a318/a319/a320/a321 airworthiness limitations section (als

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ISSUE: JAN 17/20

C80_ALS Part 3 Scheduled Revision Template_FM1404445_v4.0

A318/A319/A320/A321

Airworthiness Limitations Section (ALS)

Part 3

Certification Maintenance Requirements (CMR)

-

Revision 07 Issue 02

A320 Family

AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JAN 17/20 ALS PART 3 - TOC PAGE: 2/29

© AIRBUS SAS 2019. All rights reserved. Confidential and proprietary document.

TABLE OF CONTENTS

REVISION STATUS.............................................................................................................. 3

COMPLIANCE TIME ............................................................................................................ 5

SECTION 1. INTRODUCTION ......................................................................................... 8

1. GENERAL ................................................................................................................... 8

2. APPLICABILITY .......................................................................................................... 8

3. MAINTENANCE PROGRAM PUBLICATION ............................................................ 10

4. DEFINITION OF ALS PART 3 CONTENT ................................................................. 12

4.1 CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) ........................... 12

4.1.1 ONE STAR CMR (*) ................................................................................... 12

4.1.2 TWO STAR CMR (**) ................................................................................. 12

5. BASIC RULES .......................................................................................................... 12

5.1 CLOCK STARTING POINT FOR CMR ............................................................. 12

5.2 EXCEPTIONAL SHORT-TERM EXTENSIONS ................................................ 13

6. INTENTIONALLY LEFT BLANK ............................................................................... 14

7. PRODUCTION CONCESSIONS, REPAIRS, ALS VARIATIONS, AIRWORTHINESS DIRECTIVES AND ALTERNATIVE METHODS OF COMPLIANCE .......................... 14

8. MODIFICATIONS/REPAIRS NOT DEVELOPED BY AIRBUS DOA CERTIFICATE EASA.21J.031 ........................................................................................................... 14

SECTION 2. EXPLANATION OF TABLE FORMAT....................................................... 15

SECTION 3. CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) ................... 20

APPENDIX A. ABBREVIATIONS ..................................................................................... 21

APPENDIX B. TERMS AND DEFINITIONS ...................................................................... 23

APPENDIX C. LIST OF DELETED TASKS ....................................................................... 24

APPENDIX D. HISTORY FILE .......................................................................................... 25

APPENDIX E. SUMMARY OF CHANGES ........................................................................ 28

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - REVISION STATUS PAGE: 3/29


REVISION STATUS

The ALS Part 3 is approved and Variations must also be approved.

The technical content of this Revision is approved under the authority of the DOA ref. EASA.21J.031.

Note: the present Revision includes ALS data already approved either by EASA for major changes or by Airbus under DOA privilege for minor changes.

REVISION NUMBER APPROVAL REFERENCE APPROVAL DATE

07 D050319070 OCT 11/19

07 issue 02 D050319070 issue 02 JAN 17/20

This Revision contains all approved changes to A318/A319/A320/A321 ALS Part 3 since the last Revision.

Issue 02 of considered Revision has been published in order to introduce compliance time for CMR 282800-00006-1-C.

This including changes published through the following Variations:

VARIATION NUMBER REASON OF THE VARIATION

6.1 Issue 02

MOD 163213 introduces option to include up to three Additional Centre Tanks (ACT) to the A321 NEO ACF.

This Variation aims at providing the mandatory instructions and airworthiness limitations required following embodiment of MOD 163213.

This Variation provides also relaxations to CMRs 262300-00001-1-C and 262300-00002-1-C, applicable to the rest of the A320 family fleet fitted with cargo compartment fire extinguishing.

Reason for issue 02 is to modify APPLICABILITY of considered Variation 6.1 from A321-200NX aircraft models, to all A318/A319/A320/A321 aircraft models (in order to reflect relaxations to CMRs 262300-00001-1-C and 262300-00002-1-C).

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - REVISION STATUS PAGE: 4/29


VARIATION NUMBER REASON OF THE VARIATION

6.2

The reference aircraft for the A320 NEO ACJ is an A320 NEO. The design changes to be applied on this A320 NEO to get an A320 NEO ACJ are the following modifications:

Up to 4 ACTs [MOD 163215 / Certify up to 4 ACTs on A320 NEO ACJ]

And FL 410 [MOD 162744 / Extend Flight Envelope up to 41 000 FT (A320 NEO ACJ)]

And Airstairs [MOD 162481 / Entrance stairs install reinforced airstairs locking system].

A320 NEO ACJ aircraft are thus A320 POST MOD 163215 AND POST MOD 162744 AND POST MOD 162481.

This Variation aims to provide the impact on the mandatory instructions and airworthiness limitations published in the A318/A319/A320/A321 ALS Part 3 Revision 06 following embodiment of MOD 163215 AND MOD 162744 AND MOD 162481.

6.3

MOD 161004 introduces the new A319-151N aircraft model. MOD 165511 introduces the new A319-153N aircraft model. MOD 162338 introduces envelope for design weight of A319 NEO ACJ aircraft. This MOD is used as marker of A319 NEO ACJ configuration.

This Variation aims at providing the impact on the mandatory instructions and airworthiness limitations published in the A318/A319/A320/A321 ALS Part 3 Revision 06 following embodiment of MOD 161004 and/or MOD 165511 and/or MOD 162338.

This includes also additional changes that were not published through Variations. For detailed traceability in the SOC, group of changes have been defined as follow:

GROUP OF CHANGES REASON OF THE CHANGE

A Revision of CMRs applicability following new A320 NEO ACJ and new

A319 NEOs

B Introduction of new CMR* 282800-00006-1-C in anticipation of SA MRBR

rev. 24 tasks interval extension.

C Revision of CMR* 526000-00001-1-C from A319 NEO ACJ to all SA

aircraft fitted with airstairs.

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - COMPLIANCE TIME PAGE: 5/29


COMPLIANCE TIME

Airbus anticipates that a dedicated Airworthiness Directive (AD) will be released to mandate the update of the Operators approved Maintenance Program (OMP) according to Airbus A318/A319/A320/A321 ALS Part 3 Revision 07. The compliance chapter of this future AD will give an implementation period for introduction of the new or revised instructions and airworthiness limitations introduced by this Revision in the OMP. Airbus recommends Operators to consider the implementation of these changes in the OMP at the next scheduled opportunity in order to anticipate future AD requirements. Maintenance tasks in SECTION 3 will also be mandated by the future AD and are to be accomplished prior to the new/revised intervals provided in this Revision, except for the items listed in the below table. For these items listed in the table below, a compliance time is provided for aircraft that have already exceeded or are close to exceeding the new or revised intervals. In such a case, maintenance tasks in SECTION 3 are to be accomplished prior to the new/revised intervals provided in this Revision or by the compliance time provided for each item, whichever occurs later. When applicable, the compliance time deadlines are indicated in the table below as advanced information for Operators in order to anticipate future AD requirements.

A320 Family




SECTION REV

CODE ITEMS

VARIATION

NUMBER (when applicable)

COMPLIANCE TIME

COMPLIANCE

TIME

APPLICABILITY

3 R 361200-00001-1-C N/A

For A318 / A319 / A320 / A321 CEO aircraft PRE MOD 159954, 1st accomplishment of CMR 361200-00001-1-C must be carried out no later than :

A. following correction time : A.1. 10/SEP/2020,

[corresponding to 24 months from the Effective Date of the EASA Airworthiness Directive that has been issued to mandate the Revision 06 of A318/A319/A320/A321 ALS Part 3]

OR A.2. next planned realization of Maintenance

Procedure AMM 361251-200-001 (associated to MRBR tasks 36.12.00/01 or 36.12.00/02, depending on aircraft configuration),

whichever occurs first (between A.1. and A.2.)

OR B. within the due CMR interval [13 000 FH from aircraft Entry

Into Service, OR 13 000 FH from last accomplishment of Maintenance Procedure AMM 361251-200-001 (associated to MRBR tasks 36.12.00/01 or 36.12.00/02, depending on aircraft configuration), whichever occurs later],

whichever occurs later (between A. and B.).

A318 PRE 159954

OR

A319 PRE 161004

PRE 159954

OR

A320 PRE 161000

PRE 161003

PRE 159954

OR

A321 PRE 161002

PRE 161005

PRE 159954

A320 Family




SECTION REV

CODE ITEMS

VARIATION

NUMBER (when applicable)

COMPLIANCE TIME

COMPLIANCE

TIME

APPLICABILITY

3 N 282800-00006-1-C N/A

For A318 / A319 / A320 / A321 aircraft POST MOD 25415 without ACT installed, 1st accomplishment of CMR 282800-00006-1-C must be carried out no later than :

A. 1 000 FH from the Effective Date of the EASA Airworthiness Directive that is expected to be issued to mandate the Revision 07 Issue 02 of A318/A319/A320/A321 ALS Part 3

OR B. within the due CMR interval

[1 000 FH from aircraft Entry Into Service, OR 1 000 FH from last accomplishment of Maintenance Procedure AMM 282800-200-003 (associated to MRBR task 28.28.00/01), whichever occurs later],

whichever occurs later (between A. and B.).

POST 25415,

if no ACT installed

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - SECTION 1 PAGE: 8/29


SECTION 1. INTRODUCTION

1. GENERAL

The ALS Part 3 provides Certification Maintenance Requirements (CMR) which are system related periodic tasks (with intervals expressed in aircraft usage parameter) established during the Aircraft Type Certification. These periodic tasks are required to have mandatory status in order to maintain an appropriate level of aircraft safety and shall be complied with as per EASA Part M.A.302 – Aircraft Maintenance Program. These tasks constitute operating limitations of the aircraft.

2. APPLICABILITY

The A318/A319/A320/A321 ALS Part 3 applies to the following aircraft series and models:

AIRCRAFT SERIES AIRCRAFT MODELS

A318-100

A318-111

A318-112

A318-121

A318-122

A319-100

A319-111

A319-112

A319-113

A319-114

A319-115

A319-131

A319-132

A319-133

A319-151N

A319-153N

A320-200

A320-211

A320-212

A320-214

A320-215

A320-216

A320-231

A320-232

A320 Family




AIRCRAFT SERIES AIRCRAFT MODELS

A320-200

A320-233

A320-251N

A320-252N

A320-253N

A320-271N

A320-272N

A320-273N

A321-100

A321-111

A321-112

A321-131

A321-200

A321-211

A321-212

A321-213

A321-231

A321-232

A321-251N

A321-252N

A321-253N

A321-271N

A321-272N

A321-251NX

A321-252NX

A321-253NX

A321-271NX

A321-272NX

A320 Family




3. MAINTENANCE PROGRAM PUBLICATION

The published maintenance program content is provided for aircraft operating up to the publication trigger quoted in the table below. Operation beyond these values requires an update of the ALS Part 3 data that are approved by the EASA. Should any operator envisage future operations beyond the quoted values, they must first contact Airbus for advice.

AIRCRAFT CONFIGURATION

PUBLICATION TRIGGER (Whichever occurs first)

FLIGHT HOURS (FH) FLIGHT CYCLES (FC)

A318-1xx 60 000 48 000

A319-1xx CEO PRE 155789 (Excluding Corporate Jet Operations)

60 000 48 000

A319 CJ (Corporate Jet Operations) (A319 CEO POST 28162 POST 28238 POST 28342 OR A319 NEO POST 162338)

77 400 18 000

A319-1xx CEO POST 160080 (Excluding Corporate Jet Operations)

96 000 48 000

A319-1xx CEO POST 155789 (Excluding Corporate Jet Operations)

120 000 60 000

A320-2xx CEO PRE 37734 PRE 39020 60 000 48 000

A320-2xx CEO POST 37734 PRE 39020 80 000 37 500

A320-2xx CEO POST 39020 [excluding A320-2xx CEO POST 20139 PRE 22129 POST 39020]

120 000 60 000

A320-2xx CEO POST 20139 PRE 22129 POST 39020

63 500 45 000

A320-2xx CEO POST 160080 96 000 48 000

A320 CJ (Corporate Jet Operations) (A320 NEO POST 162339)

77 400 18 000

A321-1xx / -2xx CEO PRE 154881 PRE 156130

60 000 48 000

A321-1xx / -2xx CEO POST 154881 PRE 156130

74 000 37 000

A321-1xx / -2xx CEO POST 156130 120 000 60 000

A319 / A320 / A321 NEO aircraft (Excluding Corporate Jet Operations)

96 000 48 000

A320 Family




Note:

- A319 / A320 / A321 CEO (Current Engine Option) aircraft are A319 / A320 / A321 aircraft not fitted with NEO engines.

- A319 CEO used as Corporate Jet Operations (included in A319-VIP) have received MOD 28238, MOD 28162 and MOD 28342 in production.

A319 NEO used as Corporate Jet Operations (included in A319-VIP) have received MOD 162338 in production.

A320 NEO used as Corporate Jet Operations (A320 VIP) have received MOD 162339 in production.

- MOD 155789 refers to Design Service Goal (DSG) extension of A319-1xx CEO aircraft up to 120 000 FH or 60 000 FC, whichever occurs first.



For the particular case of A320-2xx CEO POST 20139 PRE 22129, MOD 39020 refers to Design Service Goal (DSG) extension up to 63 500 FH or 45 000 FC.

- MOD 154881 refers to Design Service Goal (DSG) extension of A321-131 aircraft (MSN 00385, MSN 00550 and MSN 00591), A321-211 aircraft (MSN 00677, MSN 00781, MSN 00815, MSN 00841, MSN 00852, MSN 01238, MSN 01250 and, MSN 01720) and A321-231 aircraft (MSN 00663, MSN 00668, MSN 00787, MSN 00878, MSN 00915 and MSN 00954) up to 74 000 FH or 37 000 FC, whichever occurs first.

- MOD 156130 refers to Design Service Goal (DSG) extension of A321-1xx / -2xx CEO aircraft up to 120 000 FH or 60 000 FC, whichever occurs first..

- MOD 160080 introduces the sharklet devices in the A319-1xx CEO or A320-2xx CEO

in-service aircraft and extends the Design Service Goal (DSG) of the A319-1xx CEO

(excluding Corporate Jets Operations) POST MOD 160080 or A320-2xx CEO POST

MOD 160080 up to 96 000 FH or 48 000 FC, whichever occurs first.

- A319 / A320 / A321 NEO aircraft includes: A319-151N (A319 POST MOD 161004), A319-153N (A319 POST MOD 165511), A320-251N (A320 POST MOD 161003), A320-252N (A320 POST MOD 162680), A320-253N (A320 POST MOD 161860), A320-271N (A320 POST MOD 161000), A320-272N (A320 POST MOD 163955), A320-273N (A320 POST MOD 162512), A321-251N (A321 POST MOD 161005), A321-251NX (A321 POST MOD 161005 POST MOD 160766), A321-252N (A321 POST MOD 162681), A321-252NX (A321 POST MOD 162681 POST MOD 160766), A321-253N (A321 POST MOD 161006), A321-253NX (A321 POST MOD 161006 POST MOD 160766), A321-271N (A321 POST MOD 161002),

A320 Family




A321-271NX (A321 POST MOD 161002 POST MOD 160766), A321-272N (A321 POST MOD 162038) and A321-272NX (A321 POST MOD 162038 POST MOD 160766). For all these aircraft (excluding A319 NEO Corporate Jet and A320 NEO Corporate Jet) a Design Service Goal (DSG) of 96 000 FH or 48 000 FC, whichever occurs first, has been set.

4. DEFINITION OF ALS PART 3 CONTENT

4.1 CERTIFICATION MAINTENANCE REQUIREMENTS (CMR)

4.1.1 ONE STAR CMR (*)

One Star CMRs specified in ALS Part 3 are mandatory tasks and cannot be changed or deleted without the concurrence of the Primary Certification Authority (EASA).

One Star CMR task intervals quoted in ALS Part 3 are absolute limitations and cannot be escalated without the concurrence of the Primary Certification Authority.

4.1.2 TWO STAR CMR (**)

Two Star CMRs specified in ALS Part 3 are mandatory tasks and cannot be changed or deleted without the concurrence of the Primary Certification Authority.

Two Star CMR task intervals may be adjusted in accordance with an Operator’s approved escalation practices or an approved reliability program.

This statement has been agreed on the basis that Operators with approved escalation practices or an approved reliability program make adjustments to their maintenance programs based on data collection and analytical techniques. It has been demonstrated that the use of such methods to manage a maintenance program does not give rise to undue escalation.

5. BASIC RULES

5.1 CLOCK STARTING POINT FOR CMR

This paragraph provides general rules related to the starting point for calculation of due dates or times for CMR identified in this document according to the different usage parameters.

For CMR tasks whose interval is given in Calendar time, the starting point to be considered is the date of Transfer of Title (TOT) to the first Operator of the aircraft, unless otherwise stated in the delivery documentation of the dedicated aircraft.

For CMR tasks whose interval is given in Flight Hours (FH), the starting point to be considered is the date of Transfer of Title (TOT) to the first Operator of the aircraft, unless otherwise stated in the delivery documentation of the dedicated aircraft. Considering the very low number of flight hours performed between first flight and delivery, and the methodology used to define CMR task intervals, EASA agrees to consider the date of delivery of the aircraft as the starting point for CMR tasks whose intervals are given in Flight Hours.

A320 Family




For CMR tasks whose interval is given in Flight Cycles (FC), the starting point to be considered is the date of the aircraft first flight, unless otherwise stated in the delivery documentation of the dedicated aircraft.

For CMR tasks whose interval is changed, the next accomplishment must be determined from previous accomplishment date unless otherwise stated.

The time to start the clock for tasks with applicability determined by post-delivery modification is the date of MOD embodiment.

5.2 EXCEPTIONAL SHORT-TERM EXTENSIONS

Since CMR intervals are based on statistical averages and reliability rates, an exceptional short-term extension for a specific CMR interval may be made on one aircraft for a limited period of time without jeopardizing safety.

The term “exceptional short-term extension” is defined as an increase in a CMR interval that may be needed to cover an uncontrollable or unexpected situation. Repeated use of such extensions, either on the same aircraft or on similar aircraft in the Operator's fleet, should not be used as a substitute for good management practices. Short-term extensions must not be used for fleet CMR escalation.

Unless noted adjacent to the task, for all CMRs (One Star and Two Star) identified in this ALS Part 3, it has been accepted by the Primary Certification Office (EASA) that short-term extensions up to the following maximum values may be granted without consultation with that office. Requests for extensions in excess of these values must be submitted with full justification to the Primary Certification Office (EASA) such that approval, if granted, can be given prior to their use.

(1) CMR controlled by Flight Hours (FH)

Extensions up to 10% or 500 FH (whichever is the lesser) may exceptionally be granted on CMR intervals quoted in terms of Flight Hours.

(2) CMR controlled by Flight Cycles (FC)

Extensions up to 5% or 250 FC (whichever is the lesser) may exceptionally be granted on CMR intervals quoted in terms of Flight Cycles.

(3) CMR controlled by Calendar Time

Where the repeat interval is 12 months or less, extensions up to 10% or 1 month (whichever is the lesser) may exceptionally be granted on CMR intervals quoted in terms of months.

Where the repeat interval is greater than 12 months, extensions up to 2 months may exceptionally be granted.

This paragraph in the ALS Part 3 is written to confirm to the Authority of the State of aircraft registry that exceptional short-term extensions of CMR intervals are permissible. Approval of such extensions rests with the Authority of the State of aircraft registry in the same way as it does for any other scheduled maintenance task interval extension.

A320 Family




6. INTENTIONALLY LEFT BLANK

7. PRODUCTION CONCESSIONS, REPAIRS, ALS VARIATIONS, AIRWORTHINESS

DIRECTIVES AND ALTERNATIVE METHODS OF COMPLIANCE

Limitations of the ALS Part 3 may be superseded by instructions given in either a production concession, a repair solution, an ALS Variation, an Alternative Method of Compliance (AMOC) an Airworthiness Directive (AD), or exemptions provided by National Aviation Authorities (e.g. exemption supported by ASAC – Airbus Statement of Airworthiness Compliance).

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

When a limitation affected by a production concession/repair solution/AD/AMOC is amended within the Revision of the ALS Part 3 subsequent to the issuance date of the production concession/repair solution/AD/AMOC, Operators are requested to contact Airbus for guidance to establish impact on the production concession/repair solution/AD/AMOC.

8. MODIFICATIONS/REPAIRS NOT DEVELOPED BY AIRBUS DOA CERTIFICATE EASA.21J.031

If an aircraft/component has a modification or repair embodied, that has not been developed under the authority of Airbus Design Organisation Approval (DOA) No EASA.21J.031, and affects the content of the ALS, the Design Approval Holder (e.g. Supplementary Type Certificate (STC) holder) is responsible to provide any necessary adaptations of the ALS Part 3 airworthiness limitations.

A320 Family




SECTION 2. EXPLANATION OF TABLE FORMAT

The Certification Maintenance Requirements (CMR) are presented in SECTION 3 of ALS Part 3. Detailed information is given below to explain table provided on subsequent pages.

CMR REF. NUMBER

CMR CAT.

TASK DESCRIPTION INTERVAL RELATED MRBR TASK NUMBER

APPLICABILITY

(1) CMR REF. NUMBER

This column indicates CMR number. It is composed of 13 digits as follows:

XXXXXX - M E F YY - Z - C

C stands for CMR.

Z is for the technical solution applicable to a same task requirement.

YY is sequential number.

F is engine type information when more than one engine from the same manufacturer is applicable to the program. 0 is default value.

E is engine/APU/… manufacturer identification. As it is not applicable to A320 CMR references, it is always set to 0.

M is used to differentiate aircraft series in Airbus numbering system to which CMR tasks are applicable. As it is not applicable to A320 CMR references, it is always set to 0.

XXXXXX is Maintenance Significant Item (MSI).

A320 Family




(2) CMR CAT.

This column identifies the CMR categorization:

- CMR*: One Star CMR.

- CMR**: Two Stars CMR.

(3) TASK DESCRIPTION

This column identifies the MSI title and the description of the task associated with the CMR. This reflects the Maintenance Review Board Report (MRBR) task wording where the identical task is required by the MRBR.

(4) INTERVAL

This column identifies the interval between successive accomplishments of the task.

(5) RELATED MRBR TASK NUMBER

This column identifies the related MRBR task (if any) whose content covers the CMR requirement in terms of maintenance procedure. Nevertheless, differences may exist between the MRBR task and the CMR concerning the interval and the applicability. For compliance with CMR requirements, the ALS Part 3 provides the limiting values.

(6) APPLICABILITY

This column indicates the aircraft type/series/model and modification status for which the task is applicable.

Examples are given below:

APPLICABILITY TASK APPLICABLE TO

ALL All A318, all A319, all A320 and all A321 aircraft.

PRE NNNNN All A318, all A319, all A320 and all A321 on which modification NNNNN has not been embodied.

A320 Family





POST NNNNN All A318, all A319, all A320 and all A321 on which modification NNNNN has been embodied.

A318 All A318 only.

A319 All A319 only.

A319N All A319 NEO only.

A319-VIP A319 Corporate Jet Operations (A319 CEO POST 28162 POST 28238 POST 28342 OR A319 NEO POST 162338).

A319-PAX All A319, excluding A319 Corporate Jet Operations.

A320 All A320 only.

A320N All A320 NEO only

A320-VIP A320 Corporate Jet Operations (A320 NEO POST 162339).

A320-PAX All A320, excluding A320 Corporate Jet Operations.

A321 All A321 only.

A321N All A321 NEO only

A3XX PRE NNNNN

All A3XX aircraft on which MOD NNNNN has not been embodied.

A3XX POST NNNNN

All A3XX aircraft on which MOD NNNNN has been embodied.

A320 Family





A318 OR

A319 OR

A320 POST NNNNN

OR A321

All A318, or All A319, or All A320 on which MOD NNNNN has been embodied, or All A321.

A320 POST NNNNN

OR A321

POST NNNNN

All A320 on which MOD NNNNN has been embodied, or All A321 on which MOD NNNNN has been embodied.

POST NNNNN POST MMMMM POST YYYYY

All A318, all A319, all A320 and all A321 on which MOD NNNNN and MOD MMMMM and MOD YYYYY have been embodied.

POST NNNNN OR

POST MMMMM All A318, all A319, all A320 and all A321 on which MOD NNNNN or MOD MMMMM have been embodied.

POST NNNNN PRE MMMMM

All A318, all A319, all A320 and all A321 on which MOD NNNNN has been embodied and MOD MMMMM has not been embodied.

FAA Only CMR limitation applicable only:

- To US registered aircraft, or - If national authority requires to apply FAA requirements.

A320 Family





ALL except FAA CMR applicable to all A318, all A319, all A320 or all A321 aircraft, except:

- US registered aircraft, and - When national authority requires to apply FAA requirements.

LEAP-1A A320 / A321 fitted with new CFM engines, also called CFM LEAP-1A engines.

PW1100G A320 / A321 fitted with new Pratt & Whitney engines.

A320 Family




SECTION 3. CERTIFICATION MAINTENANCE REQUIREMENTS (CMR)

Certification Maintenance Requirements can be found in the embedded excel file “SA ALS Part 3 Revision 07 Issue 02.xlsx”.

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - APPENDIX A PAGE: 21/29


APPENDIX A. ABBREVIATIONS

ABBREVIATION MEANING

A/C Aircraft

AC Alternative Current

ACF Airbus Cabin Flex

ACJ Airbus Corporate Jet

ACT Additional Center Tank

AD Airworthiness Directive

AGCM Airborne Ground Check Module

ALS Airworthiness Limitations Section

AMM Aircraft Maintenance Manual

AMOC Alternative Method of Compliance

APU Auxiliary Power Unit

ASAC Airbus Statement of Airworthiness Compliance

ATA Air Transport Association of America

BITE Built-In Test Equipment

Cal. Calendar

CEO Current Engine Option

CFM CFM International

CJ Corporate Jet

CMR Certification Maintenance Requirement

D Deleted

DOA Airbus Design Organization Approval

DSG Design Service Goal

EASA European Aviation Safety Agency

EFCS Electrical Flight Control System

ELAC Elevator and Aileron Computer

ESG Extended Service Goal

FAA Federal Aviation Administration

FC Flight Cycle

FH Flight Hour

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - APPENDIX A PAGE: 22/29


ABBREVIATION MEANING

FQIC Fuel Quantity Indication Computer

FQIS Fuel Quantity Indicator System

MLG Main Landing Gear

MO Months

MOD Modification

MRBR Maintenance Review Board Report

MSI Maintenance Significant Item

MSN Manufacturer Serial Number

N/A Not Applicable

N New

NEO New Engine Option

OMP Operators Maintenance Program

POB Pressure-Off Brake

PNR Part Number

PW Pratt and Whitney

R Revised

RAT Ram Air Turbine

SLFA Synchronized Locking Feedback Actuator

SOC Summary Of Changes

STC Supplemental Type Certificate

THS Trimmable Horizontal Stabilizer

TOC Table Of Contents

TOT Transfer Of Title

US United States

WTB Wing Tip Brake (pressure-off brake)

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - APPENDIX B PAGE: 23/29


APPENDIX B. TERMS AND DEFINITIONS

TERM DEFINITION

CALENDAR TIMES (Cal.)

Month(s): equivalent of 1 calendar month (can be calculated as 1/12 calendar year). Year(s): equivalent of 12 calendar month (can be calculated as 365,25 days).

COMPLIANCE TIME

Period of time given to Operators to accomplish maintenance tasks and/or replace items (at component or aircraft level) having exceeded or close to exceed the new/reduced airworthiness limitations provided in the Revision/Variation.

DETAILED INSPECTION

An intensive examination of a specific item, installation or assembly to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required.

ENTRY-INTO- SERVICE

The initial Entry-Into-Service is defined for the aircraft (systems installations) as:

- The date of Transfer Of Title to the first Operator for airworthiness limitations in flight hour or in Calendar times, unless otherwise stated in any delivery documentation to the first Operator.

- The date of aircraft first flight for airworthiness limitations in flight cycles and/or landings

EXCEPTIONAL SHORT-TERM EXTENSION

An increase in a CMR interval that may be needed to cover an uncontrollable or exceptional unexpected situation.

FLIGHT CYCLE (FC) A complete take-off and landing sequence

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

FUNCTIONAL CHECK

A quantitative check to determine if a component / item performs one or more functions within specified limits.

IMPLEMENTATION PERIOD

The period of time allocated to Operators to update their approved Maintenance Program.

INTERVAL The maximum period expressed in usage parameters between the completion of a task and its next due accomplishment.

OPERATIONAL CHECK

A qualitative check to determine that a component/item is fulfilling its intended purpose. It is a failure finding task and does not require quantitative tolerances.

VISUAL CHECK Observation to determine that a component/item is fulfilling its intended purpose. It is a failure finding task and does not require quantitative tolerances.

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - APPENDIX C PAGE: 24/29


APPENDIX C. LIST OF DELETED TASKS

TASK REFERENCE SUMMARY OF CHANGES

271400-00001-2-C Task deleted in Revision 06.






A320 Family


ISSUE: JAN 17/20 ALS PART 3 - APPENDIX D PAGE: 25/29


APPENDIX D. HISTORY FILE

RECORD OF REVISIONS

REVISION NUMBER

REASONS FOR REVISION REVISION

DATE

00 The A318/A319/A320/A321 ALS Part 3 Revision 00 is created at the opportunity of the update of CMR Documents issue 23 (EASA version) and issue 17 (FAA version).

NOV 23/11

01

The A318/A319/A320/A321 ALS Part 3 Revision 01 is mainly dedicated to introduce the Extended Service Goal 1 (ESG1) exercise, which allows continued operation of the A320-200 systems POST MOD 39020 up to 120000 FH or 60000 FC.

JUN 15/12

02

The A318/A319/A320/A321 ALS Part 3 Revision 02 is issued to introduce the Extended Service Goal (ESG) for in-service A319-100 aircraft series (MOD 155789). Revision 02 also introduced MOD 154881 allowing operation of the aircraft models A321-211 and A321-231 system installations at 74 000 FH or 37 000 FC, whichever occurs first. Besides, Revision 02 revised interval and applicability of CMR Two Star 282100-00001-1-C – MAIN FUEL PUMP SYSTEM.

NOV 05/14

03

The A318/A319/A320/A321 ALS Part 3 Revision 03 is mainly dedicated to introduce the extension of A321-100/-200 systems installations up to 74 000 FH or 37 000 FC by embodiment of MOD 154881, the extension of A320-231 POST 20139 PRE 22129 (MLG with four wheels bogie) systems installations up to 63 500 FH or 45 000 FC by embodiment of MOD 39020, the new aircraft model A320-271N (A320 fitted with new PW engines), the sharklet devices for in-service A320-200 and A319-100 aircraft (MOD 160080), the new CMR One Star for installation of a new A321 Fuel Quantity Indication System (FQIS), increases interval for several ATA 27 and ATA 29 CMR tasks and some editorial changes to harmonise with A318/A319/A320/A321 MRBR.

DEC 21/15

04 The A318/A319/A320/A321 ALS Part 3 Revision 04 is mainly to introduce the new A320-251N aircraft model (A320-200 NEO fitted with new CFM engines).

JUN 20/16

05

The A318/A319/A320/A321 ALS Part 3 Revision 05 is mainly issued :

to introduce the Extended Service Goal (ESG) for in-service A321-100 and A321-200 aircraft series (MOD 156130),

to introduce the new aircraft models A321-271N (A321 fitted with new PW engines), A321-251N (A321 fitted with new CFM engines) and A321-253N (A321 fitted with new CFM engines),

And to extend the applicability of CMR 323000-00001-1-C to ALL A318 / A319 / A320 / A321 CEO aircraft, and provide an associated compliance time

APR 06/17

A320 Family




REVISION NUMBER


DATE

06

The A318/A319/A320/A321 ALS Part 3 Revision 06 is mainly issued to include :

Changes already published through Variations : o Variation 5.1 : new CMR 282800-00002-1-C related to MOD

160832 (A321 NEO with 1 or 2 ACTs) o Variation 5.2 : introduction of new model A321-272N (CMR

table not impacted)

Changes introduced directly in the Revision : o Introduction of following new models :

A320-252N (CMR table not impacted) A321-252N (CMR table not impacted) A321 NEO ACF (new CMRs 522101-00001-1-C,

522101-00002-1-C, 522101-00003-1-C and 522101-00004-1-C introduced)

o New CMR 361200-00001-1-C ; for A320 family CEO aircraft PRE MOD 159954, EASA has agreed following compliance time : 24 months from the Effective Date of the EASA Airworthiness Directive that is expected to be issued to mandate the Revision 06 of A318/A319/A320/A321 ALS Part 3

o New, revised and deleted CMRs aiming to support MRBR rev. 23 evolution :

Revised CMRs 212800-00001-1-C, 271400-00001-1-C, 271400-00002-1-C, 273400-00001-1-C, 273400-00002-1-C, 273400-00002-3-C, 281500-00001-1-C, 291000-00005-1-C and 324000-00001-1-C

New CMR 281500-00001-2-C Deleted CMRs 271400-00001-2-C,

271400-00002-2-C, 273400-00001-2-C, 273400-00002-2-C and 324000-00001-2-C.

JUN 13/18

A320 Family




REVISION NUMBER


DATE

07at issue 01

The A318/A319/A320/A321 ALS Part 3 Revision 07 is mainly issued to include :

Changes already published through Variations : o Variation 6.1 :

Provides impact on ALS part 3 – CMR related to MOD 163213 [introduce option to include up to three Additional Centre Tanks (ACT) to the A321 NEO ACF]. This Variation provides also relaxations to CMRs 262300-00001-1-C and 262300-00002-1-C, applicable to the rest of the A320 family fleet fitted with cargo compartment fire extinguishing.

o Variation 6.2 : Provides impact on ALS part 3 – CMR for A320 NEO ACJ new configuration.

o Variation 6.3 : Provides impact on ALS part 3 – CMR related to introduction of new A319 NEO models (A319-151N and A319-153N), as well as introduction of A319 NEO ACJ new configuration.

Changes introduced directly in the Revision : o Clarify the applicability of CMR 282800-00001-1-C to make

reference to MOD 30229 (introduce upgraded FQIC stage 7)

o Clarify the applicability of CMRs 213100-00001-1C, 213100-00001-2C, 213100-00001-3C, 262300-00001-1C and 262300-00002-1C to differentiate between PAX and CJ configurations

o Extend the applicability of CMR 526000-00001-1-C from A319 NEO CJ fitted with airstairs (A319 POST 162338 POST 23398) to complete fleet of SA aircraft fitted with airstairs (POST 20062 OR POST 23398)

o In consequence of MRBR rev. 24 evolution, introduce new CMR 282800-00006-1-C ; for 1st realization of considered CMR on aircraft POST 25415, credit can be taken from last accomplishment of MRBR task 28.28.00/01

o Introduction of following new models : A320-253N, A320-272N and A320-273N (CMR table not impacted).

OCT 11/19

07at issue 02

The A318/A319/A320/A321 ALS Part 3 Revision 07 Issue 02 has been released in order to introduce compliance time for CMR 282800-00006-1-C.

JAN 17/20

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - APPENDIX E PAGE: 28/29


APPENDIX E. SUMMARY OF CHANGES

GENERAL

Summary of Changes (SOC) from previous ALS Revisions are not published within this ALS Part 3. SOC for previous Revisions could be found within the related Revision.

Except in SECTION 3, non-administrative changes are highlighted with a revision bar in the left hand margin in front of the line different from previous Revision of the ALS Part 3.

In SECTION 3, CMR changes are highlighted with the following movement codes printed in the left hand margin of the CMR when different from previous Revision of the ALS Part 3:

- <N> = CMR is new, - <R> = CMR has been revised, - <D> = CMR has been deleted.

In this section, administrative changes are not highlighted but are identified in the SOC column.

COVER PAGE

The cover page has been revised to amend the Revision number and to update Airbus logo.

TABLE OF CONTENT

Table of content has been updated accordingly to the changes performed throughout the document.

REVISION STATUS

The first frame has been updated in order to take into account subjects approved under DOA authority.

This section has been updated to provide the:

- Approval date and reference of the A318/A319/A320/A321 ALS Part 3 Revision 07,

- Reasons of the Variations compiled in this Revision,

- The revision status now displays additional changes that were not published through Variations. For detailed traceability in the SOC, group of changes have been defined in a new table.

COMPLIANCE TIME

This section has been updated to provide the list of instructions and airworthiness limitations which have been revised and introduced in the A318/A319/A320/A321 ALS Part 3 Revision 07 as well as their associated implementation period and compliance time (when applicable). This information comes from the original data which have been introduced in the current Revision.

SECTION 1 – INTRODUCTION

Page 8 - §2: Applicability table has been updated to introduce new A319-151N, A319-153N,

A320-253N, A320-272N and A320-273N aircraft models.

A320 Family


ISSUE: JAN 17/20 ALS PART 3 - APPENDIX E PAGE: 29/29


Page 10 - §3: MPPT table has been updated following new A320 NEO ACJ and A319 NEO ACJ. Notes and clarifications have been updated accordingly.

SECTION 2 – EXPLANATION OF TABLE FORMAT

Page 16 - §6: Applicability table has been updated to add A319N, A320-VIP and A320-PAX.

SECTION 3 – CERTIFICATION MAINTENANCE REQUIREMENTS (CMR)

Limitations table with its associated change description has been transferred in the embedded excel file.

APPENDIX A - ABBREVIATIONS

Following abbreviation has been added: ACJ.

Following abbreviations have been deleted: CV and SEC.

APPENDIX B - TERMS AND DEFINITIONS

No change.

APPENDIX C - LIST OF DELETED TASKS

This section lists the deleted CMR tasks from previous Revisions.

APPENDIX D - HISTORY FILE

The section has been updated to add the reason for issuance of the ALS Part 3 Revision 07.

APPENDIX E - SUMMARY OF CHANGES

This section provides the changes introduced in the ALS Part 3 Revision 07.