PANEL REMOVED 

DETAILED INSPECTION OF CONTINUITY FITTING BETWEEN FR 20 AND FR 21, AND ANGLE FITTING, BOTH SIDES OF FR 21, AT STRINGER 41 LOCATION, LH/RH 

24000 F

R 531170-01-1 LOWER RETAINERS 

REMOVED 

DETAILED INSPECTION OF COCKPIT WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-1. 

36700 F

R 531170-01-2 LOWER RETAINERS 

REMOVED 

DETAILED INSPECTION OF COCKPIT WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-2. 

36700 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 531170-02-1 LOWER RETAINERS 

REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF COCKPIT WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-1. 

36700 F

R 531170-02-2 LOWER RETAINERS 

REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF COCKPIT WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-2. 

36700 F

 531184-01-1 811 

INSULATION REMOVED 

DETAILED INSPECTION OF CENTRAL AND ADJACENT VERTICAL POSTS OF FORWARD PRESSURE BULKHEAD AND WEB ASSEMBLY, UPPER PORTION 

32100 F

 531184-01-2 811 

INSULATION REMOVED 

DETAILED INSPECTION OF CENTRAL AND ADJACENT VERTICAL POSTS OF FORWARD PRESSURE BULKHEAD AND WEB ASSEMBLY, UPPER PORTION 

34000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 532104-01-1 825 

CEILING PANELS REMOVED LINING REMOVED INSULATION DISPLACED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF 

ATTACHMENT AREA OF FR25 LH TO FR34 LH AND FR29 RH TO FR34 RH TO CABIN FLOOR BEAMS, INTERNAL STRUCTURE 

43400 FOR 86900 F

 532132-01-1 825 DETAILED INSPECTION OF FUSELAGE FORWARD 

CARGO DOOR HINGE FITTING AND EXTERNAL ATTACHMENT AREA 

24000 F

 532135-01-2 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR CUTOUT, VISIBLE PART OF LATERAL FR 24A AND FR 28 

1200 FC OR 2400 FH 

 532135-01-3 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR CUTOUT, VISIBLE PART OF LATERAL FR 24A AND FR 28 

1100 FC 

 532135-01-4 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR CUTOUT, VISIBLE PART OF LATERAL FR 24A AND FR 28 

1700 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 532137-01-1 825 DETAILED INSPECTION OF FORWARD CARGO DOOR 

CUTOUT PANELS, UPPER AND LOWER CORNERS, 

EXTERNAL SURFACE 

9700 FC OR 19400 F

 532137-01-2 825 DETAILED INSPECTION OF FORWARD CARGO DOOR 

CUTOUT PANELS, UPPER AND LOWER CORNERS, 

EXTERNAL SURFACE 

9000 FC 

 532150-01-1 833 DETAILED INSPECTION OF FORWARD EMERGENCY EXIT 

SKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE, LH 

13500 FOR 35900 F

 532150-01-2 833 DETAILED INSPECTION OF FORWARD EMERGENCY EXIT 

SKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE, LH 

12600 FOR 33500 F

 532151-01-1 843 DETAILED INSPECTION OF FORWARD EMERGENCY EXIT 

SKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE, RH 

9500 FC OR 25100 F

 532151-01-2 843 DETAILED INSPECTION OF FORWARD EMERGENCY EXIT 

SKIN CUT OUT, UPPER CORNERS, EXTERNAL SURFACE, RH 

9200 FC OR 24500 F

 532152-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND FORWARD EMERGENCY EXIT SKIN CUT OUT BETWEEN FR 35 AND FR 35.3 AND FROM STRINGER 8 TO STRINGER 23, EXTERNAL SURFACE, LH/RH NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF ZONAL TASK ZL-200-02-4. 

20000 FOR 42000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 532155-01-1 825 

CARGO FLOOR PANELS REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF FRAME SPLICES AT STRINGER 35 LH, FROM FR 24 TO FR 34 

34000 F

R 532155-01-2 825 

CARGO FLOOR PANELS REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF FRAME SPLICES AT STRINGER 35 LH, FROM FR 24 TO FR 34 

32400 F

 532156-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 35.4 AND FR 35.8 FROM STRINGER 8 TO STRINGER 14 AND STRINGER 18 TO STRINGER 23, LH/RH 

24000 FOR 42000 F

 532156-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 35.4 AND FR 35.8 FROM STRINGER 8 TO STRINGER 14 AND STRINGER 18 TO STRINGER 23, LH/RH 

24000 FOR 42000 F

 532165-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRING 

5400 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

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COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 532165-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRING 

5600 FC 

 532165-01-3 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 24 AND FR 35.8, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRING 

3600 FC 

 532165-01-4 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRING 

4000 FC 

 532165-01-7 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRING 

8100 FC 

 532165-01-8 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRING NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532165-02-5. 

1600 FC 

 532165-02-4 DELETED FROM ALS PART 2 AT REVISION 01  532165-02-5 N/A DETAILED INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 24 AND FR 35, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY BELLY FAIRING NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532165-01-8. 

5800 FC 

 532166-01-1 LINING REMOVED 

INSULATION REMOVED 

DETAILED INSPECTION OF FUSELAGE SKIN AT FR 35 AND 10 CM FORWARD, AT LEVEL OF STRINGER 30, INTERNAL SIDE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-1. 

43400 FOR 86900 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 532166-02-1 LINING REMOVED 

INSULATION REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE SKIN AT FR 35 AND 10 CM FORWARD, AT LEVEL OF STRINGER 30, INTERNAL SIDE, LH/RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-1. 

43400 FOR 86900 F

R 532170-01-1 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 25 AND FR 27A, EXTERNAL PORTION (6 PLACES) 

9300 FC 

R 532170-01-2 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 25 AND FR 27A, EXTERNAL PORTION (6 PLACES) 

9100 FC 

 532170-01-3 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 25 AND FR 26A, EXTERNAL PORTION (4 PLACES) 

9100 FC 

 532170-01-6 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 25 AND FR 27A, EXTERNAL PORTION (6 PLACES) 

8400 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 532186-01-1 N/A SPECIAL DETAILED INSPECTION (LFEC) OF 

CIRCUMFERENTIAL JOINT AT FR 35, BETWEEN STRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE 

48000 FOR 96000 F

 532186-01-2 N/A SPECIAL DETAILED INSPECTION (LFEC) OF 

CIRCUMFERENTIAL JOINT AT FR 35, BETWEEN STRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE 

42700 FOR 60000 F

 532187-01-1 N/A SPECIAL DETAILED INSPECTION (LFEC) OF 

CIRCUMFERENTIAL JOINT AT FR 35.8, BETWEEN STRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE 

44300 FOR 60000 F

R 532190-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE AROUND WATER DRAIN PANEL CUTOUT, BETWEEN FR 25 AND FR 29 AT STRINGER 43 LH 

48000 F

 532190-01-2 DELETED FROM ALS PART 2 AT REVISION 01  532190-01-3 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE AROUND WATER DRAIN PANEL CUTOUT, BETWEEN FR 25 AND FR 29 AT STRINGER 43 LH 

12000 F

 532195-01-1 DELETED FROM ALS PART 2 AT REVISION 01  532195-01-2 DELETED FROM ALS PART 2 AT REVISION 01  532195-01-3 131AC 825 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

DOOR ACTUATOR ATTACH BRACKETS, BETWEEN CABIN FLOOR BEAMS, FROM FR 25A TO FR 27A 

11400 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 533105-01-1 734 744 DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE 

PANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING SLANTED FRAMES AND SIDE BOX, LH/RH 

28400 FOR 60000 F

 533105-01-2 DELETED FROM ALS PART 2 AT REVISION 01  533105-01-4 734 744 DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE 

PANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING SLANTED FRAMES AND SIDE BOX, LH/RH 

23600 FOR 60000 F

 533105-01-6 734 744 DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE 

PANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING SLANTED FRAMES AND SIDE BOX, LH/RH 

13100 FOR 56400 F

 533105-01-8 734 744 DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE 

PANELS INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING SLANTED FRAMES AND SIDE BOX, LH/RH NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 533105-01-2. 

27100 FOR 60000 F

 533109-01-1 CABIN FLOOR 

PANELS REMOVED INSULATION REMOVED AIR CONDITIONING DUCT REMOVED 

DETAILED INSPECTION OF UPPER SURFACES OF 

PRESSURE DECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS AND SUPPORT RIBS, LH/RH 

20000 FOR 55000 F

 533109-01-2 CABIN FLOOR 

PANELS REMOVED INSULATION REMOVED AIR CONDITIONING DUCT REMOVED 

DETAILED INSPECTION OF UPPER SURFACES OF 

PRESSURE DECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS AND SUPPORT RIBS, LH/RH 

20000 FOR 55000 F

 533109-01-3 CABIN FLOOR 

PANELS REMOVED INSULATION REMOVED AIR CONDITIONING DUCT REMOVED 

DETAILED INSPECTION OF UPPER SURFACES OF 

PRESSURE DECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS AND SUPPORT RIBS, LH/RH 

13100 FOR 56400 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 533111-01-1 734 744 DETAILED INSPECTION OF LOWER SURFACE OF 

PRESSURE DECK MEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES, SUPPORT RIBS, REAR SPAR OF CENTER WING BOX AND PRESSURE BULKHEAD, LH/RH 

24000 FOR 48000 F

 533111-01-2 734 744 DETAILED INSPECTION OF LOWER SURFACE OF 

PRESSURE DECK MEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES, SUPPORT RIBS, REAR SPAR OF CENTER WING BOX AND PRESSURE BULKHEAD, LH/RH 

22000 FOR 60000 F

 533122-01-1 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREA AT FR 47, 

FROM STRINGER 10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE 

33300 F

R 533122-01-2 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREA AT FR 47, 

FROM STRINGER 10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE 

33000 F

 533122-01-3 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREA AT FR 47/51, FROM STRINGER 10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE 

33300 F

 533122-01-4 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREA AT FR 47/54, FROM STRINGER 10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE 

33300 F

 533124-01-1 DELETED FROM ALS PART 2 AT REVISION 01  533124-01-2 DELETED FROM ALS PART 2 AT REVISION 01  533124-01-3 DELETED FROM ALS PART 2 AT REVISION 01  533124-01-4 DELETED FROM ALS PART 2 AT REVISION 01  533125-01-1 DELETED FROM ALS PART 2 AT REVISION 01  533125-01-2 DELETED FROM ALS PART 2 AT REVISION 01  533125-01-3 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 533125-01-4 DELETED FROM ALS PART 2 AT REVISION 01  533126-01-1 DELETED FROM ALS PART 2 AT REVISION 01  533126-01-2 DELETED FROM ALS PART 2 AT REVISION 01  533126-01-3 DELETED FROM ALS PART 2 AT REVISION 01  533126-01-4 DELETED FROM ALS PART 2 AT REVISION 01  533126-02-1 DELETED FROM ALS PART 2 AT REVISION 01  533126-02-2 DELETED FROM ALS PART 2 AT REVISION 01  533126-02-3 DELETED FROM ALS PART 2 AT REVISION 01  533126-02-4 DELETED FROM ALS PART 2 AT REVISION 01  533127-01-1 DELETED FROM ALS PART 2 AT REVISION 01  533127-01-2 DELETED FROM ALS PART 2 AT REVISION 01  533127-01-3 DELETED FROM ALS PART 2 AT REVISION 01  533127-01-4 DELETED FROM ALS PART 2 AT REVISION 01  533128-01-1 833 834 843 

844 

DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, UPPER AND LOWER CORNERS, LH/RH 

24000 FOR 48000 F

R 533128-01-2 833 834 843 

844 

DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, UPPER AND LOWER CORNERS, LH/RH 

31100 FOR 62200 F

 533128-01-3 834 844 DETAILED INSPECTION OF EMERGENCY EXIT SKIN 

CUTOUTS, UPPER AND LOWER CORNERS, LH/RH 

24000 FOR 60000 F

 533128-01-4 833 834 843 

844 

DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, UPPER AND LOWER CORNERS, LH/RH 

24000 FOR 60000 F

 533128-01-5 834 844 DETAILED INSPECTION OF EMERGENCY EXIT SKIN 

CUTOUTS, UPPER AND LOWER CORNERS, LH/RH 

24000 FOR 60000 F

R 533128-01-6 833 834 843 

844 

DETAILED INSPECTION OF EMERGENCY EXITS SKIN CUTOUTS, UPPER AND LOWER CORNERS, LH/ RH 

24000 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

N 533128-01-7 833 834 843 

844 

DETAILED INSPECTION OF EMERGENCY EXITS SKIN CUTOUTS, UPPER AND LOWER CORNERS, LH/ RH 

28000 FOR 56000 F

 533130-01-1 DELETED FROM ALS PART 2 AT REVISION 01  533130-01-2 ANTI-COLLISION 

LIGHT COVER REMOVED ANTI-COLLISION LIGHT REMOVED 

DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 533130-01-1. 

30500 F

 533130-01-3 ANTI-COLLISION 

LIGHT COVER REMOVED ANTI-COLLISION LIGHT REMOVED 

DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE 

27800 F

R 533130-01-4 ANTI-COLLISION 

LIGHT COVER REMOVED ANTI-COLLISION LIGHT REMOVED 

DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE 

27800 F

 533131-01-1 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 533131-01-5 ANTENNA COVER 

REMOVED ANTENNA REMOVED 

DETAILED INSPECTION OF SKIN AROUND ADF 1 ANTENNA CUTOUT, BETWEEN FR 44 AND FR 45 AND 

BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK533131-01-1. 

26300 F

D 533132-01-1 DELETED FROM ALS PART 2 AT REVISION 02 

 533132-01-2 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOW 

FORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA, BETWEEN FR 35.8 AND FR 47, LH/RH, EXTERNAL SURFACE 

36300 F

 533132-01-3 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOW 

FORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA, BETWEEN FR 35 AND FR 47/51, LH/RH, EXTERNAL 

SURFACE 

36300 F

 533132-01-4 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOW 

FORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA, BETWEEN FR 35 AND FR 47/54, LH/RH, EXTERNAL 

SURFACE 

36300 F

 533132-01-5 N/A DETAILED INSPECTION OF VISIBLE PART OF WINDOW 

FORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA, BETWEEN FR 35 AND FR 47, LH/RH, EXTERNAL SURFACE 

36300 F

R 533138-01-1 LINING REMOVED 

INSULATION REMOVED 

DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNAL NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533138-02-1. 

40000 FOR 80000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 533138-01-2 LINING REMOVED 

INSULATION REMOVED 

DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNAL NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 533138-02-2. 

40000 F

R 533138-02-1 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF LOWER SKIN OF LONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNAL NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533138-01-1. 

40000 FOR 80000 F

 533138-02-2 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF LOWER SKIN OF LONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNAL NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 533138-01-2. 

40000 F

R 533139-01-1 LINING REMOVED 

INSULATION REMOVED 

DETAILED INSPECTION OF FRAME FLANGES AT FR 38 AND 39, AND AT FR 40 AND 41 BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND LONGITUDINAL BEAM FLANGE AT STRINGER 20A LH AND STRINGER 20A RH, BETWEEN FR 38 AND FR 39 AND BETWEEN FR 40 AND FR 41 

27400 FOR 54800 F

 533139-01-2 LINING REMOVED 

INSULATION REMOVED 

DETAILED INSPECTION OF FRAME FLANGES AT FR 40 AND 41, BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND LONGITUDINAL BEAM FLANGE AT STRINGER 

20A LH AND STRINGER 20A RH, BETWEEN FR 40 AND FR 41 

24000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 533139-01-3 LINING REMOVED 

INSULATION REMOVED 

DETAILED INSPECTION OF FRAME FLANGES AT FR 38 AND FR 39 AND AT FR 40 AND FR 41 BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND LONGITUDINAL BEAM FLANGE AT STRINGER 20A LH AND 

STRINGER 20A RH, BETWEEN FR 38 AND FR 39, AND BETWEEN FR 40A FR 41 

24000 F

 533140-01-1 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE 

34500 F

 533140-01-2 DELETED FROM ALS PART 2 AT REVISION 01  533140-01-3 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE 

40000 F

 533140-01-4 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47/51, FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE 

38700 F

 533140-01-5 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47/54, FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE 

33700 F

R 533140-01-7 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE 

31100 F

 533140-01-8 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER 10, LH/RH, TO CROWN CENTER LINE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 533140-01-2. 

40300 FOR 80700 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 533141-01-1 191BT 191EB 192BT 

192EB 

DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 35 AND FR 36 AND BETWEEN STRINGER 25 AND STRINGER 30, LH/RH, EXTERNAL SURFACE 

38600 FOR 77200 F

 533141-01-2 191BT 191EB 192BT 

192EB 

DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 35.8 AND FR 36 AND BETWEEN STRINGER 25 AND STRINGER 30, LH/RH, EXTERNAL SURFACE 

38600 FOR 60000 F

 533142-01-1 ALI REPLACED BY SB A320 53-1060 AT ALI DOCUMENT 

ISSUE 6 

R 533143-01-1 734 744 DETAILED INSPECTION OF SIDE BOX BEAM IN AREA 

OFATTACHMENT TO FR 46, LH/RH 

40000 FOR 80000 F

R 533144-01-1 LINING REMOVED 

INSULATION REMOVED 

DETAILED INSPECTION OF FRAME ATTACHMENTS TO PRESSURE FLOOR FROM FR 42 TO FR 46, LH/RH 

33100 FOR 66200 F

 533152-01-1 DELETED FROM ALS PART 2 AT REVISION 01  533152-01-3 131NW 131PW 

132PW INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED 

DETAILED INSPECTION OF PRESSURE BULKHEAD 

FORWARD FACE AT FR 35.8 AND PRESSURE DECK UPPER SURFACE, BETWEEN FR 35.8 AND FR 36, INCLUDING CONNECTIONS TO CENTER WING BOX AT FR35.8 AND FR 36 

31000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 533152-01-4 131NW 131PW 

132PW INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED 

DETAILED INSPECTION OF PRESSURE BULKHEAD 

FORWARD FACE AT FR 35 AND PRESSURE DECK UPPER SURFACE, BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO CENTER WING BOX AT FR 35 AND FR 36 

31000 F

 533152-01-5 131NW 131PW 

132PW INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED 

DETAILED INSPECTION OF PRESSURE BULKHEAD 

FORWARD FACE AT FR 35 AND PRESSURE DECK UPPER SURFACE, BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO CENTER WING BOX AT FR 35 AND FR 36 

31000 F

 533152-01-7 DELETED FROM ALS PART 2 AT REVISION 01  533152-01-9 131NW 131PW 

132PW 825 INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED 

DETAILED INSPECTION OF PRESSURE BULKHEAD 

FORWARD FACE AT FR 35 AND PRESSURE DECK UPPER SURFACE, BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO CENTER WING BOX AT FR 35 AND FR 36 

31000 F

R 533152-01-10 131NW 131PW 132PW 

825 INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED POTABLE WATER TANK REMOVED 

DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE AT FR 35 AND PRESSURE DECK UPPER SURFACE, BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO CENTER WING BOX AT FR 35 AND FR 36 

31000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 533154-02-1 ALI SUPERSEDED BY SB A320 53-1195 AND SB A320 53-

1196 AT ALS PART 2 REVISION 01 NOTE: NTM PROCEDURES REFERENCED IN PREVIOUS ESTABLISHED RAS AND REFERRING TO ALI 533154-02-1 REMAIN VALID. 

R 533155-03-1 734 744 SPECIAL DETAILED INSPECTION (HFEC) OF KEELBEAM 

BOX ELLIPTICAL CUTOUT AT FR 46, LH/RH 

38400 FOR 60000 F

R 533180-01-1 CABIN FLOOR 

PANELS REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF UPPER SURFACE OF PRESSURE DECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR 46, AT CONNECTIONS TO LONGITUDINAL BEAMS AND SUPPORT RIBS (INCLUDING LATERAL OUTER PART OF CONNECTION PLATES) AT Y=+/- 254 MM, Y=+/- 765 MM, Y=+/- 1292 MM AND Y=+/- 1650 MM 

48100 FOR 96200 F

 533181-01-1 734 744 

CABIN FLOOR PANELS REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF 

LONGITUDINAL BEAMS FLANGES AT ATTACHMENT AREA TO PRESSURE DECK MEMBRANE BETWEEN FR 42 AND FR 46 AT Y=+/- 254 MM, Y=+/- 765MM, Y=+/- 1292 MM AND 

SIDE BOX FLANGE AT Y=+/- 1650 MM 

48500 FOR 97000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 533185-01-1 131NW, 131PW, 

132PW 825 INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (LFEC AND ROTO) OF PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING BOX, UNDER TITANIUM ANGLE CONNECTION AND CORNER BRAKETS, AT FR 36 

48000 FOR 96000 F

R 533185-01-2 131NW, 131PW, 

132PW 825 INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED POTABLE WATER TANK REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (LFEC AND ROTO) OF PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING BOX, UNDER TITANIUM ANGLE CONNECTION AND CORNER BRAKETS, AT FR 36 

48000 FOR 96000 F

 533186-01-1 131PW 132PW 

INSULATION REMOVED RECIRCULATION FILTER REMOVED AIR CONDITIONING DUCTS REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FR 35 FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENTS, AROUND RIVETS AND HOLES BETWEEN STR 28 AND STR 31, LH/RH 

40000 FOR 80000 F

 533188-01-1 191BB 191EB 192EB 

192FB 

DETAILED INSPECTION OF FR35, PRESSURE BULKHEAD, AFT FACE, LOWER PART OF VERTICAL STRUTS (200 MM FROM BOTTOM) AT Y= +/-765 MM (2 PLACES) 

30300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 533188-01-2 191BB 191EB 192EB 

192FB 

DETAILED INSPECTION OF FR 35.8 PRESSURE BULKHEAD, AFT FACE, LOWER PART OF VERTICAL STRUTS (200 MM FROM BOTTOM) AT Y= +/-765 MM (2 PLACES) 

30300 F

 533189-01-1 191BT 192BT 

AIR CONDITIONING DUCTS REMOVED 

SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE 

FITTING FORWARD ATTACHMENT, AT FRAME 36 AT STRINGER 30, LH/RH 

26900 FOR 53800 F

R 533189-01-3 191BT 192BT 

AIR CONDITIONING DUCTS REMOVED 

SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING FORWARD ATTACHMENT, AT FRAME 36 AT STRINGER 30, LH/RH 

50100 FOR 100200 F

 534101-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534101-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534101-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534102-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534102-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534102-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534102-02-1 DELETED FROM ALS PART 2 AT REVISION 01  534102-02-2 DELETED FROM ALS PART 2 AT REVISION 01  534102-02-3 DELETED FROM ALS PART 2 AT REVISION 01  534104-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534104-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534104-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534104-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534105-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534105-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534105-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534105-01-4 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534106-01-1 252HW 252LW 252PW 

INSULATION REMOVED 

DETAILED INSPECTION OF FRAME SPLICES AND ADJACENT AREA FROM FR 53 TO FR 56, LOCATED ABOVE STRINGER 18 RH 

51300 FOR 102700 F

 534106-01-4 252HW 252LW 252PW 

INSULATION REMOVED 

DETAILED INSPECTION OF FRAME SPLICES AND ADJACENT AREA FROM FR 53 TO FR 56, LOCATED ABOVE STRINGER 18 RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534106-02-4. 

12000 FOR 69000 F

 534106-02-4 252HW 252LW 252PW 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (US) OF FRAME 

SPLICES AND ADJACENT AREA FROM FR 53 TO FR 56, LOCATED ABOVE STRINGER 18 RH NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534106-01-4. 

12000 FOR 69000 F

 534107-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534108-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 47 AND FR 70, FROM STRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BY BELLY FAIRING 

3000 FC 

 534108-01-4 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 47/51 AND FR 70, FROM STRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BY BELLY FAIRING 

3000 FC 

 534108-01-6 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 47/54 AND FR 70, FROM STRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BY BELLY FAIRING 

3000 FC 

 534108-01-7 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 47/51 AND FR 70, FROM STRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BY BELLY FAIRING 

700 FC OR 3200 FH 

 534108-01-8 N/A GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 

SURFACE, BETWEEN FR 47/54 AND FR 70, FROM STRINGER 23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BY BELLY FAIRING 

1300 FC 

 534111-01-1 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534111-01-2 ANTENNA COVER 

REMOVED ANTENNA REMOVED 

DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA CUTOUT, BETWEEN FR 47.1 AND FR 47.2 

BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: FOR PRE 20053 AIRCRAFT RETROFITTED, THRESHOLD IS TO BE COUNTED FROM SB EMBODIMENT. 

28800 FOR 60000 F

R 534111-01-3 ANTENNA COVER 

REMOVED ANTENNA REMOVED 

DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA CUTOUT, BETWEEN FR 52 AND FR 53, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: FOR PRE 20053 AIRCRAFT RETROFITTED, THRESHOLD IS TO BE COUNTED FROM SB EMBODIMENT. 

28800 FOR 60000 F

R 534111-01-4 ANTENNA COVER 

REMOVED ANTENNA REMOVED 

DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA CUTOUT, BETWEEN FR 55 AND FR 56, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: FOR PRE 20053 AIRCRAFT RETROFITTED, THRESHOLD IS TO BE COUNTED FROM SB EMBODIMENT. 

28800 FOR 60000 F

R 534111-01-7 ANTENNA COVER 

REMOVED ANTENNA REMOVED 

DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA CUTOUT, BETWEEN FR 48 AND FR 49 BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE 

28800 FOR 60000 F

 534112-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534112-01-3 ANTENNA REMOVED DETAILED INSPECTION OF SKIN AROUND VHF 3 

ANTENNA CUTOUT, BETWEEN FR 56 AND FR 57 AND 

BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE 

31200 FOR 60000 F

 534112-01-4 ANTENNA REMOVED DETAILED INSPECTION OF SKIN AROUND VHF 3 

ANTENNA CUTOUT, BETWEEN FR 61 AND FR 62 AND 

BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE 

31200 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534112-01-7 ANTENNA REMOVED DETAILED INSPECTION OF SKIN AROUND VHF 3 

ANTENNA CUTOUT, BETWEEN FR 52 AND FR 53 AND BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF 534112-01-1. 

31200 FOR 60000 F

 534113-01-1 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREAS AT FR 64, 

FROM STRINGER 10, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE 

40000 F

 534113-01-2 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREAS AT FR 64, 

FROM STRINGER 10, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE 

36000 F

 534113-01-3 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREAS AT FR 64, 

FROM STRINGER 10, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE 

12500 FOR 56600 F

 534114-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534114-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534114-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534114-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534115-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534115-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534115-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534115-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534116-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534116-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534116-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534116-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534116-02-1 DELETED FROM ALS PART 2 AT REVISION 01  534116-02-2 DELETED FROM ALS PART 2 AT REVISION 01  534116-02-3 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534116-02-4 DELETED FROM ALS PART 2 AT REVISION 01  534117-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534117-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534117-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534117-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534121-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534121-01-3 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 64, FROM STRINGER 10, LH/RH TO CROWN CENTERLINE 

12500 FOR 56500 F

 534121-01-4 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 64, FROM STRINGER 10, LH/RH TO CROWN CENTERLINE 

40000 F

 534122-01-1 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF THE SATCOM ANTENNA, IN THE AREA OF FR 58 TO FR 61, STGR 2 LH AND STGR 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME JUNCTIONS 

36200 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534122-01-3 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF THE SATCOM ANTENNA, IN THE AREA OF FR 58 TO FR 61, STGR 2 LH AND STGR 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME JUNCTIONS 

41300 FOR 60000 F

R 534123-01-1 832 842 

LINING REMOVED INSULATION REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE INTERNAL STRUCTURE, FRAME 66 AND FRAME 68 INNER CAP JOINT TO GUSSETS PLATE FROM STRINGER 10 TO STRINGER 16, LH/RH 

41600 FOR 60000 F

 534124-01-1 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF AFT 

PASSENGER/CREW DOOR CUTOUT, AFT UPPER 

CORNER BETWEEN STRINGER 8 AND STRINGER 10, FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE, LH/RH 

22100 FOR 44200 F

 534124-01-2 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF AFT 

PASSENGER/CREW DOOR CUTOUT, AFT UPPER 

CORNER BETWEEN STRINGER 8 AND STRINGER 10, FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE, LH/RH 

28300 FOR 56600 F

 534124-01-3 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF AFT 

PASSENGER/CREW DOOR CUTOUT, AFT UPPER 

CORNER BETWEEN STRINGER 8 AND STRINGER 10, FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE, LH/RH 

32700 FOR 65400 F

 534124-01-4 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF AFT 

PASSENGER/CREW DOOR CUTOUT, AFT UPPER 

CORNER BETWEEN STRINGER 8 AND STRINGER 10, FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE, LH/RH 

30900 FOR 60000 F

 534125-01-1 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT AND BELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, LH 

29400 FOR 58800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534125-01-2 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT AND BELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, LH 

32100 FOR 60000 F

R 534125-01-3 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT AND BELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, LH 

36100 FOR 72200 F

R 534125-01-4 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AT AND BELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, LH 

41500 FOR 60000 F

 534126-01-1 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOW STRINGER 33, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, RH 

27800 FOR 55600 F

R 534126-01-2 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOW STRINGER 33, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, RH 

28700 FOR 57400 F

R 534126-01-3 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOW STRINGER 33, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, RH 

30900 FOR 61800 F

R 534126-01-4 N/A SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN EXTERNAL SURFACE AT WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 BELOW STRINGER 33, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, RH 

34400 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534127-01-1 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE INTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TO UPPER FRAME 68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH 

23500 FOR 47000 F

R 534127-01-2 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE INTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TO UPPER FRAME 68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH 

27700 FOR 55400 F

R 534127-01-3 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE INTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TO UPPER FRAME 68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH 

28700 FOR 57400 F

R 534127-01-4 832 842 

LINING REMOVED INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE INTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TO UPPER FRAME 68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH 

26400 FOR 52800 F

 534129-01-1 832 842 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT 

PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 66 WEB, LH/RH 

34800 FOR 60000 F

 534129-01-2 832 42 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT 

PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 66 WEB, LH/RH 

40200 FOR 60000 F

R 534129-01-3 832 842 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 66 WEB, LH/RH 

48000 FOR 96000 F

 534129-01-4 832 842 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT 

PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 66 WEB, LH/RH 

42300 FOR 60000 F

N 534129-01-5 832 842 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 66 WEB, LH/RH 

45500 FOR 91000 F

 534130-01-1 832 842 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT 

PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 68 WEB, LH/RH 

30600 FOR 60000 F

 534130-01-2 832 42 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT 

PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 68 WEB, LH/RH 

34100 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534130-01-3 832 842 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT 

PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 68 WEB, LH/RH 

40900 FOR 81800 F

 534130-01-4 832 842 

LINING REMOVED BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF AFT 

PASSENGER/CREW DOOR CUTOUT, DOOR STOP 

FITTINGS HOLES AT FRAME 68 WEB, LH/RH 

39800 FOR 60000 F

 534131-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND AFT PASSENGER/CREW DOOR CUTOUTS, BETWEEN FRAME 65 AND FRAME 70 AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE (EXCEPT AREA UNDER SCUFF PLATE), LH/RH 

23800 FOR 47600 F

 534131-01-3 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND AFT PASSENGER/CREW DOOR CUTOUTS, BETWEEN FRAME 65 AND FRAME 70 AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE (EXCEPT AREA UNDER SCUFF PLATE), LH/RH NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534131-01-1. 

23100 FOR 46200 F

 534131-01-4 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND AFT PASSENGER/CREW DOOR CUTOUTS, BETWEEN FRAME 65 AND FRAME 70 AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE (EXCEPT AREA UNDER SCUFF PLATE), LH/RH NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534131-01-1. 

23700 FOR 47400 F

 534131-01-5 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND AFT PASSENGER/CREW DOOR CUTOUTS, BETWEEN FRAME 65 AND FRAME 70 AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE (EXCEPT AREA UNDER SCUFF PLATE), LH/RH 

28200 F

 534132-01-1 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH 

12000 F

 534132-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534132-01-3 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534132-01-4 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND 

INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534132-01-1. 

16300 FOR 32600 F

 534132-01-5 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534132-01-2. 

15900 FOR 31800 F

 534132-01-6 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534132-01-3. 

12400 FOR 24800 F

 534132-01-7 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH 

11300 FOR 22600 F

 534132-01-8 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND 

INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH 

6200 FC OR 26900 F

 534132-01-9 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH 

6700 FC OR 20200 F

N 534132-01-10 832 842 DETAILED INSPECTION OF AFT PASSENGER/CREW 

DOOR CUTOUT, UPPER CORNERS, INCLUDING SKIN AND 

INTERNALLY THE VISIBLE PORTION OF THE INTERNAL 

DOUBLER, LH/RH 

11200 FOR 22400 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534137-01-1 N/A SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL 

DOUBLER, FORWARD AND AFT OF WASTE SERVICE PANEL CUTOUT, BETWEEN STRINGER 35 AND STRINGER 39, RH 

57700 FOR 115400 F

 534137-01-2 N/A SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL 

DOUBLER, FORWARD AND AFT OF WASTE SERVICE PANEL CUTOUT, BETWEEN STRINGER 35 AND STRINGER 39, RH 

38000 FOR 60000 F

 534137-01-3 N/A SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL 

DOUBLER, FORWARD AND AFT OF WASTE SERVICE PANEL CUTOUT, BETWEEN STRINGER 35 AND STRINGER 39, RH 

41900 FOR 60000 F

 534140-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE 

25900 F

R 534140-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME 

65 AND FRAME 66 AND FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE 

31700 FOR 60000 F

 534140-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534140-01-4 DELETED FROM ALS PART 2 AT REVISION 01 

R 534140-01-5 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME 

65 AND FRAME 66 AND FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534140-01-7. 

39600 FOR 60000 F

R 534140-01-6 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME 

65 AND FRAME 66 AND FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534140-01-3. 

38400 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534140-01-7 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME 

65 AND FRAME 66 AND FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534140-01-5. 

39500 FOR 60000 F

R 534140-01-8 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME 

65 AND FRAME 66 AND FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534140-01-1 OR 534140-01-4. 

35600 FOR 71200 F

R 534140-01-9 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND OUTFLOW VALVE CUTOUT, BETWEEN FRAME 

65 AND FRAME 66 AND FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE 

37700 FOR 60000 F

 534141-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND WATER SERVICE PANEL CUTOUT, BETWEEN 

FRAME 65 AND FRAME 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE 

29900 F

 534141-01-2 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE 

32700 FOR 60000 F

 534141-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534141-01-4 DELETED FROM ALS PART 2 AT REVISION 01 

R 534141-01-5 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534141-01-1. 

29600 FOR 59200 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534141-01-6 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534141-01-3. 

29700 FOR 59400 F

 534141-01-7 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE 

30500 FOR 60000 F

 534141-01-8 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534141-01-4. 

25700 FOR 51400 F

 534141-01-9 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE 

21900 FOR 43800 F

 534141-01-10 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND WATER SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE 

14700 FOR 63200 F

N 534141-01-11 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WATER SERVICE PANEL CUTOUT, BETWEEN FR 65 AND 

FR 66 AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE 

27500 FOR 55000 F

 534142-01-1 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE 

20900 FOR 47000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534142-01-2 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 

AND FRAME 66 AND FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE 

38000 FOR 60000 F

 534142-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534142-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534142-01-5 DELETED FROM ALS PART 2 AT REVISION 01  534142-01-6 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 

AND FRAME 66 AND FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534142-01-3. 

35000 FOR 60000 F

 534142-01-7 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 

AND FRAME 66 AND FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE 

35400 FOR 60000 F

 534142-01-8 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 

AND FRAME 66 AND FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534142-01-4. 

33000 FOR 60000 F

 534142-01-9 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 

AND FRAME 66 AND FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534142-01-5 OR 534142-01-

1. 

35400 FOR 70800 F

 534142-01-10 N/A DETAILED INSPECTION OF FUSELAGE SKIN AROUND 

WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66 AND FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE 

32300 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534142-01-11 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND WASTE SERVICE PANEL CUTOUT, BETWEEN 

FR 65 AND FR 66 AND FROM STRINGER 33 TO STRINGER 

40, RH, EXTERNAL SURFACE 

12900 FOR 55800 F

 534145-01-1 N/A SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE 

PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 47.5, FROM STRINGER 16, LH/RH, TO CROWN CENTER LINE 

28300 F

 534149-01-1 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREAS AT FR 47.5, 

FROM STRINGER 16, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE 

29000 F

 534152-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534152-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534152-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534152-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534153-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534153-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534153-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534154-01-1 252NW 826 

CEILING PANEL REMOVED LINING REMOVED BOLTS REMOVED INSULATION REMOVED REAR ACT REMOVED (IF INSTALLED) 

SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE STRUCTURE AT ATTACHMENT AREA UNDER AFT CARGO DOOR OUTER HINGE FITTINGS FROM FR 55 TO FR 56 BETWEEN STRINGER 22 AND STRINGER 23 

48000 FOR 96000 F

 534157-01-3 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 53 AND FR 55A, EXTERNAL PORTION (6 PLACES) 

13100 F

 534157-01-4 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 53 AND FR 55A, EXTERNAL PORTION (6 PLACES) 

14100 FOR 28300 F

 534157-01-5 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 56 AND FR 58A, EXTERNAL PORTION (6 PLACES) 

13100 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534157-01-6 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 53 AND FR 55A, EXTERNAL PORTION (6 PLACES) 

11400 F

 534157-01-7 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 56 AND FR 58A, EXTERNAL PORTION (6 PLACES) 

7500 FC OR 32300 F

R 534159-01-1 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

UPPER AND LOWER CORNERS, EXTERNAL SURFACE 

13400 FOR 26800 F

 534159-01-2 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

UPPER AND LOWER CORNERS, EXTERNAL SURFACE 

12000 FOR 51600 F

 534159-01-3 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

UPPER AND LOWER CORNERS, EXTERNAL SURFACE NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534159-01-1. 

12000 F

N 534159-01-4 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

UPPER AND LOWER CORNERS, EXTERNAL SURFACE 

11300 FOR 22600 F

 534160-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534160-01-4 DELETED FROM ALS PART 2 AT REVISION 01  534160-01-5 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

CUTOUT, VISIBLE PART OF LATERAL FR 55A AND FR 59 

1000 FC OR 4300 FH 

R 534160-02-1 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

VISIBLE PART OF LATERAL FR 52A AND FR 56 

1400 FC OR 2800 FH 

R 534160-02-2 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

VISIBLE PART OF LATERAL FR 55A AND FR 59 

1000 FC OR 2100 FH 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

N 534160-02-3 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

VISIBLE PART OF LATERAL FR 52A AND FR 56 

1100 FC OR 2200 FH 

 534161-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534163-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534163-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534163-01-3 DELETED FROM ALS PART 2 AT REVISION 01  534163-01-4 151GC 

REAR ACT(S) REMOVED (IF INSTALLED) 

GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATOR ATTACH BRACKET, BETWEEN FLOOR BEAMS AT FR 56, FR 57 AND FR 58 

11400 F

 534171-01-1 827 SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN OF BULK CARGO DOOR CUTOUT AT UPPER CORNERS 

10900 F

R 534171-01-2 827 SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN OF BULK CARGO DOOR CUTOUT AT UPPER CORNERS NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534171-01-3. 

21000 FOR 42100 F

 534171-01-3 DELETED FROM ALS PART 2 AT REVISION 01 

N 534171-01-4 827 SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE 

SKIN OF BULK CARGO DOOR CUTOUT AT UPPER CORNERS 

19900 FOR 39800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 534172-01-2 827 GENERAL VISUAL INSPECTION OF SEALING PROFILE OF 

BULK CARGO DOOR CUTOUT AT UPPER CORNERS 

15300 FOR 30600 F

 534172-01-3 827 GENERAL VISUAL INSPECTION OF SEALING PROFILE OF 

BULK CARGO DOOR CUTOUT AT UPPER CORNERS 

5000 FC 

 534183-01-1 N/A GENERAL VISUAL INSPECTION OF CIRCUMFERENTIAL 

JOINT ABOVE AFT EMERGENCY EXIT DOOR AT FR 47.3 FROM STRINGER 6 TO STRINGER 12, EXTERNAL SURFACE, LH/RH 

24000 F

 534199-02-1 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF THE CABIN SWIFT BROADBAND ANTENNA, 

IN THE AREA OF FR 57 TO FR 59, STGR 2 LH AND STGR 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME JUNCTIONS 

45600 FOR 60000 F

 534199-02-2 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF THE CABIN SWIFT BROADBAND ANTENNA, 

IN THE AREA OF FR 59 TO FR 61, STGR 2 LH AND STGR 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME JUNCTIONS 

33600 FOR 60000 F

 534199-02-4 LINING REMOVED 

INSULATION REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF THE CABIN SWIFT BROADBAND ANTENNA, 

IN THE AREA OF FR 59 TO FR 61, STGR 2 LH AND STGR 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME JUNCTIONS 

44800 FOR 60000 F

 534252-01-1 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 534253-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534257-01-2 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 58 AND FR 59A, EXTERNAL PORTION (4 PLACES) 

12200 F

 534257-01-3 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 58 AND FR 59A, EXTERNAL PORTION (4 PLACES) 

7500 FC OR 22500 F

 534260-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534260-01-3 826 GENERAL VISUAL INSPECTION OF AFT CARGO DOOR 

CUTOUT, VISIBLE PART OF LATERAL FR 57A AND FR 60 

1000 FC OR 3000 FH 

 534260-02-1 826 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 

VISIBLE PART OF LATERAL FR 57A AND FR 60 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534260-01-2. 

1400 FC OR 2800 FH 

 534261-01-1 DELETED FROM ALS PART 2 AT REVISION 01  534261-01-2 DELETED FROM ALS PART 2 AT REVISION 01  534261-01-3 DELETED FROM ALS PART 2 AT REVISION 01  535103-01-2 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND CUTOUT FOR TAIL COMPARTMENT ACCESS DOOR, BETWEEN FR 70 AND FR 73 AND BETWEEN STRINGER 25 RH AND BOTTOM CENTER LINE, EXTERNAL SURFACE 

17500 FOR 35000 F

 535103-01-3 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

AROUND CUTOUT FOR TAIL COMPARTMENT ACCESS DOOR, BETWEEN FR 70 AND FR 73 AND BETWEEN STRINGER 25 RH AND BOTTOM CENTER LINE, EXTERNAL SURFACE 

8900 FC OR 48100 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 535119-01-1 312AR DETAILED INSPECTION OF SHEAR TIES AND FRAME 

CLIPS AT FR 72 AND FR 74, BETWEEN STRINGER 3 AND STRINGER 9, LH/RH, INTERNAL STRUCTURE 

33100 FOR 66200 F

 535162-01-1 DELETED FROM ALS PART 2 AT REVISION 01  535162-01-2 323AL 323AR DETAILED INSPECTION OF FIN TO FUSELAGE, 

FORWARD, MID AND AFT ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RH 

34100 F

 545101-01-4 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR BOLTS REMOVED 

SPECIAL DETAILED INSPECTION (ROTO) OF PYLON 

FORWARD MOUNT FITTING AND SPIGOT FITTING 

12000 FOR 51600 F

 545102-01-4 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON 

FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES 

12000 FOR 51600 F

 545102-01-5 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON 

FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES 

23600 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 545102-01-6 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON 

FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES 

24000 FOR 42000 F

 545102-01-7 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON 

FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES NOTE: CREDIT CANNOT BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF MRB TASK 545102-01-1. 

24000 FOR 42000 F

R 545102-01-8 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES 

40200 FOR 60000 F

R 545102-01-9 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES 

15200 FOR 35900 F

 545102-01-10 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON 

FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 545102-01-6. 

24000 FOR 42000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 545102-01-11 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (US) OF PYLON 

FORWARD MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1, FORWARD AND AFT ATTACHMENT, BOLT HOLES NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 545102-01-6. 

24000 FOR 42000 F

 545103-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT 

FITTING, FORWARD OF RIB 1 

5700 FC 

R 545103-01-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING, FORWARD OF RIB 1 

8300 FC 

R 545103-01-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING, FORWARD OF RIB 1 

7400 FC 

 545103-01-4 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT 

FITTING, FORWARD OF RIB 1 

20000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 545103-01-5 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT 

FITTING, FORWARD OF RIB 1 

12000 F

 545103-01-6 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT 

FITTING, FORWARD OF RIB 1 

9400 FC OR 40700 F

 545103-01-7 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT 

FITTING, FORWARD OF RIB 1 

11800 FOR 50800 F

 545103-01-8 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF PYLON FORWARD MOUNT 

FITTING, FORWARD OF RIB 1 

11900 FOR 35900 F

N 545107-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF ENGINE AFT ATTACHMENT BEAM 

48000 FOR 80000 F

D 545107-01-4 DELETED FROM ALS PART 2 AT REVISION 02 N 545114-01-2 414FR 423FL 471AL 

472AR 481AL 482AR 

DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING LUGS AT RIB 4 

48000 FOR 80000 F

N 545114-01-5 471AL 471AR 471BL 

471BR 481AL 481AR 481BL 481BR 

DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING LUGS AT RIB 4 

48000 FOR 80000 F

D 545114-01-8 DELETED FROM ALS PART 2 AT REVISION 02 D 545114-01-9 DELETED FROM ALS PART 2 AT REVISION 02 N 545115-01-2 414FR 423FL 471AL 

472AR 481AL 482AR 521BT 621BT 

DETAILED INSPECTION OF PYLON TO WING FORWARD ATTACHMENT SHACKLES AT RIB 4 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-2. 

48000 FOR 80000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

N 545115-01-5 471AL 471AR 471BL 

471BR 481AL 481AR 481BL 481BR 521BT 621BT 

DETAILED INSPECTION OF PYLON TO WING FORWARD ATTACHMENT SHACKLES AT RIB 4 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-5. 

48000 FOR 80000 F

D 545115-01-8 DELETED FROM ALS PART 2 AT REVISION 02 D 545115-01-9 DELETED FROM ALS PART 2 AT REVISION 02 N 545115-02-2 414FR 423FL 471AL 

472AR 481AL 482AR 521BT 621BT 

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING FORWARD ATTACHMENT SHACKLES AT RIB 4 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-01-2. 

48000 FOR 80000 F

N 545115-02-5 471AL 471AR 471BL 

471BR 481AL 481AR 481BL 481BR 521BT 621BT 

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING FORWARD ATTACHMENT SHACKLES AT RIB 4 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-01-5. 

48000 FOR 80000 F

D 545115-02-8 DELETED FROM ALS PART 2 AT REVISION 02 D 545115-02-9 DELETED FROM ALS PART 2 AT REVISION 02 N 545120-01-2 471CL 472BR 475BL 

476BR 481BL 482CR 485BL 486BR 

DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING LUGS AT RIB 10 

48000 FOR 80000 F

N 545120-01-5 471CR 471DL 475BL 

475BR 481CL 481DR 485BL 485BR 

DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING LUGS AT RIB 10 

48000 FOR 80000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

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D 545120-01-7 DELETED FROM ALS PART 2 AT REVISION 02 D 545120-01-8 DELETED FROM ALS PART 2 AT REVISION 02 N 545123-01-2 471CL 472BR 475AL 

475BL 476AR 476BR 481BL 482CR 485AL 485BL 486AR 486BR 

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING AFT ATTACHMENT SHACKLES AT RIB 10 

48000 FOR 80000 F

N 545123-01-6 471CR 471DL 475AL 

475AR 475BL 475BR 481CL 481DR 485AL 485AR 485BL 485BR 

SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING AFT ATTACHMENT SHACKLES AT RIB 10 

48000 FOR 80000 F

D 545123-01-9 DELETED FROM ALS PART 2 AT REVISION 02 D 545123-01-10 DELETED FROM ALS PART 2 AT REVISION 02 R 545130-01-1 415BL 415BR 425BL 

425BR 

DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 5 

AND RIB 6, LH/RH 

20000 F

 545130-01-2 DELETED FROM ALS PART 2 AT REVISION 01 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 545130-01-3 415BL 415BR 425BL 

425BR 

DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 5 

AND RIB 6, LH/RH 

13000 F

 545130-01-4 415BL 415BR 425BL 

425BR 

DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 5 

AND RIB 6, LH/RH 

17000 F

R 545130-01-5 415BL 415BR 425BL 

425BR 

DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 5 

AND RIB 6, LH/RH 

19100 F

 545130-01-6 DELETED FROM ALS PART 2 AT REVISION 01  545130-01-7 DELETED FROM ALI DOCUMENT AT ISSUE 10  545130-01-8 DELETED FROM ALI DOCUMENT AT ISSUE 10 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 552007-01-1 N/A SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF 

ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH NOTE: THRESHOLD IS 6 YEARS SINCE THE DATE OF THE FIRST 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 YE NOTE 

 552007-01-2 N/A SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF 

ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH NOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-4. 

12 YE NOTE 

 552007-01-3 ELEVATOR REMOVED SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF 

ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH NOTE: THRESHOLD IS 6 YEARS SINCE THE DATE OF THE FIRST 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 YE NOTE 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 552007-01-4 ELEVATOR REMOVED SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF 

ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH NOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-2. 

12 YE NOTE 

 562101-01-1 DELETED FROM ALI DOCUMENT AT ISSUE 7 

R 571101-02-1 734 744 SPECIAL DETAILED INSPECTION (HFEC) OF CENTER 

WING BOX, REAR SPAR, SYSTEM HOLES NEAR MAN HOLES 

37200 FOR 74400 F

 571134-01-1 191BB 191CT 191EB 

191KB 191LB 192CT 192EB 192FB 192KB 192LB 195AB 196AB 734 744 

DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN LOWER SURFACE, FROM STRINGER 11 TO STRINGER 15, BETWEEN Y=+/-1292, AS FAR AS VISIBLE 

32800 FOR 65600 F

R 571134-01-6 191BB 191CT 191EB 

191KB 191LB 192CT 192EB 192FB 192KB 192LB 195AB 196AB 734 744 

DETAILED INSPECTION OF CENTER WING BOX, BOTTOM 

SKIN LOWER SURFACE, FROM STRINGER 11 TO STRINGER 15, BETWEEN Y=+/-1292, AS FAR AS VISIBLE 

32800 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 571135-01-1 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN UPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6 TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11 TO STRINGER 15, BETWEEN Y=+/-1292 

32800 FOR 65600 F

R 571135-01-6 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, BOTTOM 

SKIN UPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6 TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11 TO STRINGER 15, BETWEEN Y=+/-1292 

32800 FOR 60000 F

R 571136-01-1 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON BOTTOM SKIN, UPPER SURFACE (12 

PLACES) 

36900 FOR 73900 F

R 571136-01-2 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON BOTTOM SKIN, UPPER SURFACE (12 

PLACES) 

20000 FOR 41700 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 571136-01-3 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON BOTTOM SKIN, UPPER SURFACE (12 

PLACES) 

19900 FOR 36200 F

R 571136-01-4 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON BOTTOM SKIN, UPPER SURFACE (12 

PLACES) 

16500 FOR 71200 F

R 571136-01-5 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON BOTTOM SKIN, UPPER SURFACE (12 

PLACES) 

20000 FOR 48000 F

 571164-01-1 CABIN FLOOR 

PANELS REMOVED LINING REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF CENTER WING BOX, UPPER PANEL, ENDS OF FLOOR BEAM, AFT FLANGE (6 PLACES) 

25400 FOR 50800 F

 571164-01-2 CABIN FLOOR 

PANELS REMOVED LINING REMOVED INSULATION REMOVED 

DETAILED INSPECTION OF CENTER WING BOX, UPPER PANEL, ENDS OF FLOOR BEAM, AFT FLANGE (6 PLACES) 

29900 FOR 48000 F

R 571170-01-1 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

34000 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REV 

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 571170-01-2 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

21000 FOR 42000 F

R 571170-01-3 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

35000 FOR 60000 F

R 571170-01-4 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

23900 FOR 42000 F

 571170-01-5 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

10100 FOR 43600 F

R 571170-01-6 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

34100 FOR 60000 F

R 571170-01-7 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

24000 FOR 48000 F

N 571170-01-8 191DT 191ET 192DT 

192ET 

SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH 

21000 FOR 42000 F

 571181-01-1 147AZ 148AZ 734 

744 FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF CWB, UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RH 

29600 FOR 59300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REV 

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 571181-01-6 147AZ 148AZ 734 

744 FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF CWB, UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND 

FR 42, LH/RH 

24000 FOR 53800 F

 571182-01-1 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WB, UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RH 

29600 FOR 59300 F

R 571182-01-6 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WB, UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RH 

24000 FOR 53800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 571183-01-1 191LB 192LB 734 

744 

SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42, LH/RH 

29600 FOR 59300 F

R 571183-01-5 191LB 192LB 734 

744 

SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42, LH/RH 

24000 FOR 37100 F

R 571185-01-1 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX (HOLES ON) UPPER HALF OF VERTICAL TEE 

FITTING AT JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH 

29000 FOR 60000 F

 571185-01-2 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX (HOLES ON) UPPER HALF OF VERTICAL TEE FITTING AT JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH 

34600 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 571185-01-3 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX (HOLES ON) UPPER HALF OF VERTICAL TEE 

FITTING AT JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH 

20000 FOR 52900 F

 571185-01-4 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX (HOLES ON) UPPER HALF OF VERTICAL TEE FITTING AT JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH 

24000 FOR 42000 F

R 571185-01-5 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX (HOLES ON) UPPER HALF OF VERTICAL TEE 

FITTING AT JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH 

24000 FOR 42000 F

R 571185-01-7 540AB 540AZ 540BZ 

640AB 640AZ 640BZ FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX (HOLES ON) UPPER HALF OF VERTICAL TEE 

FITTING AT JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH 

20000 FOR 57000 F

 571189-01-1 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, 

STRINGER WEB AT JUNCTION WITH STRUT ATTACH FITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16 

22900 FOR 48000 F

R 571189-01-3 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, STRINGER WEB AT JUNCTION WITH STRUT ATTACH FITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16 

22600 FOR 59900 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 571189-01-5 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, 

STRINGER WEB AT JUNCTION WITH STRUT ATTACH FITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 571189-01-1. 

16900 FOR 33800 F

R 571189-01-7 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, STRINGER WEB AT JUNCTION WITH STRUT ATTACH FITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16 

20200 FOR 53600 F

 571190-01-1 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, FRAME FEET, UPPER FLANGE AT JUNCTION WITH CROWN FITTING ON FR 37 TO FR 41 

30300 FOR 60600 F

 571190-01-2 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, FRAME FEET, UPPER FLANGE AT JUNCTION WITH CROWN FITTING ON FR 37 TO FR 41 

28900 FOR 48000 F

 571192-01-1 147AZ 148AZ 734 

744 FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, REAR SPAR, EDGE OF LOWER FLANGE AT CORNER FITTING, LH/RH 

21400 FOR 42800 F

 571192-01-2 147AZ 148AZ 734 

744 FASTENER SEALANT REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, REAR SPAR, EDGE OF LOWER FLANGE AT CORNER FITTING, LH/RH 

17800 FOR 45400 F

R 572004-01-1 540AB 540AZ 540BB 

540CB 640AB 640AZ 640BB 640CB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA INSIDE THE DRY BAY 

60000 FOR 120000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572004-01-2 540AB 540AZ 540BB 

540CB 640AB 640AZ 640BB 640CB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA INSIDE THE DRY BAY 

44000 FOR 60000 F

R 572004-01-4 540AB 540AZ 540BB 

540CB 640AB 640AZ 640BB 640CB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA INSIDE THE DRY BAY 

39800 FOR 60000 F

N 572004-01-5 540AB 540AZ 540BB 

540CB 640AB 640AZ 640BB 640CB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA INSIDE THE DRY BAY 

34200 FOR 68400 F

N 572004-01-6 540AB 540AZ 540BB 

540CB 640AB 640AZ 640BB 640CB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA INSIDE THE DRY BAY 

27500 FOR 55000 F

 572004-03-1 DELETED FROM ALI DOCUMENT AT ISSUE 10  572007-01-1 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

12500 FOR 20500 F

R 572007-01-2 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

11900 FOR 23800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

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REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572007-01-3 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

11200 FOR 18400 F

R 572007-01-4 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

10800 FOR 17700 F

R 572007-01-5 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

9600 FC OR 15800 F

 572007-01-6 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

10600 FOR 45500 F

R 572007-01-8 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

10600 FOR 17400 F

N 572007-01-9 N/A DETAILED INSPECTION OF OUTER WING, REAR SPAR 

AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE 

10500 FOR 21000 F

N 572008-01-4 574AB 574BB 674AB 

674BB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6 

21300 FOR 42600 F

N 572009-01-1 540AB 540BB 540BZ 

640AB 640BB 640BZ 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR SPAR FORWARD FACE, AT THE ATTACHMENT 

HOLES OF GEAR SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND RETRACTION JACK FITTING 

48000 FOR 96000 F

N 572009-01-2 540AB 540BB 540BZ 

640AB 640BB 640BZ 

SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR SPAR FORWARD FACE, AT THE ATTACHMENT 

HOLES OF GEAR SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND RETRACTION JACK FITTING 

32800 FOR 65600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

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AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572010-01-1 540AB 540BZ 640AB 

640BZ 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, UPPER AND LOWER ROOT JOINT FITTING 

36200 FOR 48000 F

R 572010-01-4 540AB 540BZ 640AB 

640BZ 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, UPPER AND LOWER ROOT JOINT FITTING 

58600 FOR 117200 F

 572010-01-5 540AB 540BZ 640AB 

640BZ 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, UPPER AND LOWER ROOT JOINT FITTING 

36200 FOR 60000 F

 572010-01-6 540AB 540BZ 640AB 

640BZ 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, UPPER AND LOWER ROOT JOINT FITTING 

34100 FOR 60000 F

R 572010-01-7 540AB 540BZ 640AB 

640BZ 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, UPPER AND LOWER ROOT JOINT FITTING 

35200 FOR 60000 F

N 572010-01-10 540AB 540BZ 640AB 

640BZ 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, UPPER AND LOWER ROOT JOINT FITTING 

44300 FOR 88600 F

R 572011-01-1 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

32900 FOR 48000 F

R 572011-01-2 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

32400 FOR 64800 F

R 572011-01-3 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

30000 FOR 60000 F

R 572011-01-4 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

30000 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572011-01-5 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

32900 FOR 60000 F

R 572011-01-6 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

32400 FOR 53300 F

R 572011-01-7 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

9000 FC OR 38700 F

N 572011-01-8 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

31500 FOR 63000 F

N 572011-01-9 540AB 540BB 540BZ 

540CB 640AB 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES 

18600 FOR 37200 F

R 572012-01-1 N/A DETAILED INSPECTION OF OUTER WING, TOP SKIN 

UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 1 AND RIB 8 

59600 FOR 119200 F

R 572014-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, TOP 

SKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR 

48300 FOR 96600FH 

 572014-01-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, TOP 

SKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR 

42700 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572014-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, TOP 

SKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR 

42800 FOR 60000 F

R 572020-01-1 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT STRAP, AT STRINGER 11, EXCLUDING 

THE AREA INSIDE THE DRY BAY 

33900 FOR 67800 F

 572020-01-3 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE 

DRY BAY 

33900 FOR 60000 F

 572020-01-4 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE 

DRY BAY 

38400 FOR 60000 F

 572020-01-5 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE 

DRY BAY 

41800 FOR 60000 F

 572020-01-6 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE 

DRY BAY 

33000 FOR 60000 F

 572020-01-7 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE 

DRY BAY 

32000 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572020-01-9 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT STRAP, AT STRINGER 11, EXCLUDING 

THE AREA INSIDE THE DRY BAY 

33900 FOR 60000 F

N 572020-01-10 540AB 540AZ 540BB 

540BZ 640AB 640AZ 640BB 640BZ 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT STRAP, AT STRINGER 11, EXCLUDING 

THE AREA INSIDE THE DRY BAY 

36700 FOR 73400 F

 572020-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 10  572026-01-1 DELETED FROM ALS PART 2 AT REVISION 01  572026-01-3 540AB 540BB 640AB 

640BB 

DETAILED INSPECTION OF OUTER WING, RIB 5, AFT OF BOLTED PANEL 

28400 FOR 48000 F

R 572026-01-6 540AB 540BB 640AB 

640BB 

DETAILED INSPECTION OF OUTER WING, RIB 5, AFT OF BOLTED PANEL NOTE: CREDIT CAN BE TAKN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572026-01-1. 

38300 FOR 60000 F

R 572032-01-1 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING 

60000 FOR 120000 F

 572032-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING 

24000 FOR 42000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572032-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING 

18000 FOR 31200 F

 572032-01-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING 

16800 FOR 72300 F

R 572032-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING 

24000 FOR 42000 F

 572032-01-6 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING 

24000 FOR 42000 F

R 572033-01-1 540AB 540BB 640AB 

640BB 

SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY MLG REINFORCING PLATE, INCLUDING ATTACHMENT TO REAR SPAR 

48000 FOR 96000 F

 572034-01-1 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE MLG REINFORCING PLATE 

31700 FOR 51400 F

 572034-01-2 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKINLOWER SURFACE MLG REINFORCING PLATE 

32700 FOR 53000 F

 572034-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE MLG REINFORCING PLATE 

32700 FOR 53000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572034-01-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE MLG REINFORCING PLATE 

27500 FOR 44700 F

D 572034-01-5 DELETED FROM ALS PART 2 AT REVISION 02 

 572034-01-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE MLG REINFORCING PLATE 

15400 FOR 66300 F

R 572034-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE MLG REINFORCING PLATE 

25000 FOR 40500 F

 572036-01-1 531AB 531BB 531CB 

631AB 631BB 631CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, FORWARD OF REAR SPAR IN AREA 

COVERED BY FLAP TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR 

41500 FOR 48000 F

R 572036-01-2 531AB 531BB 531CB 

631AB 631BB 631CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, FORWARD OF REAR SPAR IN AREA 

COVERED BY FLAP TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR 

60000 FOR 120000 F

 572036-01-3 531CB 531EB 631CB 

631EB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, FORWARD OF REAR SPAR IN AREA 

COVERED BY FLAP TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR 

35800 FOR 60000 F

 572036-01-4 531CB 531EB 631CB 

631EB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, FORWARD OF REAR SPAR IN AREA 

COVERED BY FLAP TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR 

28700 FOR 49800 F

 572036-01-5 531AB 531BB 531CB 

631AB 631BB 631CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, FORWARD OF REAR SPAR IN AREA 

COVERED BY FLAP TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR 

36500 FOR 60000 F

R 572036-01-7 531AB 531BB 531CB 

631AB 631BB 631CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, FORWARD OF REAR SPAR IN AREA 

COVERED BY FLAP TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR 

35800 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572038-01-1 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6), STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10 (RIB BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND STRINGER 15 (RIB BAY 2-3) 

54600 FOR 109200 F

 572038-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6), STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10 (RIB BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND STRINGER 15 (RIB BAY 2-3) 

24000 FOR 41700 F

 572040-03-1 540AB 540BB 640AB 

640BB 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER 

WING, BOTTOM SKIN, UPPER AND LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7 

41600 FOR 60000 F

R 572040-03-4 540AB 540BB 640AB 

640BB 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, BOTTOM SKIN, UPPER AND LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7 

51900 FOR 103800 F

R 572041-02-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, 

LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FAIRINGS AND REINFORCING PLATES 

31200 FOR 62400 F

R 572041-02-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, 

LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FAIRINGS AND REINFORCING PLATES 

31200 FOR 50700 F

 572041-02-6 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, 

LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FAIRINGS AND REINFORCING PLATES 

42800 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572041-02-7 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, 

LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FAIRINGS AND REINFORCING PLATES 

37600 FOR 60000 F

 572041-02-8 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, 

LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FAIRINGS AND REINFORCING PLATES 

36200 FOR 58800 F

 572041-02-9 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, 

LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FAIRINGS AND REINFORCING PLATES 

42400 FOR 60000 F

 572041-02-10 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, 

LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FAIRINGS AND REINFORCING PLATES 

39600 FOR 60000 F

 572042-01-1 PYLON FAIRINGS 

REMOVED 

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN AREA COVERED BY PYLON 

FAIRING 

24000 FOR 42000 F

R 572042-01-2 PYLON FAIRINGS 

REMOVED 

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN AREA COVERED BY PYLON 

FAIRING 

37300 FOR 74600 F

 572042-01-3 PYLON FAIRINGS 

REMOVED 

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN AREA COVERED BY PYLON 

FAIRING 

22500 FOR 36600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572042-01-4 PYLON FAIRINGS 

REMOVED 

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN AREA COVERED BY PYLON 

FAIRING 

24000 FOR 42000 F

 572042-01-6 PYLON FAIRINGS 

REMOVED 

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN AREA COVERED BY PYLON 

FAIRING 

14700 FOR 63400 F

R 572042-01-7 PYLON FAIRINGS 

REMOVED 

GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN AREA COVERED BY PYLON 

FAIRING NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572042-01-2. 

24000 FOR 42000 F

 572044-01-1 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY REINFORCING 

PLATES AND FAIRINGS 

29000 FOR 47100 F

R 572044-01-2 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY REINFORCING PLATES AND FAIRINGS 

38000 FOR 76000 F

 572044-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY REINFORCING 

PLATES AND FAIRINGS 

26300 FOR 42800 F

 572044-01-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY REINFORCING 

PLATES AND FAIRINGS 

19100 FOR 31000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572044-01-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY REINFORCING 

PLATES AND FAIRINGS 

29000 FOR 47100 F

 572044-01-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY REINFORCING 

PLATES AND FAIRINGS 

12700 FOR 54600 F

R 572044-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS COVERED BY REINFORCING PLATES AND FAIRINGS 

22600 FOR 36800 F

 572047-01-2 PYLON FAIRINGS 

REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER 

WING, BOTTOM SKIN LOWER SURFACE AROUND AFT PYLON ATTACHMENT FITTING CUTOUT 

42500 FOR 60000 F

 572049-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 9  572049-02-2 DELETED FROM ALI DOCUMENT AT ISSUE 9  572049-02-3 DELETED FROM ALI DOCUMENT AT ISSUE 9  572049-02-4 DELETED FROM ALI DOCUMENT AT ISSUE 9  572049-02-5 DELETED FROM ALI DOCUMENT AT ISSUE 10  572050-01-1 540AB 540BB 540CZ 

540DZ 640AB 640BB 640CZ 640DZ 

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-1. 

25000 FOR 44800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572050-01-2 540AB 540BB 540CZ 

540DZ 640AB 640BB 640CZ 640DZ 

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-2. 

12700 FOR 54600 F

 572050-01-3 540AB 540BB 540CZ 

540DZ 640AB 640BB 640CZ 640DZ 

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-3. 

28100 FOR 48000 F

R 572050-01-4 540AB 540BB 540CZ 

540DZ 640AB 640BB 640CZ 640DZ 

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-4. 

29800 FOR 59600 F

 572050-01-5 540AB 540BB 540CZ 

540DZ 640AB 640BB 640CZ 640DZ 

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-5. 

28700 FOR 51400 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572050-01-6 540AB 540BB 540CZ 

540DZ 640AB 640BB 640CZ 640DZ 

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-6. 

28700 FOR 51400 F

 572050-01-7 540AB 540BB 540CZ DETAILED INSPECTION OF OUTER WING, DRY BAY AREA

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-7. 

28100 FOR 48000 F

R 572050-01-8 540AB 540BB 540CZ 

540DZ 640AB 640BB 640CZ 640DZ 

DETAILED INSPECTION OF OUTER WING, DRY BAY AREANOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-8. 

25000 FOR 44800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572050-02-1 521AZ 521BZ 521EB 

621AZ 621BZ 621EB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-1. 

25000 FOR 44800 F

 572050-02-2 521AZ 521BZ 521EB 

621AZ 621BZ 621EB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-2. 

12700 FOR 54600 F

 572050-02-3 521AZ 521BZ 521EB 

621AZ 621BZ 621EB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-3. 

28100 FOR 48000 F

R 572050-02-4 521AZ 521BZ 521EB 

621AZ 621BZ 621EB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-4. 

29800 FOR 59600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572050-02-5 521AZ 521BZ 521EB 

621AZ 621BZ 621EB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-5. 

28700 FOR 51400 F

 572050-02-6 521AZ 521BZ 521EB 

621AZ 621BZ 621EB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-6. 

28700 FOR 51400 F

 572050-02-7 521AZ 521EB SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-7. 

28100 FOR 48000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572050-02-8 521AZ 521BZ 521EB 

621AZ 621BZ 621EB 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER WING, DRY BAY AREA NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-8. 

25000 FOR 44800 F

 572053-01-1 540AB 540AZ 540BB 

540BZ 540CB 640AB 640AZ 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY 

28100 FOR 48000 F

R 572053-01-2 540AB 540AZ 540BB 

540BZ 540CB 640AB 640AZ 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY 

37300 FOR 74600 F

 572053-01-3 540AB 540AZ 540BB 

540BZ 540CB 640AB 640AZ 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY 

28700 FOR 51400 F

 572053-01-4 540AB 540AZ 540BB 

540BZ 540CB 640AB 640AZ 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY 

12700 FOR 54600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572053-01-5 540AB 540AZ 540BB 

540BZ 540CB 640AB 640AZ 640BB 640BZ 640CB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572053-01-2. 

25000 FOR 44800 F

 572053-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 10 

R 572054-01-1 FUEL PUMP 

REMOVED 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT FUEL PUMP APERTURES BETWEEN RIB 1 AND RIB 2 

49700 FOR 99400 F

N 572054-01-8 FUEL PUMP 

REMOVED 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT FUEL PUMP APERTURES BETWEEN RIB 1 AND RIB 2 

24700 FOR 49400 F

R 572101-01-1 522AB 522CB 522EB 

522FB 522HB 522JB 522KB 522LB 522NB 522QB 622AB 622CB 622EB 622FB 622HB 622JB 622KB 622LB 622NB 622QB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS 

43000 FOR 86000 F

R 572101-01-7 522AB 522CB 522EB 

522FB 522HB 522JB 522KB 522LB 522NB 522QB 622AB 622CB 622EB 622FB 622HB 622JB 622KB 622LB 622NB 622QB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572101-01-1. 

33300 FOR 55100 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

N 572101-01-8 522AB 522CB 522EB 

522FB 522HB 522JB 522KB 522LB 522NB 522QB 622AB 622CB 622EB 622FB 622HB 622JB 622KB 622LB 622NB 622QB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS 

30500 FOR 61000 F

 572108-01-1 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

33100 FOR 48000 F

R 572108-01-2 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

35700 FOR 71400 F

 572108-01-4 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

31000 FOR 51200 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572108-01-5 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

27100 FOR 44700 F

 572108-01-6 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

29500 FOR 48700 F

 572108-01-7 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

17100 FOR 73800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

N 572108-01-8 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

30300 FOR 60600 F

N 572108-01-9 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 8 AND RIB 22 

24200 FOR 48400 F

N 572109-01-5 550AB 550BB 550CB 

550DB 650AB 650BB 650CB 650DB 560AB 660AB 

DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN RIB 22 AND RIB 27 

33900 FOR 67800 F

 572111-01-1 DELETED FROM ALS PART 2 AT REVISION 01  572111-01-2 573CB 573EB 573FB 

575AB 673CB 673EB 673FB 675AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, FROM RIB 8 TO RIB 11 

21800 FOR 35800 F

 572111-01-3 573CB 573EB 573FB 

575AB 673CB 673EB 673FB 675AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, FROM RIB 8 TO RIB 11 

24000 FOR 42000 F

 572111-01-4 573CB 573EB 573FB 

575AB 673CB 673EB 673FB 675AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, FROM RIB 8 TO RIB 11 

15900 FOR 68300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572111-01-6 573CB 573EB 573FB 

575AB 673CB 673EB 673FB 675AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, FROM RIB 8 TO RIB 11 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572111-01-1. 

21800 FOR 35800 F

R 572112-01-1 575BB 575CB 575DB 

575EB 575FB 575GB 575HB 575KB 575LB 575MB 675BB 675CB 675DB 675EB 675FB 675GB 675HB 675KB 675LB 675MB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT PLATE AT RIB 22 

21000 FOR 42000 F

 572112-01-2 575BB 575CB 575DB 

575EB 575FB 575GB 575HB 575KB 575LB 575MB 675BB 675CB 675DB 675EB 675FB 675GB 675HB 675KB 675LB 675MB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT PLATE AT RIB 22 

22800 FOR 40300 F

 572112-01-3 575BB 575CB 575DB 

575EB 575FB 575GB 575HB 575KB 575LB 575MB 675BB 675CB 675DB 675EB 675FB 675GB 675HB 675KB 675LB 675MB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT PLATE AT RIB 22 

24000 FOR 42000 F

 572112-01-4 DELETED FROM ALI DOCUMENT AT ISSUE 10 

R 572112-01-6 575BB 575CB 575DB 

575EB 575FB 575GB 575HB 575KB 575LB 575MB 675BB 675CB 675DB 675EB 675FB 675GB 675HB 675KB 675LB 675MB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT PLATE AT RIB 22 

21000 FOR 37200 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572114-01-1 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

32900 FOR 48000 F

 572114-01-2 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

37100 FOR 60000 F

 572114-01-3 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

30100 FOR 49400 F

R 572114-01-4 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

30100 FOR 60200 F

 572114-01-5 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

38900 FOR 60000 F

R 572114-01-6 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

30100 FOR 49400 F

N 572114-01-8 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

32500 FOR 65000 F

N 572114-01-9 540CB 540DB 540EB 

640CB 640DB 640EB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND BOTTOM FLANGES 

21100 FOR 42200 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572115-01-2 540FB 540GB 540HB 

540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES 

43200 FOR 86400 F

 572115-01-3 540FB 540GB 540HB 

540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES 

35600 FOR 58100 F

 572115-01-4 540FB 540GB 540HB 

540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES 

34600 FOR 56400 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572115-01-6 540FB 540GB 540HB 

540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES 

24600 FOR 40100 F

N 572115-01-8 540FB 540GB 540HB 

540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES 

11100 FOR 22200 F

N 572115-01-9 540FB 540GB 540HB 

540JB 540KB 540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES 

33500 FOR 67000 F

R 572116-02-1 N/A DETAILED INSPECTION OF OUTER WING, TOP SKIN, 

UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 8 AND RIB 22 

58800 FOR 117600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572120-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, TOP 

SKIN, UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN RIB 8 AND RIB 27 FROM FRONT SPAR TO REAR SPAR 

51700 FOR 103400 F

R 572123-01-1 540CB 540DB 540EB 

540FB 540GB 640CB 640DB 640EB 640FB 640GB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN, STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8 AND RIB 9 AND BUTT STRAP AT STRINGER 11 

53200 FOR 106400 F

N 572123-01-4 540CB 540DB 540EB 

540FB 540GB 640CB 640DB 640EB 640FB 640GB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN, STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8 AND RIB 9 AND BUTT STRAP AT STRINGER 11 

37500 FOR 75000 F

 572124-01-1 540HB 540JB 540KB 

540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18 

39900 FOR 48000 F

R 572124-01-3 540HB 540JB 540KB 

540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18 

53300 FOR 106600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572124-01-4 540HB 540JB 540KB 

540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18 

44700 FOR 60000 F

 572124-01-5 540HB 540JB 540KB 

540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18 

42900 FOR 60000 F

 572124-01-6 540HB 540JB 540KB 

540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18 

17800 FOR 76600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572124-01-7 540HB 540JB 540KB 

540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18 

43000 FOR 60000 F

N 572124-01-8 540HB 540JB 540KB 

540LB 540MB 540NB 540PB 540QB 540RB 550AB 550BB 550CB 550DB 560AB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18 

40300 FOR 80600 F

 572129-01-1 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3 FAIRING 

28900 FOR 50200 F

 572129-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3 FAIRING 

38000 FOR 60000 F

 572129-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENTS, TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3 FAIRING 

32400 FOR 56300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572129-01-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3 FAIRING 

45700 FOR 91400 F

 572129-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3 FAIRING 

14800 FOR 63600 F

R 572129-01-6 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3 FAIRING 

41400 FOR 60000 F

 572130-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

35600 FOR 60000 F

 572130-01-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

38000 FOR 60000 F

 572130-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

36700 FOR 60000 F

R 572130-01-6 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

46000 FOR 60000 F

R 572130-01-7 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR, BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

46000 FOR 92000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572134-01-1 540FB 540GB 540NB 

540PB 640FB 640GB 640NB 640PB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR SPAR 

35500 FOR 48000 F

R 572134-01-2 540FB 540GB 540NB 

540PB 640FB 640GB 640NB 640PB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR SPAR 

53500 FOR 107000 F

 572134-01-4 540FB 540GB 540NB 

540PB 640FB 640GB 640NB 640PB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR SPAR 

32000 FOR 60000 F

 572134-01-5 540FB 540GB 540NB 

540PB 640FB 640GB 640NB 640PB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR SPAR 

28300 FOR 60000 F

 572134-01-6 540FB 540GB 540NB 

540PB 640FB 640GB 640NB 640PB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR SPAR 

16400 FOR 70500 F

R 572134-01-7 540FB 540GB 540NB 

540PB 640FB 640GB 640NB 640PB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR SPAR 

29300 FOR 60000 F

 572137-01-1 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

24000 FOR 42000 F

R 572137-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

58200 FOR 116400 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572137-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

24000 FOR 42000 F

 572137-01-4 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

24000 FOR 42000 F

 572137-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

24000 FOR 42000 F

R 572137-01-6 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

19700 FOR 33400 F

 572137-01-7 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

10500 FOR 45100 F

 572137-01-8 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY 19-20) AND STRINGER 12 (RIB BAY 17-18) 

24000 FOR 42000 F

R 572139-02-1 540CB 540DB 540EB 

540FB 540GB 640CB 640DB 640EB 640FB 640GB 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND 12-13 

52800 FOR 105600 F

 572140-02-2 DELETED FROM ALS PART 2 AT REVISION 01  572140-02-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB 27 

40900 FOR 60000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572140-02-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB 27 

42900 FOR 85800 F

R 572140-02-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB 27 

34200 FOR 60000 F

 572140-02-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB 27 

9000 FC OR 38700 F

 572142-01-1 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND FLAP TRACK 3 FAIRING 

24000 FOR 42000 F

R 572142-01-2 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND FLAP TRACK 3 

FAIRING 

48300 FOR 96600 F

 572142-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND FLAP TRACK 3 FAIRING 

24000 FOR 42000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572142-01-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREAS COVERED BY PYLONFAIRING AND FLAP TRACK 3 FAIRING 

19900 FOR 33900 F

 572142-01-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREAS COVERED BY PYLONFAIRING AND FLAP TRACK 3 FAIRING 

42700 FOR 60000 F

 572142-01-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND FLAP TRACK 3 FAIRING 

12400 FOR 53300 F

R 572142-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND FLAP TRACK 3 

FAIRING 

24000 FOR 42000 F

 572143-01-1 532AB 532BB 532CB 

532DB 533AB 533BB 533CB 533DB 632AB 632BB 632CB 632DB 633AB 633BB 633CB 633DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA COVERED BY FLAP TRACK 3 

FAIRING AND FLAP TRACK 4 FAIRING 

35800 FOR 48000 F

R 572143-01-2 532AB 532BB 532CB 

532DB 533AB 533BB 533CB 533DB 632AB 632BB 632CB 632DB 633AB 633BB 633CB 633DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA COVERED BY FLAP TRACK 3 

FAIRING AND FLAP TRACK 4 FAIRING 

53500 FOR 107000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572143-01-3 532CB 532EB 533CB 

533EB 632CB 632EB 633CB 633EB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA COVERED BY FLAP TRACK 3 

FAIRING AND FLAP TRACK 4 FAIRING 

39200 FOR 60000 F

 572143-01-4 532AB 532BB 532CB 

532DB 533AB 533BB 533CB 533DB 632AB 632BB 632CB 632DB 633AB 633BB 633CB 633DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA COVERED BY FLAP TRACK 3 

FAIRING AND FLAP TRACK 4 FAIRING 

17800 FOR 76500 F

R 572143-01-5 532AB 532BB 532CB 

532DB 533AB 533BB 533CB 533DB 632AB 632BB 632CB 632DB 633AB 633BB 633CB 633DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA COVERED BY FLAP TRACK 3 FAIRING AND FLAP TRACK 4 FAIRING NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572143-01-2. 

31700 FOR 54000 F

R 572144-01-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING , 

BOTTOM SKIN, LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS BETWEEN RIB 15 AND RIB 27 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREA 

COVERED BY FLAP TRACK 4 FAIRING. 

50800 FOR 101600 F

 572148-01-1 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

24000 FOR 42000 F

R 572148-01-2 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

48300 FOR 96600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572148-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

24000 FOR 40400 F

 572148-01-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

19900 FOR 32300 F

 572148-01-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

24000 FOR 39000 F

 572148-01-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

24000 FOR 39000 F

 572148-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

24000 FOR 42000 F

 572148-01-8 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

12100 FOR 52300 F

R 572148-01-9 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 

21700 FOR 35300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572149-01-1 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

40000 FOR 48000 F

R 572149-01-2 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

56500 FOR 113000 F

 572149-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

25800 FOR 42000 F

 572149-01-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

27000 FOR 43900 F

R 572149-01-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

32200 FOR 52300 F

 572149-01-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

32200 FOR 53300 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572149-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

12600 FOR 54400 F

R 572149-01-8 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING 

22600 FOR 36700 F

 572150-01-1 532AB 532BB 532CB 

532DB 632AB 632BB 632CB 632DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREA COVERED BY FLAP TRACK 3 FAIRING 

29500 FOR 48000 F

R 572150-01-2 532AB 532BB 532CB 

532DB 632AB 632BB 632CB 632DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS COVERED BY FLAP TRACK 3 FAIRING 

53500 FOR 107000 F

 572150-01-3 532AB 532BB 532CB 

532DB 632AB 632BB 632CB 632DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREA COVERED BY FLAP TRACK 3 FAIRING 

24000 FOR 42000 F

 572150-01-4 532CB 532EB 632CB 

632EB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREA COVERED BY FLAP TRACK 3 FAIRING 

24000 FOR 42000 F

 572150-01-5 532CB 532EB 632CB 

632EB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS COVERED BY FLAP TRACK 3 FAIRING 

24000 FOR 40700 F

 572150-01-6 532AB 532BB 532CB 

532DB 632AB 632BB 632CB 632DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREA COVERED BY FLAP TRACK 3 FAIRING 

12500 FOR 53700 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572150-01-7 532AB 532BB 532CB 

532DB 632AB 632BB 632CB 632DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS COVERED BY FLAP TRACK 3 FAIRING 

24000 FOR 42000 F

R 572151-01-2 533AB 533BB 533CB 

533DB 633AB 633BB 633CB 633DB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA COVERED BY FLAP TRACK 4 FAIRING 

56500 FOR 113000 F

R 572155-01-1 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 21 

48300 FOR 96600 F

 572155-01-2 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 21 

22500 FOR 42800 F

R 572155-01-3 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 21 

30500 FOR 58100 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572155-01-4 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 21 

22800 FOR 42000 F

R 572155-01-5 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 21 

30500 FOR 58100 F

 572155-01-6 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 21 

16000 FOR 68800 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572155-01-7 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 540NB 540PB 540QB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 640NB 640PB 640QB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11, BETWEEN RIB 8 AND RIB 21 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572155-01-1. 

28700 FOR 54600 F

 572158-01-1 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 

AND 13 

29900 FOR 48000 F

R 572158-01-2 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 AND 13 

48300 FOR 96600 F

 572158-01-3 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 

AND 13 

24000 FOR 42000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 572158-01-4 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 

AND 13 

24000 FOR 42000 F

 572158-01-5 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 

AND 13 

29900 FOR 60000 F

R 572158-01-6 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 AND 13 

28600 FOR 57900 F

 572158-01-7 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 

AND 13 

15600 FOR 67000 F

R 572158-01-8 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 AND 13 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572158-01-4. 

28600 FOR 57900 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572158-01-9 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 AND 13 

28000 FOR 56500 F

N 572158-01-10 540CB 540DB 540EB 

540FB 540GB 540HB 540JB 540KB 540LB 540MB 640CB 640DB 640EB 640FB 640GB 640HB 640JB 640KB 640LB 640MB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING STRINGERS 4, 5, 6, 7, 8, 11, 12 AND 13 

42000 FOR 84000 F

 572160-01-1 540NB 540PB 540QB 

540RB 550AB 550BB 550CB 550DB 560AB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING STRINGERS 7, 8 AND 11 

36800 FOR 48000 F

 572160-01-2 DELETED FROM ALS PART 2 AT REVISION 01  572160-01-3 540NB 540PB 540QB 

540RB 550AB 550BB 550CB 550DB 560AB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING STRINGERS 7, 8 AND 11 

24000 FOR 42000 F

 572160-01-4 540NB 540PB 540QB 

540RB 550AB 550BB 550CB 550DB 560AB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING STRINGERS 7, 8 AND 11 

12700 FOR 54600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 572160-01-5 540NB 540PB 540QB 

540RB 550AB 550BB 550CB 550DB 560AB 640NB 640PB 640QB 640RB 650AB 650BB 650CB 650DB 660AB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING STRINGERS 7, 8 AND 11 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572160-01-2. 

34000 FOR 58700 F

 572164-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 9  572164-02-2 DELETED FROM ALI DOCUMENT AT ISSUE 9  572164-02-3 DELETED FROM ALI DOCUMENT AT ISSUE 9  572164-02-4 DELETED FROM ALI DOCUMENT AT ISSUE 9  572164-02-5 DELETED FROM ALI DOCUMENT AT ISSUE 10 

R 572164-02-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB 15-16 AND RIB 22-23 

48000 FOR 96000 F

R 573101-01-1 N/A DETAILED INSPECTION OF WING TIP, BOTTOM SKIN 

LOWER SURFACE JOINT, OUTBOARD OF RIB 27 

60000 FOR 120000 F

 573101-01-3 N/A DETAILED INSPECTION OF WING TIP, BOTTOM SKIN 

LOWER SURFACE JOINT, OUTBOARD OF RIB 27 

15600 FOR 67100 F

R 573101-01-4 N/A DETAILED INSPECTION OF WING TIP, BOTTOM SKIN 

LOWER SURFACE JOINT, OUTBOARD OF RIB 27 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 573101-01-1. 

27900 FOR 39000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 574101-01-3 521AB 521CB 521EB 

522AB 522CB 522FB 522KB 522LB 522NB 522QB 522SB 522UB 621AB 621CB 621EB 622AB 622CB 622FB 622KB 622LB 622NB 622QB 622SB 622UB 

DETAILED INSPECTION OF OUTER WING, FIXED LEADING EDGE, ROLLER PIN HOLES AND OTHER CUTOUTS IN TRACK RIB 1 TO 12 

52200 FOR 104400 F

N 574106-01-8 521AB 521CB 521EB 

522AB 522CB 522FB 522KB 522LB 522NB 522QB 522SB 522UB 621AB 621CB 621EB 622AB 622CB 622FB 622KB 622LB 622NB 622QB 622SB 622UB 

DETAILED INSPECTION OF OUTER WING, FIXED LEADING EDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TO 

RIB 12 

36900 FOR 73800 F

N 574112-02-3 521AB 521CB 521EB 

522AB 522CB 522FB 522KB 522LB 522NB 522QB 522SB 522UB 621AB 621CB 621EB 622AB 622CB 622FB 622KB 622LB 622NB 622QB 622SB 622UB 

GENERAL VISUAL INSPECTION OF OUTER WING, FIXED 

LEADING EDGE, BOTTOM WING SKIN, UPPER AND LOWER SURFACES, FORWARD OF FRONT SPAR, FROM 

RIB 1 TO RIB 27, INCLUDING SIGHTING ROD HOLES IN RIB BAY 8-9 AND RIB BAY 26-27, LIFTING BEAM HOLES AND RAIN HOLES 

31200 FOR 62400 F

 574114-01-1 521CB 521EB 522AB 

522CB 522FB 522KB 522LB 522NB 522QB 522SB 522UB 621CB 621EB 622AB 622CB 622FB 622KB 622LB 622NB 622QB 622SB 622UB 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER 

WING, FIXED LEADING EDGE PINION FITTING BOLTING AND ACTUATOR BOLTING LOWER BOLT HOLES ON RIBS 2, 3, 5, 6, 7, 8, 9, 10, 11 AND 12 

36900 FOR 51600 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 574114-01-3 521CB 521EB 522AB 

522CB 522FB 522KB 522LB 522NB 522QB 522SB 522UB 621CB 621EB 622AB 622CB 622FB 622KB 622LB 622NB 622QB 622SB 622UB 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, FIXED LEADING EDGE PINION FITTING BOLTING AND ACTUATOR BOLTING LOWER BOLT HOLES ON RIBS 2, 3, 5, 6, 7, 8, 9, 10, 11 AND 12 

33200 FOR 46500 F

N 575151-01-6 573AB 573BB 573CB 

574AB 574BB 673AB 673BB 673CB 674AB 674BB 

DETAILED INSPECTION OF OUTER WING, TRAILING EDGE FALSE REAR SPAR, FORWARD AND AFT FACES 

28900 FOR 57800 F

R 575155-01-4 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

TRAILING EDGE, TOP SKIN UPPER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 

55800 FOR 111600 F

N 575156-01-1 571AB 671AB 

FLAPS EXTENDED 

DETAILED INSPECTION OF OUTER WING, FIXED TRAILING EDGE, SHROUD BOX AND FITTINGS 

35100 FOR 70200 F

 575158-01-1 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS AND PYLON FAIRINGS 

24000 FOR 42000 F

 575158-01-2 DELETED FROM ALI DOCUMENT AT ISSUE 7 

R 575158-01-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS AND PYLON FAIRINGS 

25400 FOR 50800 F

R 575158-01-6 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS AND PYLON FAIRINGS 

25400 FOR 42900 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 575158-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS AND PYLON FAIRINGS 

24000 FOR 42000 F

 575159-01-1 DELETED FROM ALS PART 2 AT REVISION 01  575159-01-2 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE, CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF MLG SUPPORT RIB 5 

21800 FOR 34900 F

 575159-01-3 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE, CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF MLG SUPPORT RIB 5 

32700 FOR 48000 F

R 575159-01-5 N/A DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 

LOWER SURFACE, CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF MLG SUPPORT RIB 5 

41200 FOR 60000 F

 575160-01-1 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

24000 FOR 38400 F

 575160-01-2 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

24000 FOR 42000 F

 575160-01-3 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

24000 FOR 42000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 575160-01-4 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

24000 FOR 42000 F

R 575160-01-5 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

60000 FOR 120000 F

 575160-01-6 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

13400 FOR 57600 F

R 575160-01-7 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

23100 FOR 37000 F

 575160-01-8 574AB 674AB 

MLG SECONDARY HINGED FAIRING REMOVED 

SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR, ABOVE MLG REINFORCING 

24000 FOR 38400 F

 575161-01-1 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT RIB 9 AND SIGHTING ROD HOLE AT RIB 10 

24000 FOR 42000 F

 575161-01-2 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT RIB 9 AND SIGHTING ROD HOLE AT RIB 10 

24000 FOR 42000 F

 575161-01-3 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT RIB 9 AND SIGHTING ROD HOLE AT RIB 10 

24000 FOR 42000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

R 575161-01-5 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT RIB 9 AND SIGHTING ROD HOLE AT RIB 10 

40400 FOR 60000 F

 575161-01-7 N/A GENERAL VISUAL INSPECTION OF OUTER WING, 

TRAILING EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT RIB 9 AND SIGHTING ROD HOLE AT RIB 10 

24000 FOR 42000 F

R 575163-01-2 PYLON FAIRINGS 

REMOVED 

SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING, BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER PYLON FAIRING 

48000 FOR 96000 F

 575163-01-3 PYLON FAIRINGS 

REMOVED 

SPECIAL DETAILED INSPECTION (LFEC) OF OUTER 

WING, BOTTOM SKIN LOWER SURFACE, AFT OF REAR 

SPAR, UNDER PYLON FAIRING 

41500 FOR 60000 F

R 575163-01-5 PYLON FAIRINGS 

REMOVED 

SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING, BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER PYLON FAIRING 

48000 FOR 60000 F

 575164-01-3 531CB 531EB 631CB 

631EB 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER 

WING, BOTTOM SKIN LOWER SURFACE, AFT OF REAR 

SPAR, AROUND FLAP TRACK 2 FORWARD FITTINGS 

21400 FOR 35500 F

 575164-01-4 531CB 531EB 631CB 

631EB 

SPECIAL DETAILED INSPECTION (HFEC) OF OUTER 

WING, BOTTOM SKIN LOWER SURFACE, AFT OF REAR 

SPAR, AROUND FLAP TRACK 2 FORWARD FITTINGS 

24000 FOR 42000 F

R 575165-01-2 531EB 535AB 535BB 

631EB 635AB 635BB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER FLAP TRACK 2 FAIRING AND FLAP TAB DRIVE 1A FAIRING 

35400 FOR 58800 F

 575165-01-3 DELETED FROM ALI DOCUMENT AT ISSUE 7 

R 575165-01-4 531EB 535AB 535BB 

631EB 635AB 635BB 

DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER FLAP TRACK 2 FAIRING AND FLAP TAB DRIVE 1A FAIRING 

29000 FOR 48200 F

 575221-01-1 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF INBOARD DOUBLESLOTTED FLAP, EXTERNAL SURFACE OF UPPER AND 

LOWER SKIN, LH/RH 

4800 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 575321-01-2 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF OUTBOARD DOUBLESLOTTED FLAP, INCLUDING TAB, EXTERNAL SURFACE 

OF UPPER AND LOWER SKIN, LH/RH 

8500 FC 

 576103-01-1 575AT 575KB 575LB 

575MB 675AT 675KB 675LB 675MB 

DETAILED INSPECTION OF AILERON, HINGE FITTINGS 

AND ACTUATOR ATTACHMENT FITTINGS 

38700 F

 711300-01-1 437AL 438AR 447AL 

448AR 

GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGE FITTINGS 

7500 FC 

 711300-01-3 DELETED FROM ALI DOCUMENT AT ISSUE 10  711300-01-5 DELETED FROM ALI DOCUMENT AT ISSUE 10  711300-03-1 437AL 438AR 447AL 

448AR 

GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGE FITTINGS NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 711300-01-3. 

3000 FC 

 711300-03-2 DELETED FROM ALI DOCUMENT AT ISSUE 10  711301-01-1 437AL 438AR 447AL 

448AR 

DETAILED INSPECTION OF THE FAN COWL DOORS 

HINGES AND SURROUNDING STRUCTURE 

7500 FC 

 711302-01-1 437AL 438AR 447AL 

448AR 

DETAILED INSPECTION OF THE FAN COWL DOORS 

LATCHES AND SURROUNDING STRUCTURE 

7500 FC 

 712102-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT AND SECONDARY LOAD PATH CLEARANCE 

7500 FC OR 9300 FH 

 712102-02-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF FORWARD 

ENGINE MOUNT BOLTS 

7500 FC OR 9300 FH 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 712111-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION 

7500 FC OR 15000 F

 712111-01-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION 

3500 FC OR 7000 FH 

 712111-01-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION 

2800 FC OR 12000 F

 712111-01-4 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION 

6900 FC OR 20700 F

 712111-03-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION 

7500 FC OR 15000 F

 712111-03-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION 

4500 FC OR 9000 FH 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 712111-03-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION 

2800 FC OR 12000 F

 712111-05-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF FORWARD 

ENGINE MOUNT PYLON BOLTS 

2800 FC OR 12000 F

 712111-05-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF FORWARD 

ENGINE MOUNT PYLON BOLTS 

6900 FC OR 20700 F

 712111-05-4 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF FORWARD 

ENGINE MOUNT PYLON BOLTS 

7500 FC OR 15000 F

 712111-06-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF FWD ENGINE MOUNT PYLON BOLTS. 

7500 FC OR 15000 F

 712111-06-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF FWD ENGINE MOUNT PYLON BOLTS. 

2800 FC OR 12000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 712112-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

FORWARD ENGINE MOUNT LINK LUGS 

7500 FC OR 15000 F

 712112-01-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

FORWARD ENGINE MOUNT LINK LUGS 

2800 FC OR 12000 F

 712112-01-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

FORWARD ENGINE MOUNT LINK LUGS 

6900 FC OR 20700 F

 712112-02-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

FORWARD ENGINE MOUNT LINK LUGS 

7500 FC OR 15000 F

 712112-02-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF 

FORWARD ENGINE MOUNT LINK LUGS 

2800 FC OR 12000 F

 712202-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT AND SECONDARY LOAD PATH CLEARANCE 

7500 FC OR 9300 FH 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 712202-02-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT BOLTS 

7500 FC OR 9300 FH 

 712211-03-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT 

INSTALLATION 

7500 FC OR 15000 F

 712211-03-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT 

INSTALLATION 

2800 FC OR 12000 F

 712211-03-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT 

INSTALLATION 

6900 FC OR 20700 F

 712211-04-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT 

INSTALLATION 

7500 FC OR 15000 F

 712211-04-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT 

INSTALLATION 

2800 FC OR 12000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 712211-05-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT PYLON BOLTS 

7500 FC OR 15000 F

 712211-05-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT PYLON BOLTS 

2800 FC OR 12000 F

 712211-05-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT PYLON BOLTS 

6900 FC OR 20700 F

 712211-06-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT PYLON BOLTS 

7500 FC OR 15000 F

 712211-06-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT PYLON BOLTS 

2800 FC OR 12000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 712212-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT LINK LUGS 

7500 FC OR 15000 F

 712212-01-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT LINK LUGS 

2800 FC OR 12000 F

 712212-01-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT LINK LUGS 

6900 FC OR 20700 F

 712212-02-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT LINK LUGS 

7500 FC OR 15000 F

 712212-02-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT LINK LUGS 

2800 FC OR 12000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 712213-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT PINS 7500 FC 

OR 15000 F

 712213-01-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT PINS 2800 FC 

OR 12000 F

 712213-01-3 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT PINS 6900 FC 

OR 20700 F

 712213-02-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT PINS 7500 FC 

OR 15000 F

 712213-02-2 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT PINS 2800 FC 

OR 12000 F

 725403-01-1 DELETED FROM ALI DOCUMENT AT ISSUE 11  725403-02-1 DELETED FROM ALI DOCUMENT AT ISSUE 11  781102-02-1 451AL 452AR 461AL 

462AR 

DETAILED INSPECTION OF THE COMMON NOZZLE 

ASSEMBLY V-GROOVE (J-RING) 

7500 FC 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 783001-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR THRUST REVERSERS REMOVED HEAT SHIELDS REMOVED 

DETAILED INSPECTION OF THRUST REVERSER 12 O'CLOCK BEAM JUNCTION WITH THE FORWARD FRAME 

24000 F

 783002-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR CUT CORNERS REMOVED 

DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME TO 6 O'CLOCK BEAM JOINT 

24000 F
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 783003-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR BRACKETS REMOVEDPIPES REMOVED HEAT SHIELDS REMOVED 

DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME TO 3/9 O'CLOCK BEAM JOINT 

24000 F

 783004-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR ACTUATORS REMOVED 

SPECIAL DETAILED INSPECTION (HFEC) OF THRUST REVERSER FORWARD FRAME AT ACTUATOR ATTACHMENT 

24000 F

 783200-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR UPPER HINGE ACCESS FAIRING OPENED 

GENERAL VISUAL INSPECTION OF "C" DUCT HINGE FITTINGS 

7500 FC 

 783200-01-3 DELETED FROM ALI DOCUMENT AT ISSUE 10  783200-01-5 DELETED FROM ALI DOCUMENT AT ISSUE 10 
A318/319/320/321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©

AIRBUS SAS 2013. All ri

ghts reserved.

REV 

COD

E 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHO

 783200-03-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

GENERAL VISUAL INSPECTION OF "C" DUCT HINGE FITTINGS NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 783200-01-3. 

3000 FC 

 783200-03-2 DELETED FROM ALI DOCUMENT AT ISSUE 10  783201-01-1 437AL 438AR 447AL 

448AR 451BL 451CL 451DL 451EL 452BR 452CR 452DR 452ER 461BL 461CL 461DL 461EL 462BR 462CR 462DR 462ER 

DETAILED INSPECTION OF THE THRUST REVERSER 

HINGE FITTINGS AND ADJACENT STRUCTURE 

7500 FC 

 783202-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF THE THRUST REVERSER 

LATCH ASSEMBLY ON TWO HALVES AND SURROUNDING STRUCTURE OF LATCHES (15 CM AROUND) 

7500 FC 

 783206-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF THE THRUST REVERSER FWD V-BLADE (J-RING) 

7500 FC 

 783207-01-1 437AL 438AR 447AL 

448AR 451AL 452AR 461AL 462AR 

DETAILED INSPECTION OF THE THRUST REVERSER AFT V-BLADE 

7500 FC 

 783208-01-1 451LL 451ML 452LR 

452MR 461LL 461ML 462LR 462MR PIVOTING DOORS OPENED 

DETAILED INSPECTION OF THE ACTUATOR FITTINGS AND SURROUNDING STRUCTURE 

19200 F
A318/A319/A320/A321 AIRWORTHINESS LIMITATIONS SECTION 

REV: 02 ALS PART 2 

EASA APPROVED 

©AIRBUS SAS 2013. All rights reserved. SECTION 3 CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS

3.1 EXPLANATION OF CDCCL REQUIREMENTS

CDCCLs include reference to any information necessary to maintain those design features that have be

needed to preclude development of an unsafe condition. This information is essential to ensure that instrepairs, 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 contaappropriate text to highlight the existence of each CDCCL. Such identification is necessary in the instruction

installation, alteration, repair or modification so as to minimize the risk that the work performed compromises Regulatory oversight of the operator’s compliance with this mandatory requirement is based on the appropthe accomplishment instructions associated with the installation, alteration, repair or modification. 3.2 CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS

Ref. CDCCL Requirement Refere

1 Elevator 

weight 

To ensure that the elevator weight remains within the published limits following any maintenance action that might affect its weight such as, but not limited to, repair or painting. 

AMM

27-34-51-75-55-20-11-25-CMM

55-21-SRM

55-20-
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 "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 

30748 OR A320-100 OR A320-200 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 

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 "GROUP 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 WINDSHIELDS 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 WINDSHIELDS 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 WINDSHIELDS 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 "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 

30748 OR A320-100 OR A320-200 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 

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 "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 

30748 OR A320-100 OR A320-200 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 

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 "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 

30748 OR A320-100 OR A320-200 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 

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 "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 

30748 OR A320-100 OR A320-200 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 

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 "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 

30748 OR A320-100 OR A320-200 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 

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 "GROUP 19-1A PRE 30748 OR GROUP 19-1B PRE 

30748 OR A320-100 OR A320-200 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 

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 "A320-200 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 "EXCLUDING 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 "GROUP 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 "GROUP 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 "GROUP 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 "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 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 include "AND TOP AND BOTTOM FLANGES" 

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

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

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

R 572011-01-6 Description changed to include "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 include "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 "A320-200 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 "A320-200 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 AND 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 including 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 airframe 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 stated. Storage, maintenance, etc... do not freeze calendar time 

accumulation. 

CONTINUED 

AIRWORTHINESS 

Is the process of ensuring that the level of airworthiness guaranteed by TC is maintained for 

each individual aircraft at the time of its entry 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, inspectability, or good design practice. Under these 

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

used. 

DAMAGETOLERANT 

AIRWORTHINESS 

LIMITATION 

ITEMS 

They are all those parts of the structure whose failure 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 design 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 parameters 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 inspections and replacement times will 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 task. Subsequent accomplishment 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 aircraft 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 structural 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 FUSELAGE-REINFORCE UPPER 

STRINGLERS 

 

 21288 WINGS-CENTER FUSELAGE-REINFORCE LOWER 

SECTION (FR 37 TO 41) 

57-1018 

 21521 FUSELAGE - REINFORCE THE 

WINDSHIELD/LOWER FAIRING ATTACHMENT 

 

 21657 FUSELAGE - NOSE FUSELAGE - 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 FOUR 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 GEAR 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 COMMUNICATIONS-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/REAR 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 - NOSE GEAR - MODIFIED SPRING 

CURVE 

32-1308 

 35515 STABILIZERS - HORIZONTAL STABILIZER - 

ELEVATOR - REPLACE LIGHTNING STRAPS 

PROTECTION WITH BRONZE MESH AND REMOVE 

INSERTS AT ELEVATOR TRAILING EDGE 

 

N 36590 FUSELAGE - REAR FUSELAGE - INSTALL 

STRUCTURAL PROVISION FOR CABIN SWIFT 

BROADBAND ANTENNA 

 

 37331 WINGS - FIXED PARTITION - INTRODUCE A 

STANDARD OF BOX WITHOUT DRY BAY ON A318, 

A319 AND A320-200 

 

 37332 WINGS - FIXED PARTITION - INTRODUCE A 

VERSION OF WING BOX WITH 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 FUSELAGE - 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 PARTITION - INTRODUCE A 

STANDARD OF WING BOX WITHOUT DRY BAY ON 

A321 

 

 38617 WINGS - FIXED PARTITION - 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