A300-600 ALS Part 3 Revision 01

A300-600

Airworthiness Limitations Section (ALS) Part 3 Certification Maintenance Requirements (CMR) - Revision 01

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: AUG 28/17

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 ...... 5 1 GENERAL ...... 5 2 APPLICABILITY ...... 5 3 MAINTENANCE PROGRAM PUBLICATION ...... 5 4 DEFINITION OF ALS PART 3 CONTENT...... 6 4.1 CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) ...... 6 4.1.1 ONE STAR CMR (*) ...... 6 4.1.2 TWO STAR CMR (**) ...... 6 5 BASIC RULES ...... 6 5.1 CLOCK STARTING POINT FOR CMR ...... 6 5.2 EXCEPTIONAL SHORT-TERM EXTENSIONS ...... 7 6 INTENTIONALLY LEFT BLANK ...... 8 7 PRODUCTION CONCESSIONS, REPAIRS, ALS VARIATIONS, AIRWORTHINESS DIRECTIVES AND ALTERNATIVE METHODS OF COMPLIANCE ...... 8 8 MODIFICATIONS/REPAIRS NOT DEVELOPED BY AIRBUS DOA CERTIFICATE EASA.21J.031 .. 8

SECTION 2. EXPLANATION OF TABLE FORMAT ...... 9

SECTION 3. CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) ...... 12 1 CMR TASKS ...... 12 2 CMR TASKS SPECIFIC TO A300-600ST ...... 20

APPENDIX A. ABBREVIATIONS ...... 22

APPENDIX B. TERMS AND DEFINITIONS ...... 24

APPENDIX C. LIST OF DELETED TASKS ...... 25

APPENDIX D. HISTORY FILE ...... 26

APPENDIX E. SUMMARY OF CHANGES ...... 27

ISSUE: AUG 28/17 ALS PART 3 - TOC PAGE: 2/29

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REVISION STATUS

The Airbus A300-600 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 01 C050317010 AUG 28/17

This Revision contains all approved changes to A300-600 ALS Part 3 since the last Revision, including changes published through the following Variations:

VARIATION NUMBER REASON OF THE VARIATION This Variation aims to remove the CMR One Star 273300-A0001-1- 0.1 C Artificial Feel (Elevator). This Variation aims to introduce the new ATA 27 CMR One Star task reference 276000-00002-1-C “Operational check of spoiler 0.2 servocontrol hydraulic locking function” with the interval of 22 000 FH.

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

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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 A300-600 ALS Part 3 Revision 01. 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 is 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, accomplishment of maintenance tasks in SECTION 3 is 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.

REV VARIATION COMPLIANCE TIME SECTION ITEMS COMPLIANCE TIME CODE NUMBER APPLICABILITY (when applicable) 3 N 276000-00002-1-C 0.2 30 MO (1) ALL 3 R 323000-A0003-1-C N/A 1200 FH (2) A300-600

(1) First accomplishment must be carried out no later 30 months from the Effective Date of the Airworthiness Directive mandating the A300-600 ALS Part 3 Revision 01.

(2) Without exceeding the airworthiness limitation currently published in A300-600 ALS Part 3 Revision 00. This Compliance Time will be effective at time of issuance of the Airworthiness Directive supporting the introduction of the revised CMR* 323000-A0003-1-C into A300-600 ALS Part 3 Revision 01.

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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 A300-600 ALS Part 3 applies to the following aircraft types, series and models:

AIRCRAFT TYPES AIRCRAFT SERIES AIRCRAFT MODELS A300 B4-601 A300 B4-603 A300 B4-600 A300 B4-620 A300 B4-622 A300 C4-600 A300 C4-620 A300-600 A300 B4-605R A300 B4-600R A300 B4-622R A300 C4-600R A300 C4-605R Variant F A300 F4-605R A300 F4-600R A300 F4-622R A300-600ST N/A A300 F4-608ST

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.

PUBLICATION TRIGGER AIRCRAFT SERIES (whichever occurs first) FLIGHT HOURS (FH) FLIGHT CYCLES (FC) A300-600 89000 51000 A300-600ST 63000 36000

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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.

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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.

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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 Organization 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.

ISSUE: AUG 28/17 ALS PART 3 - SECTION 1 PAGE: 8/29

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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. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER

(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. 0 is the default value. G stands for GE engines, P stands for PW engines. M is used to differentiate aircraft series in Airbus numbering system to which CMR tasks are applicable. 0 is default value. A stands for all A300-600 A/C except A300-600ST, S stands only for A300-600ST. XXXXXX is Maintenance Significant Item (MSI)

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(2) CMR CAT.

This column identifies the CMR categorization: − CMR*: One Star CMR − CMR**: Two Star 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.

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Examples are given below:

APPLICABILITY TASK APPLICABLE TO ALL All A300-600 aircraft (A300-600ST included). A300-600ST All A300-600ST series aircraft A300-600R A300 B4-600R, A300 C4-600R and A300 F4-600R series aircraft only A300 B4-603 A300 B4-603 models aircraft only PRE XXXXX All A300-600 series aircraft on which modification XXXXX has not been embodied POST YYYYY All A300-600 series aircraft on which modification YYYYY has been embodied POST XXXXX A300-600 series aircraft only on which modification XXXXX has been embodied and modification YYYYY PRE YYYYY has not been embodied PW JT9D-7R4 All A300-600 series aircraft on which Pratt & Whitney engines are installed and on which MOD XXXXX POST XXXXX has been embodied CMR limitation applicable only: FAA Only - To US registered aircraft, or - If national authority requires to apply FAA requirements. CMR applicable to all A300-600 aircraft, except: ALL except FAA - US registered aircraft, and - When national authority requires to apply FAA requirements.

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SECTION 3. CERTIFICATION MAINTENANCE REQUIREMENTS (CMR)

1 CMR TASKS

CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 213000-A0001-1-C CMR* PRESSURIZATION CONTROL 14000 FH 21.30.00/06 A300-600 21.30.00/08 REMOVE CABIN PRESSURE SAFETY VALVES FOR FUNCTIONAL CHECK IN SHOP AND OPERATIONAL CHECK OF SAFETY VALVES OPENING INDICATION

NOTE: FIRST ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN THE AIRCRAFT ACCUMULATING 40000 FH 222000-00001-1-C CMR* SPEED ATTITUDE CORRECTION (F.A.C) 00450 FH 22.20.00/01 ALL

OPERATIONAL CHECK TO VERIFY CORRECT OPERATION OF RUDDER CONTROL WITH NO YAW DAMPER ENGAGED AND WITH YAW DAMPER 2 ONLY ENGAGED 222000-A0002-1-C CMR* SPEED ATTITUDE CORRECTION (F.A.C) 85000 FH 22.20.00/02 A300-600

OPERATIONAL CHECK TO VERIFY OVERRIDING AND DISCONNECTION OF ELECTRICAL TRIM 222000-A0003-1-C CMR* SPEED ATTITUDE CORRECTION (F.A.C) 85000 FH 22.20.00/03 A300-600

OPERATIONAL CHECK TO VERIFY CORRECT PITCH TRIM DISENGAGEMENT FOLLOWING AUTOPILOT OVERRIDE 222000-A0004-1-C CMR* SPEED ATTITUDE CORRECTION (F.A.C) 85000 FH 22.20.00/04 A300-600

OPERATIONAL CHECK TO VERIFY CORRECT SAFETY DEVICES IN PITCH TRIM ENGAGEMENT 242000-A0001-1-C CMR* AC GENERATION 04000 FH 24.20.00/02 A300-600

OPERATIONAL CHECK OF AC ESSENTIAL CIRCUIT (GEN. 1 OR GEN. 2 OVER- RIDE SUPPLY)

NOTE: FIRST ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN THE AIRCRAFT ACCUMULATING 75000 FH

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 261500-A0001-1-C CMR** AVIONICS COMPARTMENT SMOKE DETECTION 00460 FH 26.15.00/01 ALL CARGO COMPARTMENT SMOKE DETECTION 26.16.00/01

OPERATIONAL CHECK OF ALL SMOKE DETECTION CHANNELS INCLUDING ASSOCIATED WARNINGS AND CLOSURE OF VALVES IN VENTILATED CARGO COMPARTMENTS 261900-00001-1-C CMR** SMOKE DETECTION, UPPER DECK CARGO COMPARTMENT 00400 FH 26.19.00/01 A300 C4-600

OPERATIONAL CHECK OF ALL SMOKE DETECTION CHANNELS INCLUDING ASSOCIATED WARNINGS 262300-A0001-1-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING 00500 FH 26.23.00/01 A300-600

SQUIB TEST 262300-A0002-1-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING 01600 FH 26.23.00/08 POST 06403

CHECK FIRING CIRCUIT CONTINUITY AND PERFORM OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT AND PRIORITY SWITCHING 262300-A0002-2-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING 08000 FH 26.23.00/04 POST 03699 PRE 04357 CHECK FIRING CIRCUIT CONTINUITY AND PERFORM OPERATIONAL CHECK OR OF LOW PRESSURE INDICATING CIRCUIT AND PRIORITY SWITCHING POST 03699 PRE 06403 262300-A0003-1-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING 008000 FH 26.23.00/12 POST 04357 PRE 06403 CHECK FIRING CIRCUIT CONTINUITY AND PERFORM OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT 262300-A0006-1-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING 14000 FH 26.23.00/13 POST 06403

REMOVAL OF PRESSURE REDUCING VALVE, CHECK VALVE, WATER ADSORBING FILTER, SOLID PARTICLE FILTER FOR RESTORATION AND WORKSHOP CHECK, PERFORM CLEANING AND CHECK OF DIAPHRAGM AND PERFORM CHECK DISTRIBUTION PIPING FOR LEAKAGE AND OBSTRUCTION 262300-A0007-1-C CMR** CARGO COMPARTMENT FIRE EXTINGUISHING 14000 FH 26.23.00/05 PRE 06403

CHECK DISTRIBUTION PIPING FOR LEAKAGE AND OBSTRUCTION

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 271400-00001-1-C CMR** HYDRAULIC ACTUATION - AILERON, RUDDER, ELEVATOR, TRIMMABLE 04000 FH 27.14.00/07 ALL HORIZONTAL STABILIZER, SPOILER/SPEED BRAKES

OPERATIONAL CHECK OF RUDDER, AILERON AND ELEVATOR JAMMING DETECTION SYSTEM 271400-00002-1-C CMR** HYDRAULIC ACTUATION - AILERON, RUDDER, ELEVATOR, TRIMMABLE 00800 FH 27.14.00/03 ALL HORIZONTAL STABILIZER, SPOILER/SPEED BRAKES

OPERATIONAL CHECK OF RUDDER SERVOCONTROLS WITH INDIVIDUAL HYDRAULIC SYSTEMS 271400-00003-1-C CMR* HYDRAULIC ACTUATION - AILERON, RUDDER, ELEVATOR, TRIMMABLE 00350 FH 27.14.00/01 ALL HORIZONTAL STABILIZER, SPOILER/SPEED BRAKES

OPERATIONAL CHECK OF TRIMMABLE HORIZONTAL STABILIZER JAMMING DETECTION SYSTEM. 271400-00004-1-C CMR* HYDRAULIC ACTUATION - AILERON, RUDDER, ELEVATOR, TRIMMABLE 00700 FH 27.14.00/02 ALL HORIZONTAL STABILIZER, SPOILER/SPEED BRAKES

OPERATIONAL CHECK OF TRIMMABLE HORIZONTAL STABILIZER GREEN/YELLOW OVHT WARNING INHIBITION 271400-00005-1-C CMR** HYDRAULIC ACTUATION - TRIMMABLE HORIZONTAL STABILIZER 16000 FH 27.14.00/10 ALL

FUNCTIONAL CHECK OF YELLOW PRIORITY VALVE (FOR TRIMMABLE HORIZONTAL STABILIZER ACTUATOR) AND FUNCTIONAL CHECK OF YELLOW SERVOCONTROLS PRIORITY FUNCTION (FLAPS PCU) 273100-00001-1-C CMR** ELEVATOR MECHANICAL CONTROL AND PITCH UNCOUPLING 02000 FH 27.31.00/01 ALL

OPERATIONAL CHECK OF PITCH CONTROL UNCOUPLING 273100-00002-1-C CMR** ELEVATOR MECHANICAL CONTROL AND PITCH UNCOUPLING 18000 FH 27.31.00/05 ALL

FUNCTIONAL CHECK OF PITCH CONTROL UNCOUPLING AND COUPLING D 273300-A0001-1-C TASK DELETED

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 274000-00001-1-C CMR** TRIMMABLE HORIZONTAL STABILIZER (THS) 00700 FH 27.40.00/01 ALL

OPERATIONAL CHECK WITH INDIVIDUAL HYDRAULIC SYSTEMS 275000-00001-1-C CMR* FLAPS 06500 FC 27.50.00/06 ALL

CHECK PRIMARY AND SECONDARY LOAD PATHS OF FLAP TRANSMISSION AND SCREW JACKS AND DETAILED INSPECTION OF PRIMARY AND SECONDARY SCREW JACK ATTACHMENTS 275000-00002-1-C CMR** FLAPS 00800 FH 27.50.00/01 ALL LIFT AUGMENTING (SLATS AND KRUEGER FLAPS) 27.80.00/01

READ LATERAL PANEL MFA “SFCC1 AND 2 BITE DISPLAY”

NOTE: THIS TASK COVERS BOTHS FLAPS (27.50.00) AND SLATS (27.80.00) SYSTEMS 275000-00003-1-C CMR** FLAPS 00800 FH 27.50.00/02 ALL LIFT AUGMENTING (SLATS AND KRUEGER FLAPS) 27.80.00/02

OPERATIONAL CHECK OF SYS 1 AND SYS 2

NOTE: THIS TASK COVERS BOTHS FLAPS (27.50.00) AND SLATS (27.80.00) SYSTEMS 275000-00004-1-C CMR** FLAPS 12000 FH 27.50.00/07 ALL LIFT AUGMENTING (SLATS AND KRUEGER FLAPS) 27.80.00/08

OPERATIONAL CHECK OF PRESSURE OFF BRAKES

NOTE: THIS TASK COVERS BOTHS FLAPS (27.50.00) AND SLATS (27.80.00) SYSTEMS 275000-00005-1-C CMR** FLAPS 12000 FC 27.50.00/08 ALL

CHECK BACKLASH OF FLAP SCREW-JACK NO-BACK DEVICE, SCREWJACKS 4, 5 AND 6

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 275000-00006-1-C CMR** FLAPS 16000 FC 27.50.00/11 ALL

DETAILED INSPECTION OF THE CASINGS OF ALL FLAP DOWNDRIVE GEARBOXES, JACKHEADS AND SCREW NUTS, AND TEE GEARBOX AND BEVEL BOX FOR FLAP SCREWJACKS N°1 276000-A0001-1-C CMR** SPOILERS AND SPEED BRAKES 00500 FH 27.60.00/01 ALL

OPERATIONAL CHECK OF GROUND SPOILER ELECTRICAL CIRCUIT N 276000-00002-1-C CMR* SPOILERS AND SPEED BRAKES 22000 FH - ALL

OPERATIONAL CHECK OF SPOILER SERVOCONTROL HYDRAULIC LOCKING FUNCTION 282200-A0001-1-C CMR** TANK ISOLATION SYSTEM 02000 FH 28.22.00/02 A300-600R

OPERATIONAL CHECK OF TRIM TANK ISOLATION VALVE MANUAL CLOSING INCLUDING INDICATION 282200-A0002-1-C CMR** TANK ISOLATION SYSTEM 20000 FH 28.22.00/03 A300-600R

OPERATIONAL CHECK TO ENSURE THAT FUEL FLOW IS INHIBITED WHEN THE TRIM TANK ISOLATION VALVE IS INDICATED OFF 282600-A0001-1-C CMR** FUEL TRANSFER (CG) CONTROL 04500 FH 28.26.00/01 A300-600R

OPERATIONAL CHECK OF MANUAL FORWARD TRANSFER CONTROL 282800-00001-1-C CMR** AUXILIARY CARGO TANKS SYSTEM 00500 FC - POST 05470 POST 05471 GENERAL VISUAL INSPECTION OF FLAMESHIELD, BAY SIDEWALLS AND PIPE COLLARS FOR DAMAGE AND SECURITY (ACTS FITTED)

NOTE: TASK APPLICABLE TO MSN 00354 AND 00374 ONLY 282800-00002-1-C CMR** AUXILIARY CARGO TANKS SYSTEM 08000 FH - POST 05470 POST 05471 OPERATIONAL CHECK OF ACT/CTR TANK INCORRECT FUEL DISTRIBUTION WARNING (DIRECT FROM CTR TK 12T AND ACT LO LEVEL SENSORS)

NOTE: TASK APPLICABLE TO MSN 00354 AND 00374 ONLY

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 282800-00003-1-C CMR** AUXILIARY CARGO TANKS SYSTEM 08000 FH - POST 05470 POST 05471 SYSTEM FUNCTION AND PRESSURE TEST USING TAPPINGS IN THE AIR SUPPLY SYSTEM

NOTE: TASK APPLICABLE TO MSN 00354 AND 00374 ONLY 282800-00004-1-C CMR** AUXILIARY CARGO TANKS SYSTEM 08000 FH - POST 05470 POST 05471 FUNCTIONAL CHECK OF THE AUXILIARY TANKS PRESSURE RELIEF VALVE (IN THE CENTRE TANK)

NOTE: TASK APPLICABLE TO MSN 00354 AND 00374 ONLY 282800-00005-1-C CMR** AUXILIARY CARGO TANKS SYSTEM 08000 FH - POST 05470 POST 05471 CHECK FOR GENERAL CONDITION AND SECURITY OF DRAIN/VENT SYSTEM PIPES, HOSES AND FLOOR DRAINS, AND FOR CONTAMINATION OF FLOOR DRAINS AND BILGES BY FUEL

NOTE: TASK APPLICABLE TO MSN 00354 AND 00374 ONLY 291000-00001-1-C CMR* MAIN AND AUXILIARY (HYDRAULIC POWER) 30 MO 29.10.00/11 PRE 05161

FUNCTIONAL CHECK OF RAM AIR TURBINE, FOLLOWED BY INSPECTION AND REPLACEMENT OF FILTER ELEMENT (WITH NEW OR RESTORED UNIT) 291000-00002-1-C CMR* MAIN AND AUXILIARY (HYDRAULIC POWER) 30 MO 29.10.00/18 POST 05161

FUNCTIONAL CHECK OF RAM AIR TURBINE FOLLOWED BY CHECK OF FILTER INDICATOR POSITION 314600-A0001-1-C CMR** CG CONTROL SYSTEM 04000 FH 31.46.00/02 A300-600R PRE 10778 OPERATIONAL CHECK OF AFT CG WARNING USING DADC BITE 323000-00001-1-C CMR** EXTENSION AND RETRACTION/POSITION AND WARNING 12 MO 32.30.00/04 ALL

OPERATIONAL CHECK OF LANDING GEAR UPLOCK MECHANICAL CONTROL

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 323000-A0002-1-C CMR* EXTENSION AND RETRACTION/POSITION AND WARNING 00500 FH 32.30.00/11 A300-600

OPERATIONAL CHECK OF THE SELECTOR VALVE

NOTE: FIRST ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN THE AIRCRAFT ACCUMULATING 75000 FH R 323000-A0003-1-C CMR* EXTENSION AND RETRACTION/POSITION AND WARNING 01200 FH 32.30.00/08 A300-600

OPERATIONAL CHECK OF - RETRACTION REDUNDANCY ON SYSTEM 1 AND SYSTEM 2 - RETRACTION INHIBITION ON SYSTEM 1 AND SYSTEM 2

NOTE: FIRST ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN THE AIRCRAFT ACCUMULATING 75000 FH 525111-00001-1-C CMR** COCKPIT DOOR 11000 FH 52.51.11/05 POST 12693 OR OPERATIONAL CHECK OF DECOMPRESSION FLAP RELEASE MECHANISM POST 12716 OR POST 12683 730000-0P001-1-C CMR** ENGINE FUEL AND CONTROL 01000 FH 73.00.00/03 PW 4000

INTERROGATE FADEC (FADEC GROUND AND BITE TEST) 783000-0P001-1-C CMR** THRUST REVERSER ACTUATION AND COWLING 07000 FH 78.30.00/09 PW JT9D-7R4 PW 4000 POST 12261 FUNCTIONAL CHECK OF THE SYNCHRONISING SHAFT LOCK OR 78.30.00/09 PW 4000 JT9D-7R4H1 POST 12262 783000-0P002-1-C CMR** THRUST REVERSER ACTUATION AND COWLING 07000 FH - PW JT9D-7R4 POST 12261 SELECTOR VALVE STOW LATCHING FORCE CHECK OR PW 4000 POST 12262

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 783000-0P003-1-C CMR** THRUST REVERSER ACTUATION AND COWLING 07000 FH - PW JT9D-7R4 POST 12261 VISUAL INSPECTION OF THE TRANSLATING SLEEVE COMPRESSION SEAL OR PW 4000 POST 12262 783100-0G002-1-C CMR** THRUST REVERSER CONTROL/ACTUATION SYSTEM 07000 FH - GE CF6-80C2 POST 12511 THRUST REVERSER ELECTRICAL CHECK COMPRISING: OR - THIRD LOCKS AND DUAL RELAYS TEST GE CF6-80C2 - THRUST LEVERS DISAGREE TEST POST 12512 - LANDING GEAR GROUND FUNCTION TEST OR GE CF6-80C2 (CMR INCLUDES REQUIREMENTS OF MRB REPORT TASK 78.31.00/02 FOR POST 19541 CF6-80C2 AND TASK 78.31.00/04 FOR CF6-80C2A5F)

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2 CMR TASKS SPECIFIC TO A300-600ST

CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 213000-S0001-1-C CMR* PRESSURIZATION CONTROL 07000 FH - A300-600ST

FUNCTIONAL CHECK OF SAFETY VALVES PNEUMATIC DEVICES AND OPERATIONAL TEST OF SAFETY VALVES OPENING 255900-S0001-1-C CMR* MAIN DECK CARGO LOADING SYSTEM 00400 FH - A300-600ST

VISUAL CHECK OF PLUs AND LOCKING PAWLS WITH SPECIAL ATTENTION TO PLU ATTACHMENT BOLTS 261500-S0001-1-C CMR** AVIONICS COMPARTMENT SMOKE DETECTION 01200 FH - A300-600ST CARGO COMPARTMENT SMOKE DETECTION

OPERATIONAL CHECK OF ALL SMOKE DETECTION CHANNELS INCLUDING ASSOCIATED WARNINGS AND INTEGRATED FANS

NOTE: THIS SUPERSEDES CMR TWO STAR TASK 261500-A0001-1-C IN SECTION 3-1 272300-S0001-1-C CMR** ARTIFICIAL FEEL AND RUDDER TRAVEL LIMITING 02000 FH - A300-600ST POST 19505 OPERATIONAL CHECK OF VARIABLE LEVER ARM (VLA) ACTUATORS SOLENOID VALVES EV2 273600-S0001-1-C CMR* STALL WARNING DAILY - A300-600ST

OPERATIONAL CHECK OF STICK PUSHER SYSTEM 276000-S0001-1-C CMR** SPOILERS AND SPEEDBRAKES 00350 FH - A300-600ST

OPERATIONAL CHECK OF GROUND SPOILER ELECTRICAL CIRCUIT

NOTE: THIS SUPERSEDES CMR TWO STAR 276000-A0001-1-C IN SECTION 3-1 282100-S0001-1-C CMR* FUEL PUMP SYSTEM 03000 FH - A300-600ST

OPERATIONAL CHECK TO CONFIRM FUEL FLOW FROM OUTER TANKS

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CMR REF. CMR RELATED MRBR TASK DESCRIPTION INTERVAL APPLICABILITY NUMBER CAT. TASK NUMBER 523700-S0001-1-C CMR** MAIN CARGO DOOR 07200 FH - A300-600ST

FUNCTIONAL CHECK OF MCD OVERCENTERING DEVICES 523700-S0002-1-C CMR** MAIN CARGO DOOR 05600 FH - A300-600ST

FUNCTIONAL CHECK OF MCD LATCHING MECHANISM

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APPENDIX A. ABBREVIATIONS

ABBREVIATION MEANING A/C Aircraft AC Alternating Current ACT Additional Center Tank AD Airworthiness Directive ALS Airworthiness Limitations Section 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 CG Center of Gravity CMR Certification Maintenance Requirement CTR TK Center Tank D Deleted DADC Digital Air Data Computer DOA Airbus Design Organization Approval EASA European Aviation Safety Agency FAA Federal Aviation Administration FAC Flight Augmentation Computer FADEC Full Authority Digital Engine Control FC Flight Cycle FH Flight Hour GE General Electric GEN Generator MCD Main Cargo Door

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ABBREVIATION MEANING MFA Memorized Fault Annunciator MO Months MOD Modification MRBR Maintenance Review Board Report MSI Maintenance Significant Item MSN Manufacturer Serial Number N New OMP Operators approved Maintenance Program OVHT Overheat PCU Power Control Unit PLU Power Locking Unit PW Pratt & Whitney R Revised SFCC Slat/Flap Control Computer SOC Summary Of Changes STC Supplemental Type Certificate SYS System THS Trimmable Horizontal Stabilizer TOC Table Of Contents TOT Transfer of Title US United States VLA Variable Lever Arm

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APPENDIX B. TERMS AND DEFINITIONS

TERM DEFINITION Month(s): equivalent of 1 calendar month (can be calculated as CALENDAR TIMES 1/12 calendar year). (Cal.) Year(s): equivalent of 12 calendar month (can be calculated as 365,25 days) Period of time given to Operators to accomplish maintenance tasks and/or replace items (at component or aircraft level) having exceeded or COMPLIANCE TIME close to exceed the new/reduced airworthiness limitations provided in the Revision/Variation An intensive examination of a specific item, installation or assembly to detect damage, failure or irregularity. Available lighting is normally DETAILED supplemented with a direct source of good lighting at an intensity deemed INSPECTION appropriate. Inspection aids such as mirrors, magnifying lenses etc. may be necessary. Surface cleaning and elaborate access procedures may be required. EXCEPTIONAL An increase in a CMR interval that may be needed to cover an SHORT-TERM uncontrollable or exceptional unexpected situation EXTENSION Unless otherwise stated, the use of this term in the ALS Part 3 implies FIRST FLIGHT that the life accumulated before the aircraft delivery date/ transfer of title date (e.g. as a result of test flights) must be taken into account. FLIGHT CYCLE (FC) A complete take-off and landing sequence FLIGHT HOUR (FH) The accumulated time intervals between "wheels-off" and "wheels-on" FUNCTIONAL A quantitative check to determine if a component/item performs one or CHECK more functions within specified limits IMPLEMENTATION The period of time allocated to Operators to update their approved PERIOD Maintenance Program The maximum period expressed in usage parameters between the INTERVAL completion of a task and its next due accomplishment A qualitative check to determine that a component/item is fulfilling its OPERATIONAL intended purpose. It is a failure-finding task and does not require CHECK quantitative tolerances Observation to determine that a component/item is fulfilling its intended VISUAL CHECK purpose. It is a failure finding task and does not require quantitative tolerances

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APPENDIX C. LIST OF DELETED TASKS

TASK REFERENCE SUMMARY OF CHANGES 262300-A0004-1-C Task deleted in ALS Part 3 Revision 00 262300-A0005-1-C Task deleted in ALS Part 3 Revision 00 783100-0G001-1-C Task deleted in ALS Part 3 Revision 00

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APPENDIX D. HISTORY FILE

RECORD OF REVISIONS

REVISION REVISION REASONS FOR REVISION NUMBER DATE At the opportunity of the update of A300-600 CMR Document Issue 13, its content has been transferred to the ALS Part 3 revision 00. ALS Part 3 has been reformatted, compared to A300-600 CMR Document Issue 12. This document is divided into the following sub- parts: • Subpart 3-0, which includes the introduction and generic paragraphs related to CMR. 00 • Sub-parts 3-1 and 3-2, which provides the list of CMR tasks APR 18/12 in a single CMR table. • Summary of changes have been transferred to appendices of ALS Part 3 - CMR. • A list of abbreviations is appended. • Revision 00 introduces in the ROR a paragraph titled “Revision 00 compliance time”.

This revision aims at introducing changes on some CMR* tasks for 01 ATA 27 and ATA 32. The opportunity was also taken to harmonize AUG 28/17 the format with others ALS Parts and Aircraft Programs.

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APPENDIX E. SUMMARY OF CHANGES

GENERAL

The full template for Revision of A300-600 ALS Part 3 has been modified in order to harmonize content between ALS Parts and Aircraft Programs. Thus and for greater clarity, changes are not highlighted with a revision bar in this Revision.

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.

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: − = CMR is new, − = CMR has been revised, − = CMR has been deleted.

COVER PAGE

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

TABLE OF CONTENT

The structure of the A300-600 ALS Part 3 has been entirely reviewed to fit with the new Airbus ALS process and to guarantee harmonization between ALS Parts and Aircraft Programs.

REVISION STATUS

This section has been created to provide the approval dates and references of the current Revision and the reason of all the Variations which have been introduced in it.

COMPLIANCE TIME

This section provides the list of items for which the instructions and airworthiness limitations have been revised and introduced in the A300-600 ALS Part 3 Revision 01 as well as their associated compliance time (when applicable). This information comes from the original Variations and/or additional approved changes which have been introduced in the current Revision.

SECTION 1 - INTRODUCTION

This section has been reviewed to organize the existing chapters in a logical way and rewrite them simpler and clearer when necessary.

SECTION 2 - EXPLANATION OF TABLE FORMAT

The explanation of table format of the airworthiness limitations provided in A300-600 ALS Part 3 Revision 00 has been moved to this dedicated section.

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SECTION 3 - CERTIFICATION MAINTENANCE REQUIREMENTS (CMR)

Additional approved change that was not published through Variations 0.1 and 0.2 is identified by “N/A” in the Variation Number column. This change is linked to the removal of some items of the A300-600 ALS Part 1.

REV VARIATION ITEMS CHANGE DESCRIPTION CODE NUMBER (when applicable) D 273300-A0001-1-C 0.1 Task deleted. N 276000-00002-1-C 0.2 New task added. R 323000-A0003-1-C N/A Interval reduced from 2300FH to 1200FH.

APPENDIX A - ABBREVIATIONS

This appendix has been created to centralize the abbreviations and their meanings previously located in Appendix 2 of ALS Part 3 Revision 00.

The following abbreviations have been removed: DSG, FWD, ICAO, IPC, JAR, LDG, MPD, MRO, RAT, ROR and SB.

The following abbreviations have been added: A/C, AC, ACT, APU, ASAC, ATA, CG, CRI, CTR TK, DGAC, DOA, FAR, FAC, GEN, MSN, OMP, OVHT, PCU, PLU, SOC, SSI, STC, TOT, US and VLA.

APPENDIX B - TERMS AND DEFINITIONS

This appendix has been created to centralize all terms and definitions used in the ALS Part 3 previously located in Sub-part 3-0 of ALS Part 3 Revision 00.

The following terms have been added: Compliance time, Exceptional short-term extension, Implementation period and Visual check.

The following definitions have been updated: Calendar time, Interval, Operational check and Functional check.

APPENDIX C - LIST OF DELETED TASKS

This appendix has been created to list all tasks deleted in previous Revisions. Tasks deleted at the opportunity of this Revision (A300-600 ALS Part 3 Revision 01) appear in Section 3 of this SOC.

APPENDIX D - HISTORY FILE

This section has been created to provide the general reason for issuance of Revisions.

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APPENDIX E - SUMMARY OF CHANGES

This section replaces the previous Appendix 1 and provides the changes introduced in the A300- 600 ALS Part 3 Revision 01.

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