a320 family als part 3 revision 06 - regulations.gov

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ISSUE: JUN 13/18

C80_ALS Part 3 Scheduled Revision Template_FM1404445_v3.0

A318/A319/A320/A321

Airworthiness Limitations Section (ALS)

Part 3

Certification Maintenance Requirements (CMR)

-

Revision 06

AIRWORTHINESS LIMITATIONS SECTION

ISSUE: JUN 13/18 ALS PART 3 - TOC PAGE: 2/42

© AIRBUS SAS 2018. All rights reserved. Confidential and proprietary document.

TABLE OF CONTENTS

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

COMPLIANCE TIME ...................................................................................................................... 4

SECTION 1. INTRODUCTION ................................................................................................... 7

1. GENERAL ............................................................................................................................. 7

2. APPLICABILITY .................................................................................................................... 7

3. MAINTENANCE PROGRAM PUBLICATION ........................................................................ 9

4. DEFINITION OF ALS PART 3 CONTENT ........................................................................... 11

4.1 CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) ..................................... 11

4.1.1 ONE STAR CMR (*) .........................................................................................11

4.1.2 TWO STAR CMR (**) .......................................................................................11

5. BASIC RULES .................................................................................................................... 11

5.1 CLOCK STARTING POINT FOR CMR ....................................................................... 11

5.2 EXCEPTIONAL SHORT-TERM EXTENSIONS .......................................................... 12

6. INTENTIONALLY LEFT BLANK ......................................................................................... 13

7. PRODUCTION CONCESSIONS, REPAIRS, ALS VARIATIONS, AIRWORTHINESS DIRECTIVES AND ALTERNATIVE METHODS OF COMPLIANCE .................................... 13

8. MODIFICATIONS/REPAIRS NOT DEVELOPED BY AIRBUS DOA CERTIFICATE EASA.21J.031 ..................................................................................................................... 13

SECTION 2. EXPLANATION OF TABLE FORMAT................................................................. 14

SECTION 3. CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) ............................. 18

APPENDIX A. ABBREVIATIONS ............................................................................................... 31

APPENDIX B. TERMS AND DEFINITIONS ................................................................................ 34

APPENDIX C. LIST OF DELETED TASKS ................................................................................. 36

APPENDIX D. HISTORY FILE .................................................................................................... 37

APPENDIX E. SUMMARY OF CHANGES .................................................................................. 39


ISSUE: JUN 13/18 ALS PART 3 - REVISION STATUS PAGE: 3/42


REVISION STATUS

The Airbus A318/A319/A320/A321 ALS Part 3 is approved and Variations must also be approved.

The present Revision includes already EASA approved ALS data. The technical content of this Revision is approved under the authority of DOA Ref.: EASA.21J.031.

REVISION NUMBER APPROVAL REFERENCE APPROVAL DATE

06 D050318060 JUN 13/18

This Revision contains all approved changes to A318/A319/A320/A321 ALS Part 3 since the last Revision, including changes published through the following Variations:

VARIATION NUMBER REASON OF THE VARIATION

5.1

This Variation aims to provide the impact on the mandatory instructions and airworthiness limitations published in the Revision 05 of A318/A319/A320/A321 ALS Part 3 - CMR, as a result of the introduction of a new CMR task 282800-00002-1-C in the frame of certification of MOD 160832. MOD 160832 extends introduction of 1 or 2 Additional Center Tanks (ACTs) on A321 NEO.

5.2

MOD 162038 introduces the new A321-272N aircraft model. This Variation to Revision 05 of the A318/A319/A320/A321 ALS Part 3 – CMR aims at providing the mandatory instructions and airworthiness limitations for Certification Maintenance Requirements (CMRs) when installed on aircraft Post-MOD 162038.

Additional approved changes that were not published are introduced by this Revision and can be identified in the APPENDIX E – Summary Of Changes.


ISSUE: JUN 13/18 ALS PART 3 - COMPLIANCE TIME PAGE: 4/42


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 06. 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. Accomplishment of maintenance tasks in SECTION 3 will also be mandated by the future AD and are to be accomplished prior to the new/revised thresholds and/or 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 thresholds and/or intervals. In such a case, accomplishment of maintenance tasks in SECTION 3 are to be accomplished prior to the new/revised thresholds and/or 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.




SECTION REV

CODE ITEMS

VARIATION

NUMBER (when applicable)

COMPLIANCE TIME

COMPLIANCE

TIME

APPLICABILITY

3

323000-00001-1-C N/A

For A318 / A319 / A320 / A321 CEO aircraft, next CMR 323000-00001-1-C accomplishment must be carried out no later than :

A. following correction time : A.1. 21/SEP/2018

[corresponding to 12 months from the Effective Date of the EASA Airworthiness Directive that has been issued to mandate the Revision 05 of A318/A319/A320/A321 ALS Part 3],

OR A.2. within the due MRBR interval (36 MO from

aircraft Entry Into Service, OR from last accomplishment of MRBR task 32.30.00/08, whichever occurs later),

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

OR

B. within the due CMR interval (7 700 FH from aircraft Entry Into Service, OR from last accomplishment of MRBR task 32.30.00/08, whichever occurs later),

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

A318

OR

A319

OR

A320 PRE 161000

PRE 161003

OR

A321 PRE 161002

PRE 161005




SECTION REV

CODE ITEMS

VARIATION

NUMBER (when applicable)

COMPLIANCE TIME

COMPLIANCE

TIME

APPLICABILITY

3 N 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. 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,

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 159954

OR

A320 PRE 161000

PRE 161003

PRE 159954

OR

A321 PRE 161002

PRE 161005

PRE 159954


ISSUE: JUN 13/18 ALS PART 3 - SECTION 1 PAGE: 7/42


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

A320-200

A320-211

A320-212

A320-214

A320-215

A320-216

A320-231

A320-232




AIRCRAFT SERIES AIRCRAFT MODELS

A320-200

A320-233

A320-251N

A320-252N

A320-271N

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




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 SERIES

PUBLICATION TRIGGER (Whichever occurs first)

FLIGHT HOURS (FH) FLIGHT CYCLES (FC)

A318-100 60 000 48 000

A319-100 PRE 155789 (Excluding Corporate Jet Operations)

60 000 48 000

A319-100 CJ (Corporate Jet Operations) (A319 POST 28162 POST 28238 POST 28342)

77 400 18 000

A319-100 POST 160080 (Excluding Corporate Jet Operations)

96 000 48 000

A319-100 POST 155789 (Excluding Corporate Jet Operations)

120 000 60 000

A320-200 PRE 37734 PRE 39020 60 000 48 000

A320-200 POST 37734 PRE 39020 80 000 37 500

A320-200 POST 39020 120 000 60 000

A320-200 POST 20139 PRE 22129 POST 39020

63 500 45 000

A320-200 POST 160080 96 000 48 000

A321-100 PRE 154881 PRE 156130 60 000 48 000

A321-100 POST 154881 PRE 156130 74 000 37 000

A321-200 PRE 154881 PRE 156130 60 000 48 000

A321-200 POST 154881 PRE 156130 74 000 37 000

A321-100 POST 156130 120 000 60 000

A321-200 POST 156130 120 000 60 000

A318 / A319 / A320 / A321 NEO aircraft 96 000 48 000




Note:

- A319-100 used as Corporate Jet Operations (A319-VIP) have received MOD 28238, MOD 28162 and MOD 28342 in production.

- MOD 155789 refers to Design Service Goal (DSG) extension of A319-100 aircraft up to 120 000 FH or 60 000 FC, whichever occurs first.



- MOD 39020 refers to Design Service Goal (DSG) extension of A320-200 POST 20139 PRE 22129 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 160080 introduces the sharklet devices in the A319-100 or A320-200 in-service

aircraft and extends the Design Service Goal (DSG) of the A319-100 (excluding

Corporate Jets Operations) POST MOD 160080 or A320-200 POST MOD 160080 up

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

- A318 / A319 / A320 / A321 NEO aircraft includes: A320-251N (A320 POST MOD 161003), A320-252N (A320 POST MOD 162680), A320-271N (A320 POST MOD 161000), 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), 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 models a Design Service Goal (DSG) of 96 000 FH or 48 000 FC, whichever occurs first, has been set.

- MOD 156130 introduces the Extended Service Goal (ESG) of the A321-100 POST

MOD 156130 and A321-200 POST MOD 156130 up to 120 000 FH or 60 000 FC,

whichever occurs first.




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.

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.




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.




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).




(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.

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.

A320 All A320 only.

A320N All A320 NEO only

A321 All A321 only.

A321N All A321 NEO only

A319-VIP A319 Corporate Jet Operations (POST 28162 POST 28238 POST 28342).

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

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.

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.

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.




SECTION 3. CERTIFICATION MAINTENANCE REQUIREMENTS (CMR)

CMR REF. NUMBER

CMR CAT.


APPLICABILITY

R 212800-00001-1-C CMR** CARGO COMPARTMENT, VENTILATION AND HEATING AND AFT CARGO COMPARTMENT GROUND COOLING SYSTEM OPERATIONAL CHECK OF THE GROUND COOLING ISOLATION VALVE TO VERIFY CLOSING IN CASE OF SMOKE WARNING

12 000 FH 21.28.00/04 A320 POST 20819

213100-00001-1-C CMR** PRESSURE CONTROL AND MONITORING FUNCTIONAL CHECK OF POSITIVE/NEGATIVE DELTA P PROTECTION OF SAFETY VALVES

50 000 FH 21.31.00/06 A318 OR A319-PAX PRE 155789 PRE 160080 OR A320 PRE 37734 PRE 39020 PRE 160080 PRE 161000 PRE 161003 OR A320 POST 20139 PRE 22129 POST 39020 OR A321 PRE 154881 PRE 156130 PRE 161002 PRE 161005




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

213100-00001-2-C CMR** PRESSURE CONTROL AND MONITORING FUNCTIONAL CHECK OF POSITIVE/NEGATIVE DELTA P PROTECTION OF SAFETY VALVES

44 000 FH 21.31.00/06 A319-VIP OR A320 POST 37734 PRE 39020 PRE 160080 PRE 161000 PRE 161003 OR A321 POST 154881 PRE 156130 PRE 161002 PRE 161005




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

213100-00001-3-C CMR** PRESSURE CONTROL AND MONITORING FUNCTIONAL CHECK OF POSITIVE/NEGATIVE DELTA P PROTECTION OF SAFETY VALVES NOTE: FOR A321 POST 156130 AIRCRAFT, FIRST ACCOMPLISHMENT

OF CMR TASK 213100-00001-3-C MUST BE CARRIED OUT NO LATER THAN THE AIRCRAFT ACCUMULATING 36 000 FH SINCE THE ENTRY INTO SERVICE, OR SINCE THE LAST ACCOMPLISHMENT OF MRBR TASK 21.31.00/06, OR SINCE THE LAST ACCOMPLISHMENT OF CMR 213100-00001-1-C, OR SINCE THE LAST ACCOMPLISHMENT OF CMR 213100-00001-2-C, WHICHEVER OCCURS THE LATEST.

36 000 FH 21.31.00/06 A319-PAX POST 155789 OR A319-PAX POST 160080 OR A320 POST 39020 PRE 20139 OR A320 POST 39020 POST 22129 OR A320 POST 160080 OR A320 POST 161000 OR A320 POST 161003 OR A321 POST 156130 OR A321 POST 161002 OR A321 POST 161005




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

242000-00001-1-C CMR* AC GENERATION OPERATIONAL CHECK OF STATIC INVERTER

90 FH 24.20.00/18 A320 POST 24701 PRE 28160 OR A320 POST 28917

242000-00001-2-C CMR** AC GENERATION OPERATIONAL CHECK OF STATIC INVERTER

750 FH 24.20.00/17 A318 OR A319 OR A320 POST 28160 PRE 28917 OR A321

242000-00002-1-C CMR* AC GENERATION OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM

120 FH 24.20.00/15 A318 OR A319 OR A320 POST 27189 PRE 28413 OR A321

242000-00002-2-C CMR* AC GENERATION OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM

90 FH 24.20.00/16 A320 POST 24701 PRE 27189 OR A320 POST 28413

262300-00001-1-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING CHECK FIRING CIRCUIT CONTINUITY

12 000 FH 26.23.00/03 26.23.00/07

A/C fitted with cargo compartment fire extinguishing




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

262300-00002-1-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND OBSTRUCTION

18 000 FH 26.23.00/04 A/C fitted with cargo compartment fire extinguishing

R 271400-00001-1-C CMR** AILERON HYDRAULIC ACTUATION OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE

5 000 FH 27.14.00/01 ALL

D 271400-00001-2-C TASK DELETED

R 271400-00002-1-C CMR** AILERON HYDRAULIC ACTUATION CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC RESERVOIR DEPRESSURIZED

24 000 FH 27.14.00/02 ALL


R 273400-00001-1-C CMR** ELEVATOR AND HYDRAULIC ACTUATION OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE

5 000 FH 27.34.00/01 ALL


R 273400-00002-1-C CMR** ELEVATOR AND HYDRAULIC ACTUATION CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC RESERVOIR DEPRESSURIZED

24 000 FH 27.34.00/02 ALL


R 273400-00002-3-C CMR* ELEVATOR AND HYDRAULIC ACTUATION CHECK OF THE DIFFERENTIAL PRESSURE INDICATOR AND POSITION OF FLUID RESERVE PISTON OF ELEVATOR SERVOCONTROLS

36 000 FH 27.34.00/04 FAA Only

274000-00001-1-C CMR* TRIMMABLE HORIZONTAL STABILIZER (THS) CHECK INTEGRITY OF THS ACTUATOR BALLSCREW SHAFT (PRIMARY AND SECONDARY LOAD PATH)

12 000 FH 27.40.00/16 ALL




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

274000-00002-1-C CMR** TRIMMABLE HORIZONTAL STABILIZER (THS) OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL HYDRAULIC SYSTEMS

750 FH 27.40.00/01 ALL

274000-00003-1-C CMR** TRIMMABLE HORIZONTAL STABILIZER (THS) OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION DEVICE

4 000 FH 27.40.00/02 ALL

275000-00001-1-C CMR** FLAPS OPERATIONAL CHECK OF WTB/POB AND CHECK OF FLAPS TRANSMISSION SHAFTING INTEGRITY, INCLUDING INSPECTION OF SEAL WITNESS DRAINS

12 000 FH 27.50.00/04 27.50.01/04

A318 OR A319-PAX OR A320 OR A321

275000-00001-2-C CMR** FLAPS OPERATIONAL CHECK OF WTB/POB AND CHECK OF FLAPS TRANSMISSION SHAFTING INTEGRITY, INCLUDING INSPECTION OF SEAL WITNESS DRAINS

7 500 FH 27.50.00/04 A319-VIP

278000-00001-1-C CMR** LIFT AUGMENTING (SLATS) OPERATIONAL CHECK OF WTB/POB AND CHECK OF SLATS TRANSMISSION SHAFTING INTEGRITY, INCLUDING INSPECTION OF SEAL WITNESS DRAINS

12 000 FH 27.80.00/04 A318 OR A319-PAX OR A320 OR A321

278000-00001-2-C CMR** LIFT AUGMENTING (SLATS) OPERATIONAL CHECK OF WTB/POB AND CHECK OF SLATS TRANSMISSION SHAFTING INTEGRITY, INCLUDING INSPECTION OF SEAL WITNESS DRAINS

7 500 FH 27.80.00/04 A319-VIP




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

279000-00001-1-C CMR* ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS) OPERATIONAL CHECK: - OF LOGICS ACTIVATING ELAC 1, ELAC 2 AND SEC. 1 STANDBY POWER SUPPLIES - TO CONFIRM ABILITY OF SEC. 1 AND SEC. 2 TO ACHIEVE PITCH CONTROL - TO CONFIRM ABILITY OF SIDESTICK PRIORITY FUNCTION

400 FH 27.90.00/02 ALL

R 281500-00001-1-C CMR** INTERCELL TRANSFER SYSTEM OPERATIONAL CHECK OF INDIVIDUAL TRANSFER VALVES TO ENSURE VALVE SHAFT ROTATES VALVE TO OPEN POSITION

10 000 FH 28.15.00/02 A318 OR A319 OR A320 PRE 161000 PRE 161003

N 281500-00001-2-C CMR** INTERCELL TRANSFER SYSTEM OPERATIONAL CHECK OF INDIVIDUAL TRANSFER VALVES TO ENSURE VALVE SHAFT ROTATES VALVE TO OPEN POSITION

7 500 FH 28.15.00/02 A320 POST 161000 OR A320 POST 161003

282100-00001-1-C CMR** MAIN FUEL PUMP SYSTEM OPERATIONAL CHECK TO ENSURE THAT BOTH CENTER TANK PUMPS FEED FOR 2 MINUTES AFTER ENGINE START

10 000 FH 28.21.00/03 A318 OR A319 PRE 154327 OR A320 PRE 154327




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

282800-00001-1-C CMR** ADDITIONAL CENTER TANK TRANSFER SYSTEM OPERATIONAL CHECK OF THE ACT MANUAL TRANSFER SYSTEM NOTE: EMBODIMENT OF FQIC 7 (MOD 30229) OR LATER STANDARD CANCELS THE CMR STATUS. NOTE THAT FOR A321 POST 28653, FQIC 6 IS PERMITTED ONLY WITH ONE ACT REMOVED NOTE: IF NO ACT(S) ARE FITTED WHEN THE TASK BECOMES DUE, TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION NOTE: TASK IS INCLUDED IN THE ACT INSTALLATION PROCEDURE. CREDIT CAN BE TAKEN FROM ACCOMPLISHMENT OF THE TASK AT THIS OPPORTUNITY

7 900 FH 28.28.00/13 A321 POST 25453 POST 25504 IF ACT(S) INSTALLED NOTE OR A321 POST 28653 POST 25504 IF ACT(S) INSTALLED NOTE

N 282800-00002-1-C CMR* ADDITIONAL CENTER TANK TRANSFER SYSTEM FUNCTIONAL CHECK OF THE VENT/TRANSFER PIPE SHROUDS AND ACT DRAIN PIPE CONNECTORS

10 700 FH 28.28.00/12 A321 POST 161002 POST 25415 IF ACT(S) INSTALLED OR A321 POST 161005 POST 25415 IF ACT(S) INSTALLED

284200-00001-1-C CMR* QUANTITY INDICATING OPERATIONAL CHECK OF FUEL TEMPERATURE INDICATIONS

31 600 FH - A321 POST 155635




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

291000-00001-1-C CMR* MAIN AND AUXILIARY HYDRAULIC POWER OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT, FOLLOWED BY CHECK OF FILTER INDICATOR

1 500 FH OR

8 MO (WHICHEVER

COMES FIRST)

29.10.00/07 A320 PRE 27189 OR A320 POST 28413

291000-00001-2-C CMR* MAIN AND AUXILIARY HYDRAULIC POWER OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT, FOLLOWED BY CHECK OF FILTER INDICATOR

3 600 FH OR

18 MO (WHICHEVER

COMES FIRST)

29.10.00/29 A318 OR A319 OR A320 POST 27189 PRE 28413 OR A321

291000-00002-1-C CMR* MAIN AND AUXILIARY HYDRAULIC POWER OPERATIONAL CHECK OF RAT AUTOMATIC DEPLOYMENT

3 600 FH OR

18 MO (WHICHEVER

COMES FIRST)

29.10.00/08 ALL

291000-00003-1-C CMR* MAIN AND AUXILIARY HYDRAULIC POWER FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF BLUE HYDRAULIC SYSTEM

12 000 FH 29.10.00/12 ALL

291000-00004-1-C CMR** MAIN AND AUXILIARY HYDRAULIC POWER CHECK NITROGEN CHARGE PRESSURE ON THE BLUE MAIN SYSTEM ACCUMULATOR

400 FH 29.10.00/04 A320 PRE 21414 PRE 21999

R 291000-00005-1-C CMR** MAIN AND AUXILIARY HYDRAULIC POWER REMOVE RAM AIR TURBINE AGCM AND PUMP FOR IN SHOP FUNCTIONAL CHECK

24 000 FH 29.10.00/26 A320 PRE 27189 OR A320 POST 28413




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

291000-00006-1-C CMR* MAIN AND AUXILIARY HYDRAULIC POWER DETAILED INSPECTION OF RAT CARBON BLADES FOR EVIDENCE OF PLATING CRACKS

3 600 FH OR

18 MO (WHICHEVER

COMES FIRST)

29.10.00/34 A/C fitted with PNR 762308

323000-00001-1-C CMR* EXTENSION/RETRACTION OPERATIONAL CHECK OF FREE-FALL MECHANICAL CONTROL

7 700 FH 32.30.00/08 ALL

R 324000-00001-1-C CMR* WHEELS AND BRAKES OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM

11 600 FH 32.40.00/08 PRE 26925


324000-00002-1-C CMR* WHEELS AND BRAKES FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM

60 000 FH 32.40.00/17 A320 PRE 26925 PRE 20139 OR A320 PRE 26925 POST 20139 POST 22129

324500-00002-1-C CMR* WHEELS AND BRAKES FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF BRAKING SYSTEM COMPONENTS (PARK BRAKE SELECTOR VALVE, PRESSURE RELIEF VALVE AND ALTERNATE BRAKE SELECTOR VALVE)

14 800 FH - A319 POST 28238 POST 26925




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

352000-00001-1-C CMR** PASSENGER OXYGEN SYSTEM (CHEMICAL) OPERATIONAL CHECK OF MANUAL MASK RELEASE

8 500 FH 35.20.00/01 A318 OR A319 PRE 33125 OR A320 OR A321

352000-00002-1-C CMR** PASSENGER OXYGEN SYSTEM (CHEMICAL) FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE, DETAILED INSPECTION OF MASKS AND VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS

24 000 FH 35.20.00/02 A318 OR A319 PRE 33125 OR A320 OR A321

352000-00003-1-C CMR** PASSENGER OXYGEN SYSTEM (GASEOUS) REMOVE PRESSURE REGULATORS FOR IN SHOP FUNCTIONAL CHECK

8 000 FH 35.20.01/04 A319 POST 33125

N 361200-00001-1-C CMR* APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS CHECK OF APU BLEED CHECK VALVE FOR CONDITION

13 000 FH 36.12.00/01 36.12.00/02

A318 PRE 159954 OR A319 PRE 159954 OR A320 PRE 161000 PRE 161003 PRE 159954 OR A321 PRE 161002 PRE 161005 PRE 159954




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

N 522101-00001-1-C CMR* AUTOMATIC OVERWING EMERGENCY EXIT DOOR OPERATIONAL CHECK OF EMERGENCY OVERWING DOOR MECHANISMS NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY OVER-WING DOOR

16 300 FH - A321 POST 160766

N 522101-00002-1-C CMR* AUTOMATIC OVERWING EMERGENCY EXIT DOOR OPERATIONAL CHECK OF ESCAPE SLIDE RELEASE MECHANISM NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY OVER-WING DOOR

23 800 FH 52.21.01/02 A321 POST 160766 FAA ONLY

N 522101-00003-1-C CMR* AUTOMATIC OVERWING EMERGENCY EXIT DOOR FUNCTIONAL CHECK OF FLIGHT LOCK MECHANISM NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY OVER-WING DOOR

23 800 FH 52.21.01/03 A321 POST 160766

N 522101-00004-1-C CMR* AUTOMATIC OVERWING EMERGENCY EXIT DOOR FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE RELEASE SIGNAL NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY OVER-WING DOOR

23 800 FH - A321 POST 160766

783100-0CL01-1-C CMR* THRUST REVERSER CONTROL AND INDICATING OPERATIONAL CHECK OF SYNCHRONIZED LOCKING FEEDBACK ACTUATOR (SLFA) FOR LOCKING CAPABILITY

22 500 FH - LEAP-1A




CMR REF. NUMBER

CMR CAT.


APPLICABILITY

783100-0CL02-1-C CMR* THRUST REVERSER CONTROL AND INDICATING DETAILED INSPECTION OF THE ATTACHMENT OF THE SYNCHRONIZED LOCKING FEEDBACK ACTUATOR (SLFA) TO THE TRANSLATING SLEEVE AND TO THE FORWARD FRAME

22 500 FH - LEAP-1A


ISSUE: JUN 13/18 ALS PART 3 - APPENDIX A PAGE: 31/42


APPENDIX A. ABBREVIATIONS

ABBREVIATION MEANING

A/C Aircraft

AC Alternative Current

ACF Airbus Cabin Flex

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

CV Check Valve

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

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

SEC Spoiler and Elevator Computer

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)


ISSUE: JUN 13/18 ALS PART 3 - APPENDIX B PAGE: 34/42


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.


ISSUE: JUN 13/18 ALS PART 3 - APPENDIX B PAGE: 35/42


TERM DEFINITION

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.


ISSUE: JUN 13/18 ALS PART 3 - APPENDIX C PAGE: 36/42


APPENDIX C. LIST OF DELETED TASKS

TASK REFERENCE SUMMARY OF CHANGES

291000-00001-3-C Task deleted in Revision 03.


ISSUE: JUN 13/18 ALS PART 3 - APPENDIX D PAGE: 37/42


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


ISSUE: JUN 13/18 ALS PART 3 - APPENDIX D PAGE: 38/42


REVISION NUMBER

REASONS FOR REVISION REVISION

DATE

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

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


ISSUE: JUN 13/18 ALS PART 3 - APPENDIX E PAGE: 39/42


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, 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.

COVER PAGE

The cover page has been revised to amend the Revision number.

TABLE OF CONTENT

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

REVISION STATUS

This section has been updated to provide the:

- Approval date and reference of the A318/A319/A320/A321 ALS Part 3 Revision 06,

- Reasons of the Variations compiled in this Revision.

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 06 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 – Applicability, General applicability table: A320-252N, A321-252N, A321-272N, A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX models have been added.

Page 10 – MAINTENANCE PROGRAM PUBLICATION, note A318 / A319 / A320 / A321 NEO aircraft: A320-252N, A321-251NX, A321-252N, A321-252NX, A321-253NX, A321-271NX, A321-272N and A321-272NX have been added.




SECTION 2 – EXPLANATION OF TABLE FORMAT

Page 14 – Paragraph (1) updated for harmonization purpose.

SECTION 3 – CERTIFICATION MAINTENANCE REQUIREMENTS (CMR)

Additional approved changes that were not published through Variations 5.1 and 5.2 are identified by “N/A*”, “N/A**” and “N/A***” in the Variation Number column as follows:

N/A*: This change aims at providing the impact on the mandatory instructions and airworthiness limitations for Certification Maintenance Requirements (CMRs) when installed on aircraft Post-MOD 160766 (new models A321 NEO ACF).

N/A**: This change aims at providing the mandatory instructions and airworthiness limitations for Certification Maintenance Requirements (CMRs) following revision and introduction of CMR tasks following MRBR evolution.

N/A***: This change aims at providing the mandatory instructions and airworthiness limitations for Certification Maintenance Requirements (CMRs) following revision of ATA 27 CMR tasks applicable only to US registered aircrafts.

N/A****: This change aims at providing the impact on the mandatory instructions and airworthiness limitations for Certification Maintenance Requirements (CMRs) following introduction of new CMR 361200-00001-1-C.

REV CODE

ITEMS VARIATION NUMBER

CHANGE DESCRIPTION

R 212800-00001-1-C N/A** Interval updated from 6 000 FH to 12 000 FH.

R 271400-00001-1-C

N/A** Interval updated from 4 000 FH to 5 000 FH.

N/A*** Applicability updated from ‘ALL except FAA’ to ‘ALL’.

D 271400-00001-2-C N/A*** Task deleted.

R 271400-00002-1-C




R 273400-00001-1-C N/A** Interval updated from 4 000 FH to 5 000 FH.






R 273400-00002-1-C




R 273400-00002-3-C N/A*** Interval updated from 12 000 FH to 36 000 FH.

R 281500-00001-1-C N/A**

Interval updated from 7 500 FH to 10 000 FH. Applicability updated from ‘A318 OR A319 OR A320’ to ‘A318 OR A319 OR A320 PRE 161000 PRE 161003’ (CEO aircraft only).

N 281500-00001-2-C N/A** New CMR task added for A320 NEO aircraft (previously applicable through CMR 281500-00001-1-C).

N 282800-00002-1-C 5.1 New CMR task added.

R 291000-00005-1-C N/A**

Description updated from ‘REMOVE RAM AIR TURBINE AGCM AND PUMP FOR FUNCTIONAL CHECK’ to ‘REMOVE RAM AIR TURBINE AGCM AND PUMP FOR IN SHOP FUNCTIONAL CHECK’.

R 324000-00001-1-C N/A** Interval updated from 6 300 FH to 11 600 FH

D 324000-00001-2-C N/A** Task deleted.

N 361200-00001-1-C N/A**** New CMR task added.

N 522101-00001-1-C N/A* New CMR task added.




APPENDIX A - ABBREVIATIONS

The following abbreviations have been added: ACF, AMM, Cal., CEO, CV, MLG, N/A.




APPENDIX B - TERMS AND DEFINITIONS

The following definitions have been added: Entry-Into-Service

APPENDIX C - LIST OF DELETED TASKS

No change.

APPENDIX D - HISTORY FILE

The section has been updated to add the reason for issuance of the ALS Part 3 Revision 06.

APPENDIX E - SUMMARY OF CHANGES

This section provides the changes introduced in the ALS Part 3 Revision 06.