Post on 05-Apr-2018
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
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
HMSJF/CAME/01/2017
ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
CAME Cover Page Page i
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
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
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
HMSJF/CAME/01/2017
ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
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:
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
HMSJF/CAME/01/2017
ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
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.
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
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ISSUE REVISION DATE
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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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CAME Table of Contents Page vi
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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CAME Table of Contents Page viii
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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CAME Table of Contents Page x
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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CAME Table of Contents Page xii
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:
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
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CAME List of Effective Pages Page xv
PART PAGE REVISION
NO.
DATE PART PAGE REVISION
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
Reviewed by Continuing Airworthiness Management
Manager
Verified by Quality Assurance Manager
Approved by DCA Malaysia
Date: Date: Date:
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
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CAME List of Effective Pages Page xvi
PART PAGE REVISION
NO.
DATE PART PAGE REVISION
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
Reviewed by Continuing Airworthiness Management
Manager
Verified by Quality Assurance Manager
Approved by DCA Malaysia
Date: Date: Date:
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
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ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
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
ABBREVIATIONS DEFINITIONS
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
ABBREVIATIONS DEFINITIONS
SL Service Letter
SOC Statement of Compliance
SRP Sector Record Pages
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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
MADOS’S HOLDINGS SDN BHD – HIS MAJESTY SULTAN OF JOHOR’S FLIGHT
(MADOSS – HMSJF)
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
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
Immediate Superior: Continuing Airworthiness Management Manager
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.
10. To carry out any other task as directed by immediate superior.
0.5.6 Technical Records Executive
Immediate Superior: Continuing Airworthiness Management Manager
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.
8. To carry out any other task as directed by immediate superior.
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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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CAME Part 0 – General Organisation Page 0-22
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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- THIS PAGE IS INTENTIONALLY LEFT BLANK -
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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
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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
Maintenance Programme.
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
Maintenance Programme.
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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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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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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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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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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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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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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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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CAME Part 4A – Permit to Fly Page 4A-1
PART 4A
PERMIT TO FLY
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– RESERVED –
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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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ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
CAME Part 5 – Appendices Page 5-19
APPENDIX 2 – LIST OF ARR SIGNATORY
NO. NAME APPROVAL NO.
1 Onn Ab Mutalip - TBA -
2 Mohd Amirul Ismail - TBA -
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
HMSJF/CAME/01/2017
ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
CAME Part 5 – Appendices Page 5-20
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 -
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
HMSJF/CAME/01/2017
ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
CAME Part 5 – Appendices Page 5-21
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
CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION
HMSJF/CAME/01/2017
ISSUE REVISION DATE
MADOSS - HMSJF 01 00 01/04/2017
CAME Part 5 – Appendices Page 5-22
APPENDIX 5 – COPY OF CONTRACTS WITH APPROVED MAINTENANCE ORGANISATIONS
CLASSIFIED – Kept by QAM and available upon request.