continuing airworthiness management exposition (came)asiaaerotechnics.com/imr/techpubs/files/hm...

MADOS’S HOLDINGS SDN BHD – HIS MAJESTY SULTAN OF JOHOR’S FLIGHT

CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION

(CAME)

DOCUMENT REF.: HMSJF/CAME/01/2017

ISSUE 01 REV 00 01 APRIL 2017


HMSJF/CAME/01/2017

ISSUE REVISION DATE

MADOSS - HMSJF 01 00 01/04/2017

CAME Cover Page Page i


CONTINUING AIRWORTHINESS

MANAGEMENT EXPOSITION

(CAME)

DOCUMENT REF.: HMSJF/CAME/01/2017

ISSUE 01 REV 00

01 APRIL 2017

Official Correspondence Address:

H.M. SULTAN OF JOHOR’S FLIGHT,

Royal Flight Hangar,

Senai International Airport,

81250 Johor Bahru,

Johor Darul Takzim,

MALAYSIA.

Tel: +607 599 6655

Fax: +607 599 6611


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CAME Approval Page Page ii

TITLE CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION

ISSUE 01

REVISION 00

PREPARED BY:

ZAIHASRY ZAINOREN

DESIGNATION:

CONTINUING AIRWORTHINESS MANAGEMENT MANAGER

DATE:

SIGNATURE:

VERIFIED BY:

AZMAN HJ RAMLEE

DESIGNATION:

QUALITY ASSURANCE MANAGER

DATE:

SIGNATURE:

ENDORSED BY:

DATO’ HJ MAZELAN ABU

DESIGNATION:

ACCOUNTABLE MANAGER

DATE:

SIGNATURE:

AUTHORITY APPROVAL:

DEPARTMENT OF CIVIL AVIATION MALAYSIA

DATE:

SIGNATURE:


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CAME Foreword Page iii

FOREWORD

This Continuing Airworthiness Management Exposition (CAME) serves to lay down the

organisational structure, responsibilities, resources, policies, processes and procedures of

Mados’s Holdings Sdn Bhd – His Majesty Sultan of Johor’s Flight (MADOSS – HMSJF) in

performing aircraft continuing airworthiness management to the standards of the

Department of Civil Aviation Malaysia (DCAM) as an Approved Continuing Airworthiness

Management Organization (CAMO).

MADOSS – HMSJF shall have a continuing airworthiness management system that ensures

effective supervision and control of all continuing airworthiness activities, performed by

MADOSS – HMSJF as well as those activities contracted out in accordance with MADOSS –

HMSJF own standards and the requirements of the DCAM.

All MADOSS – HMSJF personnel are therefore required to be guided by the continuing

airworthiness management policies and procedures in accordance with this exposition.

This exposition also specifies the basic quality policies and defines the overall quality

management system.

This exposition is organised into 7 parts and covers the continuing airworthiness management

policy and procedures for an Approved Continuing Airworthiness Management Organisation

to meet the requirements of the DCAM.


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CAME Condition of Use Page iv

CONDITION OF USE

This CAME is the property of Mados’s Holdings Sdn Bhd – His Majesty Sultan of Johor’s Flight

(MADOSS – HMSJF). It is not to be copied of communicated in part or as a whole, to any

person not employed by the organisation, without the expressed written consent of the

Accountable Manager.

The exposition is not intended to conflict with or override Civil Aviation Regulation of Malaysia

2016 or any relevant aviation authorities’ requirements.


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CAME Table of Contents Page v

TABLE OF CONTENTS

TITLE PAGE NO.

FRONT PAGE Page i

APPROVAL PAGE Page ii

FOREWORD Page iii

CONDITION OF USE Page iv

TABLE OF CONTENTS Page v

LIST OF EFFECTIVE PAGES

AMENDMENT RECORD

DISTRIBUTION LIST

ABBREVIATIONS AND DEFINITIONS

PART 0 GENERAL ORGANISATION Page 0-1

0.1 CORPORATE COMMITMENT BY THE ACCOUNTABLE

MANAGER

Page 0-3

0.2 GENERAL INFORMATION Page 0-4

0.2.1 Description of the Organisation Page 0-4

0.2.2 Relationship with Other Organisation Page 0-4

0.2.3 Aircraft Managed – Fleet Composition Page 0-5

0.2.4 Type of Operation Page 0-5

0.2.5 Base Location Page 0-5

0.3 SCOPE OF WORK Page 0-6

0.3.1 Privileges of an Approved Continuing Airworthiness

Management Organisation

Page 0-6

0.3.2 Conditions of Approval Page 0-7

0.3.3 Validity of Approval Page 0-7

0.3.4 Renewal of Approval Page 0-7

0.4 MANAGEMENT PERSONNEL Page 0-8

0.4.1 Accountable Manager Page 0-8

0.4.2 Continuing Airworthiness Management Manager Page 0-9

0.4.2.1 Continuing Airworthiness Management Manager Qualification

Requirements

Page 0-9


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TITLE PAGE NO.

0.4.3 Quality Assurance Manager Page 0-10

0.4.3.1 Quality Assurance Manager Qualification Requirements Page 0-10

0.5 DUTIES AND RESPONSIBILITIES OF MANAGEMENT

PERSONNEL

Page 0-11

0.5.1 Accountable Manager Page 0-11

0.5.2 Continuing Airworthiness Management Manager Page 0-12

0.5.3 Quality Assurance Manager Page 0-14

0.5.4 Technical Publication Executive Page 0-16

0.5.5 Maintenance Planning Executive Page 0-17

0.5.6 Technical Records Executive Page 0-18

0.6 MANPOWER RESOURCES AND TRAINING POLICY Page 0-20

0.6.1 Manpower Resources and Analysis Page 0-20

0.6.2 Training Policy Page 0-21

0.7 MANAGEMENT ORGANISATION CHART Page 0-22

0.7.1 General Organisation Chart Page 0-22

0.7.1.1 Continuing Airworthiness Management Organisation Chart Page 0-22

0.8 NOTIFICATION PROCEDURE TO THE DCAM REGARDING

CHANGES TO THE OPERATOR’S CONTINUING

AIRWORTHINESS MANAGEMENT ARRANGEMENT /

LOCATIONS / PERSONNEL / ACTIVITIES / APPROVALS

Page 0-23

0.8.1 Changes Page 0-23

0.9 CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION

AMENDMENT PROCEDURES

Page 0-24

0.9.1 Procedures Page 0-24

0.9.2 CAME Review Page 0-25

0.10 FACILITIES Page 0-26

0.10.1 Royal Flight Hangar, Senai International Airport (JHB) Page 0-26

0.10.2 Bukit Serene Hangar (IBS) Page 0-27

0.10.3 CAMO Office Layout Plan, Royal Flight Hangar, Senai

International Airport

Page 0-28


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CAME Table of Contents Page vii

TITLE PAGE NO.

PART 1 CONTINUING AIRWORTHINESS MANAGEMENT PROCEDURES Page 1-1

1.1 CONTINUING AIRWORTHINESS MANAGEMENT PROCEDURES Page 1-3

1.2 AIRCRAFT JOURNEY LOG SYSTEM UTILISATION AND

MINIMUM EQUIPMENT LIST APPLICATION

Page 1-4

1.2.1 The Journey Log Page 1-4

1.2.1.1 The Journey Log Contents Page 1-5

1.2.1.2 Instruction for Use Page 1-6

1.2.2 MEL Application Page 1-8

1.2.2.1 MEL Procedures Page 1-8

Flowchart 1 Defer Defect Procedures Page 1-10

1.2.2.2 Acceptance by the Pilot Page 1-11

1.2.2.3 Management of the MEL Rectification Intervals (RI’s) Page 1-11

1.2.2.4 MEL Rectification Interval Expiry Page 1-11

1.3 AIRCRAFT MAINTENANCE PROGRAMME – GENERAL Page 1-12

1.3.1 The Programme – Contents – Sources Page 1-12

1.3.2 Structural Inspections, Corrosion Control, Reliability and

Engine Health Monitoring

Page 1-13

1.3.3 Mandatory Life Limitations Page 1-13

1.3.4 Inspection Standards Page 1-13

1.3.5 Maintenance Certification Page 1-13

1.3.6 Fuel Contamination Page 1-13

1.3.7 Maintenance Programme Owner – Responsibilities Page 1-14

1.3.8 Holders of the Maintenance Programme Page 1-14

1.3.9 Maintenance Programme Review, Development and

Amendment

Page 1-14

1.3.9.1 Review and Development Page 1-14

1.3.9.2 Maintenance Programme Meetings Page 1-15

1.3.9.3 Maintenance Programme Amendments Page 1-16

1.4 TIME AND CONTINUING AIRWORTHINESS RECORDS:

RESPONSIBILITIES, RETENTION AND ACCESS

Page 1-17

1.4.1 Hours and Cycles Recording Page 1-17

1.4.2 Sector Record Page Retention Page 1-17


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TITLE PAGE NO.

1.4.3 Access to Continuing Airworthiness Records Page 1-18

1.4.4 Control and Preservation of Records Page 1-18

1.4.5 Transfer of Continuing Airworthiness Records in the Event of a

Sale or other Disposal of the Aircraft

Page 1-19

1.4.6 Access to Continuing Airworthiness Records in the Event of an

Accident / Incident

Page 1-19

1.5 ACCOMPLISHMENT AND CONTROL OF MANDATORY

REQUIREMENTS FOR AIRWORTHINESS

Page 1-20

1.5.1 Access to Airworthiness Directives & Service Bulletins

Requirements

Page 1-20

1.5.2 AD,SB, SL & SI Decision & Implementation Page 1-20

1.5.3 AD/SB/SL/SI Control – Compliance Monitoring Page 1-21

1.5.4 AD/SB/SL/SI Control – Recording of AD/SB Compliance Page 1-21

Flowchart 2 Processing of Technical Compliance Documents Page 1-22

1.6 ANALYSIS OF THE EFFECTIVENESS OF THE MAINTENANCE

PROGRAMME

Page 1-23

1.6.1 Liaison Meetings Page 1-23

1.6.2 Frequency of Meetings Page 1-23

1.7 NON-MANDATORY CHANGES (MODIFICATION) EMBODIMENT

POLICY

Page 1-24

1.7.1 Changes (Modifications) General Page 1-24

1.7.2 Service Bulletins Page 1-24

1.7.3 Other Changes (Modifications) Page 1-24

1.7.4 Minor Changes (Modifications) Page 1-25

1.7.5 Instructions for Continuing Airworthiness Page 1-25

1.7.6 Recording of Changes (Modifications) Page 1-25

1.8 MAJOR CHANGE (MODIFICATION) STANDARD Page 1-26

1.8.1 Major Changes (Modifications) General Page 1-26

1.8.2 Review of Modifications Page 1-26

1.8.3 Instructions for Continuing Airworthiness Page 1-27

1.8.4 Recording of Changes (Modifications) Page 1-27


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CAME Table of Contents Page ix

TITLE PAGE NO.

1.9 DEFECT REPORTS Page 1-28

1.9.1 Analysis Page 1-28

1.9.2 Liaison with Manufacturers and Regulatory Authorities Page 1-28

1.9.3 Deferred Defect Policy Page 1-29

1.9.4 Non-Deferrable Defects Away from Base Page 1-30

1.9.5 Repetitive Defects Page 1-30

1.9.6 Mandatory Occurrence Reporting Page 1-31

1.9.7 Liaison Meetings Page 1-31

1.10 ENGINEERING ACTIVITY Page 1-32

1.10.1 General Page 1-32

1.10.2 Application Process Page 1-32

1.11 RELIABILITY PROGRAMME Page 1-33

1.12 PRE-FLIGHT INSPECTOR AND PILOT AUTHORISATION Page 1-34

1.12.1 The Pre-Flight Inspection Page 1-34

1.12.2 Pilot Authorisation for Daily Inspection Page 1-35

1.12.3 Subcontracted Ground Handling Functions Page 1-36

1.12.4 Security of Cargo and Baggage Loading Page 1-36

1.12.5 Control of Aircraft Refuelling, Quantity/Quality Page 1-36

1.12.6 Control of Snow, Ice, Dust and Sand Contamination to an

Approved Standard

Page 1-36

1.13 AIRCRAFT WEIGHING Page 1-37

1.14 AIRWORTHINESS FLIGHT TEST PROCEDURES Page 1-38

1.14.1 Airworthiness Flight Test Schedule (AFTS) Page 1-38

1.14.2 Contents of the Airworthiness Flight Test Schedule (AFTS) Page 1-39

1.14.3 Pilot Approval to Carry Out Airworthiness Flight Test Page 1-39

1.14.4 Insurance Cover for Airworthiness Flight Test Page 1-40

1.14.5 Post Flight Procedures and Aircraft Performance Analysis Page 1-40

1.14.6 Post Flight Reporting Page 1-41

1.14.7 Quality Audits by DCAM Page 1-41


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TITLE PAGE NO.

1.15 PLANNING PROCEDURES Page 1-42

1.15.1 Planning of Aircraft Maintenance Programme Tasks,

Modifications, Airworthiness Directives, Service Bulletins etc.

Page 1-42

1.15.2 Monitoring of Maintenance between Scheduled Maintenance Page 1-43

1.15.3 Maintenance Programme Variations Page 1-43

1.15.4 Variations in Excess of that Allowed by Programme Page 1-45

1.16 AIRWORTHINESS DATA CONTROL Page 1-46

1.17 CONTROL OF PERSONNEL COMPETENCY Page 1-47

1.17.1 Training Requirements Page 1-47

1.17.2 Records Page 1-48

1.18 SAMPLE OF DOCUMENTS, TAGS AND FORMS USED Page 1-49

PART 2 QUALITY SYSTEM Page 2-1

2.1 CONTINUING AIRWORTHINESS QUALITY POLICY, PLAN &

AUDIT PROCEDURES

Page 2-3

2.1.1 Continuing Airworthiness Quality Policy Page 2-3

2.1.2 Quality Programme Page 2-3

2.1.3 Quality Audit Procedure Page 2-4

2.1.4 Quality Audit Remedial Action Procedure Page 2-5

2.1.4.1 Non-Conformance Findings Classification Page 2-6

2.1.4.2 Corrective / Preventive Action Page 2-6

Flowchart 1 Quality Audit Programme Page 2-7

2.2 MONITORING OF CONTINUING AIRWORTHINESS

MANAGEMENT ACTIVITIES

Page 2-8

Table 1 CAMO Quality Assurance Audit Plan Page 2-9

2.3 MONITORING THE EFFECTIVENESS OF THE MAINTENANCE

PROGRAMME

Page 2-10


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TITLE PAGE NO.

2.4 MONITORING THAT ALL MAINTENANCE IS CARRIED OUT BY

AN APPROPRIATELY APPROVED PART 145 ORGANISATION

Page 2-11

Table 2 Maintenance Contractor Quality Assurance Audit Plan Page 2-12

2.5 MONITORING THAT ALL CONTRACTED MAINTENANCE IS

CARRIED OUT IN ACCORDANCE WITH THE CONTRACT,

INCLUDING SUBCONTRACTORS USED BY THE MAINTENANCE

CONTRACTOR

Page 2-13

2.6 QUALITY AUDIT PERSONNEL Page 2-14

2.6.1 Quality Audit Personnel Requirement Page 2-14

2.6.2 Quality Audit Personnel Training Requirement Page 2-15

2.6.3 Quality Audit Personnel Records Page 2-15

PART 3 CONTRACTED MAINTENANCE Page 3-1

3.1 CONTRACTED MAINTENANCE Page 3-3

3.2 MAINTENANCE CONTRACT AGREEMENT Page 3-4

3.3 MAINTENANCE CONTRACTOR SELECTION PROCEDURE Page 3-5

3.3.1 Advising the DCAM of Changes to the Maintenance Support Page 3-6

3.4 DETAILED LIST OF MAINTENANCE CONTRACTORS Page 3-7

3.5 RELEVANT TECHNICAL PROCEDURES IDENTIFIED IN THE

MAINTENANCE CONTRACT(S)

Page 3-8

3.6 QUALITY AUDIT OF AIRCRAFT Page 3-9

PART 4 AIRWORTHINESS REVIEW PROCEDURES Page 4-1

4.1 AIRWORTHINESS REVIEW PROCEDURES Page 4-3

4.2 AIRWORTHINESS REVIEW STAFF Page 4-4

4.2.1 Qualification Requirement Page 4-4


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TITLE PAGE NO.

4.2.2 Airworthiness Review Staff Assessment Page 4-4

4.2.3 Issuance, Restriction and Withdrawal of Company

Authorisation

Page 4-5

4.2.4 Staff Records Page 4-6

4.3 REVIEW OF AIRCRAFT RECORDS Page 4-7

4.4 PHYSICAL SURVEY Page 4-9

4.5 RECOMMENDATION TO DCAM Page 4-10

PART 4A PERMIT TO FLY Page 4A-1

4A.1 RESERVED Page 4A-3

PART 5 APPENDICES Page 5-1

APPENDIX 1 SAMPLE DOCUMENTS Page 5-3

Item 1 Aircraft Journey Log Format Page 5-4

Item 2 Aircraft Deferred Defect Log Format Page 5-5

Item 3 Airworthiness Review Report Checklist Form Page 5-6

Item 4 Aircraft Physical Survey Form Page 5-7

Item 5 Airworthiness Review Report Format Page 5-9

Item 6 Notice to Crew Form Page 5-15

Item 7 MEL Deferred Defect Extension Request Form Page 5-16

Item 8 Concession Request Form Page 5-17

Item 9 Occurrence Report Form Page 5-18

APPENDIX 2 LIST OF ARR SIGNATORY Page 5-19

APPENDIX 3 LIST OF APPROVED CONTRACTED MAINTENANCE

ORGANISATIONS

Page 5-20


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TITLE PAGE NO.

APPENDIX 4 LIST OF APPROVED MAINTENANCE PROGRAMME Page 5-21

APPENDIX 5 COPY OF CONTRACTS WITH APPROVED MAINTENANCE

ORGANISATIONS

Page 5-22


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CAME List of Effective Pages Page xiv

LIST OF EFFECTIVE PAGES

This list shows the revision status of each page in the exposition. This page will be reissued

with each new amendment to reflect the current revision status to confirm that the correct

pages are incorporated.

PART PAGE REVISION

NO.

DATE PART PAGE REVISION

NO.

DATE

FRONT i 00 01/04/2017 PART 0 0-4 00 01/04/2017

APPROVAL ii 00 01/04/2017 PART 0 0-5 00 01/04/2017

FOREWORD iii 00 01/04/2017 PART 0 0-6 00 01/04/2017

CONDITION iv 00 01/04/2017 PART 0 0-7 00 01/04/2017

TOC v 00 01/04/2017 PART 0 0-8 00 01/04/2017

TOC vi 00 01/04/2017 PART 0 0-9 00 01/04/2017

TOC vii 00 01/04/2017 PART 0 0-10 00 01/04/2017

TOC viii 00 01/04/2017 PART 0 0-11 00 01/04/2017

TOC ix 00 01/04/2017 PART 0 0-12 00 01/04/2017

TOC x 00 01/04/2017 PART 0 0-13 00 01/04/2017

TOC xi 00 01/04/2017 PART 0 0-14 00 01/04/2017

TOC xii 00 01/04/2017 PART 0 0-15 00 01/04/2017

TOC xiii 00 01/04/2017 PART 0 0-16 00 01/04/2017

LEP xiv 00 01/04/2017 PART 0 0-17 00 01/04/2017

LEP xv 00 01/04/2017 PART 0 0-18 00 01/04/2017

LEP xvi 00 01/04/2017 PART 0 0-19 00 01/04/2017

AMENDMENT xvii 00 01/04/2017 PART 0 0-20 00 01/04/2017

DISTRIBUTION xviii 00 01/04/2017 PART 0 0-21 00 01/04/2017

ABBREVIATIONS xix 00 01/04/2017 PART 0 0-22 00 01/04/2017

ABBREVIATIONS xx 00 01/04/2017 PART 0 0-23 00 01/04/2017

ABBREVIATIONS xxi 00 01/04/2017 PART 0 0-24 00 01/04/2017

ILB xxii 00 01/04/2017 PART 0 0-25 00 01/04/2017

PART 0 0-1 00 01/04/2017 PART 0 0-26 00 01/04/2017

PART 0 0-2 00 01/04/2017 PART 0 0-27 00 01/04/2017

PART 0 0-3 00 01/04/2017 PART 0 0-28 00 01/04/2017

Reviewed by Continuing Airworthiness Management

Manager

Verified by Quality Assurance Manager

Approved by DCA Malaysia

Date: Date: Date:


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PART PAGE REVISION

NO.


NO.

DATE

PART 1 1-1 00 01/04/2017 PART 1 1-33 00 01/04/2017

PART 1 1-2 00 01/04/2017 PART 1 1-34 00 01/04/2017

PART 1 1-3 00 01/04/2017 PART 1 1-35 00 01/04/2017

PART 1 1-4 00 01/04/2017 PART 1 1-36 00 01/04/2017

PART 1 1-5 00 01/04/2017 PART 1 1-37 00 01/04/2017

PART 1 1-6 00 01/04/2017 PART 1 1-38 00 01/04/2017

PART 1 1-7 00 01/04/2017 PART 1 1-39 00 01/04/2017

PART 1 1-8 00 01/04/2017 PART 1 1-40 00 01/04/2017

PART 1 1-9 00 01/04/2017 PART 1 1-41 00 01/04/2017

PART 1 1-10 00 01/04/2017 PART 1 1-42 00 01/04/2017

PART 1 1-11 00 01/04/2017 PART 1 1-43 00 01/04/2017

PART 1 1-12 00 01/04/2017 PART 1 1-44 00 01/04/2017

PART 1 1-13 00 01/04/2017 PART 1 1-45 00 01/04/2017

PART 1 1-14 00 01/04/2017 PART 1 1-46 00 01/04/2017

PART 1 1-15 00 01/04/2017 PART 1 1-47 00 01/04/2017

PART 1 1-16 00 01/04/2017 PART 1 1-48 00 01/04/2017

PART 1 1-17 00 01/04/2017 PART 1 1-49 00 01/04/2017

PART 1 1-18 00 01/04/2017 PART 1 1-50 00 01/04/2017

PART 1 1-19 00 01/04/2017 PART 2 2-1 00 01/04/2017

PART 1 1-20 00 01/04/2017 PART 2 2-2 00 01/04/2017

PART 1 1-21 00 01/04/2017 PART 2 2-3 00 01/04/2017

PART 1 1-22 00 01/04/2017 PART 2 2-4 00 01/04/2017

PART 1 1-23 00 01/04/2017 PART 2 2-5 00 01/04/2017

PART 1 1-24 00 01/04/2017 PART 2 2-6 00 01/04/2017

PART 1 1-25 00 01/04/2017 PART 2 2-7 00 01/04/2017

PART 1 1-26 00 01/04/2017 PART 2 2-8 00 01/04/2017

PART 1 1-27 00 01/04/2017 PART 2 2-9 00 01/04/2017

PART 1 1-28 00 01/04/2017 PART 2 2-10 00 01/04/2017

PART 1 1-29 00 01/04/2017 PART 2 2-11 00 01/04/2017

PART 1 1-30 00 01/04/2017 PART 2 2-12 00 01/04/2017

PART 1 1-31 00 01/04/2017 PART 2 2-13 00 01/04/2017

PART 1 1-32 00 01/04/2017 PART 2 2-14 00 01/04/2017


Manager



Date: Date: Date:


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PART PAGE REVISION

NO.


NO.

DATE

PART 2 2-15 00 01/04/2017 PART 5 5-7 00 01/04/2017

PART 2 2-16 00 01/04/2017 PART 5 5-8 00 01/04/2017

PART 3 3-1 00 01/04/2017 PART 5 5-9 00 01/04/2017

PART 3 3-2 00 01/04/2017 PART 5 5-10 00 01/04/2017

PART 3 3-3 00 01/04/2017 PART 5 5-11 00 01/04/2017

PART 3 3-4 00 01/04/2017 PART 5 5-12 00 01/04/2017

PART 3 3-5 00 01/04/2017 PART 5 5-13 00 01/04/2017

PART 3 3-6 00 01/04/2017 PART 5 5-14 00 01/04/2017

PART 3 3-7 00 01/04/2017 PART 5 5-15 00 01/04/2017

PART 3 3-8 00 01/04/2017 PART 5 5-16 00 01/04/2017

PART 3 3-9 00 01/04/2017 PART 5 5-17 00 01/04/2017

PART 3 3-10 00 01/04/2017 PART 5 5-18 00 01/04/2017

PART 4 4-1 00 01/04/2017 PART 5 5-19 00 01/04/2017

PART 4 4-2 00 01/04/2017 PART 5 5-20 00 01/04/2017

PART 4 4-3 00 01/04/2017 PART 5 5-21 00 01/04/2017

PART 4 4-4 00 01/04/2017 PART 5 5-22 00 01/04/2017

PART 4 4-5 00 01/04/2017 PART 4 4-6 00 01/04/2017 PART 4 4-7 00 01/04/2017 PART 4 4-8 00 01/04/2017 PART 4 4-9 00 01/04/2017 PART 4 4-10 00 01/04/2017 PART 4A 4A-1 00 01/04/2017 PART 4A 4A-2 00 01/04/2017 PART 4A 4A-3 00 01/04/2017 PART 4A 4A-4 00 01/04/2017 PART 5 5-1 00 01/04/2017 PART 5 5-2 00 01/04/2017 PART 5 5-3 00 01/04/2017 PART 5 5-4 00 01/04/2017 PART 5 5-5 00 01/04/2017 PART 5 5-6 00 01/04/2017


Manager



Date: Date: Date:


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CAME Amendment Record Page xvii

AMENDMENT RECORD

AMENDMENT

NO. DATE AMENDMENT DETAILS

AMENDED

BY

DATE OF

INCLUSION

Issue 01, Rev No. 00

01/04/2017

-

-

-


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CAME Distribution List Page xviii

DISTRIBUTION LIST

COPY NO. HOLDER DOC. REF. NO. LOCATION FORMAT

Master Copy Technical Publication HMSJF/CAME/01/2017 JHB HC & EC

1 CAMO Office Rotor

Wings

HMSJF/CAME/01/2017

– IBS IBS HC

2 Accountable Manager HMSJF/CAME/01/2017

– AM JHB HC

3 Quality Assurance

Manager

HMSJF/CAME/01/2017

– QAM JHB HC

4

Continuing

Airworthiness

Management Manager

HMSJF/CAME/01/2017

– CAMM JHB HC

5

Department of Civil

Aviation Malaysia

(DCAM)

HMSJF/CAME/01/2017

– DCAM

DCAM AW

SECTOR HC

LEGEND:

HC – HARD COPY

EC – ELECTRONIC COPY (MS WORDS and PDF Format)

IMPORTANT NOTE:

New amendments will be distributed to all holders via e-mail (soft copy). It will be the holders’

responsibility to insert the revised List of Effective Pages and the newly amended pages. The

previous revision copies are to be removed and disposed of as necessary.


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CAME Abbreviations and Definitions Page xix

ABBREVIATIONS AND DEFINITIONS

This list shows all of the abbreviations used in this CAME and their definitions.

ABBREVIATIONS DEFINITIONS

AAIB Air Accidents Investigation Bureau

ACF Aircraft Certificate File

AFT Airworthiness Flight Test

AFTS Airworthiness Flight Test Schedule

AD Airworthiness Directive

ADD Acceptable Deferred Defect

AFM Approved Flight Manual

AJL Aircraft Journey Log

AN Airworthiness Notice

AMM Aircraft Maintenance Manual

AMO Approved Maintenance Organisation

AMP Approved Maintenance Programme

AOG Aircraft on Ground

APU Auxiliary Power Unit

ARR Airworthiness Review Report

ARS Airworthiness Review Staff

BMR Base Maintenance Release

CAME Continuing Airworthiness Management Exposition

CAMM Continuing Airworthiness Management Manager

CAMO Continuing Airworthiness Management Organisation

CAR Civil Aviation Regulations

CCD Certification Compliance Document

CDL Configuration Deviation List

C of A Certificate of Airworthiness

C of G Centre of Gravity


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CAME Abbreviations and Definitions Page xx


C of R Certificate of Registration

CP Chief Pilot

DCAM Department of Civil Aviation Malaysia

DDL Deferred Defect Log

DOA Design Organisation Approval

DOW Dry Operating Weight

FTC Flight Test Certificate

IBS Istana Bukit Serene

ICA Instructions for Continuing Airworthiness

INOP Inoperative

JHB Johor Bahru

LAE Licensed Aircraft Engineer

LLP Life Limited Parts

MADOSS – HMSJF Mados’s Holdings Sdn Bhd – His Majesty Sultan of

Johor’s Flight

MEL Minimum Equipment List

MMEL Master Minimum Equipment List

MOR Mandatory Occurrence Report

MPD Maintenance Planning Document

NAA National Aviation Authority

NCR Non Compliance Report

NDT Non Destructive Test

NTC Notice to Crew

OEM Original Equipment Manufacturer

PTF Permit to Fly

QAM Quality Assurance Manager

SB Service Bulletin

SI Service Information


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CAME Abbreviations and Definitions Page xxi


SL Service Letter

SOC Statement of Compliance

SRP Sector Record Pages


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CAME Page xxii

- THIS PAGE IS INTENTIONALLY LEFT BLANK -


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CAME Part 0 – General Organisation Page 0-1

PART 0

GENERAL ORGANISATION


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0.1 CORPORATE COMMITMENT BY THE ACCOUNTABLE MANAGER


(MADOSS – HMSJF)


This exposition defines the organisation and procedure upon which the Department

of Civil Aviation Malaysia (DCAM) Part M – Subpart G is based.

These procedures are approved by the undersigned and must be complied with, as

applicable, in order to ensure that all the continuing airworthiness activities including

maintenance for aircraft managed by MADOSS – HMSJF is carried out on time and to

an approved standard.

It is accepted that these procedures do not override the necessity of complying with

any new or amend regulation published in the Civil Aviation Regulations 2016 (CAR

2016), DCAM Airworthiness Notices and other regulatory requirements. When new or

amended regulations are in conflict with these procedures, the regulations will take

precedence.

It is understood that the DCAM will approve this organisation whilst DCAM is satisfied

that the procedures are being followed. It is further understood that the DCAM

reserves the right to suspend, vary or revoke the continuing airworthiness

management approval of the organisation, as applicable, if the DCAM has evidence

that procedures are not followed and the standards not upheld.

Signed : …………………………………… Date : …………………………….

Name : Dato’ Hj Mazelan Abu

Title : Accountable Manager

Mados’s Holdings Sdn Bhd – His Majesty Sultan of Johor’s Flight


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0.2 GENERAL INFORMATION

0.2.1 Description of the Organisation

His Majesty Sultan of Johor’s Flight (HMSJF) is structured under Mados’s

Holdings Sdn Bhd as a division to manage all continuing airworthiness activities

for H.M Sultan of Johor. These are carried out under the management of the

assigned manager, Dato’ Hj Mazelan Abu.

Mados’s Holdings Sdn Bhd is incorporated on 4 October 2010. The company’s

main activity is oil palm cultivation and currently managing nine (9) oil palm

plantations of various sizes in the state of Johor.

MADOSS – HMSJF is based in Royal Flight Hangar, Senai International Airport;

with another facility located at Bukit Serene Hangar, Johor Bahru, Johor Darul

Ta’zim. Its main functions are to organise and manage all the aircrafts owned

by His Majesty Sultan of Johor. These includes:

1. Boeing B737-800 BBJ2

2. Gulfstream G 650

3. Gulfstream G 550

4. Gulfstream G IV

5. Sikorsky S-76B

MADOSS – HMSJF engages a suitably approved DCAM Part-145 maintenance

contractor to satisfy the requirements of DCAM Part M.

Details of the current maintenance contractor are provided in Appendix 3 of

CAME Appendices.

0.2.2 Relationship with Other Organisations

MADOSS – HMSJF currently performs the Continuing Airworthiness

Management functions on His Majesty’s fleet of aircrafts. It operates

independently of any other organisations with the exception of maintenance

support which is provided by the Part-145 maintenance organisation(s) given

in Appendices of this CAME, Appendix 3.


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0.2.3 Aircraft Managed – Fleet Composition

The continuing airworthiness of the following aircraft type is managed by

MADOSS – HMSJF:

AIRCRAFT TYPE NUMBER OF

AIRCRAFT

AIRCRAFT

REGISTRATION

Boeing B737-800 BBJ2 1 9M – III

Gulfstream GVI (G650ER) 1 9M - ZZZ

Gulfstream GV-SP 1 9M – JJJ

Gulfstream GIV 1 9M - ISJ

Sikorsky S-76B 2 9M – SJI 9M - JSI

0.2.4 Type of Operation

All aircraft managed by MADOSS – HMSJF are for the personal intent of His

Majesty Sultan of Johor. It is a non-commercial division under Mados’s

Holdings Sdn Bhd.

0.2.5 Base Location

Main Base Operation Office: Royal Flight Hangar,

Senai International Airport,

81250 Johor Bahru, Johor.

Tel: +607 599 6655

Fax: +607 599 6611

Bukit Serene Office: Bukit Serene Hangar,

East Lodge, Jalan Straits View,

80200 Johor Bahru, Johor.

Tel: +607 221 6686

Fax: +607 221 6686


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0.3 SCOPE OF WORK

0.3.1 Privileges of an Approved Continuing Airworthiness Management

Organisation

MADOSS – HMSJF as a Continuing Airworthiness Management Organisation

(CAMO) approved under DCAM Part M will carry out the following tasks:

a. manage the continuing airworthiness (DCAM Part M, Subpart G)

of aircraft as listed on the DCAM Approval Certificate;

b. issue an Airworthiness Review Report (DCAM Part M, Subpart I)

and make recommendation for the Certificate of Airworthiness

issuance or renewal to DCAM;

MADOS – HMSJF shall applies his privilege under CAMO for the following

aircrafts operated at both Royal Flight Hangar in Senai International Airport

(JHB) and Istana Bukit Serene (IBS) Hangar in Johor Bahru:

NO. AIRCRAFT

TYPE ENGINE TYPE

MANAGED

AT SITE

APPROVED

MAINTENANCE

PROGRAMME

1 Boeing 737-

800

CFM56-7B27E JHB HMSJF/737-

800/ISS00

2 Gulfstream GVI

(G650ER) RR BR700-

725A1-12

JHB HMSJF/G650ER/ISS00

3 Gulfstream GV-

SP RR BR700-

710C4-11

JHB HMSJF/G550

4 Gulfstream GIV RR Tay Mark

611-8

JHB JMF (U) / GIV

5 Sikorsky S-76B P&W PT6B-

36B

IBS HMSJF/S76B/ISS00

All maintenance checks (scheduled and unscheduled) including defect

rectification is contracted to an Approved Maintenance Organisations.


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0.3.2 Conditions of Approval

MADOSS – HMSJF as an Approved CAMO will manage aircraft which it is

approved for only when all necessary facilities, documentation, staffing are

available and the organisation is in compliance with the DCAM requirements.

0.3.3 Validity of Approval

The approval is valid till the date as stated on the DCAM Approval Certificate,

which should not exceed one (1) year, unless the approval has been

surrendered, superseded, suspended, revoked or expired by virtue of

exceeding the expiry date specified in the approval certificate.

The continued validity of approval is dependent upon:

a. MADOS – HMSJF remaining in compliance with DCAM Part M

requirements, in accordance with the provisions related to the

handlings of findings as specified by DCAM.

b. DCAM being granted access to MADOS – HMSJF to determine

continued compliance with the requirements of DCAM Part M.

c. The approval certificate not being suspended or revoked.

d. Adherence to the requirements specified in this CAME.

0.3.4 Renewal of Approval

An application to renew or vary the approval shall be made to DCAM through

QAM by submitting:

a. Application form DCA/AW/6102-1;

b. Proposed revision of CAME;

c. Applicable fee as stipulated by the regulation.


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0.4 MANAGEMENT PERSONNEL

The current management personnel of MADOSS – HMSJF comprises of the

Accountable Manager and Nominated Post Holders as follows:

NO. DESIGNATION NAME

1 Accountable Manager Dato’ Hj Mazelan Abu

2 Continuing Airworthiness

Management Manager

Zaihasry Zainoren

3 Quality Assurance Manager Azman Hj Ramlee

Note: Changes to all of the above position shall be notified to the DCAM

Airworthiness Section through DCAM Form 4.

0.4.1 Accountable Manager

The duties and responsibilities associated with this post are held by the

nominated person in Para 0.4 of this CAME.


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0.4.2 Continuing Airworthiness Management Manager

The duties and responsibilities associated with the post of Continuing

Airworthiness Management Manager (CAMM) are currently assumed by the

nominated person in Para. 0.4 of this CAME, in support of the Accountable

Manager.

The CAMM is responsible for determining what maintenance is required, when

it has to be performed and by whom and to what standard, in order to ensure

the continued airworthiness of the aircraft being operated.

0.4.2.1 Continuing Airworthiness Management Manager Qualification

Requirements

To carry the duties and responsibilities as laid out in Para. 0.5.2, the

CAMM shall has the following qualifications:

1. A practical experience and expertise in the application of

aviation safety standards and safe operating practices;

2. At least five (5) years relevant work experience of which at

least two (2) years should be from the aviation industry;

3. Relevant engineering degree acceptable to Director General

or an appropriate license in compliance with DCAM AN

1101;

4. Thorough knowledge with the MADOSS – HMSJF’s CAME;

5. Knowledge of maintenance methods;

6. Knowledge of applicable regulations and any relevant

regulatory requirements.


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0.4.3 Quality Assurance Manager

The duties and responsibilities associated with this post are currently assumed

by the nominated person in Para 0.4 of this CAME, in support of the

Accountable Manager.

The post of QAM and associated responsibility for the management of the

operator’s quality system for both operational aspects and the continuing

airworthiness aspects may be held by one person, subject to the acceptance

by the DCAM.

0.4.3.1 Quality Assurance Manager Qualification Requirements

To carry the duties and responsibilities as laid out in Para. 0.5.3, the

QAM shall has the following qualifications:

1. A practical experience and expertise in the application of

aviation safety standards and safe operating practices;

2. Knowledge of quality systems;

3. At least five (5) years relevant work experience of which at

least two (2) years should be from the aviation industry;

4. Relevant engineering degree acceptable to Director General

or an appropriate license in compliance with DCAM AN

1101;

5. Thorough knowledge with the MADOSS – HMSJF’s CAME;

6. Knowledge of maintenance methods;

7. Knowledge of applicable regulations and any relevant

regulatory requirements.


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0.5 DUTIES AND RESPONSIBILITIES OF MANAGEMENT PERSONNEL

0.5.1 Accountable Manager

Immediate Superior: Board of Directors

Responsibilities:

The Accountable Manager has the overall responsibility to ensure compliance

with DCAM Continuing Airworthiness Requirements. He/she is responsible for

ensuring that all the continuing airworthiness management activities can be

financed and are carried out to the standard required by the DCAM.

In particular, he/she is responsible for ensuring that adequate contractual

arrangement exist. This includes, among others, provision of facilities, material

and tools, sufficient competent and qualified personnel in relation to the work

to be undertaken.

All of this with a view to ensure that all due for continuing airworthiness

activities including all maintenance is performed on time and in accordance

with the applicable requirements, regulations and approved standards and

that the aircraft has a valid Certificate of Airworthiness for all flights

undertaken.

The Accountable Manager has the financial responsibility for all of the

continuing airworthiness arrangements.

Specific Functions:

1. Establish and maintain an organisational structure with competent

post holders and staff with clearly specified functions, roles and

responsibilities.

2. Ensure safe operations in compliance with relevant rules and

regulations, and that every flight is conducted with the provisions of

operations manuals.


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3. Maintain and manage the financial capability of the MADOS – HMSJF

ensuring all resources are efficiently financed.

4. Ensure all MADOSS – HMSJF personnel are adequately trained with

the required skills and competencies to perform their roles and

responsibilities.

5. Liaise and communicate with external stakeholders including the

governmental and aviation authorities, media etc.

0.5.2 Continuing Airworthiness Management Manager

Immediate Superior: Director of Aviation / Accountable Manager

Responsibilities:

This person is the nominated post holder for continuing airworthiness. He will

ensure that all maintenance is carried out on time and to an approved

standard. He will act to ensure that MADOSS – HMSJF’s responsibilities in the

following areas can be met:

1. Establishment and development of continuing airworthiness policy,

including the approval of MADOSS - HMSJF aircraft maintenance

programme.

2. To control the relationship with Part-145 maintenance contractor(s)

and establishment of a Maintenance Contract

3. Timely accomplishment and delivery, to the required standards, of all

continuing airworthiness management activities.

4. Ensuring that the Quality Assurance System required is effective in its

application and any follow up actions required to address findings.

5. Ensuring that operations are conducted in a safe and secure manner

within his area of responsibilities.


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Specific Functions:

1. Analysis of the effectiveness of the Maintenance Programme and

ensure it is amended and approved in a timely manner.

2. Approval, by the DCAM of MADOSS – HMSJF Journey Log, including

any subsequent amendment thereto.

3. Review of Airworthiness Directive (AD), Service Bulletin (SB), Service

Letter (SL) and Service Information (SI) status and ensure

embodiment.

4. Monitor line and base maintenance of all fleet under MADOSS –

HMSJF and rectification of all defects.

5. Work planning and follow up, which includes technical follow up.

6. Ensuring that all modifications and repairs (changes) are carried out

to an approved standard.

7. Taking the necessary corrective action resulting from quality audit

non-conformances in the areas for which he is responsible.

8. To set-up non mandatory modification embodiment policy.

9. Responsible for the control, distribution and preservation of records

relating to the maintenance activities of the company.

10. That MADOSS – HMSJF pilots are duly trained and authorised to issue

Maintenance Release, where necessary and appropriate.

11. That the Certificate of Airworthiness for each aircraft operated by the

company remains valid in respect of:

i. the airworthiness of the aeroplane,

ii. the expiry date specified on the Certificate, and

iii. any other condition specified in the Certificate.


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12. Review and implementation, as appropriate, of any additional DCAM

requirements.

13. Ensure that all Maintenance Data (AMM, SRM, IPC, CMM and WDM)

is updated at all times.

14. Responsible for reviewing this CAME and for preparing any

amendments.

15. Responsible for review and approval of tooling & equipment

requests.

16. To carry out any other task as directed by the immediate superior.

0.5.3 Quality Assurance Manager

Immediate Superior: Director of Aviation / Accountable Manager (has direct

access to Accountable Manager on urgent safety and

continuous airworthiness matters)

Responsibilities:

Quality Assurance Manager is responsible for the following functions:

1. Establishing a Quality Monitoring Programme which addresses all of

the areas of MADOSS – HMSJF’s contracted maintenance support.

2. Monitoring that all activities carried out under DCAM Airworthiness

Notices 6102, DCAM Part M Subpart G are being performed in

accordance with the approved procedures;

3. Monitoring all contracted maintenance activities is carried out in

accordance with the contract;

4. Monitoring continued compliance with the requirement of DCAM AN

6102 and any other DCAM requirements.


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5. Responsible to the Accountable Manager on quality matters and also

has direct access to the Accountable Manager in the event of any

reported discrepancy not adequately attended to.

Specific Functions:

1. Monitoring amendments of this CAME and the submission to DCAM.

2. Ensuring that all maintenance is performed in compliance to the

quality standards defined.

3. Act as correspondence with authority.

4. Ensuring that all continuing airworthiness documentation is used

properly and accordingly.

5. Performing quality surveillance on the continuing airworthiness

system in accordance with the approved annual planned audit

programme to ensure compliance with regulatory requirements and

organisation policies.

6. Proposing all corrective action necessary for eliminating non-

compliance and ensuring that these corrective actions are

implemented.

7. Reporting any occurrences of a maintenance nature to the DCA

Malaysia and the aircraft manufacturers. This includes both

Mandatory Occurrences and Occurrences related to maintenance

findings, which fall outside the Mandatory scheme.

8. To carry out any other Quality Assurance related task as directed by

the immediate superior.


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0.5.4 Technical Publication Executive

Immediate Superior: Continuing Airworthiness Management Manager

Responsibilities:

1. Maintain an up-to-date systematic filing system of all publications

(filing management).

2. Ensure all online subscriptions for publications are up-to-date and

readily available when required.

Specific Functions:

1. Establish and maintain an up-to-date filing system for Technical

Publication.

2. Establish a Master Copies for all publications and ensure availability

upon request.

3. Ensure all online subscription be prompt and up-to-date.

4. Review the revision services of all publication at least 3 months

before the expiry date.

5. Maintain a proper housekeeping in Technical Publication.

6. Refer immediate superior of any discrepancy found and take

immediate corrective action as required.

7. To carry out any other task as directed by immediate superior.


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0.5.5 Maintenance Planning Executive


Responsibilities:

Plan, coordinate and control the MADOSS – HMSJF’s aircraft maintenance

activities to enable the accomplishment of the maintenance requirements

within an established schedule in the most economical and efficient manner.

Specific Functions:

1. Ensure effective pre-planning on aircraft check package, including

package study and resources requirement and check downtime

evaluation.

2. Verify that the necessary materials, equipment and tooling are made

available and provided for prior to the aircraft check tasks

commencement.

3. Coordinate initiate Review Meeting with the contracted

Maintenance Organisations and perform pre-input survey of the

aircraft detailing any additional requirements to be performed during

the aircraft check.

4. Monitor check in progress, keep tab on feedbacks and inputs to

ensure a planning driven environment within the aircraft check

management.

5. Liaise with the contracted Maintenance Organisations for quotation

related issue and to submit Request for Quotation (RFQ) in timely

manner.

6. Prepare, compile and control work packages for all MADOSS –

HMSJF’s aircraft and make available necessary supporting documents

and preparations to enable work package control.


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7. To verify that the necessary materials, equipment and tooling are

made available and provided for prior to the aircraft check tasks

commencement.

8. Ensure the work packages or any other specific maintenance tasks

are studied and the required manhours are known prior to scheduling

the task.

9. Control the completed work package and make necessary

compilation and submit to Technical Records.


0.5.6 Technical Records Executive


Responsibilities:

1. Maintain up-to-date records and establish a systematic storage of all

technical records which includes the Journey Log SRP, AD / SB

compliance, modifications records and all completed check package

for all aircrafts operated by MADOSS – HMSJF.

2. Maintenance of Technical Records documents pertaining to effective

and fail-safe storage system to prevent contamination / corrupted or

damage of the records.

Specific Functions:

1. Establish a Master Index for all Technical Records and update as

necessary.

2. Maintain a proper filing system for storage of all hard copies in

Technical Records.


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3. Maintain a proper storage system and identify with proper index the

location for all CD/DVD type records.

4. Carry out immediate corrective action for replacement of

contaminated or damage records.

5. Ensure records and other documents related to maintenance are

retained and present for a minimum period of three (3) years.

6. Maintain a proper housekeeping in Technical Records.

7. Refer immediate superior of any discrepancy found and take

immediate corrective action as required.



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0.6 MANPOWER RESOURCES AND TRAINING POLICY

0.6.1 Manpower Resources and Analysis

MADOSS – HMSJF shall at all times ensure that the appropriate qualified staffs

are sufficient so that the expected work that required to be performed

fulfilled.

NO POSITION TOTAL

1 Management

i. Accountable Manager

ii. Continuing Airworthiness

Management Manager

iii. Quality Assurance Manager

1

1

1

2 Continuing Airworthiness Management

i. Technical Publications

ii. Technical Records

iii. Maintenance Planning

iv. Airworthiness Review Staff

1

1

1

2

TOTAL 8

1 man year = 2000 hrs. Full

Time

Staff

Part

Time

Staff

Part Time Staff

as Equivalent

Full Time Staff

Total

Staff

Total

Hours

Management 3 0 0 3 6000

Continuing

Airworthiness

Management

5

0

0

5

10000

Total 8 0 0 8 16000


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0.6.2 Training Policy

Training will be provided by MADOSS – HMSJF to ensure that each member of

staff is adequately trained to carry out the functions of, and satisfy the

responsibilities associated with, the DCAM AN 6102, Part M Subpart G

continuing airworthiness management functions.

Listed below is the mandatory training required for personnel working under

MADOSS – HMSJF:

1. Company policy awareness as laid out in this CAME.

2. Human Factor

3. Safety Management System

4. Continuing Airworthiness Management awareness.

5. Certifying personnel to comply with DCAM AN 1101 Part 66

requirements.

The Quality Assurance Manager will review training needs at intervals not

exceeding two years or at more frequent intervals if, and when, significant

changes occur to the organisation, procedures and aircraft types operated.


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0.7 MANAGEMENT ORGANISATION CHART

0.7.1 General Organisation Chart

0.7.1.1 Continuing Airworthiness Management Organisation Chart

Continuing Airworthiness Management Manager

Director of Aviation

Quality Assurance Manager

Technical Publication

Technical Record

Airworthiness Review Staff

Maintenance Planning

LEGEND: Accountable Approved Manager Signatory Post Holder Direct Access to AM

MADOSS – HMSJF (CAMO)

MADOS’S HOLDINGS SDN BHD

Rotary Wing (Istana Bukit Serene Hangar)

Fixed Wing (Royal Flight Hangar)


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0.8 NOTIFICATION PROCEDURE TO THE DCA REGARDING CHANGES TO THE OPERATOR’S

CONTINUING AIRWORTHINESS MANAGEMENT ARRANGEMENTS / LOCATIONS /

PERSONNEL / ACTIVITIES / APPROVAL

The AM will undertake to advise the DCAM of any proposal to carry out any of the

following changes before such changes take place:

a) The name and location of the organization.

b) Additional locations of the organization.

c) The AM, CAMM and QAM are considered as nominated post holder.

Application for approval shall be made using DCAM Form 4 together with copy

of resume of proposed nominated post holder.

d) The facilities, procedures, work scope and staff that could affect the approval.

0.8.1 Changes

Any proposal to carry out any of the following changes, it shall be notified to

the DCAM as soon as practicable, before such changes take place by the

Accountable Manager to enable the DCAM to determine continued

compliance with DCAM Part M requirements.

In the case of proposed changes in personnel not known to the MADOSS –

HMSJF’s management before-hand, these changes shall be notified to the

DCAM at the earliest opportunity. DCAM approval is required prior to

incorporation and to make any necessary amendments to the appropriate

documentation.


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0.9 CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION AMENDMENT

PROCEDURES

CAME shall be reviewed on an annual basis by the CAMM and amendments

incorporated, taking the decisions of the MADOSS – HMSJF, AM.

Any amendments will be submitted to the DCAM, by the QAM, for approval prior to

their incorporation in the CAME.

It is necessary to comply with any new or amended regulation published by the

authority from time to time. New or amended procedures should not be in conflict

with the regulation. Regulation changes as well as any relevant changes within the

company that affect the approved CAME therefore call for an amendment thereof.

The original issue of this CAME manual shall be Issue 01. Changes shall be identified

by way of revision to the issued number, which will be in numerical order. Where there

are extensive revisions necessitating a complete reissue, a new issue number will be

allocated in numerical order.

Revisions to the new issue will begin again from Revision 00.

0.9.1 Procedures

The following amendment procedure has to be followed:

i) The CAMM is responsible for reviewing the CAME and preparing any

amendments.

ii) The affected page has to be replaced if the content is amended or

changed.

iii) The changed text passages have to be marked with a vertical line at

the left side of the page.

iv) Issue/Revision/Date in the header has to be changed accordingly for

each amendment made.


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v) List of Effective Pages shall be updated (Revision and Date) each time

amendment is made.

vi) QAM verifies amendment as per approved procedures, by approval

stamp of the List of Effective Pages and submit to DCAM for approval.

vii) The old pages that are affected by any amendment shall be replaced

after the approval for the revision is granted.

viii) The approved revision pages shall be distributed to the recipients

according to the distribution list.

ix) All amendments will be submitted to the DCAM for approval prior to

their incorporation in the CAME.

x) All the continuing airworthiness staff and MADOSS – HMSJF staff shall

be advised about the changes.

0.9.2 CAME Review

CAME will be reviewed at intervals not exceeding 12 months or more

frequently when significant changes occur which affect the content of the

CAME.


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0.10 FACILITIES

0.10.1 Royal Flight Hangar, Senai International Airport (JHB)


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0.10.2 Bukit Serene Hangar (IBS)


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0.10.3 CAMO Office Layout Plan in Royal Flight Hangar, Senai International Airport


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CAME Part 1 – Continuing Airworthiness Management Procedures Page 1-1

PART 1

CONTINUING AIRWORTHINESS

MANAGEMENT PROCEDURES


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1.1 CONTINUING AIRWORTHINESS MANAGEMENT PROCEDURES

This Part One defines the continuing airworthiness management procedures which

MADOSS – HMSJF uses to ensure compliance with the continuing airworthiness

aspects of DCAM Part M and other DCAM requirements. Where some aspects of these

function are sub-contracted, then this will be clearly defined in the text.


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1.2 AIRCRAFT JOURNEY LOG SYSTEM UTILISATION AND MINIMUM EQUIPMENT LIST

APPLICATION

1.2.1 The Journey Log

The Journey Log in use in MADOSS – HMSJF is designed to allow recording of

defects, malfunctions and maintenance performed on the aircraft to which it

applies whilst the aircraft is operating between scheduled maintenance

inspections.

In addition, it includes maintenance information required by the operating

crew and is used for recording operating information relevant to flight safety.

The continuing airworthiness information includes:

1) the operating crews observations and remarks as a result of aircraft

operation in service including the aircraft, engine(s), components system

technical status;

2) defects or incidents having effect on airworthiness;

3) results of technical inspections requested by the maintenance

organisation;

4) maintenance performed by the contracted maintenance organisation

which details:

a) defect rectification action taken and associated responses to crews

requests and/or remarks;

b) scheduled maintenance inspections performed;

c) next due scheduled maintenance inspections;

d) where applicable, any MEL technical limitations proposed by the

Maintenance Organisation.


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1.2.1.1 The Journey Log Contents

The MADOSS –HMSJF Journey Log contains four sections:

Section 1 This section details the operator’s name and address, the

aircraft type and the registration.

Section 2 This section contains the Sector Record Pages as provided

in the Journey Log book.

Section 3 This section contains the Deferred Defect Log pages, an

example of which is provided within Appendix 1 of

Appendices, Item 2.

Section 4 This section contains details of part(s) being replaced with

regards to any defects arising and rectifications carried

out.

The samples of document are given within Appendix 1 of CAME

Appendices, Item 1.

CAMM shall prepare for any amendment to the Journey Log Book and

submit to QAM for review and approval to ensure compliance with

any applicable requirements. Once approved, the changes of the

Journey Log will be submitted to DCAM Airworthiness Sector for final

approval.

CAMM, through the function of Technical Records Executive will

ensure that copies of all Journey Log Sector Record Pages, and any

other pertinent maintenance related information are forwarded

promptly to the Technical Record, to allow them to perform their

planning and maintenance coordination functions.

MADOSS – HMSJF shall ensure that aircraft Journey Log is retained

for at least 36 months after the date of the last entry.


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1.2.1.2 Instruction for Use

1. General

a. Journey logs are printed in duplicate – White Copy, Technical

Records copy and Yellow Copy, book copy (original).

b. All entries must be clearly written in BLOCK LETTERS in black

ink pen. Where errors are made, they should be neatly ruled

through and signed by person who made the erroneous entry.

Errors that are corrected shall remain readable and

identifiable.

2. Flight Crew to Record

a. Aircraft Type

b. Aircraft Registration

c. Names of Pilot in Command

d. Flight Number

e. Sector

f. Departure (UTC) – DATE/TIME

g. Arrival (UTC) – DATE/TIME

h. Additional Landing (if applicable)

i. Defects Column – If nil defect, enter ‘NIL’ at crew change or

end of day

3. LAE to Record

a. Defects Column – Enter defects as applicable

b. Action Column

i. Action all recorded defects prior to further flight.

ii. If defect is deferred:

- Transfer defect to Deferred Defect Log. Annotate

Journey Log serial number and defect number in

source Journey Log box.

- Enter Deferred Defect Log serial number in

“TRANSFERRED TO DDL NO” box, in action column of

Journey Log.


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iii. When deferring MEL defects, annotate in action column

of the Journey Log:

- Transferred to DDL serial number

- MEL reference number

- MEL expiry date

- MEL repair category (A, B, C or D)

NOTE: Calculation of expiry date starts at 0001 hours on

the day following the raising of the DDL.

Example: When a DDL is raised at 1300 hours on 1st May,

the repair interval limitation takes effect at 0001 hours

on 2nd May.

- The part number of the defective part if determined.

iv. If nil defect is reported in Defects Column, enter ‘NIL

NOTED’ in action column.

v. If parts are replaced, record the following details:

- Part Number and Part Description

- Removed Position

- Serial Number On and Serial Number Off

- Batch Number

vi. Enter LAE signature, LAE No. (stamp) and enter date.

Ensure all pages are stamped.

vii. If a new Journey Log page is used, enter Aircraft Type

and Aircraft Registration.

c. Certify for any Daily / Stay-over Check carried out and record

APU HR Meter & number of starts as required.

4. Removal / Distribution of Journey Log – Maintenance Action

a. Whenever defect(s) is entered; or

b. At every crew change; or

c. At the end of each day.

5. At Base

a. Remove the completed White Copy.

b. Attach applicable Serviceable Label to the White Copy.

c. Forward the White Copy (with Serviceable Label if any) to

Technical Records.

d. Yellow Copy to remain in the Journey Log Book until book is

replaced.


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1.2.2 MEL Application

A Minimum Equipment List (MEL) duly approved by the authorities shall be

used for dispatching an aircraft with permitted system / component

inoperative. The MEL shall be based upon the relevant Master MEL accepted

by the authorities having jurisdiction.

The objective of using the approved MEL is to improve the aircraft utilisation

by minimising delays to aircraft movement and thereby providing more

convenient and economic air transportation for the public while meeting

airworthiness requirements.

Defects that are allowed to be deferred per approved MEL shall be recorded

appropriately in the aircraft Journey Log. Penalties or limitations if any shall be

highlighted to the commander or ground crew by appropriate means such as

using ‘Notice to Crew’ (NTC) or appropriate placards.

The sample of Notice to Crew form is given within Appendix 1 of CAME

Appendices, Item 6.

It shall be CAMM responsibility in liaison with contracted Part-145 organisation

to maintain and update approved MEL of the aircraft. The approved MEL will

be reviewed and amended accordingly in a timely manner.

1.2.2.1 MEL Procedures

MADOSS – HMSJF’s approved Minimum Equipment List (MEL)

represents a listing of items of equipment, which may, under

circumstances be unserviceable.

When a defect has been raised in ‘Defects’ column of the Journey Log

Sector Record Page (SRP) and is deemed to be within the allowance

quoted in the approved MEL then it may be subject to carry forward

action.


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Consideration should also be given by the person carrying forward the

defect to the possible affect that multiple and related defects may

have even where these are covered as individual items in the

approved MEL. The entry in the ‘Action Taken’ column of the SRP

should be annotated ‘Defect carried forward in accordance with the

MEL reference ….. DDL No. ….. raised’ this entry may be made by the

operating crew or maintenance personnel.

The Deferred Defect Log (DDL) record pages must be suitably

annotated with details of the defect and a time limit must be specified

(date and time or remaining flight hours and/or cycles). No

Maintenance Release is to be issued for the carried forward item until

the defect has been cleared on a subsequent SRP.

Refer to Flowchart 1 of this Part 1 for Defer Defect Procedures.


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Flowchart 1 Defer Defect Procedures

NO

YES

Part-145 fix the defect

Route Penalties Disarm / INOP the system

Placard cockpit control where applicable

Clear the defect in Journey Log

Transfer item to Acceptable Defer Defect Log

Schedule for work Route Penalties

Defer Defect as per MEL and raise NTC if applicable

CAMM inform Part-145 AMO

Inform CP

Ground the Aircraft

Journey Logbook Entry

Item in the MEL

Dispatch Flight

Release the aircraft Captain acceptance in the

Journey Log


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1.2.2.2 Acceptance by the Pilot

When there are multiple inoperative items, qualified personnel

dispatching the aircraft shall disclose all the information to the

commander to enable him to make an assessment of his workload or

exposure to additional failure during the continued operation.

Where the MEL item has been entered by maintenance personnel,

the decision to accept the carried forward item allowed by the

approved MEL/CDL remains the responsibility of the pilot in

command. This acceptance of any open deferred items is indicated

by his/her signature on the SRP in ‘Captain’s Acceptance’ space.

1.2.2.3 Management of the MEL Rectification Intervals

The time limit for the defect rectification or “rectification interval” is

specified in the MEL in Flight Hours/Cycles/Calendar Time (A, B, C or

D) so that the defect rectification may be performed within the

specified MEL limit.

All deferred defects shall be recorded and monitored/tracked by the

CAMM.

1.2.2.4 MEL Rectification Interval Expiry

Dispatch of the aircraft is not allowed after expiry of the Rectification

Interval specified in the MEL, unless:

a) The Rectification Interval is extended in accordance with an

“Extension Procedure” which is agreed between Continuing

Airworthiness Management Manager and the Chief Pilot of

respective section (Fixed/Rotor Wing) through an application of

MEL Deferred Defect Extension Request Form submitted by

Quality Assurance Manager to DCAM. Refer to Appendix 1 of

CAME Appendices, Item 7 for MEL Deferred Defect Extension

Request Form sample document.

b) The defect has been rectified.


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1.3 AIRCRAFT MAINTENANCE PROGRAMME – GENERAL

The Aircraft Maintenance Programme is to provide maintenance planning instructions

necessary for the safe operation of the aircraft. The aircraft maintenance schedule is

part of Aircraft Maintenance Programme which reflect the latest requirements which

is provided by DCAM, manufacturer’s and MADOSS – HMSJF’s operating experience.

Refer to Appendix 5 of CAME Appendices for List of Approved Maintenance

Programme.

1.3.1 The Programme – Contents – Sources

The Programme is based upon the manufacturer’s Maintenance Planning

Document or Maintenance Review Board Report for aeroplanes and

helicopters, which has been amended to reflect in full the maintenance

recommendations of the airframe, engine and equipment fitted on the aircraft.

The operators’ experience also can be used to develop the Aircraft

Maintenance Programme. The outcome from the Liaison Meeting as per

Chapter 1.6.1 of this exposition shall be the base for the development and

amendments of the Aircraft Maintenance Programme, as applicable.

All the latest and approved engineering data (Maintenance Manual, Service

Bulletins, Modification Bulletins, etc.) for MADOSS - HMSJF aircrafts can be

viewed and downloaded from:

NO.

AIRCRAFT

AIRFRAME

ENGINE

1 B737-800

BBJ2 www.myboeingfleet.com https://cwciportal.cfm56.com

2 G 650 www.mygulfstream.com DVD Rolls Royce (updated

every 4 months)

3 G 550 www.mygulfstream.com DVD Rolls Royce (updated

every 4 months)

4 G IV www.mygulfstream.com www.mygulfstream.com

5 S-76B www.sikorsky360.com http://www.pwc.ca

http://www.myboeingfleet.com/

https://cwciportal.cfm56.com/

http://www.mygulfstream.com/




http://www.sikorsky360.com/

http://www.pwc.ca/


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1.3.2 Structural Inspections, Corrosion Control, Reliability and Engine Health

Monitoring

Due to the nature of operational usage of the aircraft operated, i.e. low

hours/cycles utilisation; there are currently no specific requirements for a

Structural Inspection, Corrosion Control, Reliability or Engine Health

Monitoring Programmes other than those generally applied as part of the

manufacturers’ maintenance recommendations.

1.3.3 Mandatory Life Limitations

Mandatory Life Limitations are those imposed by the manufacturers and any

additional requirements from the DCAM. A listing of this mandatory life

limitations are provided in the applicable Approved Aircraft Maintenance

Programme.

1.3.4 Inspection Standards

The Inspection Standards applicable are those given by the manufacturers of

the airframe, engine and equipment and detailed in Approved Maintenance

Programme. Any additional Inspection Standards will be adopted if and when

these are promulgated by DCAM.

1.3.5 Maintenance Certification

All maintenance above the pre-flight level, shall be certified by authorised

persons through the issuance of a Maintenance Release as applicable to

aircraft on the Malaysia register and as per DCAM AN 12 and AN 6501.

1.3.6 Fuel Contamination

Fuel contamination checks are addressed in Part 1 of this CAME Para. 1.12.5.

Also, the Daily Inspection / Pre-Flight Check includes a fuel water drain sample

to be carried out prior to the first flight of the day.


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1.3.7 Maintenance Programme Owner – Responsibilities

The Maintenance Programme has been produced by MADOSS – HMSJF who is

the owner of the programme and is responsible for its development in

accordance with DCAM requirements. The Maintenance Programme is

submitted for approval to the DCAM by the QAM, on behalf of MADOSS –

HMSJF.

1.3.8 Holders of the Maintenance Programme

A copy of the Maintenance Programme will be held by:

a) Continuing Airworthiness Management Manager

b) Quality Assurance Manager

c) Technical Publication Executive

d) Contracted Approved Maintenance Organisation

e) DCAM Airworthiness Sector

1.3.9 Maintenance Programme Review, Development and Amendment

1.3.9.1 Review and Development

The Aircraft Maintenance Programme provides maintenance

instructions or arrangements for safe operation of the aircraft.

Maintenance Programme shall be reviewed annually. As a minimum,

revisions of documents affecting the programme basis need to be

considered by MADOSS – HMSJF for inclusion in the Maintenance

Programme during the annual review.

Applicable mandatory requirements for compliance with Type

Certificate Holder or Supplemental Type Certificate Holder shall be

incorporated into the Maintenance Programme as soon as possible.


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Development and amendment of the Maintenance Programme is the

product of CAMM’s actions in monitoring the effectiveness of the

Programme (see Para. 1.6). This together with the recommendations

received from the contracted Maintenance Organisations, and the

CAMM’s response to continued airworthiness information published

by the manufacturers of aircraft, engines and equipment in the form

of Airworthiness Directive (AD), Service Bulletins (SB), Service Letters

(SL) and also will reflect the latest information which is provided by

DCAM.

The Approved Maintenance Programme shall be maintained by the

CAMM in order to reflect the latest requirements, which may

originate from DCAM, other regulatory bodies, manufacturers or for

general improvement in aircraft engineering.

The QAM is responsible to submit the final draft of the Maintenance

Programme to DCAM and DCAM will issue a Maintenance

Programme Approval, which signifies approval of the Maintenance

Programme.

1.3.9.2 Maintenance Programme Meetings

Liaison Meetings between CAMM and the contracted Maintenance

Organisation will be held at intervals not exceeding six months to

discuss and review the effectiveness of the Maintenance Programme.

Refer to this CAME Para. 1.6.1 for Liaison Meetings.


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1.3.9.3 Maintenance Programme Amendments

Where changes are identified as being necessary, and agreed

between the CAMM and approved Maintenance Organisations, these

will be submitted by the QAM to the DCAM as an amendment.

Under its indirect approval, the organisation will manage and amend

the maintenance programmes for Malaysian registered aircraft.

i) Amendments will be fully supported and recorded as detailed

in Para. 1.3.9.1 above.

ii) The CAMM will be independent of the decision making process

for an amendment. The QAM will approve all amendments to a

Maintenance Programme.

iii) The QAM is responsible to review, approve and submit the final

draft of the Maintenance Programme to DCAM for approval.

iv) Any amendment to Maintenance Programme is categorised as

A, B and C Amendments:

1. “A” Amendments: Mandatory amendments promulgated

by DCAM.

2. “B” Amendments: Amendments which have been

requested by the operators of the aircraft and approved

by DCAM.

3. “C” Amendments: Amendments which have been

requested by the operator of the aircraft and approved by

QAM. Approval from the DCAM is NOT required in making

“C” amendments and is limited to typographical error.


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1.4 TIME AND CONTINUING AIRWORTHINEES RECORDS: RESPONSIBILITIES, RETENTION

AND ACCESS

At the completion of any maintenance, the associated maintenance release shall be

entered in the aircraft continuing airworthiness records to enable the organisation to

maximise the value and utilisation of its assets. Each entry shall be made as soon as

possible but in no case more than 30 days after the day of the maintenance action.

1.4.1 Hours and Cycles Recording

Continuing airworthiness records, including hours and cycles recording for

MADOSS - HMSJF aircrafts are the responsibility of CAMM. These records

include:

a) The aircraft Log Books for Airframe, Engine(s)

b) Modification records.

c) Inspection records (Work-package).

d) Component life records.

e) Aircraft Journey Log Sector Record Pages.

f) Overhaul records.

g) Repair records.

h) Airworthiness Directive / Airworthiness Notice compliance records.

i) Service Bulletin etc. compliance records.

j) Deferred defect records.

k) Concession.

The maintenance records such as Journey Log Book held by the Maintenance

Contractors will be upheld by CAMM in the form of copies of the Journey Log

Sector Record Pages which are forwarded to the MADOSS – HMSJF at the

intervals defined between both parties in the Maintenance Contract.

1.4.2 Sector Record Page Retention

Top copies of the Journey Log Sector Record Pages are retained by MADOSS –

HMSJF for at least 36 months after the date of the last entry.


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1.4.3 Access to Continuing Airworthiness Records

All of the records may be accessed by CAMM or an authorised person by QAM

at any reasonable time and remain the property of MADOSS – HMSJF at all

times. Access to the records by duly authorised members of the DCAM will be

arranged where this is necessary. This is to ensure that all the records will not

be altered during retention period.

1.4.4 Control and Preservation of Records

All continuing airworthiness records as listed in Para. 1.4.1 will be filed and

stored in such a manner acceptable by DCAM and will be readily accessible to

authorised personnel or auditors. The filing and storage system shall promote

ease of retrieval, accessibility and adequate control. All records shall be

retained by MADOSS – HMSJF for the duration of two (2) years after the aircraft

has been permanently withdrawn from service.

Hardcopy records in the form of paper or compact disc shall be stored in a safe

way with regards to fire, flood, theft or unauthorised alteration. Paper used

must be of robust material, which can withstand normal handling and filing. All

paper form records shall remain legible throughout the required retention

period.

Continuing airworthiness records which are stored in the computer system

should be secured with adequate programmer’s security systems to protect

from unauthorised alteration. The records should also be of continuous with

multiple backup systems.

In the event of records being lost or destroyed, reconstruction can be done by

reference to other records which reflect the time in service and research of

records maintained by contracted Maintenance Organisations. When these

procedures are done but the records are still incomplete, MADOSS – HMSJF

may make a statement in the new records describing the loss and establishing

the time in service based on the research and the best estimate time in service.

The reconstructed records should be submitted to DCAM for acceptance.


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1.4.5 Transfer of Continuing Airworthiness Records in the Event of a Sale or other

Disposal of the Aircraft

In the event of sale or other disposal (lease-in, lease-out) of an aircraft,

MADOSS – HMSJF is required to make all the aircraft continuing airworthiness

records available and transfer all the records to the new owner or operator of

the aircraft.

1.4.6 Access to Continuing Airworthiness Records in the Event of an Accident /

Incident

In the event of an accident or serious incident the CAMM will hold the records

secure until requested by the Air Accidents Investigation Bureau (AAIB),

Ministry of Transport. Any maintenance activities on the affected aircraft shall

only proceed after clearance from AAIB.


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1.5 ACCOMPLISHMENT AND CONTROL OF MANDATORY REQUIREMENTS FOR

AIRWORTHINESS (INCLUDING AIRWORTHINESS DIRECTIVES, SERVICE BULLETIN AND

DCAM MANDATORY REQUIREMENTS)

1.5.1 Access to Airworthiness Directives & Service Bulletins Requirements

The CAMM is responsible for the accomplishment of all applicable

airworthiness directives and DCAM requirements. The following mandatory

requirements for Airworthiness Directives (AD) and Service Bulletin (SB)

publications as applicable to the aircraft operated and subscribed to and

controlled by daily check of the publication email and manufacturer’s website

and states of design website to ensure all the publications are currently

updated.

1.5.2 AD, SB, SL & SI Decision and Implementation

The contracted maintenance organisation will be advised by CAMM of any

AD’s, SB’s, SL’s, SI’s or revision thereto, which affect MADOSS – HMSJF aircraft,

engines, or equipment at the earliest possible opportunity with a view to

establishing compliance.

The necessary actions will be agreed between the CAMM and the approved

Maintenance Organisation to schedule the compliance with the AD/SB at the

first reasonable maintenance inspection within the AD/SB’s required

compliance time.

In the case where an Alert SB has been issued, the Continuing Airworthiness

Management Manager shall take all reasonable steps immediately to ensure

affected aircraft complied with the task(s) detailed in the Alert SB before

further flight.

Where necessary, and required by the AD/SB, Repetitive Inspections will be

introduced until full compliance is achieved. The maintenance organisation will

be notified of any emergency airworthiness directives or Alert SB’s on receipt.


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1.5.3 AD/SB/SL/SI Control – Compliance Monitoring

Airworthiness Directive, Alert Service Bulletin, Service Bulletin, Service Letter,

Service Information compliance monitoring is the responsibility of MADOSS –

HMSJF CAMM.

The QAM will review this monitoring at the Liaison Meetings indicated in Para.

1.6.1. Compliance with AD/SB will be verified by the QAM as part of MADOSS

– HMSJF quality system.

Refer to Flowchart 2 for the Processing of Technical Compliance Document.

1.5.4 AD/SB/SL/SI Control – Recording of AD/SB Compliance

The method of compliance and when such compliance was achieved will be

recorded in the aircraft airworthiness records (Log Books) or Modification

Record Book by the CAMM. For AD/SB’s with repetitive inspection content

then each and every inspection will be recorded on completion with an

AD/SB/SL/SI is established.


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Flowchart 2 Processing of Technical Compliance Documents

AD/SB received by TP. TP issue MICL to be reviewed by CAMM

Doc applies to MADOSS – HMSJF

fleet?

CAMM mark MICL Doc as N/A

and send bi-weekly to QAM

Is it Mods/Insp Action?

CAMM will annotate ‘done’ on the sharing network MICL

database for MP to act

MP issue W/O for P-145 MO to c/out Insp/Mod

CAMM liaises with P-145 to c/out

Insp/Mod

MP issue W/O together with log card if compt. is a life limited part

Is it a compt. change?

CAMM liaises with P-145 for compt. change

Any changes to manual?

Does the Maint. Prog. require amendment?

CAMM advises P-145/Flt Ops if needed through a Transmittal

Letter

CAMM amends Maint. Prog. & submit amendment to QAM

CAMM liaises with P-145 for the amended App. Maint. Prog.

TR updates AD/SB compliance status (once off/recurring/N/A in the Mod. Record book

MP schedules action. TR monitors AD action w.r.t. compliance dates

CAMM files MICL Doc with note on action planned/taken

End

NO

NO

YES

YES

YES

NO

NO

YES

YES

NO

Note: 1. CAMM shall liaise with

QA/MP/P-145 if urgent action is required.

2. If AD/SB is a revision, check previous action for any need for further action.

3. CAMM shall monitor to ensure action is carried out not later than the target compliance date for MOD, INSP & CC card.

4. CAMM shall inform Chief Pilot of any changes to AFM.

Abbreviations: 1. AD – Airworthiness

Directive 2. Doc – Document 3. CAMM – Continuing

Airworthiness Management Manager

4. QAM – Quality Assurance Manager

5. MP – Maintenance Planning

6. SB – Service Bulletin 7. TR – Technical Records 8. MICL – Maintenance

Instruction Checklist form 9. TP – Technical

Publication 10. P-145 – Approved Part

145 11. W/O – Work Order 12. Org – Organisation 13. CC – Component Change 14. N/A – Not Applicable 15. Mod – Modification 16. Insp – Inspection 17. Prog – Programme 18. Compt – Component


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1.6 ANALYSIS OF THE EFFECTIVENESS OF THE MAINTENANCE PROGRAMME

MADOSS – HMSJF remains responsible for this subject. The CAMM will analysis and

monitor the effectiveness of the Maintenance Programme through regular Liaison

Meetings with the contracted Maintenance Organisation and the QAM.

1.6.1 Liaison Meetings

These meetings will address the following areas:

a) The Maintenance Programme content.

b) The effect on the Maintenance Programme of any ADs, modifications

or repairs.

c) Changes to the operation, which may affect the Maintenance

Programme.

d) Maintenance findings.

e) Other defect reports i.e. air turn-backs, spares reliability, technical

delays, technical incidents, repetitive defects and pilot reports.

f) Quality monitoring product samples (aircraft surveys).

g) Changes to the manufacturer’s maintenance guidance material,

Service Bulletins, Service Letters etc. and how these affect the


h) Other Quality System findings as they impinge upon the contracted

Maintenance Organisations.

i) Changes to the regulations and requirements by the DCAM, including

the Flight Operations Directives.

Where appropriate and necessary, amendments to the Maintenance

Programme will be raised by the CAMM and forwarded to the QAM for review

and approval. Once approved, QAM shall submit to DCAM for approval.

1.6.2 Frequency of Meetings

Liaison meetings will be held at a minimum of six (6) monthly intervals and the

results of any meeting recorded with any actions required allocated to the

responsible person.


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1.7 NON-MANDATORY CHANGES (MODIFICATION) EMBODIMENT POLICY

1.7.1 Changes (Modifications) General

Non-mandatory changes (modifications) will normally take the form of

manufacturer’s Service Bulletins, or will be derived from them. Any other

changes, i.e. those not covered by a manufacturer’s bulletin will be initiated by

the Continuing Airworthiness Management Manager in consultation with the

contracted Maintenance Organisations or with an Approved Design

Organisation (DOA).

1.7.2 Service Bulletins

All manufacturer’s Service Bulletins applicable to the aircraft operated by

MADOSS – HMSJF will be reviewed in the first instance by the CAMM for

applicability. Where compliance with the Service Bulletins may be seen as

beneficial to MADOSS – HMSJF then the approved Maintenance Organisation

will be advised.

All relevant SBs will be discussed during the Liaison Meetings.

1.7.3 Other Changes (Modifications)

For all changes (modifications) other than those introduced by manufacturer’s

SBs, i.e. those proposed by MADOSS – HMSJF or the contracted Maintenance

Organisation for operational advantage or other reasons must be produced by

Approved Design Organisation (DOA) or equivalent.

In the first instance the DCAM Airworthiness Sector will be consulted for advice

with an outline of the proposed change with a view to ascending whether or

not a change deemed to be classified as ‘Major’ or ‘Minor’.


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1.7.4 Minor Changes (Modifications)

All minor changes will be agreed by the CAMM before submission either to a

suitably approved Design Organisation (DOA) or DCAM. Where application is

made to DCAM, the CAMM will be responsible for raising and submitting the

Minor change approval through Statement of Compliance (SOC) and

modification procedures outlined in DCAM AN 78.

1.7.5 Instructions for Continuing Airworthiness

Any applicable Instructions for Continuing Airworthiness (ICA) derived from

the modifications will be inserted into the Approved Maintenance Programme

by CAMM.

Refer to Part 1.3.9.3 of this CAME for Maintenance Programme Amendments.

1.7.6 Recording of Changes (Modifications)

Incorporation of all non-mandatory changes, whether introduced through

Service Bulletins or by DCAM approved Minor/Major change, is to be recorded

in the Modification Record Book.


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1.8 MAJOR CHANGE (MODIFICATION) STANDARDS

1.8.1 Major Changes (Modifications) General

Major modifications are changes that:

a. have appreciable effect on the weight, balance, structural strength,

reliability, operational characteristics, or other characteristics

affecting the airworthiness of the product; or

b. are not done according to accepted practices or cannot be done by

elementary operations; or

c. require the particulars given in the Certificate of Airworthiness, or

associated documents, be amended, even though no physical change

to the product is involved.

All Major Modifications will be raised through suitably approved Design

Organisation (DOA) and submitted to DCAM by CAMM

1.8.2 Review of Modifications

At an early stage of the design of a modification, CAMM shall provide brief

particulars to the DCAM so that the modification may be classified and

certification basis may be defined.

The approval of the major modification will be granted by DCAM. Application

for major modifications shall only be made by a DOA via the Statement of

Compliance (SOC) form, signed by an approved signatory. A Certification

Compliance Document (CCD) shall also be presented as part of application

documents.

Under the subcontract arrangement, the MADOSS – HMSJF may use the

services of a competent design organisation outside Malaysia to assist MADOS

– HMSJF in preparing data package for modification.


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MADOSS – HMSJF shall ensure, where necessary through the medium of DOA

approved by the DCAM for the purpose, that the proposed modification is such

that the design of the aircraft, when modified, complies with the following:

a. The requirements in force at the time the aircraft type was originally

certified. Regulatory and design requirement that have been

amended since the issue of the initial Type Certificate will also be

considered.

b. Such other requirements as the DCAM may notify, in writing, in

respect of the aircraft design.

All amendments to documents, such as Maintenance Data, Weight and

Balance Report/Schedule and Flight Manual Supplement, affected by the

modification shall be submitted to DCAM.

CAMM will look into the requirement for any amendment of such documents.

He will also be responsible to notify the Chief Pilot with regards to any

Supplemental Flight Manual and amendment to Minimum Equipment List.

1.8.3 Instructions for Continuing Airworthiness

Any applicable Instructions for Continuing Airworthiness (ICA) derived from

the modifications will be inserted into the Approved Maintenance Programme

by CAMM.

Refer to Part 1.3.9.3 of this CAME for Maintenance Programme Amendments.

1.8.4 Recording of Changes (Modifications)

Incorporation of all major changes, will need to be recorded and held in the

Modification Record Book.


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1.9 DEFECT REPORTS

All defects occurring on MADOSS – HMSJF aircrafts will be subjected to review and

analysis for their effect upon airworthiness and the safe operation of the aircraft.

1.9.1 Analysis

Journey Log Sector Record pages are examined at regular intervals by CAMM

to provide information concerning defects occurring, pilot’s reports,

maintenance actions and defects of a repetitive nature. Maintenance input

records (work-packs) will also be reviewed for significant findings by the

CAMM and the contracted Maintenance Organisation which may have

airworthiness or operational implications.

The CAMM will assess the findings as necessary and any action required agreed

before implementation. Implementation may take the form of a Maintenance

Programme amendment or modification action.

Refer to Para. 1.6 of this CAME for Analysis of the Effectiveness of the


1.9.2 Liaison with Manufacturers and Regulatory Authorities

MADOSS – HMSJF is responsible to liaise with DCAM and manufacturer(s) on

all matters concerning the airworthiness of MADOSS – HMSJF aircraft. The

CAMM is to be advised when such action is necessary by the Maintenance

Organisation and will take action required to ensure the continued

airworthiness of the aircraft.


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1.9.3 Deferred Defect Policy

MADOSS – HMSJF will seek to ensure that the minimum number of open

Deferred Defects exist. All open Deferred Defects will be monitored by the

CAMM in consultation with the approved Maintenance Organisation to ensure

earliest rectification and subsequent closure.

All defects that are subjected to deferral action will be as per the approved

Minimum Equipment List (MEL) and its guidelines for use. Defects such as

cracks and structural defects that are not addressed in the MEL, AMM or SRM

may only be deferred after agreement with the Type Certificate holder and

that the defect is not of a safety concern.

When a Deferred Defect is raised, the CAMM will consult with the approved

Maintenance Organisation with a view to arranging the earliest possible

rectification action to be taken. This will involve the pre-allocation of down

time, spares, personnel, tooling etc. as appropriate. A Maintenance Release

will be issued in the Journey Log upon clearance of any Deferred Defects.

Penalties or Limitations if any shall be highlighted to the flight or ground crew

by appropriate means such as using “Notice to Crew” (NTC) or appropriate

placards as provided within Appendix 1 of Appendices, Item 6. Refer to

Flowchart 1 of this part for Defer Defect Procedure.


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1.9.4 Non-Deferrable Defects Away from Base

Where defects occur that are not listed in the MEL then the following actions

must be taken:

a) The CAMM shall consult the Approved Maintenance Organisation to

establish the extent of the defect and the rectification action

required.

b) Action will be taken to position a member of the contracted

Approved Maintenance Organisation’s certifying staff, together with

the necessary spares, tooling and technical publications to rectify and

provide a Maintenance Release in the Journey Log for the defect.

c) When an arrangement cannot be made between MADOSS – HMSJF

and the contracted Approved Maintenance Organisation, the QAM of

MADOSS – HMSJF will then ascertain if there is a suitably Approved

Maintenance Organisation, with the appropriate ratings on their

Certificate of Approval in proximity of the AOG aircraft. Suitable

contractual action will be taken to have the defect rectified, and duly

certified by the organisation.

NOTE: Where the rectification action exceeds the stipulated limits in the

Maintenance Contract then the agreement of the QAM must be

sought before any action is taken.

1.9.5 Repetitive Defects

Repetitive Defects are those defects reoccurring e.g. on three occasions

between 50 hour of Scheduled Maintenance Inspections. The Journey Log is

monitored by the CAMM to identify these defects as and when they arise.

Remedial action will be taken by the approved Maintenance Organisation in

consultation with the CAMM through a Liaison Meetings as mentioned in Para

1.6.1.


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1.9.6 Mandatory Occurrence Reporting

All incidents and occurrences that fall within the reporting criteria defined in

Regulation 165 of Malaysia Civil Aviation Regulation 2016 and DCAM AN 11

will be reported to the DCAM as soon as practicable, but within 48 hours as

required. A copy of that report shall also be sent to the organisation

responsible for the Type Design of the aircraft, engine or equipment.

All occurrences, which have maintenance implications, will be analysed by the

CAMM in consultation with the approved Maintenance Organisation.

Any MORs raised by the contracted Part-145 Approved Maintenance

Organisation on MADOS – HMSJF aircraft will also be advised to the CAMM.

Both organisations will hold copies of any MORs that have been raised that

affect maintenance.

Refer to Appendix 1 of Appendices, Item 9 of this CAME for sample of

documents.

1.9.7 Liaison Meetings

Liaison Meetings, in addition to those identified in Para. 1.6.1 will be held

between CAMM, the approved Maintenance Organisation, the QAM and any

other interested parties to discuss airworthiness, quality and MOR issues. The

frequency of these meetings will not be less than every six (6) months or more

frequently if operational circumstances and maintenance findings warrant it.

This meeting may be arranged to occur at the same time as the Maintenance

Programme / Management meeting identified in Para. 1.6.1. All of the formal

meetings will be recorded and minuted. All actions required in response to

maintenance findings, follow up actions, audit corrective actions etc. will be

duly allocated with respect to responsibility. Minutes of these meetings will be

held by the CAMM and the approved Maintenance Manager or equivalent. The

minutes will be available on request to any authorised member of the DCAM.


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1.10 ENGINEERING ACTIVITY

1.10.1 General

MADOSS – HMSJF Engineering Activity is limited to Design Control and shall be

contracted to any approved Design Organisation Approval (DOA). Design

activities shall be in accordance with approved DOA Design Organization

Exposition. Design changes shall be appropriately approved by the relevant

National Aviation Authority (NAA). Design changes which constitute a

modification or amendments shall be reviewed by a DOA for implementation.

Any changes to the structure or systems and power plant of the aircraft or its

equipment shall be controlled, documented and fall under the limitation

granted by the DOA.

Approved modification to any aircraft and its equipment shall be completed

for particular, equipment or part number/serial number of component within

a stipulated time frame. Changes and modification which affect the

airworthiness of aircraft and its equipment shall be performed within the time

allocated by the manufacturer or appropriate NAA.

Validation to the product shall be performed by relevant airworthiness

authority as appropriate. LAE to ensure that the work instructions issued by

DOA is signed and stamped before accepting it.

1.10.2 Application Process

The development and submission of changes (modification and repairs) for

approval is contracted to suitably DOA under the control of CAMM.

Application for the approval of such changes will be made on the appropriate

DCAM application form. Each application will be submitted to DCAM

accompanied by a data pack, which provides technical justification for

approval of the change as per DCAM AN 78.


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1.11 RELIABILITY PROGRAMME

A reliability programme provides an appropriate means of monitoring the

effectiveness of the maintenance programme and is only required for large aircraft

whose AMP is based upon MSG logic or includes condition monitored components or

does not contain overhaul time periods for all significant system components.

Whereas the complexity of the reliability programme should be tailored to the amount

of the aircraft managed.

The occurrence of significant problems should be recorded and diagnosed from

following sources:

• Safety information promulgated by the applicable OEM

• Pilots Reports

• Journey Logs

• Maintenance Worksheets

• Workshop Reports

• Reports on Functional Checks

• Reports on Special Inspections

• Stores Issues/Reports

• Air Safety Reports

• Reports on Technical Delays and Incidents

The reliability data form an important basis for the escalation or deletion of a

maintenance task, as well as the de-escalation or addition of a maintenance task.


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1.12 PRE-FLIGHT INSPECTIONS AND PILOT AUTHORISATION

The preparation of the aircraft for flight is the responsibility of MADOSS – HMSJF’s

Pilot. Pre-flight inspections shall be carried out before every flight to ensure the

aircraft is fit for the intended flight. The pilot-in-command shall be responsible for the

satisfactory accomplishment of the pre-flight inspection.

Prior to the first flight of the day at main base, the Daily Inspection will be carried out

and the Maintenance Release is issued by the Type rated LAE of the contracted

Maintenance Organisation or by DCAM Authorised Person.

When the aircraft is being operating away from main base, the Daily Inspection can be

certified by an Authorised Pilot only when a travelling engineer is not on board. If,

however the aircraft has a planned or unplanned night stop at stations, an LAE will be

required to carry out the Daily Inspection.

1.12.1 The Pre-flight Inspection

The pre-flight inspection is carried out by a Pilot, who will be flying the aircraft.

The inspection shall typically include but are not necessarily limited to:

a. A walk-around type inspection of the aircraft and its emergency

equipment for condition including, in particular, any obvious signs of wear,

damage or leakage. In addition, the presence of all required equipment

including emergency equipment shall be established.

b. An inspection of the aircraft Journey Log to ensure that the intended flight

is not adversely affected by any outstanding deferred defects and that no

required maintenance action shown in the maintenance statement is

overdue or will become due during the flight.

c. A verification of the Certificate of Airworthiness validity.

d. A control that consumable fluids, gases etc. uplifted prior to flight are of

the correct specification, free from contamination, and correctly recorded

as required.

e. A control that all doors are securely fastened.

f. A control that control surface and landing gear locks, pitot/static covers,

restraint devices and engine/aperture blanks have been removed.

g. A control that all the aircraft’s external surfaces and engines are free from

ice, snow, sand, dust etc.


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Details of the pre-flight inspection may be referred to the respective aircraft’s

Flight Manual (AFM).

This pre-flight inspection carried out by a Pilot does not require Maintenance

Release or any engineering involvement. The pilot-in-command doing the pre-

flight inspection shall certify acceptance in the aircraft Journey Log.

MADOSS – HMSJF shall demonstrate to the DCAM that the pre-flight

inspection personnel have received appropriate training for the relevant pre-

flight inspection task. The training need analysis shall be the responsibility of

the QAM with consultation of the Chief Pilot. Training records shall be kept

under the monitoring of QAM.

1.12.2 Pilot Authorisation for Daily Inspection

Pilot’s certifying the Daily Inspection will be selected by MADOSS – HMSJF

QAM based on the followings requirements:

a. Nominated pilot shall possess a valid ATPL

b. Total flying hours more than 1,500 hours, based on flight log (no

specific aircraft type)

c. Nominated pilot is type rated on the aircraft

The selected pilot will then be subjected to the provision of suitable initial and

continuation training ‘on the job’ with the MADOSS – HMSJF’s aircraft.

The training may be provided by the Part-145 Maintenance Organisation. The

QAM of MADOSS – HMSJF will conduct a training needs analysis together with

the AMO’s QAM. Upon satisfactory completion of training, the AMO QAM will

issue a report and submit to MADOSS – HMSJF QAM. An authorised letter

together with their limitations will be issued by the QAM to selected Pilots.

The authorisations of any Pilot of MADOSS – HMSJF remain the prerogative of

the QAM and may be withdrawn or suspended at any time. The authorisation

is valid for a period of six (6) months and will require the Pilots to quote their

individual Authorisation Number when certifying the Daily Inspection.


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1.12.3 Subcontracted Ground Handling Functions

MADOSS – HMSJF is currently engaging Universal Weather and Aviation, Inc.

for its ground handling operations away from base. There is no contracted

ground handling functions for operation at base.

1.12.4 Security of Cargo and Baggage Loading

The security of cargo and baggage loading is the responsibility of the Pilot.

Cargo and baggage will only be carried on board the aircraft in those areas

specifically designed to do so and in accordance with the limitations quoted in

the Approved Flight Manual and Weight and Centre of Gravity Schedule.

1.12.5 Control of Aircraft Refuelling Quantity / Quality

The responsibility for aircraft refuelling lies with the operating Pilot. This

includes responsibility for the right quantity of fuel being carried on board for

the intended flight and the specification and quality of the fuel taken on board.

1.12.6 Control of Snow, Ice, Dust and Sand Contamination to an Approved Standard

The control of snow, ice, dust and sand contamination, as applicable, before

flight is the responsibility of the Pilot. He/she will take whatever steps they

consider necessary to ensure the aircraft is free from such contamination

before flight.


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1.13 AIRCRAFT WEIGHING

Aircraft weighing may be performed by either a suitably approved Maintenance

Organisation with weighing approval, an approved DOA or any organisations approved

by DCAM to conduct weighing. The CAMM will review the reports produced by that

organisation. The CAMM in consultation with the approved Maintenance Organisation

will maintain a record of each aircraft operated.

Re-weighing will be carried out at intervals not exceeding two (2) years from the date

of manufacture and subsequently not exceeding five (5) years or at any time

determined by DCAM. Outside regular required intervals, the aircraft requires to be

weighed:

a) After a major repairs.

b) After a major modifications.

c) After a major re-painting of an aircraft.

d) When the weight or centre of gravity (C of G) cannot be determined in an

arithmetical way.

e) Whenever the basic empty weight of the aircraft has change by an estimated

more or less than 2%.

f) At any time as determined by DCA Malaysia.

Contracted Maintenance Organisation is responsible for the whole process for the

preparation of aircraft weighing and performing tasks detailed in the weighing

procedure sheets.

Appropriately qualified and approved personnel shall carry out the weighing and

approved Maintenance Organisation LAE shall certify the task card. The Maintenance

Organisation shall ensure issuance of a new Weight and Centre of Gravity Schedule

and ensure that the Dry Operating Weight (DOW) document is issued to all concerned.

When a new Weight Schedule is issued, the old Weight Schedule must be retained for

a minimum of 36 months.


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1.14 AIRWORTHINESS FLIGHT TEST PROCEDURES

Airworthiness flight testing is established as part of an aircraft’s Certificate of

Airworthiness initial issuance requirements as well as the approval of aircraft

modification after the issuance of C of A. The flight test may also arises as specified by

the aircraft manufacturer and normally included in the maintenance programme for

instance after a particularly extensive maintenance check affecting the aircraft

performance that cannot be checked on ground.

The Airworthiness Flight Tests (AFT) are accomplished to establish that the aircraft’s

performance, handling characteristics and system functionality do not differ

significantly from those similar aircraft that were type certificated.

If the C of A is invalid due to modification or maintenance action, an authorised person

must issue a Permit to Fly in accordance with DCAM AN 45 before the AFT is allowed

to take place.

1.14.1 Airworthiness Flight Test Schedule (AFTS)

MADOSS – HMSJF shall prepare the AFTS and submit together with a

completed DCAM’s Statement of Compliance (SOC) to enable DCAM to review

and approve the AFTS.

Any amendments to the approved AFTS shall be submitted together with a

completed SOC for DCAM review and approval. Upon satisfactory review of

the amended AFTS, DCAM Airworthiness Division shall approve the AFTS by

endorsing the SOC.


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1.14.2 Contents of the Airworthiness Flight Test Schedule (AFTS)

MADOSS – HMSJF AFTS shall contain the following information:

a. AFTS Reference Number and Date

b. Policies / Procedures in respect of Minimum Flight Test Crew including

Cabin Crew, Carriage of Passengers during Test Flight, Aircraft Flight

Manual limitations and Approved Pilots for Flight Test.

c. Flight Test Certificate

d. Mandatory placards/markings checking

e. Defects encountered during the test flight and their rectifications

f. Individual tests, for example, climb test, low speed handling test,

autorotation test, stall test, dive to never-exceed speed test etc.

g. Load sheet

1.14.3 Pilots Approval to Carry Out Airworthiness Flight Test

MADOSS – HMSJF shall nominate pilots who are properly qualified and

adequately experienced to carry out the AFT. The pilot’s requirements shall be

divided as follows:

For aircraft > 5,700 kg;

a. Recent experience on the particular aircraft type, amounting to at

least 50 hours in the last 12 months, and are designated as DCAM

Authorised Examiners;

b. DCAM may accept if they are professional test pilots or flying

instructors;

c. When a pilot does not meet the above requirements, MADOSS –

HMSJF will submit an official application to DCAM and subject to

DCAM’s deliberation for issuance of the approval.

For helicopter;

a. A minimum of 400 hours total flying time for single-engine

helicopters, or 800 hours total flying time for twin-engine helicopters;

AND

b. Recent experience on the particular helicopter type or, for single-

engine helicopters below 2,730 kg, similar helicopter types,

amounting to at least 20 hours in the last 12 months.


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Nominated pilots shall completed DCAM’s application form “Pilot’s Application

to Conduct Airworthiness Flight Test” and submit to DCAM Airworthiness

Division for review and approval.

Note: Pilots that were previously approved by DCAM to conduct Airworthiness

Flight Testing shall also complete and submit DCAM’s application forms for

DCAM Airworthiness Division’s review and approval.

Pilots intending to carry out the AFT shall be briefed by DCAM on the safety

precautions and flight test techniques. After the briefing, DCAM may fly

together with the pilot to complement the briefing. When the process is

satisfactory completed, DCAM shall approve the pilot concerned.

1.14.4 Insurance Cover for Airworthiness Flight Test

When the AFT involves any DCAM personnel, MADOSS – HMSJF shall ensure

that each DCAM personnel are provided with insurance coverage against all air

risks. This insurance coverage for DCAM personnel shall be at par with

MADOSS – HMSJF’s Pilot insurance coverage.

1.14.5 Post Flight Procedures and Aircraft Performance Analysis

Upon completion of the AFT, the pilot shall record in the Flight Test Certificate

(FTC), as well as, in the Journey Log any defects arising from the AFT. If a re-

flight test is required, the pilot shall ensure that all areas to be flight tested are

completed.

The pilot shall also ensure that the aircraft’s performance analysis is completed

and compared with the Aircraft Flight Manual’s performance data. If the

aircraft’s performance is found to be worse when compared with the AFM, the

pilot shall record in the FTC, as well as, in the Journey Log for corrective action.

If an AFT Engineer or Aircraft Maintenance Engineer is part of the AFT Team,

his engineer shall ensure that the flight test results including aircraft’s

performance analysis are complete and properly recorded.

The CAMM through the function of Technical Records shall ensure that a copy

of the FTC is kept in relevant files for future reference.


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1.14.6 Post Flight Reporting

MADOSS – HMSJF CAMM shall ensure that the AFT Report is completed

satisfactorily prior to submission to DCAM Airworthiness Division. Any

incomplete or unsatisfactory AFT Report submitted may be rejected and the

aircraft may be subjected to a repeat of the flight test.

MADOSS – HMSJF shall submit the following together with the AFT Report, i.e.:

a) Load sheet

b) Achieved / Actual Performance Climb Graph

c) Scheduled Performance Climb calculations including Flight Manual’s

climb graph / chart.

d) Scheduled Stall calculations including Flight Manual’s stall graph / chart.

e) Power Assurance Checks calculations including Flight Manual’s power

assurance graph / chart (for helicopters)

f) Autorotation Checks calculations including autorotation graph / chart

(for helicopters)

g) Aircraft defects encountered during AFT and their rectifications.

1.14.7 Quality Audits by DCAM

MADOSS – HMSJF shall notify DCAM Airworthiness Division in advance of AFT

plans, for example, annually, semi-annually or quarterly to enable DCAM

personnel to conduct appropriate quality audits of AFT.


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1.15 PLANNING PROCEDURES

The CAMM, through the function of Maintenance Planning, shall ensure that all

maintenance tasks of the Approved Maintenance Programme, modifications, ADs,

SBs, defects rectifications, repetitive inspections etc. are carried out by the Approved

Maintenance Organisations within the stipulated time period.

The Maintenance Planning Officer shall be given access to all airworthiness and

maintenance records to ensure the tasks required for continuing airworthiness of the

aircraft managed by MADOSS –HMSJF are being planned.

1.15.1 Planning of Aircraft Maintenance Programme Tasks, Modifications,

Airworthiness Directives, Service Bulletins etc.

The CAMM, through the function of Maintenance Planning is responsible to

plan all scheduled maintenance checks as per Approved Maintenance

Programme (AMP) and communicate with the Maintenance Contractor. A

suitable control documents, i.e. Maintenance Work Package, which among

other includes modifications to be incorporated, Airworthiness Directives,

Service Bulletins etc. shall be furnished and forwarded to the Maintenance

Contractor for work accomplishment.

A work scope planning meeting may be organised between MADOSS – HMSJF

and Maintenance Contractor so that the tasks to be performed may be

commonly agreed without affecting the continuing airworthiness of the

aircraft.

Upon completion of the planned task, the Maintenance Contractor will submit

all completed task cards to MADOSS – HMSJF for record keeping purposes.


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1.15.2 Monitoring of Maintenance between Scheduled Maintenance

The CAMM, through the function of Maintenance Planning will provide the

maintenance contractors a prior notice for any inspection and component due

with reference to the Maintenance Programme, as part of monitoring of any

inspections or components which is due in hours, calendar month or cycle.

This will form a short-term forecast of maintenance items, which will be due

during the intervening period between base maintenance inspections, i.e. an

Out of Phase, forecast. These items will be monitored by the CAMM and the

Approved Maintenance Organisation through the Journey Log Sector Record

Pages.

1.15.3 Maintenance Programme Variations

All variations to the Maintenance Programme will be agreed between the

CAMM and the Approved Maintenance Organisation. These variations will only

be requested when circumstances arise which could not reasonably have been

anticipated. The concession is applicable for any extension of check hours and

component hours. The QAM is responsible for submission of any application

of concession to DCAM.

Concession shall be based upon:

1. No exemption is permitted from Aircraft Maintenance Programme

unless prior written approval is given by DCAM. However, QAM shall do

so within limitations granted.

2. Concessions beyond the scope of authority granted to the QAM shall be

referred to the DCAM, which shall be submitted in advance, so that

DCAM approval is available before concession becomes effective. It must

also be taken into consideration the risks involved in the concession

application.

3. All concession shall be serially numbered and controlled with original

copies kept by the QAM and made available to the DCAM if required.

Validity period shall be specified for all concessions.


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4. CAMM shall update the records in all relevant documents that are

affected by the approved concession and MADOSS – HMSJF shall ensure

that the concession are terminated within the specified time.

5. Where concession is for extension of check, MADOSS – HMSJF shall

ascertain that the scheduled removal of components, inspections,

modifications and safety related items are not due during the extension

period. A concession shall not be granted for items classified as

mandatory by DCAM or other Airworthiness Authority.

6. Mandatory requirement deviation can only be approved by DCAM which

includes Airworthiness Directives (AD). Airworthiness Limitations (AL);

provided agreed originally by the Original Equipment Manufacturer

(OEM).

7. If component removal, inspection or modification is due during the

extension period, the originator shall make necessary arrangements to

carry out the removal, inspection or modification before the expiry time.

If it is not possible to carry out the work, a concession for deferment of

the work shall be applied for together with the request for the extension

of the check.

8. If a concession for extension of the check cycle is approved by DCAM, the

LAE shall insert together with the Base Maintenance Release (BMR) in

the Aircraft Certificate File (ACF) as evidence of authorisation for the

extension of the check interval. The main copy of concession shall be filed

and retained by the CAMM for as long as the aircraft is in service plus two

(2) years.

Refer to Appendix 1 of CAME Appendices, Item 8 for Concession for Aircraft or

Component Maintenance Exemption Form sample of documents.


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1.15.4 Variations in Excess of that Allowed by Programme

Any requests for variations to the Maintenance Programme outside the

limitations given in Para. 1.15.3 will be submitted by the QAM to the DCAM

following consultation, and agreement between CAMM and the Approved

Maintenance Organisation. These variations will only be sought in very

exceptional circumstances.


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1.16 AIRWORTHINESS DATA CONTROL

The requirements for proper administration and control in procurement, loan and

control of approved maintenance data and technical instructions and their availability

and amendment services to user, shall be complied with.

Maintenance work performed on aircraft and related component by any personnel

shall be carried out in accordance with up-to-date approved data. Literatures

necessary for the satisfactory functioning of an Approved Maintenance Organisations

at base and line stations must be made available and in sufficient quantity for ease of

reference.

For aircraft weight and balance data, all documentations and records are as per the

policies, procedures and processes laid out in the Weighing Procedure Manual.

The CAMM through the function of Technical Publication is responsible to:

a. Maintain an up-to-date list of all technical references.

b. Ensure that a Master List of all airworthiness data is available, perform a monthly

check for the current status of data against the Master List and action on any

discrepancies as required.

c. Ensure necessary and prompt corrective actions are taken for any outdate

airworthiness data.

An audit to confirm the status of technical data held under Technical Publication shall

be carried out by the QAM.

Control of ‘uncontrolled copies’ of manuals / part of manuals:

a. All certifying staff is to ensure that maintenance data prints (AMM prints etc.)

are destroyed immediately following task completion.

b. Any uncontrolled copy shall be clearly identified (by stamping or labelling) and

segregated from controlled copy documents.


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1.17 CONTROL OF PERSONNEL COMPETENCY

The CAMM is responsible to ensure that all personnel involve in the continuing

airworthiness activities are competent to carry out their tasks in accordance with the

regulations, requirements, safety, and best economical and practical standard.

All personnel should be able to carry out their functions efficiently with an

understanding of the requirements of continuing airworthiness, while not neglecting

the element of human performance.

1.17.1 Training Requirements

The purpose of the training policy is to provide training for MADOSS – HMSJF

staff whose work affects continuing airworthiness management of aircraft and

possess appropriate knowledge and skills to meet the standard set by the

company and the DCAM.

Training shall be carried out internally or externally through Part-147 Approved

Training Organisation and shall be in the form of classroom training, or on-job-

training (OJT), as appropriate.

The training requirement shall be as follows:

i. Company policy awareness as laid out in this CAME

ii. Safety Management System

iii. Human Factor

iv. Part-M Awareness

NOTE: In meeting the above requirements, QAM may provide waiver for

specific requirements upon being satisfied that those have been accomplished

by the staff.

Any recurrent training requirements will be monitored by QAM. For any due

courses, QAM will take actions to alert the staff and schedule for a

continuation training.


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1.17.2 Records

Records on courses attended, results, authorization and qualification

documents for each individual shall be available and up-to-date and kept by

the QAM.

Training records shall reflect the initial and continuation training. Records shall

be kept and securely stored at the management office and retained so long as

staff is in the employment of MADOSS – HMSJF. The organisation shall retain

the record for at least three years after the staff have ceased employment with

the organisation.

At least once a year, the policy relating to training requirements shall be

reviewed.


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1.18 SAMPLE OF DOCUMENTS, TAGS AND FORMS USED

The examples of documents and forms used by MADOSS – HMSJF are given as

Appendices of this CAME.


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CAME Part 2 – Quality System Page 2-1

PART 2

QUALITY SYSTEM


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2.1 CONTINUING AIRWORTHINESS QUALITY POLICY, PLAN AND AUDIT PROCEDURES

This Part Two (2) of MADOSS – HMSJF CAME defines the continuing airworthiness

quality policy, planning and procedures to meet the requirements of DCAM Part M

Subpart G. It forms part of MADOSS – HMSJF Quality System required by DCAM.

2.1.1 Continuing Airworthiness Quality Policy

The Quality System and associated Quality Assurance Programme enables

monitoring of MADOSS – HMSJF compliance with DCAM, the Continuing

Airworthiness Management Exposition and any other standards specified by

MADOSS – HMSJF or the DCAM, to ensure safe operations and airworthy

aircraft.

2.1.2 Quality Programme

The Quality Audit Programme (QAP) will be developed by the QAM in liaison

with the CAMM. The QAM will implement an audit programme which during a

twelve-month period will address the whole continuing airworthiness

management activity and all of the aspects of DCAM Part M which have a

bearing on the continuing airworthiness arrangements of MADOSS – HMSJF.

(This includes any sub-contracting activities).

The Quality Audit Programme (QAP) will also address those aspects of the

individual aircraft's continuing airworthiness, which would have been covered

by the Airworthiness Review Report (ARR) process.

Table 1 is for CAMO Quality Assurance Audit Plan and Table 2 is for

Maintenance Contractor Quality Assurance Audit Plan.


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2.1.3 Quality Audit Procedure

The primary purpose of the audit(s) will be to observe, in an objective manner,

a particular event/action/document etc. in order to verify whether established

operational and continuing airworthiness procedures and requirements are

followed during the accomplishment of that event. This with a view of ensuring

that the required standard is being achieved.

Every audit is undertaken by a quality auditor as part of the overall audit

programme and will be the subject of an audit report. The quality auditor shall

be independent of the audited function, audited area and have no direct

responsibilities for these activities. It is the responsibilities of the auditor to

ensure the Quality Audit Programme (QAP) audits for which they have been

delegated are carried out in accordance with the Quality Assurance Manager

instructions during the date or months in which the audits are due to be carried

out.

The auditor shall prepare and compile the audit package consisting of:

a) Audit guide

b) Audit check list index

c) NCR forms

The audit activities and findings shall be recorded on the audit report via:

a) Recommended Audit Report Form

b) Audit programme notes, and

c) Audit checklist.

The audit reports are distributed to the following persons:

a) The person responsible for the audited areas/department.

b) The Accountable Manager of MADOSS – HMSJF.

c) The Continuing Airworthiness Management Manager.

d) The Part-145 Maintenance Organisation.


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2.1.4 Quality Audit Remedial Action Procedure

The QAM, in liaison with the CAMM and the AM, will conduct an annual review

of the corrective actions recommendations issued as a result of audits carried

out during the preceding twelve (12) months to ensure they have been

appropriately implemented.

Where it is decided that appropriate action has not been taken by the

contracted Maintenance Organisation or the person responsible for the

audited areas (or department) or the CAMM, then the person responsible will

be reminded and a copy of the reminder sent to the AM. If the matter remains

unresolved, it will be referred to a Quality Review Meeting by QAM ultimately,

to the AM. If the fault lies within MADOSS – HSMJF, then immediate clearance

action will be undertaken with the AM.

The maintenance contractors, the CAMM, or the person responsible for the

audited areas (or department) are responsible for ensuring their staffs comply

with procedures and requirements. Each department manager in MADOSS –

HMSJF or approved maintenance organisation relevant managers are

responsible for disciplinary action in event of non-compliance.

Where non-compliance with procedures is repeatedly demonstrated or the

matters remains unresolved by a maintenance contractor, the maintenance

contractor will be subjected to a maintenance contract review by Quality

Department. Maintenance Contract may be suspended by the AM in counsel

with QAM pending investigation. The Maintenance Contract may be cancelled

and subjected to litigation. The Accountable Manager is responsible for

suspension and cancellation of the Maintenance Contract.

In all matters, the AM is ultimately responsible for ensuring problems and

discrepancies are dealt with correctly, and as such will be kept informed of

problems encountered in due course.


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2.1.4.1 Non-Conformance Findings Classification

All non-compliance findings are recorded in the Non-Compliance

Report (NCR) and shall be categorised as LEVEL 1, LEVEL 2 or LEVEL 3

as described below:

LEVEL FINDING CLOSURE PERIOD

LEVEL 1 Non-compliance to

Airworthiness or Safety

requirements.

Action will be immediate,

not more than one (1)

week from date of audit.

LEVEL 2 Non-compliance not

directly related to

Airworthiness or Safety

requirements.

Action shall be taken, not

more than one (1) month

from date of audit.

LEVEL 3 Observation

Improvements and/or

Enhancement issues.

Action will be taken as

soon as practicable, not

more than three (3)

month from date of audit.

2.1.4.2 Corrective / Preventive Action

The auditor is responsible to maintain the registry for all NCRs raised

and send reminder to respective Head of Department for their NCRs

responses.

The person responsible for the audited areas or department / the

CAMM / the contracted Maintenance Organisations shall be

responsible for any findings/concerns to take corrective action,

implement preventive action and respond to all NCRs.

For all NCR response, a follow up audit or through Surveillance

Program (SP) shall be conducted to access implementation and

effectiveness of the corrective action taken. All close NCR shall be

compiled and recorded by auditor.


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Flowchart 1 Quality Audit Programme

PERFORM AUDIT

RAISE AUDIT REPORT & NCR FOR ANY NON-

COMPLIANCE FINDINGS

NCR REGISTER, COMPILE & RESPONSE

MONITOR & UPDATE

STATUS

ACCEPTANCE

END

FOLLOW UP

AUDIT

YES

NO

START

PREPARE, COMPILE & SUBMIT

QAP AUDIT PACKAGE TO QAM.

COMPILE & ISSUE AUDIT PACKAGE TOGETHER

WITH PREVIOUS AUDIT PLAN NCR & SP’S NCR

YES

NO


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2.2 MONITORING OF THE OPERATORS CONTINUING AIRWORTHINESS MANAGEMENT

ACTIVITIES.

The Audit Plan includes an assessment of the Continuing Airworthiness Management

activities against the procedures defined in the CAME and in particular the ability of

the Continuing Airworthiness Management personnel ability to discharge their

responsibilities effectively with respect to DCAM Part M.

Refer to Table 1 for CAMO Quality Assurance Audit Plan.


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Table 1 CAMO Quality Assurance Audit Plan

NO SUBJECT JAN FEB MAR APR MAY JUN JUL AUG SEP OCT NOV DEC

1 Extent of approval

2Continuing airworthiness

management exposition

3 Facilities

4 Personnel requirement

5Continuing airworthiness

management

6 Responsibilities

7 Occurrence report

8 Aircraft maintenance program

9 Airworthiness directives

10Data for modifications and

repairs

11Aircraft continuing

airworthiness record system

12Operator's technical log

system

13Transfer of aircraft continuing

airworthiness records

14 Documentations

15 Quality system

16 Records keeping

17

Changes to the approved

continuing airworthiness

organisation

18Components, equipment and

tools


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2.3 MONITORING OF THE EFFECTIVENESS OF THE MAINTENANCE PROGRAMME.

The Audit Plan as carried out by QAM includes a review of the effectiveness of the

Maintenance Programme. This review will critically analyse the findings and actions

taken as a result of Para 1.6 of this CAME.


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2.4 MONITORING THAT ALL MAINTENANCE IS CARRIED OUT BY AN APPROPIATELY

APPROVED PART-145 ORGANISATION.

The Annual Audit Plan includes verification that the contracted Maintenance

Organisation’s approval granted by the DCAM is relevant to the maintenance being

performed on the aircraft operated by MADOSS – HMSJF.

Any feedback information requiring amendments to the maintenance contracts for

aircraft, engines or components should be reviewed and the contracts amended

accordingly.

Refer to Table 2 for Maintenance Contractor Quality Assurance Audit Plan.


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Table 2 Maintenance Contractor Quality Assurance Audit Plan

NO SUBJECT JAN FEB MAR APR MAY JUN JUL AUG SEP OCT NOV DEC

1 Extent of approval

2Maintenance

organization manual

3 Facilities

4personnel

requirement

5 Certifying staff

6Component,

equipment and

7 Maintenance data.

8Maintenance work

orders

9Maintenance

standards

10Aircraft certificate of

release to service

11 Maintenance records

12Privileges of the

organisation

13Organisational

review


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2.5 MONITORING THAT ALL CONTRACTED MAINTENANCE IS CARRIED OUT IN

ACCORDANCE WITH THE CONTRACT, INCLUDING SUBCONTRACTORS USED BY THE

MAINTENANCE CONTRACTOR.

The Audit Programme will include a review of all maintenance provided to MADOSS –

HMSJF by the contracted Maintenance Organisation, including subcontractors. This

review will assess all maintenance is carried out in accordance with the Maintenance

Contract.


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2.6 QUALITY AUDIT PERSONNEL.

The quality management is exclusively subordinate to the AM. The Quality Audit

Personnel works independently, should not be one of the nominated post holders and

must not be directly involved in the activity he/she has been asked to audit.

The QAM is responsible for ensuring that the Quality Assurance Program is properly

established, implemented and maintained.

The QAM must;

a) have direct access to the Accountable Manager

b) be one of the nominated post holders; and

c) have access to all parts of MADOSS – HMSJF CAMO

The QAM has the full authority and support from MADOSS – HMSJF CAMO to perform

her/his duty within the system. The QAM may delegate audits to additional auditors

and/or an audit team if he/she deems it necessary. He also establishes the audit and

inspection schedule to be completed during a specific calendar period according the

present situation.

2.6.1 Quality Audit Personnel Requirement

All quality auditors shall be suitably qualified, trained and experienced to meet

the requirements of the audit tasks. Where the quality audit personnel are

contracted on a part time basis, the auditor must not be directly involved in

the activity they have been asked to audit.

Quality auditor is responsible for carrying out audits for monitoring compliance

with the airworthiness requirements and approved company procedures. They

shall be completely independent of the areas they are auditing.


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2.6.2 Quality Audit Personnel Training Requirement

Quality auditor shall be trained to gain experience in entire audit process by

participating in an actual audit exercise including performing at least one audit

unsupervised. The training shall include documentation review, actual audit

activities, audit reporting and shall be approved by QAM.

The quality auditor shall be trained in a manner to fulfil the required

knowledge as required to perform quality system tasks. The quality auditor

must be trained as a minimum:

a) Part-M

b) Quality management

c) Audit technique

d) Technical expertise on the subject audited

A list of training/competencies and personnel records of each quality auditor

is kept by the QAM. All training certificates of such quality auditors shall be

verified correct and stamped accordingly by QAM.

2.6.3 Quality Audit Personnel Records

Staff qualifications are recorded in each individual training file by the QAM.

This file recorded staff qualification and the relevant aviation training received

by staff. This record will be updated annually.

Training file consists of summary of training form and other relevant training

certificate, notification or memo. The responsibility of updating individual

training file is on the individual staff.

Continuous training needs and summary is available in file and viewing is

restricted only to MADOSS – HMSJF management. Prior expiring, staff shall be

scheduled for the recurrent training. The training attendance summary and

certificates will be issued by the QAM for staff who resigned from MADOSS –

HMSJF.


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CAME Part 3 – Contracted Maintenance Page 3-1

PART 3

CONTRACTED MAINTENANCE


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3.1 CONTRACTED MAINTENANCE

This Part Three (3) of the CAME describes the contracted maintenance arrangements

of MADOSS – HMSJF. It includes details of these arrangements, together with the

division of responsibility for these arrangements, between MADOSS – HMSJF and the

contracted Maintenance Organisations, together with copies of the Maintenance

Contracts in force for Base and Line Maintenance support, as appropriate.


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3.2 MAINTENANCE CONTRACT AGREEMENT

This Maintenance Support Arrangement for MADOSS – HMSJF is contracted to

Approved Maintenance Organisations under DCAM Part-145 requirements of AN

6501. The Maintenance Contract Agreement shall contains, but not limited to, the

following items:

a. General arrangements for support of the operation by MADOSS – HMSJF and for

the technical liaison between MADOSS – HMSJF and the Maintenance

Contractor.

b. Accomplishment of maintenance at the approved locations of MADOSS – HMSJF

base(s) or other locations being agreed.

c. Provisioning of appropriately authorised/licensed maintenance personnel

sufficient in numbers for the completion and certification of scheduled

maintenance, rectification of defects and the completion of duplicate inspection.

d. Training of maintenance personnel.

e. Arrangement for line maintenance and ground handling, including unscheduled

maintenance arising from operations such as engine change and defect

rectification requiring major dismantling or jacking.

f. Maintaining logbooks, component service history, maintenance and other

technical records and the transmission of Sector Record Page information from

Maintenance Contractor to MADOSS – HMSJF.

g. Provision of spares, their storage and acceptance.

h. Ensuring the availability of the necessary tools and equipment to complete the

scheduled maintenance and any other work arising under the terms of the

agreement.

i. Provision of suitable maintenance accommodation at all locations where the

maintenance shall take place, appropriate to the task.

A copy of all Maintenance Contract Agreement shall be made visible to DCAM. Access

shall be given to any side letters or subcontracted arrangements for the provision of

special services such as radio, avionics, NDT etc. or for any other support including

that is provided at line stations.


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3.3 MAINTENANCE CONTRACTOR SELECTION PROCEDURE

Before any contract is signed with a maintenance organisation the CAMM will verify

that:

a. The maintenance organisation must have the relevant scope of approval by

DCAM to meet the intended contractual obligation.

b. The maintenance organisation is appropriately approved in accordance with

DCAM Part-145 requirements as stipulated in DCAM AN 6501, and has the

necessary qualified manpower, facilities, tooling, technical documentation etc.

This verification shall take into account any engine, or component maintenance

capability that may be required (though this may be available through sub-

contracting to other suitably Approved Maintenance Organisations).

c. It will be confirmed that the Approved Maintenance Organisation has adequate

capacity to undertake the proposed maintenance support. Where this includes

aspects of the continuing airworthiness management then competency or

experience will also be criteria for consideration.

d. The Approved Maintenance Organisations shall be pre-audited as per

Maintenance Contractor Quality Assurance Audit Plan by MADOSS – HMSJF

Quality Assurance Manager. If the maintenance contractors meet the DCAM

requirements, a draft of Maintenance Contract will be prepared by either

MADOSS – HMSJF or the Approved Maintenance Organisations.

e. The draft of Maintenance Contract as per requirements of DCAM AN 6101 will

be reviewed and agreed by both parties with a view to ensure that:

i. The contract is comprehensive and covers all aspects of the maintenance

scope and work package agreed.

ii. Everyone involved in the contract (Both at the MADOS – HMSJF’s Continuing

Airworthiness Management Organisation and the maintenance contractor)

agrees with the term of contract and fully understand his/her responsibility.

iii. Functional responsibilities of all parties are clearly identified.

A copy of each signed continuing airworthiness management contract shall be

submitted to the DCAM Director General.


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3.3.1 Advising the DCAM of Changes to the Maintenance Support

The DCAM Airworthiness Sector will be advised of any proposed change to the

continuing airworthiness management arrangements in writing giving the

notice required by DCAM.

Any proposal to carry out any changes to the nominated Maintenance

Contractor will be advised to DCAM Airworthiness Sector by the Accountable

Manager giving the required 28 days notice before such changes take place.

Refer to Part 0.8 of this CAME for Notification Procedure to the DCAM

Regarding Changes to the Operator’s Continuing Airworthiness Management

Arrangements / Locations / Personnel / Activities / Approval.


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3.4 DETAILED LIST OF MAINTENANCE CONTRACTORS

List of approved contracted maintenance organisations and their capabilities are

provided within Appendix 3 of CAME Appendices.


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3.5 RELEVANT TECHNICAL PROCEDURES IDENTIFIED IN THE MAINTENANCE

CONTRACT(S)

The relevant maintenance procedures are included in the Maintenance Contracts

copies of which, less the financial, details are provided in the MADOSS – HMSJF

Contract File. MADOSS – HMSJF Technical Procedures are identified in Part One and

Part Two of this CAME.

The performance of maintenance on MADOSS – HMSJF aircraft by the Approved

Maintenance Organisations shall be of methods, techniques, standards and

instructions specified by the approved maintenance data only.


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3.6 QUALITY AUDIT OF AIRCRAFT

Quality audit of aircraft shall be periodically performed against the established

standards or requirements in accordance with a planned audit programme or as

directed by the management. The audits are performed by MADOSS – HMSJF QAM,

on sampling basis or inspections as means to ensure products conform to

requirements and person responsible for executing the work comply with the required

procedures.

The quality audits of aircraft shall consist of:

1. Planned audits, carried out on a programmed basis according to an approved

Audit Plan, and;

2. General surveillance, which is carried out on ad hoc basis.

Planned audit shall be conducted as per audit programme approved by QAM, the

frequency may be adjusted based on the result of audit/surveillance of base and line

maintenance activities constitute product audit. Surveillance of these activities shall

be performed either during day or night as deemed fit by the auditor.

It is recommended to carry out a quality audit of aircraft whilst the aircraft is in the

hangar undergoing a base maintenance check and should cover at a minimum of the

following areas:

a) Monitoring that all continuing airworthiness management activities are being

performed in accordance with the approved procedures.

b) Monitoring that all contracted maintenance is carried out in accordance with the

contract.

c) Monitoring the continued compliance with the DCAM Part M Requirements.

On completion of an audit, and after NCRs are raised and issued to relevant auditee

for action, the auditor shall issue a summary of his findings, picked-up during the audit

to the auditee. A Surveillance Report shall be raised after any general surveillance

findings.


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The auditee shall be responsible to take corrective action and implement preventive

action for Non-Compliance findings. Feedback on the corrective and preventive

actions must be provided to the MADOSS – HMSJF QAM in a timely manner. NCR

raised shall be evaluated by QAM for closure. Refer to Part 2.1.3 of this CAME for

Quality Audit Procedure.


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CAME Part 4 – Airworthiness Review Procedures Page 4-1

PART 4

AIRWORTHINESS REVIEW

PROCEDURES


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4.1 AIRWORTHINESS REVIEW PROCEDURES

This Part Four (4) of MADOSS – HMSJF CAME describes the working procedures for

the airworthiness review according to DCAM AN 6102, Part M, Subpart G and AN 6101

Subpart I. The purpose of the airworthiness review is the verification of the continuing

airworthiness of an aircraft.

The approval for this privilege is granted by DCAM. To ensure validity of the aircraft

Certificate of Airworthiness, an airworthiness review of an aircraft and its continuing

airworthiness records have to be carried out within the period allowed prior to the

certificate expiry, i.e. 90 days.

The airworthiness review will include a full documented review of the aircraft records

and a physical survey of the aircraft.

MADOSS – HMSJF shall no sub-contracted the Airworthiness Review task.

NOTE: ARS has a direct access to the AM with regards to airworthiness review

matters.


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4.2 AIRWORTHINESS REVIEW STAFF

4.2.1 Qualification Requirement

To carry out airworthiness reviews, and if applicable to issue permit to fly,

MADOSS –HMSJF shall have appropriate airworthiness review staff to carry out

airworthiness review and to issue Airworthiness Review Report (ARR) and if

applicable, to issue permit to fly.

These staff shall have acquired:

i. at least 5 years' experience in continuing airworthiness;

ii. an appropriate license in compliance with Notice 1101 or relevant

engineering degree acceptable to the Director General;

iii. formal aeronautical maintenance training;

iv. a position within the approved organisation with appropriate

responsibilities, and

v. notwithstanding paragraphs 4.2.1(i) to 4.2.1(iv) of this CAME, the

requirement laid down in paragraph 4.2.1(ii) may be replaced by 5 years

of experience in continuing airworthiness additional to those already

required by paragraph 4.2.1(i).

4.2.2 Airworthiness Review Staff Assessment

MADOSS – HMSJF shall ensure that the ARS are acceptable to the DCAM. They

should have conducted a full airworthiness review under supervision prior to

their nomination. If this is part of an initial organisation approval application,

the nominated signatory will need to demonstrate their competency to the

DCAM in the first instance. Subsequent nominees could then be supervised by

the now approved signatory.

When submitting a new nominated airworthiness review staff to the DCAM,

an evidence must be provided, i.e. recommendation letter together with the

application form to show proof that the new nominated ARS has been

conducting its functions under-supervision. Once the new ARS has been

accepted by the DCAM, the inclusion of their name in the CAME constitutes

the formal authorization by MADOSS – HMSJF.


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ISSUE REVISION DATE

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For the airworthiness review staff to carry out the physical survey of the

aircraft, a suitably type rated DCAM Part 66 LAE should be utilised to assist

with this part of the review.

The QAM shall ensure that ARS can demonstrate appropriate recent

continuing airworthiness management experience acceptable to the DCAM.

ARS shall be identified by listing each person in the CAME together with their

airworthiness review authorisation reference.

Refer Appendix 2 of CAME Appendices for List of ARR signatory.

4.2.3 Issuance, Restriction and Withdrawal of Company Authorisation

The nominated ARS that is acceptable to conduct the airworthiness review by

DCAM, will be issued with company authorisation letter by QAM. This letter

will states the individual scope of work, i.e. aircraft type, their dedicated

authorisation number and validity of their authorisation.

The QAM in consultation with the AM is responsible for the issuance,

restriction and withdrawal of the authorisation. Upon being selected, the QAM

will conduct an assessment before the candidate is proposed to DCAM. The

assessment will cover the ARS working knowledge, but not limited to:

i. Physical survey of the aircraft

ii. General audit technique

iii. Applicable DCAM regulations

iv. Company procedures

v. Issuance of ARR

A restriction takes place in cases of when the verification of practice for certain

authorisations is insufficient. In addition, a restriction also applies to cases of

traceable frequently mistakes within the scope of the permit. In case of gross

negligence, fatal professional or disciplinary mistakes, MADOSS – HMSJF will

withdraw the permit.

A validity status list is kept in the respective files. An authorisation is valid for

two (2) years from date of issuance. When extension is necessary, a new

authorisation letter will be issued and signed by the AM, QAM and the

authorisation holder after completion of assessment.


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4.2.4 Staff Records

The QAM shall maintain a record of all airworthiness review staff, which shall

include details as listed below:

1. Personal Data

2. Basic Education

3. Experience

4. Aeronautical Degree and/or an appropriate license in compliance

with DCA AN 1101

5. Initial Training received

6. Type Training received

7. Continuation Training received

8. Experience in continuing airworthiness and within the organisation

9. Responsibilities of current role in the organisation

10. Copy of the authorisation.

11. Copy of approved signatory issued by DCAM

This record shall be retained until two (2) years after the airworthiness review

staff have left the organisation. Personal details are kept in the respective

personnel file.


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ISSUE REVISION DATE

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4.3 REVIEW OF AIRCRAFT RECORDS

To satisfy the requirement for the airworthiness review of an aircraft as per DCAM AN

6101, a full documented review of the aircraft records shall be carried out to satisfy

that:

1. Airframe, engine and propeller flying hours and associated flight cycles have

been properly recorded;

2. The flight manual is applicable to the aircraft configuration and reflects the latest

revision status;

3. All the maintenance due on the aircraft according to the approved maintenance

programme has been carried;

4. All known defects have been corrected or, when applicable, carried forward in a

controlled manner;

5. All applicable airworthiness directives have been applied and properly

registered;

6. All modifications and repairs applied to the aircraft have been registered and are

approved in accordance with the DCAM specified requirements;

7. All service life limited components installed on the aircraft are properly

identified, registered and have not exceeded their approved service life limit;

8. All maintenance has been released in accordance with DCAM AN 6102;

9. The current mass and balance statement reflects the configuration of the aircraft

and is valid;

10. The aircraft complies with the latest revision of its type design, and

11. If required, the aircraft holds a noise certificate corresponding to the current

configuration of the aircraft.


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ISSUE REVISION DATE

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The following documents shall be part of the aircraft records to be reviewed:

a. Certificate of Registration (C of R)

b. Aircraft continuing airworthiness record system

c. Aircraft journey log system

d. List of deferred defects, MEL and CDL if applicable

e. Aircraft flight manual (AFM)

f. Aircraft maintenance programme

g. Relevant work package inclusive of any applicable component certificate

h. AD and SB status

i. List of airworthiness limitation item

j. Mass and balance report and equipment list

k. Aircraft, engine TCDS

Result of review shall be documented inside the MADOSS – HMSJF Airworthiness

Review Report (ARR).


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ISSUE REVISION DATE

MADOSS – HMSJF 01 00 01/04/2017


4.4 PHYSICAL SURVEY

The ARS of MADOSS – HMSJF shall carry out a physical survey of the aircraft. For this

survey, ARS not appropriately qualified to the aircraft type being surveyed shall be

assisted by such qualified personnel, i.e. LAE with Type Rating on the aircraft being

surveyed.

Through the physical survey of the aircraft, the ARS shall ensure that:

1. all required markings and placards are properly installed;

2. the aircraft complies with its approved flight manual;

3. the aircraft configuration complies with the approved documentation;

4. all defect has been addressed accordingly as per DCAM AN 6101;

5. no inconsistencies can be found between the aircraft and the documented review

of records specified in paragraph 4.3 of this CAME.

The airworthiness review must be performed to a maximum period of 90 days prior

to expiry of the Certificate of Airworthiness, without loss of continuity of the

airworthiness review pattern, to allow the physical review to take place during a

maintenance check.


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ISSUE REVISION DATE

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4.5 RECOMMENDATION TO DCAM

An ARR can only be issued by ARS appropriately authorised in accordance with Para.

4.2 of this CAME, when he/she is satisfied that the airworthiness review has been

properly carried out and there is no non-compliance which is known to endanger flight

safety.

Should the outcome of the airworthiness review be inconclusive the airworthiness

review report shall not be issued until all findings have been closed.

A copy of any ARR issued for an aircraft shall be sent to the DCAM by the QAM

together with the application and official letter stating MADOSS – HMSJF commitment

for the issuance or renewal of the Certificate of Airworthiness.


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MADOSS - HMSJF 01 00 01/04/2017

CAME Part 4A – Permit to Fly Page 4A-1

PART 4A

PERMIT TO FLY


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– RESERVED –


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CAME Part 5 – Appendices Page 5-1

PART 5

APPENDICES


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APPENDIX 1 – SAMPLE DOCUMENTS

ITEM DESCRIPTION

1 Aircraft Journey Log Format

2 Deferred Defect Log Format

3 Airworthiness Review Report Checklist Form

4 Aircraft Physical Survey Form

5 Airworthiness Review Report Format

6 Notice to Crew Form

7 MEL Deferred Defect Extension Request Form

8 Concession Request Form

9 Occurrence Report Form


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Item 1 – Aircraft Journey Log Format


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Item 2 – Aircraft Deferred Defect Log Format


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Item 3 – Airworthiness Review Report Checklist Form


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Item 4 – Aircraft Physical Survey Form


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Item 5 – Airworthiness Review Report Format


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Item 6 – Notice to Crew Form


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Item 7 – MEL Deferred Defect Extension Request Form


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Item 8 – Concession Request Form


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Item 9 – Occurrence Report Form


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APPENDIX 2 – LIST OF ARR SIGNATORY

NO. NAME APPROVAL NO.

1 Onn Ab Mutalip - TBA -

2 Mohd Amirul Ismail - TBA -


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APPENDIX 3 – LIST OF APPROVED CONTRACTED MAINTENANCE ORGANISATIONS

NO. MAINTENANCE CONTRACTOR DCAM PART-

145 APPROVAL

NO.

CONTRACT REFERENCE NO.

1

Asia Aero Technic Sdn. Bhd.

M14, Skypark Terminal,

Sultan Abdul Aziz Shah Airport,

47200 Subang,

Selangor Darul Ehsan

AO/0265/15

Engineering Services

Agreement Contract No.:

OO4/10-

02/2016C&W/MADOS

2

Jet Aviation (Asia Pacific) Pte.

Ltd.

1071 West Camp Road,

Seletar Airport,

Singapore 797799

AO/0099/98

Agreement on Contracted

Maintenance Contract No.:

9M-ISJ/TMJ, MAA2015003

Rev 1

3

Weststar Aviation Sdn. Bhd.

Level 6, Menara Weststar,

Dataran Weststar,

Jalan Lingkaran Tengah II,

68000 Ampang,

Selangor Darul Ehsan

AO/0158/09

Agreement on Contracted

Maintenance Contract No.:

- TBA -


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APPENDIX 4 – LIST OF APPROVED MAINTENANCE PROGRAMME

NO. AIRCRAFT TYPE ENGINE TYPE DCAM MAINTENANCE

PROGRAMME REFERENCE

1

Boeing B737-800 BBJ2

CFM56-7B27E

HMSJF/737-800/ISS00

2

Gulfstream G 650

RR BR700-725A1-12

HMSJF/G650ER/ISS00

3

Gulfstream G 550

RR BR710-C411

HMSJF/G550

4

Gulfstream G IV

RR TAY 611-8

JMF (U) / GIV

5

Sikorsky S-76B

P&W PT6B-36B

HMSJF/S76B/ISS00


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APPENDIX 5 – COPY OF CONTRACTS WITH APPROVED MAINTENANCE ORGANISATIONS

CLASSIFIED – Kept by QAM and available upon request.