A318/A319/A320/A321 Airworthiness Limitations Section (ALS) Part 3 Certification Maintenance Requirements (CMR) - Revision 06 AIRBUS SAS 2018. 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. ISSUE: JUN 13/18 C80_ALS Part 3 Scheduled Revision Template_FM1404445_v3.0 AIRWORTHINESS LIMITATIONS SECTION 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 - TOC PAGE: 2/42 © AIRBUS SAS 2018. All rights reserved. Confidential and proprietary document. AIRWORTHINESS LIMITATIONS SECTION 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 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 5.1 certification of MOD 160832. MOD 160832 extends introduction of 1 or 2 Additional Center Tanks (ACTs) on A321 NEO. MOD 162038 introduces the new A321-272N aircraft model. This Variation to Revision 05 of the A318/A319/A320/A321 ALS 5.2 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 - REVISION STATUS PAGE: 3/42 © AIRBUS SAS 2018. All rights reserved. Confidential and proprietary document. AIRWORTHINESS LIMITATIONS SECTION 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. ISSUE: JUN 13/18 ALS PART 3 - COMPLIANCE TIME PAGE: 4/42 © AIRBUS SAS 2018. All rights reserved. Confidential and proprietary document. AIRWORTHINESS LIMITATIONS SECTION COMPLIANCE REV VARIATION SECTION ITEMS COMPLIANCE TIME TIME CODE NUMBER (when applicable) APPLICABILITY 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 A318 has been issued to mandate the Revision 05 of OR A318/A319/A320/A321 ALS Part 3], A319 OR A.2. within the due MRBR interval (36 MO from OR 3 323000-00001-1-C N/A aircraft Entry Into Service, OR from last A320 PRE 161000 accomplishment of MRBR task 32.30.00/08, PRE 161003 whichever occurs later), OR whichever occurs first (between A.1. and A.2.) A321 PRE 161002 OR PRE 161005 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.). ISSUE: JUN 13/18 ALS PART 3 - COMPLIANCE TIME PAGE: 5/42 © AIRBUS SAS 2018. All rights reserved. Confidential and proprietary document. AIRWORTHINESS LIMITATIONS SECTION COMPLIANCE REV VARIATION SECTION ITEMS COMPLIANCE TIME TIME CODE NUMBER (when applicable) APPLICABILITY 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 A318 PRE 159954 issued to mandate the Revision 06 of OR A318/A319/A320/A321 ALS Part 3, OR A319 PRE 159954 A.2. next planned realization of Maintenance OR Procedure AMM 361251-200-001 (associated to A320 PRE 161000 3 N 361200-00001-1-C N/A MRBR tasks 36.12.00/01 or 36.12.00/02, PRE 161003 depending on aircraft configuration), whichever occurs first (between A.1. and A.2.) PRE 159954 OR OR A321 PRE 161002 PRE 161005 B. within the due CMR interval [13 000 FH from aircraft Entry Into Service, OR 13 000 FH from last PRE 159954 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.). ISSUE: JUN 13/18 ALS PART 3 - COMPLIANCE TIME PAGE: 6/42 © AIRBUS SAS 2018. All rights reserved. Confidential and proprietary document. AIRWORTHINESS LIMITATIONS SECTION SECTION 1. INTRODUCTION 1. GENERAL The ALS Part 3 provides Certification Maintenance Requirements (CMR) which are system related periodic