CAME - Amnd 10 - Approved

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CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION

COVER PAGE

CONTINUING AIRWORTHINESS

MANAGEMENT EXPOSITION(CAME)

CAA Reference Number MV.CAME.001

Document Reference Number IASL/CM/MT/2

CAMO Approval Number MV.MG.001

Amendment Status Amendment 10, 17 May 2015

Manual Copy Number Original

Name of Manual Holder Maldives Civil Aviation Authority

This Manual shall not be reproduced, duplicated in whole or in parts without prior consent,

approval or permission of Island Aviation Services Limited.




LIST OF AMENDMENTS

Amendment 10 LOA-1 17 May 2015

I. LIST OF AMENDMENTS

Retain this record in the Manual. Upon receipt of amendments, insert amended pages orremove deleted pages and make an entry in the table below.

Amendment No Amendment Date Insert ion Date Inserted By

Initial Issue 10 Sep 2008 - S&Q Department

1 25 Dec 2008 - S&Q Department

2 20 Jul 2009 - S&Q Department

3 20 Aug 2010 - S&Q Department

4 1 Feb 2012 - S&Q Department

5 5 Aug 2012 - S&Q Department

6 10 Jul 2013 - S&Q Department

7 1 Feb 2014 - S&Q Department

8 30 Sep 2014 - S&Q Department

9 26 Oct 2014 - S&Q Department

10 17 May 2015 - S&Q Department




DISTRIBUTION LIST

Amendment 8 DL-1 30 Sep 2014

II. DISTRIBUTION LIST

Manual CopyNumber

Manual Holder Copy Format

Original Head of Safety and Quality Paper Copy

Original Maldives Civil Aviation Authority Paper Copy +Soft Copy

1 Manager Maintenance – DHC-8 and A320Fleet

Paper Copy

2 Manager Maintenance – DHC-6 Fleet Paper Copy

- Managing Director Soft Copy

- Staff of Engineering Department Soft Copy

- Head of Flight Operations Soft Copy

- Head of MGO Soft Copy



i#*###' NnED

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III. LIST

OF

EFFECTIVEAGES

PageNo

Amendment

No

Amendment

Date

CoverPaqe

cP-1

Amendment0 17 Mav2015

l. List

of

Amendments

LOA-1

Amendment0 17

Mav2015

ll. Distributionist DL-1

Amendment 30

Seo

2014

lll. Listof Effective aqes LEP-1 Amendment

0 17 Mav2015

lV. Tableof Contents TOC-1 o TOC-S Amendment0 17

Mav2015

Part

0

-

GeneralOrqanisation 0-1 o 0-26 Amendment0 17 Mav 2015

Part1

-

Continuous

inrorthiness

Manaqementrocedures

1-1to1-43 Amendment0 17

May2015

Part2

-

Qualitv

Svstem

2-1 o 2-18 Amendment0 17 Mav2015

Part3

-

Contracted

Maintenance 3-1 o 3-5

Amendment0 17

Mav

2015

Part

4

-

Airworthiness eview

Procedures

4-1

o

4-2 Amendment0 17 May2015

Part5 - Appendices 5-1 o 5-41 Amendment0 17 Mav2015

MALOIVES

CTVIL

VIATION

AUTHORITY

Amendment

0 LEP-I

17

May

2015




TABLE OF CONTENTS

Amendment 10 TOC-1 17 May 2015

IV. TABLE OF CONTENTS

Subject Page No

Cover Page CP-1

I List of Amendments LOA-1

II Distribution List DL-1

III List of Effective Pages LEP-1

IV Table of Contents TOC-1

Part 0 General Organisation 0-1

0.1 Corporate Commitment by the Accountable Manager 0-2

0.2 General Information 0-3

0.2.1 Description of the Organisation 0-3

0.2.1.1 Location and Contact 0-3

0.2.2 Relationship with other Organisations 0-4

0.2.3 Aircraft Managed – Fleet Composition 0-4

0.2.4 Type of Operation 0-5

0.2.5 Scope of Work 0-5

0.3 Management Personnel 0-6

0.3.1 Accountable Manager 0-60.3.2 Nominated Postholder for Continuing Airworthiness Activities 0-6

0.3.3 Designated Quality Manager 0-6

0.3.4 Continuing Airworthiness Coordination 0-7

0.3.5 Airworthiness Review Staff 0-7

0.3.6 Duties and Responsibilities 0-7

0.3.6.1 Accountable Manager 0-7

0.3.6.2 Head of Engineering 0-8

0.3.6.3 Head of Safety and Quality 0-9

0.3.6.4 Head of CAMO 0-9

0.3.6.5 Head of Technical Training 0-11

0.3.6.6 Head of Procurement and Logistics 0-12

0.3.6.7 Airworthiness Inspector 0-120.3.7 Manpower Resources and Training Policy 0-14

0.3.7.1 Manpower Resources 0-14

0.3.7.2 Training Policy 0-14

0.3.7.2.1 Induction Training 0-14

0.3.7.2.2 Continuation Training 0-15

0.3.7.3 Staff Records 0-15

0.4 Management Organisation Chart 0-16

0.4.1 General Organisation Chart 0-16

0.4.2 Continuing Airworthiness Management Organisation Chart 0-17

0.5 Notification Procedure to CAA regarding changes to Continuing Airworthiness Management Arrangements /Locations /

Personnel/Approval

0-18

0.6 CAME Amendment Procedure 0-19

0.6.1 CAME Review 0-19

0.7 Facilities 0-20

0.7.1 Location of Facilities 0-21

0.7.2 Layout of CAMO Facilities 0-23

0.7.3 Layout of Safety and Quality Office 0-25

0.8 Use of Q-Pulse Software 0-26

Part 1 Continuing Airworthiness Management Procedures 1-1

1.0 Continuing Airworthiness Management Procedures 1-2




TABLE OF CONTENTS


1.1 Aircraft Technical Log Utilisation & Minimum Equipment List Application

1-3

1.1.1 The Technical Log 1-3

1.1.1.1 The Technical Log Contents 1-3

1.1.2 MEL Application 1-10

1.1.2.1 MEL Procedure 1-10

1.1.2.2 Acceptance by the Pilot 1-111.1.2.3 Management of the MEL Rectification Intervals ( IR’s ) 1-11

1.1.2.4 MEL Rectification Interval Expiry 1-11

1.2 Approved Maintenance Programme (AMP) 1-12

1.2.0 General 1-12

1.2.0.1 Approved Maintenance Programme – Contents - Sources 1-12

1.2.0.2 Structural Inspections, Corrosion Control, Reliability & EngineHealth Monitoring

1-12

1.2.0.3 Mandatory Life Limitations 1-13

1.2.0.4 Inspection Standards 1-14

1.2.0.5 Maintenance Certification 1-14

1.2.0.6 Fuel Contamination 1-14

1.2.0.7 The Approved Maintenance Programme Owner –

Responsibilities

1-14

1.2.0.8 Holders of AMP 1-14

1.2.1 AMP Review, Development & Amendment 1-14

1.2.1.1 Development and Amendment 1-14

1.2.1.2 AMP Meetings 1-14

1.2.1.3 AMP Amendments 1-15

1.2.1.4 AMP Variations 1-15

1.2.1.5 Variations in excess of that allowed by the MaintenanceProgramme

1-16

1.3 Time and Continuing Airworthiness Records: Responsibilities,Retention and Access

1-17

1.3.1 Continuing Airworthiness Records 1-17

1.3.2 Monitoring of Scheduled Maintenance 1-181.3.3 Record Retention 1-18

1.3.4 Access to Continuing Airworthiness Records 1-20

1.3.5 Transfer of Continuing Airworthiness Records in the event of asale or other disposal of the Aircraft

1-20

1.3.6 Access to Continuing Airworthiness Records in the event of an Accident/Incident

1-20

1.4 Accomplishment and Control of Mandatory Requirements for Airworthiness

1-21

1.4.1 Airworthiness Directives 1-21

1.4.2 Airworthiness Directive Decision and Implementation 1-21

1.4.3 Airworthiness Directive Control 1-21

1.4.4 Recording of Airworthiness Directive Compliance 1-22

1.5 Analysis of the Effectiveness of the AMP 1-23

1.5.1 Liaison Meetings 1-23

1.5.2 Frequency of Meetings 1-23

1.6 Non-Mandatory Changes (Modification) Embodiment Policy 1-24

1.6.1 Changes (Modifications) General 1-24

1.6.2 Service Bulletins 1-24

1.6.3 Other Changes (Modifications) 1-24

1.6.4 Minor Changes (Modifications) 1-24

1.6.5 Recording of Changes (Modifications) 1-25




TABLE OF CONTENTS


1.7 Major Change (Modification) Standards 1-26

1.8 Defect Reports 1-27

1.8.1 Analysis 1-27

1.8.2 Liaison with Manufacturers and Regulatory Authorities 1-27

1.8.3 Deferred Defect Policy 1-27

1.8.3.1 Non-Airworthiness Defects 1-28

1.8.3.2 Acceptance by the Pilot 1-291.8.3.3 Management of the Non-Airworthiness Defect Rectification

Interval1-29

1.8.4 Non Deferrable Defects Away from Base 1-29

1.8.5 Repetitive Defects 1-29

1.8.6 Mandatory Occurrence Reporting 1-30

1.8.7 Liaison Meetings 1-30

1.9 Engineering Activity 1-31

1.10 Reliability Programs 1-32

1.11 Pre-Flight Inspections 1-33

1.11.1 The Pre-Flight Inspection 1-33

1.11.2 The Daily Check 1-33

1.11.3 Pilot Authorisation 1-33

1.11.4 Sub-Contracted Ground Handling Functions 1-33

1.11.5 Security of Cargo and Baggage Loading 1-33

1.11.6 Control of Aircraft Refueling Quantity /Quality 1-34

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

1-35

1.11.8 Certificate of Airworthiness and Airworthiness Review CertificateValidity

1-35

1.12 Aircraft Weighing 1-36

1.12.1 Weighing 1-36

1.12.2 Mass and Centre of Gravity Calculation 1-36

1.12.3 Change in Basic Mass 1-37

1.13 Check Flight Procedures 1-38

1.13.1 Certification before Check Flight 1-381.13.2 Check Flight 1-38

1.13.3 Release to Service 1-39

1.14 Sample of Documents, Tags and Forms Used 1-40

1.15 Maintenance Data 1-41

1.16 Documents to be carried onboard the Aircraft 1-42

1.17 Extended Range Twin Engine Operations (ETOPS) 1-43

Part 2 Quality System 2-1

2.1 Continuing Airworthiness Quality Policy, Plan and AuditProcedures

2-2

2.1.1 Continuing Airworthiness Quality Policy 2-2

2.1.2 Quality Assurance Programme 2-3

2.1.3 Quality Audit Procedure 2-3

2.1.3.1 Selection of Auditors 2-3

2.1.3.2 Audit Notification 2-4

2.1.3.3 Audit Process 2-4

2.1.4 Quality Audit Remedial Action Procedure 2-6

2.1.5 Audit Records 2-7

2.1.6 Management Review 2-7

2.2 Monitoring of Continuing Airworthiness Management Activities 2-8

2.3 Monitoring of the Effectiveness of the Maintenance Programme 2-9

2.4 Monitoring that all Maintenance is carried out by an 2-10




TABLE OF CONTENTS


appropriately Approved MCAR-145 Organisation

2.5 Monitoring that all Contracted Maintenance is carried out inaccordance with the Contract, including Sub-contractors usedby the Maintenance Contractor

2-11

2.6 Quality Audit Personnel 2-12

2.6.1 Competence Assessment 2-12

2.7 CAMO Personnel 2-142.7.1 Competence Assessment of CAMO Personnel 2-14

2.7.2 Issuing of Approval Stamp to CAMO Personnel 2-16

2.8 Training Personnel 2-17

2.8.1 Competence Assessment of Training Personnel 2-17

Part 3 Contracted Maintenance 3-1

3.0 Contracted Maintenance 3-2

3.1 Maintenance Contractor Selection Procedure 3-2

3.1.1 Advising the CAA of Changes to the Maintenance Support 3-3

3.2 Detailed List of Maintenance Contractors 3-4

3.3 Relevant Technical Procedures identified in the MaintenanceContract(s)

3-4

3.4 Quality Audit of Aircraft 3-4

Part 4 Airw orth iness Review Procedures 4-14.0 Introduction 4-2

Part 5 Appendices 5-1

5.1 Sample Documents 5-2

5.1.1 Technical Log Book 5-2

5.1.1.1 Cover Page 5-2

5.1.1.2 Notice to Flight and Maintenance Crew 5-3

5.1.1.3 Notice to Flight and Maintenance Crew Log Transfer Record 5-4

5.1.1.4 Deferred Items Log 5-5

5.1.1.5 Deferred Items Log Transfer Record 5-6

5.1.1.6 Non-Airworthiness Deferred Items Log 5-7

5.1.1.7 Non-Airworthiness Deferred Items Log Transfer Record 5-8

5.1.1.8 Technical Log Page 5-95.1.1.8.1 DHC-8 and DHC-6 Aircraft 5-9

5.1.1.8.2 A320 and A321 Aircraft 5-10

5.1.2 DHC-8-200/300 Pre-Flight Checklist 5-11

5.1.3 Non Destructive Test Report 5-13

5.1.4 Engineering Delay Report 5-14

5.1.5 Airworthiness Review Report (reserved)) 5-15

5.1.6 AD/SB Compliance Form 5-15

5.1.7 CAA Concession Request Form 5-16

5.1.8 In-House Concession Request Form 5-17

5.1.9 Purchase Order 5-18

5.1.10 Repair Order 5-19

5.1.11 Compass Swing Record 5-205.1.12 Pre-Weighing Check List (DHC-8 Aircraft) 5-21

5.1.13 Weighing Record (DHC-8 Aircraft) 5-23

5.1.14 Basic Weight Change Record 5-24

5.1.15 CAA Form 1 5-25

5.1.16 EASA Form 1 5-26

5.1.17 FAA Form 8130-3 5-27

5.1.18 Work Package 5-28

5.1.18.1 Work Package Sheet (Cover Page) 5-28

5.1.18.2 Task Card 5-29




TABLE OF CONTENTS


5.1.18.3 Maintenance Statement 5-30

5.1.19 Non-Routine Task Card (NRTC) 5-31

5.1.20 Removal / Installation Record Card 5-32

5.1.21 Certificate of Fitness for Flight 5-33

5.1.22 Flight Test Certificate 5-34

5.1.23 List of Airworthiness Review Staff 5-35

5.1.24 List of Approved Contractors 5-365.1.25 List of Approved Sub-Contractors 5-37

5.1.26 Contracts with Approved Maintenance Organisations 5-38

5.1.27 Manual Change Request 5-39

5.1.28 DHC-6 Pre-Flight Checklist 5-40




PART 0 – GENERAL ORGANISATION

Amendment 10 Page 0-1 17 May 2015

PART 0

GENERAL ORGANISATION



ISI A]YD

O

CONTINUING

AIRWORTHINESS MANAGEMENT

EXPOSITION

PART O GENERAL

ORGANISATION

0.1

CorporateCommitmdnt

y the AccountableManager

This Exposition

efines he organisation

nd

procedures

ponwhichMCAR-

M

Subpart

G approval f IASLunderMCAR-M

s based.

Thesbprocedures re approved y the undersignednd must be compliedwith as

applicable n order

o ensure hat all the

Continuing irworthiness

ctivitiesncluding

maintenanceor aircraftmanaged

by IASL is

carriedout on

time to an approved

standard.

It is

acceptedhat hese

procedures

o notoverride

he

necessity

f complying

ithany

new or amended egulation

ublished

y CAA

from

ime o time where

hesenew

or

amendedegulations

re n conflict ith

hese

procedures.

It is

understoodhat CAAwill

approve his organisationhilst

CAA s

satisfiedhat he

procedures

re being ollowed. t is further

understood

hat CAA reserves

he

right

o

suspend ary

or

revoke

he MCAR-M

ubpartG Continuing inruorthiness

anagement

approval

f the organisationf

CAA

has

evidencehat

procedures

re not ollowed

nd

the standards otupheld.

It is further

understood

hat

or

commercial

ir transport perations

he suspension

r

revocation

f the

approvalof the MCAR-M

Subpart G

continuingainruorthiness

managemelt

pprovalwouldnvalidate

he AOC.

/

[

l-

Abdul

l{ris I

ManagillgirilctorAccountableanager

lsland

Aviation ervices imited

Date:

2October 015

Amendment

0

Page

0-2

17May 2015






0.2 General Information

0.2.1 Descrip tion of the Organisation

Island Aviation Services Ltd. is wholly owned by the Government of Maldives andadministrated by a Board of Directors.

Island Aviation Services Ltd. began inter-atoll operation on 13 April 2000 with oneDHC-8 aircraft and one Do228 aircraft to serve domestic destinations. Thepresent fleet strength is given under Para 0.2.4 and they operate to domestic andinternational destinations.

The Company’s core business activities include the following services:

a) Domestic and International Air Servicesb) Engineering and Maintenance Servicesc) Flight Operationsd) Ground Handlinge) Cargo Servicesf) Operation of CIP Loungesg) Airport Operations

Engineering Department provides Engineering and Maintenance Services toIASL aircraft and to third party aircraft operating into Ibrahim Nasir International Airport.

Sections of Engineering Department include Administration, CAMO (Continuing Airworthiness Management Organisation), Maintenance (Line Maintenance, BaseMaintenance and Workshops), Procurement and Logistics, and Stores.

Safety and Quality Department is independent of the Engineering Departmentand carries out safety and quality functions of the organisation.

0.2.1.1 Location and Contact

Dispersed in both Male’, Ibrahim Nasir International Airport and domestic airportsof the country, a number of buildings are used for various purposes by Island Aviation Services Ltd. Corporate office is located in the capital city, Male’ whilstEngineering Department, the principle focus of the Manual is situated at IbrahimNasir International Airport.

Address and contact details of the corporate office is as appended below:

Head QuartersIsland Aviation Services Limited

345 Majeedhee MaguMale’ 20345Republic of Maldives

Telephone (operator): + 960 3331260Facsimile: + 960 3314806






Address and contact particulars of the Engineering Department:

Engineering DepartmentIASL HangarIsland Aviation Services Ltd.,Ibrahim Nasir International Airport,Republic of Maldives

Telephone (operator): + 960 3331370Facsimile: + 960 3332022

Address and contact particulars of the Safety and Quality Department:

Safety and Quality DepartmentIASL HangarIsland Aviation Services Ltd.,Ibrahim Nasir International Airport,Republic of Maldives

Telephone : + 960 3331372Facsimile: + 960 3332022

0.2.2 Relationship with other Organisations

IASL CAMO and IASL AMO are located at IASL Hangar and share the samefacilities. All functions of IASL CAMO and IASL AMO, with the exception ofquality and safety functions, are performed under the administrative setup ofEngineering Department of IASL.

The following functions of IASL AMO are performed by IASL CAMO:

Provision, updating and control of applicable maintenance data

Retention of maintenance records

The following staff perform functions of IASL CAMO and IASL AMO:

Head of Engineering

Head of Safety and Quality

Head of Procurement and Logistics

Airworthiness Inspectors

Procurement and Logistics staff

0.2.3 Aircraft Managed – Fleet Composition

The continuing airworthiness of the following aircraft types (as of date ofamendment) is managed by IASL.

Ai rcraft Type Number of Ai rcraft

DHC-6-200 1

DHC-6-300 5

DHC-8-202 2

DHC-8-314 2

DHC-8-315 4

A320-214 1

A321-211 1

Total Number of Aircraft 16






0.2.4 Type of Operation

A320 and A321 Aircraft are used for transportation of domestic and internationalpassengers and cargo. The aircraft are also used for medical evacuationpurposes.

DHC-8 Aircraft are used for transportation of domestic and internationalpassengers and cargo. DHC-8 Aircraft are also used for medical evacuationpurposes.

DHC-6 Aircraft are used for transportation of domestic passengers and cargo.

Air Operator Certificate Number 007 was initially issued by CAA on 26 June2000.

0.2.5 Scope of Work

Continuing Airworthiness Management Organisation’s Capability:

Ai rc raft Type Engine Type Managed at Si te:DHC-6-200 PT6A-27 IASL Seaplane Base, Ibrahim Nasir Intl’ Airport

DHC-6-300 PT6A-27 IASL Seaplane Base, Ibrahim Nasir Intl’ Airport

DHC-8-200 PW 123 IASL Hangar, Ibrahim Nasir Intl’ Airport

DHC-8-300 PW 123 IASL Hangar, Ibrahim Nasir Intl’ Airport

A320 CFM56-5B IASL Hangar, Ibrahim Nasir Intl’ Airport

A321 CFM56-5B IASL Hangar, Ibrahim Nasir Intl’ Airport






0.3 Management Personnel

The following table provides a list of management personnel of IASL CAMO.

Appointed Person Deputy

Accountable Manager Mr. Abdul HarisManaging Director

Capt. Mohamed AmeenDirector, Flight Operations

Nominated Post Holder forContinuing Airworthiness Activities

Mr. Ali FiragHead of Engineering

Mr. Mohamed HassanManager Maintenance

Head of CAMO Mr. Ahmed Hussain Suresh PeriyannanTechnical Services Engineer

Head of Procurement andLogistics

Mr. Ahmed Naseem Mr. Mohamed AkramSupervisor, Logistics

Head of Technical Training Mr. Zain Fahmy Hassan Mr. Mohamed Guraishy AbdulRazzagSenior Engineer

Designated Quality Manager Mr. Ibrahim IyasHead of Safety and Quality

Mr. Mohamed Shafaan Airworthiness Inspector

Any permanent changes to the following management personnel require notification toCAA and their prior approval on CAA Form 4.

Accountable Manager

Head of Engineering

Head of CAMO


If any of the listed management person is or is expected to be away from normal duties,his duties shall be delegated to the appointed deputy. If the appointed deputy is also notavailable, a temporary replacement shall be appointed by Managing Director or Head ofEngineering. The overall responsibilities of a management person cannot be delegated.

Notification of delegation of duties shall be communicated to all listed managementpersonnel via e-mail or other suitable communication medium.

0.3.1 Accountable Manager

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

Mr. Abdul HarisManaging Director

0.3.2 Nominated Post Holder for Continuing Airworthiness Activities


Mr. Ali FiragHead of Engineering

0.3.3 Designated Quality Manager


Mr. Ibrahim IyasHead of Safety and Quality






0.3.4 Continuing Airwor thiness Coordination

The following job functions cover the continuing airworthiness responsibilities ofIASL CAMO.

Technical Service Engineers

Planners

Job Descriptions of the Continuing Airworthiness Management Staff are given inSOP201 (General Information, Job Descriptions). The Job Descriptions includesthe detailed job functions to show that all the continuing airworthiness functionsas described in the MCAR-M are covered.

0.3.5 AIRWORTHINESS REVIEW STAFF

Name Designation Scope of Author isation

Author isationNo

Ibrahim Iyas Head of Safetyand Quality

ARC Extension Only ARS 01

MohamedShafaan

AirworthinessInspector

ARC Extension Only ARS 02

0.3.6 Duties and Responsibil ities

0.3.6.1 Accountable Manager

The Accountable Manager is responsible for:

a) Ensuring that continuing airworthiness activities carried out by IASLCAMO meets the requirements of Part M.

b) Ensure that the necessary finance, facilities, material and tools,sufficient competent and qualified personnel are available to enablethe IASL CAMO to perform the continuing airworthiness activities tothe standard required by the CAA.

c) Ensure that any charges are paid, as prescribed by CAA in respect ofMCAR-M Subpart G approval.

d) Establishing and promoting the safety and quality policy.

e) Nominating the management staff.

f) Ensuring the competence of all personnel, including management

personnel has been assessed.

g) Supervision of the progress of the corrective actions/review of theoverall results in terms of quality.






0.3.6.2 Head of Engineering

The Head of Engineering is responsible for:

a) Ensuring that the organisation has:

i) facilities appropriate to the planned work

ii) office accommodation appropriate to the management of theplanned work

iii) a working environment appropriate to the tasks being undertaken

iv) sufficient competent personnel to plan, perform, supervise, inspectand certify the work being performed

v) tools, equipment and materials to perform the planned tasks

vi) all necessary maintenance data as required by MCAR-M Subpart

G

b) Notifying the Accountable Manager whenever deficiencies emergewhich require his attention in respect of finance and the acceptabilityof standards.

c) Ensuring Continuing Airworthiness procedures are established andpublished within the organisation, to achieve good maintenancemanagement practices and compliance with CAA requirements. Heshall ensure compliance with the established Safety and QualitySystem of the organisation to confirm that work is accomplished to thehighest standards of airworthiness and workmanship.

d) Ensuring that all maintenance is correctly certified and that records ofmaintenance carried out are retained safely and securely for thestatutory period.

e) Selection and establishment of maintenance contracts withcontractors (approved maintenance organisations) and sub-contractors in consultation with Head of Safety and Quality.

f) Ensuring that corrective actions to audit findings are taken in a timelymanner.

g) Implementation of the safety and quality policy and good human factorpractices.

Qualification: Degree in Aeronautical Engineering and/or MCAR-66Licence or equivalent, preferably with type ratings onaircraft types operated by IASL.

Experience: 15 years maintenance certifying or aviationmanagement experience, including at least 5 yearsexperience in CAMO and/or AMO.

Note: Comply with qualifications and experiencerequirements specified in MCAR-M AMC M.706(4).






0.3.6.3 Head of Safety and Quality

Head of Safety and Quality is responsible for:

a) Establishing an independent quality system to monitor compliance ofthe CAMO activities, including sub-contracted activities, MCAR-M,CAME and SOPs.

b) Follow-up and closure of quality audit findings.

c) Establish regular meetings with the Accountable Manager to appraisethe effectiveness of the quality system. This will include details of anyreported discrepancy not being adequately addressed by the relevantperson or in respect of any disagreement concerning the nature ofdiscrepancy.

d) Preparing CAME and approval of related Standard OperatingProcedures and ensuring their adequacy regarding MCAR-M and anysubsequent amendments to the regulation.

e) Submission of CAME and any associated amendments to CAA forapproval (which includes completion of and submission of CAA Form2 and CAA Form 4).

f) Investigation of safety occurrences and reporting of mandatoryoccurrences to CAA and Manufacturer.

g) Liaising with CAA on safety and quality issues.

h) Approval of maintenance contractors and sub-contractors.

Qualification: Degree in Aeronautical Engineering and/or MCAR-66

Licence or equivalent, preferably with type ratings onaircraft types operated by IASL.

Experience: 10 years experience in an aviation regulatory roleand/or aircraft maintenance environment, including atleast 5 years experience as quality auditor.

0.3.6.4 Head o f CAMO

The Head of CAMO will act to ensure that IASL’s responsibilities in thefollowing areas can be met:

a) All maintenance is carried out in accordance with the approved

maintenance programme and released by an appropriately approvedmaintenance organisation.

a) Develop and control a maintenance programme for the aircraftmanaged including any applicable reliability programme.

b) Analysis of the effectiveness of the maintenance programme.

c) Approval, by the CAA of IASL’s Technical Log, including anysubsequent amendments to the Technical Log.






d) Manage and retain all continuing airworthiness records and TechnicalLog.

e) Work planning and follow up are carried out regularly.

f) Technical follow up is carried out regularly.

g) Modifications and repairs (changes) are carried out to an approvedstandard.

h) Accomplishment of all applicable Airworthiness Directives andOperational Directives with a continuing airworthiness impact.

i) Non mandatory modification embodiment policy.

j) Rectification of all deferred defects are carried out in a timely manner.

k) Accomplishment of pre-flight inspections at specified periods/timings.

l) Certificate of Airworthiness and Airworthiness Review Certificate foreach aircraft operated by IASL remains valid in respect of;

i) the airworthiness of the aircraft,ii) the expiry date specified on the Certificate, andiii) any other condition specified in the Certificate;

m) Maintenance check flights are carried out when necessary.

n) All applicable maintenance data and other technical publications arekept up-to-date.

o) Corrective actions to audit findings are taken in a timely manner.

p) Establish Standard Operating Procedures to achieve compliance withCAME and CAA requirements, and keep SOP’s up-to-date.

q) Review requirements for spare parts, three months in advance.

r) Administration of Quantum Software.

s) Review and implement, as appropriate, any additional CAArequirements

Qualification: Aeronautical degree and/or MCAR-66 Licence orequivalent, preferably with type ratings on aircraft types

operated by IASL.

Experience: 10 years maintenance certifying experience and/orcontinuing airworthiness experience.






0.3.6.5 Head of Technical Training

Head of Technical Training is responsible for:

a) Identify required/mandatory trainings in co-ordination with Head ofCAMO, prepare course material for the trainings andconduct/coordinate in-house trainings.

b) Ensure that all IASL CAMO training activities are being performed inaccordance with, CAME, SOP’s and applicable civil aviationregulations.

c) Ensure that all contracted training is carried out in accordance with thecontract and in compliance with the regulatory requirements.

d) Ensure that records of trainings conducted/contracted are maintainedcurrent at all times.

e) Ensure that a copy of all training records is provided to Head of Safetyand Quality.

f) Develop and maintain an up-to-date training calendar to demonstratethe organisation’s plan to conduct mandatory trainings. This calendarshall be made available to Head of Engineering and Head of Safetyand Quality.

g) Monitor due dates of all mandatory trainings and ensure that recurrenttrainings are conducted before the due dates.

h) Develop in-house training capabilities in-line with the policies of theEngineering Department.

i) Notify Head of Engineering and Head of Safety and Quality of thetraining schedule, including details of the training provider, prior toconduction of trainings (including trainings conducted through externalorganisations).

j) Ensure that corrective actions to audit findings with regard to trainingactivities are taken in a timely manner.

Qualification: Aeronautical degree and/or MCAR-66 Licence orequivalent, preferably with type ratings on aircraft typesoperated by IASL

Experience: One year experience in an aircraft maintenance

environment






0.3.6.6 Head of Procurement and Logis tics

Head of Procurement and Logistics is responsible for:

a) Procurement of all spare parts, materials, tools and equipmentrequested by Stores from approved suppliers in a timely manner.

b) Sending unserviceable components to approved contractors in atimely manner.

c) Ensuring that the logistics requirement of all incoming and outgoingparts, materials, tools and equipment are met in the most efficient andtimely manner, including customs clearance.

d) Ensuring that contractors and sub-contractors fulfill their warrantyobligations.

e) Ensuring compliance with approved procedures and regulationsregarding procurement functions.

f) Ensuring that corrective actions to audit findings are taken in a timelymanner.

Qualification: Completed GCE O’ Level, preferably should hold adiploma in Aviation/Materials/Logistics/InventoryManagement.

Experience: 5 years experience in procurement or logistics oraircraft maintenance environment.

0.3.6.7 Airworthiness Inspector

Airworthiness Inspector is responsible for:

a) Carry out quality audits and inspections.

b) Monitor the implementation and effectiveness of the corrective actionstaken as a result of audit findings.

c) Monitor validity of regulatory approvals.

d) Provide assistance to Head of Safety and Quality to comply with allapplicable civil aviation regulations and improve quality standards ofthe company.

e) Process applications for deviation from approved maintenanceprogrammes.

f) Process applications for issue/renew of certification authorisations andother quality approvals.

g) Investigate safety occurrences, possible violations and unsafepractices in the area of aircraft maintenance and continuingairworthiness, and prepare reports for the purpose of preventingsimilar occurrences in the future.






h) Monitor and analyse safety data to identify trends and concerns.

i) Prepare and disseminate safety information for promoting safetyawareness.

j) Compilation of periodical data as input to management review.

k) Provide administrative support and assistance to Head of SafetyQuality.

Qualification: Degree in Aeronautical Engineering or MCAR-66Licence or completed Basic Aircraft MaintenanceTraining or equivalent.

Experience: 2 years experience in an aircraft maintenanceenvironment, including at least 1 year experience asquality auditor.






0.3.7 Manpower Resources and Training Policy

0.3.7.1 Manpower Resources

As of the date of amendment, the number of available resource (in manhours) involved in continuing airworthiness management andairworthiness review activities are shown in the following table:

Function Full Time Part Time

Head of Engineering 0 1 X 4 X 5 X 48 = 960

Head of Safety and Quality 0 1 X 4 X 5 X 48 = 960

Head of CAMO 1 X 8 X 5 X 48 = 1920 0

Head of Technical Training 0 1 X 4 X 5 X 48 = 960

Quality Monitoring 0 2 X 4 X 5 X 48 = 960

Continuing AirworthinessManagement 8 X 8 X 5 X 48 = 15360 0

Man Hour Sub Total 17280 3840

Total Man Hours (per year) 21120

Some personnel have been classified as ‘Part Time’ staff as they perform

functions of both IASL CAMO and IASL AMO.

Calculation of the Man Hours is based on the following equation:

Man Hours (per year) = No. of Staff X Working Hours X Days per WeekX Working Weeks per Year

Head of Engineering shall maintain an up-to-date man hour plan, showingthe number of man hours required for continuing airworthiness tasks andthe number of man hours available to perform continuing airworthinesstasks.

When there are changes such as addition of a new aircraft to the fleet,

which may affect the man power resource requirements, the maintenanceman-hour plan shall be reviewed by Head of Engineering and updatedaccordingly.

Head of Engineering shall distribute the current man-hour plan toManaging Director and Head of Safety and Quality.

0.3.7.2 Training Pol icy

Training will be provided by IASL CAMO to ensure that each member ofstaff is adequately trained to carry out the functions of the MCAR-MSubpart G Continuing Airworthiness Management Organisation.

0.3.7.2.1 Induction Training

All IASL CAMO staff shall undergo induction training within 3months of joining the organisation.

This training shall cover as a minimum; Applicable Regulations(refer to Chapter 5 of Safety Management Manual), CAME,Standard Operating Procedures (SOP’s), Human Factors,Safety Management System, Aircraft Familiarisation, TechnicalPublications, Q-Pulse, Fuel Tank Safety Training and QuantumSoftware.






0.3.7.2.2 Continuation Training

All IASL CAMO staff shall undergo continuation training onceevery two years.

Continuation training shall include changes to CAME, SOP’s,Regulations, Human Factors, Fuel Tank Safety Training and Aircraft Type specific information applicable to CAMO.

Continuation training may be in the form of self-studyingcourse material, read and sign, formal classroom, on-the-jobtraining or computer based training.

The Head of Technical Training shall keep original copies of trainingrecords and shall provide copies of training records to Head of Safety andQuality.

0.3.7.3 Staff Records

Head of Safety and Quality shall maintain a list (on computer) of allContinuing Airworthiness Management Staff and keep a record of theirqualifications.






0.4 Management Organisation Chart

0.4.1 General Organisation Chart






0.4.2 Continuing Airworthiness Management Organisation Chart






0.5 Notification Procedure to CAA regarding changes to Continuing AirworthinessManagement Arrangements/Locations/Personnel/Approval

The Head of Safety and Quality is responsible for notifying CAA in writing of thefollowing changes, before such changes take place:

Name of the organisation

Location(s) of the organisation

Persons specified in Para 0.3 of this CAME

Facilities, procedures, maintenance support arrangements and staff that couldaffect the approval

It is the responsibility of Head of Engineering and Head of CAMO to notify Head ofSafety and Quality of changes within their functional areas that may affect theorganisation’s approval.

The changes shall be notified to CAA as follows:

a) By letter for any changes affecting the MCAR-M Subpart G Approval

b) By CAA Form 4 for any changes to management persons at least 10 calendardays before the change takes place

c) If the change requires CAME to be amended, by submitting amended CAMEpages to CAA at least 10 calendar days before the change takes place

In the case of changes not known to the management beforehand, these changes willbe notified at the earliest opportunity.






0.6 CAME Amendment Procedure

a) Head of Safety and Quality takes overall responsibility for reviewing the CAME andfor preparing any amendments.

b) Procedures specific to continuing airworthiness activities shall be drafted by Headof CAMO in consultation with Head of Engineering and he is responsible forensuring that the procedures are adequate, up-to-date and relevant to IASLCAMO. Any changes to such procedures shall be promptly notified to Head ofSafety and Quality with the draft of the procedure.

c) All CAME procedures shall take into account human factors and humanperformance limitations to ensure good continuing airworthiness managementpractices.

d) The amended text shall be identified by a vertical line on the left margin.

e) Head of Safety and Quality shall ensure that the amended procedures areadequate, comply with MCAR-M requirements and prepare final amendments to

CAME.

f) Head of Safety and Quality shall seek the concurrence of Head of Engineeringbefore obtaining CAA approval for the amendments.

g) All amendments shall be submitted to CAA for approval prior to their incorporationin the CAME.

h) Once the amendments have been approved, Head of Safety and Quality shall sendapproved copies of the amendments to all recipients listed in the Distribution Listvia Q-Pulse Software and it is their responsibility to update their CAME Paper Copy(if applicable) and ensure CAME is kept current at all times.

i) Once the amendments have been received, manual holders shall acknowledgereceipt of amendments via Q-Pulse Software within 15 working days from the dateof distribution of the amendments via Q-Pulse Software.

j) Any staff of Engineering Department may propose amendments to CAME, bysubmitting a Change Request via Q-Pulse Software.

0.6.1 CAME Review

CAME shall be reviewed by Head of Safety and Quality at intervals notexceeding 12 months or more frequently when significant changes occur whichaffect the content of the CAME.

CAME shall be reviewed by Head of CAMO at intervals not exceeding 6months to ensure procedures described in CAME are an accuraterepresentation of how the continuing airworthiness activities are performedand the procedures comply with MCAR-M requirements. Followingcompletion of every review of CAME, Head of CAMO shall send a reviewreport to Head of Engineering and Head of Safety and Quality.






0.7 Facilities

The following facilities are provided to continuing airworthiness staff:

Office accommodation located on the first floor of IASL AMO Hangar thatmeasures about 42 ft X 22 ft. IASL AMO Hangar is located on the westernside of Ibrahim Nasir International Airport.

12 working stations equipped with computer, internet and telephone

Archive room located on the ground floor of IASL AMO Hangar that measuresabout 20 ft X 14 ft

Quantum Control software

Technical library

Filing racks

Printer/Scanner

The following facilities are provided to quality staff:

Office accommodation located on the first floor of IASL AMO Hangar thatmeasures about 32 ft X 22 ft

7 working stations equipped with computer, internet and telephone

Q-Pulse software

Filing racks

Printer

Scanner

The following facilities are shared by continuing airworthiness and quality staff:

‘Training/Conference’ room that measures about 19 ft X 16 ft

‘Conference’ room that measures about 14 ft X 10 ft

If the provided facilities are not adequate for performance of continuing airworthinessmanagement activities or if there are conditions in the workplace which lead to undue

disturbance at work, CAMO staff are required to report such cases in writing to Headof Engineering with copy to Head of Safety and Quality.






0.7.1 Location of Facilit ies

Location of offices of ‘Head of Engineering’, ‘CAMO’, ‘Conference/TrainingRoom’, ‘Safety and Quality’ and ‘Conference Room’ on the first floor of IASL AMO Hangar:






Location of offices of Archive Room on ground floor of IASL AMO Hangar:






0.7.2 Layout of CAMO Facilit ies

Office of Head of Engineering is located on the first floor of IASL AMO Hangar.Layout of office is given below:

Office of Head of CAMO and CAMO staff is located on the first floor of IASL AMO Hangar. Layout of office is given below:






Archive room is located on the ground floor of IASL AMO Hangar and layout ofthe room is given below:

Conference/Training room is located on the first floor of IASL AMO Hangar andlayout of the room is given below:






Conference room is located on the first floor of IASL AMO Hangar and layout ofthe room is given below:

0.7.3 Layout of Safety and Quality Office

Office of Head of Safety and Quality and Safety and Quality staff is located onthe first floor of IASL AMO Hangar. Layout of office is given below:






0.8 Use of Q-Pulse Software

All IASL CAMO staff have been provided access to Q-Pulse Software and they arerequired to use the software for carrying out the following tasks.

a) Access to electronic copies of manuals, standard operating procedures, memos,regulations, and other such documents and acknowledge receipt of thosedocuments distributed to them via Q-Pulse Software in a timely manner.

b) If necessary, raise change requests for documents distributed to them via Q-Pulse Software.

c) Report safety occurrences and hazards.

d) View scheduled trainings and related handouts/documents (if any), if they havebeen scheduled to attend a training course.

All tasks assigned to staff through Q-Pulse Software and which are to be completed,could be viewed from the ‘Workload’ module of Q-Pulse. Hence, it is a requirement tolog-in to Q-Pulse at least once per week or more frequently (except when on leave)and ensure all the outstanding tasks are completed in a timely manner. If an e-mailaddress has been provided, once a task has been assigned to a staff through Q-Pulse, Q-Pulse will send a notification to the e-mail address.




PART 1 – CONT. AW MANAGEMENT PROCEDURES


PART 1

CONTINUING AIRWORTHINESS

MANAGEMENT PROCEDURES






1.0 Continuing Airworthiness Management Procedures

This Part 1 defines the continuing airworthiness management procedures which IASLCAMO uses to ensure compliance with the continuing airworthiness aspects of MCAR-M. Where some aspects of these functions are sub-contracted, then this will be clearlydefined in the text.






1.1 Aircraft Technical Log Utilisation and Minimum Equipment List Application

1.1.1 The Technical Log

The Technical Log in use with IASL is designed to allow recording of defects,malfunctions, and maintenance performed on the aircraft to which it applies whilstthe aircraft is operating between scheduled base maintenance inspections. Inaddition it includes maintenance information required by the operating crew and isused for recording operating information relevant to flight safety. The continuingairworthiness information includes:

a) The operating crews observations and remarks as a result of aircraftoperation in service including the aircraft, engines, propellers, componentsand system technical status.

b) Defects or incidents having an effect on airworthiness.

c) Results of technical inspections requested by the Approved MaintenanceOrganisation.

d) Maintenance performed by the Approved Maintenance Organisation whichdetails:

i) Defect rectification action taken and associated responses to crewsrequests and/or remarks.

ii) Scheduled maintenance inspections performed

iii) Next due maintenance inspections are not included in the TechnicalLog. IASL CAMO shall provide on a daily basis, a MaintenanceForecast Report for the next 3 days, which includes details of next duemaintenance inspections to Maintenance Operations Centre (MOC),

Operations Control Centre (OCC), Head of Engineering, ManagerMaintenance, Head of Procurement and Logistics, Head of Stores andHead of Safety and Quality. OCC is responsible for insertingMaintenance Forecast Report in the Dispatch Folder and providing theinformation to operating crew.

iv) Where applicable, any MEL and CDL technical limitations proposed bythe Approved Maintenance Organisation.

1.1.1.1 The Technical Log Contents

The IASL Technical Log contains the following sections:

Cover Page Cover Page of the Technical Log contains the followinginformation:

Name and address of IASL

‘REG No’ - Aircraft registration

‘MSN’ - Aircraft serial number

‘A/C Type’ - Aircraft type

‘Log Number’ - First and last serial log number






Section 1 This section is titled as ‘Notice to Flight & MaintenanceCrew’ and is used for conveying technical information ofa temporary nature to flight crew and/or maintenancepersonnel. The entries shall be made by a maintenancecertifying staff. Once the technical information is nolonger relevant, the entry shall be cleared by amaintenance certifying staff. This section consists ofserial numbered pages titled as ‘Notice to Flight &Maintenance Crew’ and a page titled as ‘Notice to Flight& Maintenance Crew Log Transfer Record’.

Serial numbered pages contain the followinginformation:

Contact details of IASL AMO. Contact details of sub-contracted maintenance organisations located atout-stations are listed in the ‘list of important contactdetails’ kept in the aircraft certificate file.

Aircraft type

‘MSN’ - Aircraft serial number Aircraft registration

Signature, stamp and date of the maintenancecertifying staff entering the notice

Notice to flight crew and/or maintenance personnel

Signature, stamp and date of the maintenancecertifying staff clearing the notice

‘Notice to Flight & Maintenance Crew Log TransferRecord’ page is used as a record to certify that allnotices to flight crew and maintenance personnel notcleared in the previous technical log have beentransferred to this log by a maintenance certifying staff.

Section 2 This section is titled as ‘Deferred Items Log’ andcontains serial numbered ‘Deferred Items Log’ pagesand a ‘Deferred Items Log Transfer Record’ page.

Defects which are deferred under MEL are recorded inthe ‘Deferred Items Log’. This page contains the followinginformation:

MSN – Aircraft serial number

Aircraft type

Aircraft registration

‘#’ – Deferred Defect ‘Item No’

‘Date’ – The date the defect was deferred

‘Tech Log #’ – The serial of ‘Aircraft Technical Log’page corresponding to the defect entry

‘ITEM Description / MEL Reference’

‘Expiry’ – MEL rectification interval expiry

‘Sign’ – signature of the person deferring the defect

‘Clearance’ – Tech Log #, name of the personclearing the defect and date






‘Deferred Items Log Transfer Record’ page is used as arecord to certify that all deferred defects not rectified inthe previous technical log have been transferred to thislog by a maintenance certifying staff.

Section 3 This section is titled as ‘Non-Airworthiness DeferredItems Log’ and contains serial numbered ‘Non- Airworthiness Deferred Items Log’ pages and a ‘Non- Airworthiness Deferred Items Log Transfer Record’page.

Defects which are considered as Non-AirworthinessDefects are deferred in accordance with Para 1.8.4 ofthis CAME and recorded in the ‘Non-AirworthinessDeferred Items Log’. This page contains the followinginformation:

‘MSN’ – Aircraft serial number

‘Aircraft type’

‘Aircraft registration’ ‘Tech Log #’ - The serial of ‘Aircraft Technical Log’

page corresponding to the defect entry

‘Date’ – The date the defect was deferred

‘ITEM #’ – Deferred Defect ‘Item No’

‘ITEM Description’

‘Sign’ – signature of the person deferring the defect

‘Clearance’ – Tech Log #, name of the personclearing the defect and date

‘Non-Airworthiness Deferred Items Log Transfer Record’page is used as a record to certify that all non-airworthiness deferred defects not rectified in the

previous technical log have been transferred to this logby a maintenance certifying staff.

Section 4 This section is titled as ‘Aircraft Technical Log’ andcontains serialised pages. Each page contains thefollowing information:

Aircraft Type

Aircraft Registration

Purpose of Flight

Date

Flight Details

Fuel Quantity Details Engine Trend Data (for DHC-6 and DHC-8 fleet)

Work package number for all scheduledmaintenance performed on the aircraft in accordancewith the Approved Maintenance Programme.

Line defect entries and corrective action, includingcomponent replacement details

Pre-flight inspection

Engine oil uplift and total oil quantity

Daily inspection






APU oil uplift and total oil quantity*

Hydraulic fluid uplift quantity

Transit Check*

ETOPS Check*

Ground de-icing*

Information marked with an ‘*’ are only applicable to A320/A321 aircraft.

Sample format of all sections of Technical Log is given in Para 5.1.1 ofthis CAME.

Any changes to the Technical Log shall be submitted to Maldives Civil Aviation Authority (CAA) for approval prior to being put into use.

Instructions for use of the Technical Log:

General

Date and Time entries shall be made in UTC (Coordinated UniversalTime) format.

Correction of entries shall be made by drawing a single line through theincorrect text and entering the signature and stamp (if applicable) of theperson making the correction next to the corrected text.

In the event that unscheduled maintenance and/or defect rectification isrequired to be carried out away from main base, by another MCAR-145 Approved Maintenance Organisation, the organisation carrying out suchmaintenance shall be required to issue a Certificate of Release toService in the Technical Log.

IASL CAMO shall ensure that copies of all Technical Log pages andany other pertinent maintenance-related information are forwardedpromptly to the maintenance contractor, to allow them to perform theirplanning and maintenance co-ordination functions.

DHC-8 and DHC-6 Fleet

This section contains serialised Technical Log Pages (TLP) andthere are three pages for each serial number. The informationentered on the first page is automatically copied to the other twopages.

Page No Colour Purpose

1 (Original) Blue CAMO2 Yellow Flight Operations

3 White Stays with Technical Log

Name of Block Descrip tion ResponsiblePerson

Aircraft Type Enter tick in the appropriate box Flight Crew

Aircraft Registration 8Q-(three letter registration number) Flight Crew

Flight Purpose Enter tick in the appropriate box Flight Crew

DHC8 1st FLT Checks Enter tick upon completion of 1st FLT Checks Flight Crew






by PIC

Date Enter calendar date in DD-MM-YY format Flight Crew

Flight Number Q2-(flight number) Flight Crew

From Aerodrome code of departing aerodrome Flight Crew

To Aerodrome code of destination aerodrome Flight Crew

Take Off Time Enter time in HH:MM format (UTC) Flight Crew

Landing Time Enter time in HH:MM format (UTC) Flight CrewFlight Time = Landing Time – Take Off Time Flight Crew

No. LDG Enter number of landings for the sector Flight Crew

Cycle (L) Enter number of LH Engine cycles for the sector Flight Crew

Cycle (R) Enter number of RH Engine cycles for the sector Flight Crew

This Log Total Enter total of; Flight Time, No. LDG and Cycle(L, R) in the appropriate box

Flight Crew

Fuel (PLND DEP) Enter the fuel quantity required for the sector inLBS

Flight Crew

Fuel (Uplift) Enter uplifted fuel quantity in LBS Flight Crew

Fuel (ACT DEP) Enter fuel quantity in the tanks at the time ofdeparture in LBS

Flight Crew

Fuel (ARR) Enter fuel quantity in the tanks at the time of

arrival in LBS

Flight Crew

Pre-Flight Performed Upon completion of pre-flight inspection, enterlicence number of PIC and signature

Flight Crew

Oil Uplift (L, R) Enter uplifted oil quantity in quarts for each engine AMO

Oil Total (L, R) Enter total oil level in each engine in quarts AMO

Engine Trend Enter engine parameters in the relevant box Flight Crew

Flight Hours (PreviousLog)

Enter total flight hours brought forward fromprevious log in HH:MM format

AMO

Flight Hours (This Log) Enter total flight hours for this log in HH:MMformat

AMO

Flight Hours (Total) = Flight Hours (Previous Log) + Flight Hours (ThisLog)

AMO

Landings (PreviousLog) Enter total landings brought forward from previouslog AMO

Landings (This Log) Enter total landings for this log AMO

Landings (Total) = Landings (Previous Log) + Landings (This Log) AMO

Defect Enter ITEM # (starts at 1 for each log page).

Tick ‘Pilot Report’ or ‘Maintenance Report’.

Enter ‘Leg #’ related to the defect.

If the defect has been deferred, enter ‘DD#’.

Each defect must be entered into a separate item

area and if there are no defects state ‘NIL’. Ifmore space is required, continue on to the nextdefect box and enter the same ITEM#.

Flight Crew AMO

Corrective Action Enter ITEM# (should match the Defect ITEM#).

If the defect is to be deferred under MEL,complete MEL, CAT, ATA and DEFFERALboxes.

Enter details of corrective action taken, by giving

AMO






reference to Maintenance Data.

If any parts have been replaced, enter details atthe bottom of the page. ITEM# should match theITEM# of the ‘CORRECTIVE ACTION’ box.

Certification Issue Certificate of Release to Service (CRS) byentering signature, stamp and date.

AMO

Daily Inspection Enter signature, stamp, date and time (UTC).STN indicated the station where Daily Inspectionwas carried out.

AMO

Records Checked &Updated by CAMO

Review log page information, update relevantrecords and enter signature and stamp

CH – Component HistoryRC – Authorised Release CertificatePU – Software updated with component detailsLB – Relevant Log Books updatedJC – Software policy related to unscheduled

component removals updated

CAMO

A320 and A321 Fleet

This section contains serialised Technical Log Pages (TLP) andthere are four pages for each serial number. The informationentered on the first page is automatically copied to the other threepages.

Page No Colour Purpose

1 (Original) White CAMO

2 Yellow Flight Operations

3 Blue Out-Station

4 White Stays with Technical Log

Name of Block Descrip tion ResponsiblePerson

Aircraft Type A320 pre-printed -

Aircraft Registration 8Q-(three letter registration number) Flight Crew

Flight Purpose Enter tick in the appropriate box Flight Crew

Date Enter calendar date in DD-MM-YY format Flight Crew

Flight Number Q2-(three letter flight number) Flight Crew

Chocks ON Enter time in HH:MM format (UTC) Flight Crew

Chocks OFF Enter time in HH:MM format (UTC) Flight Crew

Block Time = Chock ON – Chocks OFF Flight Crew

Landing Time Enter time in HH:MM format (UTC) Flight CrewTake-Off Time Enter time in HH:MM format (UTC) Flight Crew

Flight Time = Landing Time – Take-Off Time Flight Crew

Landings B/F Enter total airframe landings from previous page AMO

This Log Enter number of landings for the sector AMO

Total Landings = Landings B/F + This Log AMO

Hours B/F Enter total airframe hours from previous page inHHH:MM format

AMO

This Log Enter Flight Time in HH:MM format AMO

Total Hours = Hours B/F + This Log AMO






Fuel Used IND Enter fuel consumption for Engine #1 and Engine#2 in KG

Flight Crew

Total = Fuel Used IND for Engine #1 + Engine #2 Flight Crew

Go Around, Auto Land,...

Enter tick in the appropriate box Flight Crew

Defect Enter ITEM # (starts at 1 for each log page).Tick ‘Pilot Report’ or ‘Maintenance Report’

Enter licence no in the ‘APPRL#’ box

If the defect has been deferred, enter DD#

Each defect must be entered into a separate itemarea and if there are no defects state ‘NIL’. Ifmore space is required, continue on to the nextdefect box and enter same ITEM#

Flight Crew AMO

Corrective Action Enter ITEM# (should match Defect ITEM#).

If the defect is to be deferred under MEL,

complete MEL, CAT, ATA and DEFFERALboxes.

Enter details of corrective action taken, by givingreference to Maintenance Data.

If any parts have been replaced, enter details atthe bottom of the page. ITEM# should match theITEM# of the ‘CORRECTIVE ACTION’ box.

Issue CRS by completing ‘CERTIFICATION’ box.

AMO

Required Fuel (A) Enter the fuel quantity required for the flight in KG Flight Crew

Before Refuel QTY (B) Enter fuel quantity in the tank prior to refuelling AMO

Required Uplift (C) C = A – B (KG) AMOSpecific Gravity (D) Enter specific gravity of the fuel in KG/LTR AMO

Metered Uplift Volume(E)

Enter uplifted fuel volume in Litres. The figure isobtained from the fuel receipt.

AMO

Calculated UpliftVolume (F)

F = C/D (LTR) AMO

Discrepancy (G) G = E - F (LTR). The maximum alloweddiscrepancy is 1.0% for both FULL TANKS andFUEL ONBOARD.

AMO

Fuel Used on Ground = Total Arrival Fuel – Before Refuel Quantity (KG) AMO

Arrival Total Enter fuel quantity on arrival in KG as indicated inthe respective tanks

Flight Crew

Left Outer TankLeft Inner TankCenter TankRight Inner TankRight Outer TankTotal Fuel

After refuelling, enter the distributed fuel quantity(KG) in the relevant tanks and the total fuelquantity in ‘TOTAL FUEL’ block

‘TOTAL FUEL’ quantity must be transferred to thenext log page in ‘DEPARTURE FUEL’ block

AMO

Departure Fuel Brought forward from previous log page (KG) AMO

Metered Fuel Uplift Brought forward from previous log page (KG) AMO

Engine/APU Oil QTY Enter uplifted QTY in US QTS and the indicatedoil quantity on ECAM

AMO

Hydraulic Quantity Enter hydraulic quantity uplifted in QTS for all AMO






hydraulic systems

HYD/OIL SVC Signature and Authorisation No of personcertifying ENG/APU oil quantity and hydraulic fluidquantities

AMO

FUEL SVC Signature and Authorisation No of personcertifying fuel quantities

AMO

APU Hours APU Cycles

Entre figures as indicated on the MaintenanceTest Panel

AMO

Ground De-Icing Enter START TIME, END TIME, TYPE of fluid,RATIO (FLUID/WATER). The responsible personmust sign in the ‘SIGN’ box.

AMO

Transit Transit Check requires CRS. Tick box and entersignature, authorisation number, Date and Time

AMOFlight Crew

Pre-Flight Tick box and enter signature, authorisationnumber, Date and Time.

Flight Crew

Daily Daily Check requires CRS. Tick box and entersignature, authorisation number, Date and Time

AMO

Avionics Daily/PF This check requires CRS. Tick box and enter

signature, authorisation number, Date and Time

AMO

ETOPS SVC. Check This check requires CRS. Tick box and entersignature, authorisation number, Date and Time

AMO

Commander’s Acceptance

Signature of the Commander Commander

Arrival Data Certification Enter Commander’s Name, ATPL # andSignature

Commander

Records Checked &Updated by CAMO

Review log page information, update relevantrecords and enter signature and stamp

CAMO

1.1.2 MEL Application

Minimum Equipment List (MEL) represents a listing of equipment, which may,

under certain circumstances be unserviceable.

Configuration Deviation List (CDL) lists all parts which are permitted to be missingwhen the aircraft is operated, and specifies the performance penalty incurred by amissing part where applicable.

It is the responsibility of the Flight Operations Department to obtain CAA approvalfor the MEL, including any amendments to it.

1.1.2.1 MEL Procedure

a) When a defect has been raised in ‘Defects’ column of the TLP and isdeemed to be within the allowance quoted in the MEL, then it may besubject to carry forward action.

b) Consideration should also be given by the person carrying forward thedefect to the possible effect that multiple and related defects mayhave even where these are covered as individual items in the MEL.

c) Issue a Deferred Defect ‘Item No’ and update the ‘Deferred Items Log’in the Technical Log. This number begins at 001 and terminates at999, and again begins at 001.






d) The entry in the ‘Corrective Action’ column of the TLP should beannotated ‘Defect deferred in accordance with MEL Reference …..,DD Item No ……’ This entry may be made by the operating crew ormaintenance personnel. Operating crew are only allowed to deferdefects under MEL if the deferral procedure given in the MEL doesnot involve performing additional maintenance on the aircraft andrequire maintenance certification.

e) Placard the inoperative item.

f) Certificate of Release to Service shall not be issued for the DeferredDefect until the defect has been cleared on a subsequent TLP.

g) The IASL Approved Maintenance Organisation shall maintain a list ofall outstanding defects deferred under MEL and CDL. This list shall bedistributed daily to Head of Engineering, Head of CAMO, ManagerMaintenance and Head of Safety and Quality.

h) If a defect has been deferred under MEL at an Out-Station by flightcrew or maintenance certifying staff, details of the deferred defectshall be promptly communicated to the Duty Engineer, who shall

ensure that the MOC Display Board is updated and CAMO has beeninformed of the deferred defect(s).

1.1.2.2 Acceptance by the Pilot

Where the MEL item has been entered by maintenance personnel, thedecision to accept the carried forward item allowed by the MEL/CDLremains the responsibility of the pilot in command. This acceptance ofany open deferred items is indicated by his/her signature on the TLP inthe ’Pre-Flight Performed & Aircraft is fit for intended Flight’ block.

1.1.2.3 Management of the MEL Rectif ication Intervals (RI’s)

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).

IASL CAMO shall ensure that all deferred items are rectified as soon aspossible and within the rectification interval.

1.1.2.4 MEL Rectif ication Interval Expiry

Dispatch of the aircraft is not allowed after expiry of the RectificationInterval specified in the MEL, unless:

a) The defect has been rectified.

b) The Rectification Interval is extended by CAA in accordance with thefollowing procedure.

i) Head of CAMO in consultation with Head of Engineering shallsend a CAA Concession Request form to CAA via Head of Safetyand Quality to seek approval for the extension of the RectificationInterval due to unforeseen circumstances.

ii) When an extension has been granted, an entry shall be entered inthe ‘Deferred Defects Log’ section in the Technical Log and acopy of the approved concession form shall be placed in theaircraft documents file.






1.2 Approved Maintenance Programme (AMP)

1.2.0 General

The purpose of a maintenance programme is to provide maintenance planninginstructions necessary for the safe operation of the aircraft.

The Approved Maintenance Programmes are as follows:

CAAReference No

IASL ReferenceNo

Aircraf t Type Aircraf t S/N AircraftRegistration

MP/A320/01 IASL/CM/MT/7 A320, A321 2347, 2599 8Q-IAN, 8Q-IAI

MP/DHC-8/10 IASL/CM/MT/9 DHC-8-300 499, 557,491, 544,546, 591

8Q-IAM, 8Q-IAK,8Q-IAP, 8Q-IAO,8Q-IAS, 8Q-IAR

MP/DHC-8/11 IASL/CM/MT/13 DHC-8-200 429, 542 8Q-AMD, 8Q-IAQ

MP/DHC-6/04 IASL/CM/MT/10 DHC-6-200/300

358, 276,382, 447,226, 629

8Q-IAL, 8Q-IAJ,8Q-IAH, 8Q-IAF,8Q-IAG, 8Q-IAE

1.2.0.1 Approved Maintenance Programme – Contents - Sources

AMP is based upon the recommendations of the airframe, engine,propeller and equipment manufacturers (Type Certificate holder)maintenance recommendations as specified in Type Certificate holder’s Aircraft Maintenance Manuals (AMM), Engine Maintenance Manuals(EMM), Component Maintenance Manual (CMM), Maintenance PlanningDocuments (MPD, OAMP, etc.) and approved Maintenance ReviewBoard (MRB) Reports, as applicable. The main references for the AMP’sare given below:

Approved Maintenance Programme Manufacturers PublicationReference

MP/DHC-8/10

MP/DHC-8/11

Bombardier PSM 1-82-7, PSM

1-83-7, PWC MM 3036432, HSMM 14SF-15/23

MP/A320/01 Airbus A318/A319/A320/A321MPD

MP/DHC-6/04 Viking PSM 1-6-7 (IC) , PSM1-6-7, PSM 1-6-11, PWC MM3013242, Hartzell Propeller’sOwner Manual

1.2.0.2 Structural Inspections, Corros ion Control, Reliability and EngineHealth Monitoring

Structural inspections (including Structural Deviation InspectionRequirements) and Corrosion Protection and Control Programme (CPCP)are as recommended by the manufacturer’s maintenance requirements.

Reliability Programme has been established to monitor the effectivenessof the AMP. Details of the Reliability Programme are given in the AMP.

An Engine Condition Trend Monitoring (ECTM) programme has beenestablished for PW123, PT6-27 and CFM56-5B engines. ECTM detailsare provided in the AMP. IASL has sub-contracted ECTM services tothe following organisations:






Name of the Organisation Sub-contractedservice

Approvals

Danish Engine Trend Analysing (DETA)

ECTM analysis forPW123 and PT6engines

P&WCDesignated Analysis Centre

CFM International ECM analysis ofCFM56-5B engines

OEM

1.2.0.3 Mandatory Life Limitations

Mandatory Life Limitations are those imposed by the manufacturersand/or the CAA. The limitations include the following:

Safe Life Airworthiness Limitations Items - This provides mandatoryreplacement time, structural inspection interval, and related structuralinspection procedure, or other procedure (e.g. modifications)determined as necessary for compliance with regulatory requirements.Such Limitations are applicable to structures that are designed to “safelife” concept. They apply to all those parts of the structure whose failure

could result in catastrophic failure of the aircraft.

Damage-Tolerant Airworthiness Limitation Items - These are mandatoryreplacement times, structural inspection intervals, and related structuralinspection procedure, or other procedures (e.g. modifications)determined as necessary and such limitations are applicable tostructures that are designed to “damage tolerance/fail-safe” concept.They apply to all those parts of the structure whose failure could resultin catastrophic failure of the aircraft.

Certification Maintenance Requirements (CMR) - CMR are associatedwith systems and are identified following an evaluation of tasksnecessary to maintain compliance with certification requirements. The

majority is associated with compliance with applicable regulations and isconsidered as the systems equivalent to the Damage Tolerant Airworthiness Limitations Items. For this reason it is consideredappropriate to identify them as part of the ALS.

Ageing Systems Maintenance (ASM) - The ASM refers to limitationsapplicable to aircraft systems that operate beyond their originalqualification. Beyond this point, ageing effects may affect thecharacteristics of the system leading to an increased potential for failure.The maintenance associated with failure conditions shown to besensitive to the ageing effects on system components, is subject tolimitations.

Fuel Airworthiness Limitations (FAL) - Fuel Airworthiness Limitations aremandatory maintenance instructions arising from compliance with FuelTank Safety requirements. These requirements are determined asnecessary to preclude the development of unsafe conditions within thefuel system as a result of maintenance actions, repairs or alterationsthroughout the operational life of the aircraft. FAL comprise ofmaintenance/inspection tasks and Critical Design Configuration ControlLimitation (CDCCL).






1.2.0.4 Inspection Standards

The Inspection Standards applicable are those given by themanufacturers of the airframe, engine, propellers and equipment anddetailed in MCAR-M. Other Inspection Standards may be adopted ifand when these are promulgated by the CAA.

1.2.0.5 Maintenance Certification

All maintenance above the pre-flight level shall be certified by acertification authorisation holder through the issuance of a Certificate ofRelease to Service and as per MCAR-145.

1.2.0.6 Fuel Contamination

Fuel contamination checks are addressed in Part 1 of this CAME Para1.11.4. Also, the Daily Check includes water drain from fuel tanks to becarried out prior to the first flight of the day.

1.2.0.7 The Approved Maintenance Programme Owner – Responsibilities

The Approved Maintenance Programme has been produced by IASLwho being the owner of the programme is responsible for itsdevelopment in accordance with MCAR-M.708(b).

1.2.0.8 Holders of AMP

Original copy of Approved Maintenance Programme is held by Head ofCAMO and CAA. Head of CAMO shall provide a soft copy of AMP toHead of Safety and Quality to be uploaded to Q-Pulse.

AMP shall be distributed to the following persons via Q-Pulse:

Head of Engineering


Manager Maintenance of IASL AMO

1.2.1 AMP Review, Development and Amendment

1.2.1.1 Development and Amendment

Development and amendment of the AMP is the product of theoperator's actions in monitoring the effectiveness of the Programme byIASL CAMO (see Paragraph 1.5), together with the recommendationsreceived from the contracted MCAR-145 maintenance organisations,

and the response from IASL to continued airworthiness informationpublished by the manufacturers of aircraft, engines, propellers andequipment in the form of Service Bulletins (SB) and AirworthinessDirectives (ADs) issued by State of Design and CAA.

1.2.1.2 AMP Meetings

Liaison Meetings, attended by the following persons or theirrepresentatives, shall be held at intervals not exceeding six months todiscuss and review the effectiveness of the AMP.






Head of CAMO (Convener)

Head of Engineering


Head of Technical Training

Manager Maintenance (IASL AMO)

Head of Procurement and Logistics

Head of Stores CAA Representative

1.2.1.3 AMP Amendments

Where changes are identified as being necessary by IASL CAMO andIASL AMO, the amendments shall be prepared by Head of CAMO andapproved by Head of Engineering before it is submitted to Head ofSafety and Quality for onward submission to CAA for approval.

1.2.1.4 AMP Variations

All variations to the AMP shall be within the guidelines defined in the

AMP. These variations shall only be requested when circumstances arisewhich could not reasonably have been anticipated by IASL. Acceptablereasons would be, for example, the aircraft being unable to return on timeto the maintenance base due to weather or an AOG situation.

The Head of CAMO shall raise an ‘in-house concession request’ form andsubmit the form to Head of Safety and Quality for approval.

The Head of Safety and Quality may grant a variation to a maintenanceinterval specified in the AMP, provided that such variations are within thelimits given in the following table.

Period Involved Maximum Variation of the

Prescribed Perioda) Items controlled by Flight Hours (FH)

i) 5000 FH or less 10%

ii) More than 5000 FH 500 FH

b) Items controlled by Calendar Time

i) 1 Year or less 10% or 1 Month, whichever is less

ii) More than 1 Year butless than 3 Years

2 Months

iii) More than 3 Years 3 Months

c) Items controlled by Landing/Cycles

i) 500 Landing/Cycles orless

10% or 25 Landing/Cycles,whichever is less

ii) More than 500Landing/Cycles

10% or 500 Landing/Cycles,whichever is less

d) Items controlled by more than one limit

For items controlled by more than one limit, e.g. items controlled byFlight Hours and Calendar Time or Flight Hours andLandings/Cycles, the more restrictive limit shall be applied.

The variations permitted above do not apply to:






a) Those components for which an ultimate (scrap) or retirement lifehas been prescribed (e.g. primary structure, components withlimited fatigue lives, and high energy rotating parts for whichcontainment is not provided).

b) Those tasks included in the AMP, which have been classified as Airworthiness Limitations Items (ALI) and mandatory by the TypeCertificate holder or the CAA.

c) Certification Maintenance Requirements (CMR) unless specificallyapproved by the Manufacturer and agreed by the CAA.

1.2.1.5 Variations in excess of that allowed by Maintenance Programme

Any requests for variations in excess of that allowed by the AMP andoutside the limitations given in 1.2.1.4 shall be submitted by the Head ofCAMO to Head of Safety and Quality on ‘CAA concession request’ form.These variations shall only be sought in very exceptional circumstances.

The ‘CAA concession request’ form shall be submitted by Head ofSafety and Quality to CAA for approval.






1.3 Time and Continuing Airworthiness Records: Responsibili ties, Retention & Access

1.3.1 Continuing Airworthiness Records

Continuing Airworthiness records include:

The aircraft Log Books for Airframe, Engines, Propellers and APU

Component History Card for any service life limited component

Modification Log Book and records

Inspection records (Work Packages)

Non-Routine Task Card (NRTC)

Component life records

Technical Log

Overhaul records

Repair records

Airworthiness Directive compliance records

Current status of

- Airworthiness Directives, Service Bulletins and measures mandated byCAA in immediate reaction to a safety problem

- Modifications and repairs- Compliance with AMP- Service life limited components- Mass and balance report- List of deferred maintenance

IASL AMO is responsible for the proper and accurate completion of continuingairworthiness records.

IASL CAMO is responsible for the following tasks:

a) Control the continuing airworthiness records and present the records to theCAA upon request.

b) Ensure that continuing airworthiness records are kept current and stored in amanner that ensures protection from damage, alteration and theft.

c) At the completion of any maintenance, the details of the maintenanceperformed shall be entered in the aircraft continuing airworthiness records.Each entry shall be made as soon as practicable but in no event more than7 days after the day of the maintenance action. When the maintenance hasbeen carried out as per a Work Package or a Non-Routine Task Card(NRTC), the Work Package or NRTC reference shall be entered in therecords.






d) The aircraft type and registration mark, the date, together with total flighttime and/or flight cycles, as appropriate, shall be entered in the aircraftlogbooks. The Quantum software shall be updated with flight time and flightcycles on a daily basis.

e) All entries made in the aircraft continuing airworthiness records shall beclear and accurate. When it is necessary to correct an entry, the correctionshall be made in a manner that clearly shows original entry. If it is necessaryto delete any information, the entry shall be deleted by drawing a single linethrough the middle of the text and, reason for deletion, date, signature andstamp of IASL CAMO staff shall be entered near deleted information.

f) Maintenance Records and Technical Log shall be checked for propercompleteness of information.

g) The following information relevant to any serialised component installed shallbe entered in the appropriate aircraft log book and component life records.

i. Identification of the component

ii. The type, serial number and registration of the aircraft to which theparticular component has been fitted, along with the reference to theinstallation and removal of the component

iii. The particular component accumulated total flight time and/or flightcycles and/or calendar time, as appropriate

h) All computer hardware used to ensure backup shall be stored in a differentlocation from that containing the working data and in an environment thatensures they remain in good condition. The backup shall be updated on a dailybasis.

1.3.2 Monitoring of Scheduled Maintenance

All scheduled maintenance in accordance with the AMP are monitored usingQuantum Software.

Performance of scheduled maintenance by IASL Approved MaintenanceOrganisation is requested by issuing a Work Package. The Work Package shallinclude Work Package Cover sheet and Task Cards. The Work Package shallalso include a Maintenance Statement for base maintenance.

1.3.3 Record Retention

The continuing airworthiness records are held by IASL CAMO. IASL CAMO shallensure that it receives the following properly completed maintenance records fromIASL AMO:

Work Packages

CAA Form 1 or equivalent for components installed on aircraft

Technical Log pages






IASL CAMO shall ensure that records are stored in a manner that ensuresprotection from damage, alteration and theft.

All computer hardware used to ensure backup is stored in a different location fromthat containing the working data in an environment that ensures they remain ingood condition. Computer systems have a backup system which is updated within24 hours of any new entry. Each terminal contains password safeguards againstthe ability of unauthorised personnel to alter the database.

IASL CAMO keeps time and continuing airworthiness records for the period asindicated in the following tables:

Type of Records Duration of Retention Medium ofRetention

All detailed maintenance records inrespect of the aircraft and any life-limited component fitted thereto

24 months after theaircraft or componentwas permanentlywithdrawn from service

Hard Copy

The total time and flight cycles as

appropriate, of the aircraft and all life-limited components

12 months after the

aircraft or componenthas been permanentlywithdrawn from service

Hard Copy

Soft Copy

The time and flight cycles asappropriate, since last scheduledmaintenance of the componentsubjected to a service life limit

At least until thecomponent scheduledmaintenance has beensuperseded by anotherscheduled maintenanceof equivalent workscope and detail

Hard CopySoft Copy

The current status of compliancewith AMP such that compliance withthe AMP can be established

At least until the aircraftor componentscheduled maintenance

has been supersededby other scheduledmaintenance ofequivalent work scopeand detail

Soft Copy

The current status of airworthinessdirectives applicable to the aircraftand components

At least 12 months afterthe aircraft orcomponent has beenpermanently withdrawnfrom service

Hard CopySoft Copy

Details of current modifications andrepairs to the aircraft, engines,propellers and any other component

vital to flight safety

At least 12 months afterthey have beenpermanently withdrawn

from service

Hard Copy

Aircraft Technical Log 36 months after thedate of the last entry

Hard Copy






1.3.4 Access to Continuing Airworthiness Records

All of the records may be accessed by IASL CAMO staff, Quality Auditors,authorised members of IASL AMO and other persons permitted by IASL CAMO,and remain the property of IASL at all times.

Access to the records by duly authorised members of the CAA shall be arrangedwhere this is necessary.

1.3.5 Transfer of Continuing Airwor thiness Records in the event of a sale or otherdisposal of the Aircraft

In the event of sale or other disposal (lease-in, lease-out) of an aircraft, IASL isrequired to transfer the records to the new owner or operator of the aircraft. Allrecords shall be made available by IASL for transfer to the new owner/operator.

1.3.6 Access to Continu ing Airworthiness Records in the event of an Accident/Incident

In the event of an accident or serious incident, Head of Safety and Quality shallhold the records secure until requested by the Accident Investigation Co-ordination Committee (AICC) and/or the CAA.






1.4 Accomplishment and Control of Mandatory Requirements for Airworthiness

1.4.1 Airworthiness Directives

IASL CAMO is responsible for the accomplishment of all applicable AirworthinessDirectives (ADs) issued by CAA and the State of Design. Hence, IASL CAMOshall obtain and maintain current applicable copies of Airworthiness Directivesissued by:

Description CAA TransportCanada

EASA

A320/A321 Aircraft X X

CFM 56-5B Engines X X

DHC-8 Aircraft X X

PW123 Engines X X

DHC-6 Aircraft X X

PT6-27 Engines X X

IASL CAMO shall check the website of the above authorities for new ADs orrevisions to ADs at least on a monthly basis.

1.4.2 Airworthiness Directive Decision and Implementation

a) When a new AD or revisions thereto has been received and if it is applicable toIASL aircraft, IASL CAMO shall review the AD and an ‘AD/SB Compliance’Form shall be raised. In case of new AD’s which are applicable to the aircrafttype and model but not applicable to IASL aircraft, affix disposition stamp, enterreceived date, state the non-applicability, date and sign on the stamp. All nonapplicable AD’s shall me marked as ‘Not Applicable’.

b) Head of CAMO, in consultation with Head of Engineering and IASL Approved

Maintenance Organisation, shall take necessary actions to comply with the ADbefore the deadline.

c) Head of CAMO is responsible for ensuring that appropriate action is taken tocomply with the AD. If any maintenance is required, a Work Package shall beissued.

d) In case of an emergency Airworthiness Directive to be complied immediately,Head of CAMO shall inform IASL Approved Maintenance Organisation andinitiate immediate compliance.

1.4.3 Airworthiness Directive Control

IASL CAMO shall maintain a current status of all applicable AirworthinessDirectives (on computer) for each aircraft. This list shall include the followinginformation:

Terminated ADs and repetitive ADs

Details of last compliance action and if applicable, when the nextcompliance is due

Work Package reference






1.4.4 Recording of Airworthiness Directive Compliance

The method of compliance and when compliance with an AD was achieved shallbe recorded by IASL CAMO in the Modification Logbook. If Alternate Methods ofCompliance (AMOC) are applied, this must be mentioned in the ModificationLogbook.

For AD with a repetitive inspection content then each and every inspection mustbe recorded on completion in the Modification Logbook.

In addition, IASL CAMO shall record compliance and when compliance with an AD was achieved in relevant IASL CAMO Microsoft Excel AD status sheets.






1.5 Analysis of the Effectiveness of the AMP

Head of CAMO shall, analyse and monitor the effectiveness of the AMP through regularLiaison Meetings attended by the personnel listed under 1.2.1.2 and with theparticipation of IASL AMO.

Head of CAMO shall send an invitation to CAA through Head of Safety and Quality toparticipate in Liaison Meetings.

1.5.1 Liaison Meetings

These meetings shall address the following areas:

a) The AMP content

b) The effect on the AMP of any ADs, modifications or repairs

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

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, ServiceBulletins, Service Information Letters etc. and how these affect theMaintenance Programme

h) Other Quality System findings as they impinge upon the contracted MCAR-145maintenance organisations.

Where appropriate and necessary, amendments to the Maintenance Programmeshall be promulgated by the Head of CAMO for submission to CAA as anamendment.

1.5.2 Frequency of Meetings

Liaison meetings shall be held at a minimum of six monthly intervals and theresults of any meeting recorded with any actions required allocated to theresponsible person.






1.6 Non-Mandatory Changes (Modification) Embodiment Policy

1.6.1 Changes (Modifications) General

Non-mandatory changes (modifications) shall normally take the form ofmanufacturer's Service Bulletins, or shall be derived from them. Any otherchanges (i.e. those not covered by a manufacturer's Bulletin) shall be initiated bythe Head of CAMO in consultation with IASL Approved Maintenance Organisation.

1.6.2 Service Bul letins

a) All manufacturer’s Service Bulletins applicable to IASL aircraft shall bereviewed by Head of CAMO. For each applicable SB, an ‘AD/SB Compliance’Form shall be raised.

b) In the ‘AD/SB Compliance’ Form No IASL/ENG/09, Head of CAMO shallinclude his recommendations on compliance with the SB.

c) Head of Engineering shall make the final decision on compliance with the SB’swhich are in the category of operator’s discretion, after giving due considerationto its airworthiness impact and how beneficial it would be to IASL and hisdecision shall be recorded on the ‘AD/SB Compliance’ Form.

d) Compliance with Alert Service Bulletins shall be considered mandatory.

e) When it has been decided to comply with the SB, Head of CAMO shall decide,in consultation with IASL Approved Maintenance Organisation, on a date forcompliance action and a Work Package shall be issued.

f) The compliance action shall be recorded in the Modification Logbook by IASLCAMO.

g) IASL CAMO shall maintain a current status of all applicable Service Bulletins(on computer) for each aircraft.

Applicable SB’s and decision on its compliance

Details of compliance action

Work Package reference

1.6.3 Other Changes (Modifications)

For all changes (modifications) other than those introduced by manufacturer'sSBs' i.e. those proposed by IASL or IASL Approved Maintenance Organisation foroperational advantage or other reasons then these shall be subject to the current

CAA change procedures. In the first instance CAA shall be consulted for advicewith an outline of the proposed change with a view to ascertaining whether or nota change is deemed to be classified as 'Major' or 'Minor'.

1.6.4 Minor Changes (Modifications)

All minor changes shall be agreed between Head of CAMO and Head of Safetyand Quality before submission to CAA. Head of CAMO shall be responsible forraising the CAA Modification Approval Form with supporting documentation and






Head of Safety and Quality shall be responsible for submitting the form to CAA forapproval along with the required fee as per MCAR-187.

Data for minor changes shall be obtained from a design organisation approved byCAA or from a design organisation acceptable to CAA.

Records of the modification including supporting documentation and CAAapproval shall be retained by IASL CAMO.

1.6.5 Recording of Changes (Modifi cations)

Incorporation of all non-mandatory changes, whether introduced through ServiceBulletins or by CAA Approved Minor/Major change, are to be recorded in theModification Logbook.






1.7 Major Change (Modification) Standards

All Major Changes require a Supplemental Type Certificate (STC) which meets SubpartE requirements of MCAR-21. CAA Modification Approval Form shall be submitted alongwith the STC and other supporting documents.

Records of the modification including supporting documentation and CAA approval shallbe retained by IASL CAMO.






1.8 Defect Reports

All defects occurring on IASL aircraft shall be subject to review and analysis for theireffect upon airworthiness and the safe operation of the aircraft.

1.8.1 Analysis

Technical Log Pages and Non-Routine Task Cards (NRTCs) are examined atregular intervals by IASL to provide information concerning defects occurring,Pilot's reports, maintenance actions and defects of a repetitive nature.

Maintenance input records (Work Packages) shall also be reviewed for significantfindings by IASL CAMO and IASL Approved Maintenance Organistion which mayhave airworthiness or operational implications.

Head of CAMO shall assess the findings as necessary and any action requiredshall be agreed in the Liaison Meetings before implementation. Implementationmay take the form of an AMP amendment or modification action.

1.8.2 Liaison with Manufacturers and Regulatory Author ities

Head of CAMO may liaise with the Manufacturer(s) on all matters concerning theairworthiness of IASL aircraft. It is the responsibility of the Head of Safety andQuality to liaise with CAA on such matters.

1.8.3 Deferred Defect Policy

IASL shall seek to ensure that the minimum number of open Deferred Defectsexist. All open Deferred Defects shall be monitored by the Head of CAMO inconsultation with the IASL Approved Maintenance Organisation to ensure earliestrectification and subsequent closure. Defects may be deferred in the followingmanner.

Under MEL, in accordance with the requirements of Para 1.1.2

Non-airworthiness defects may be deferred in accordance with therequirements of Para 1.8.3.1

Defects which do not meet the above criteria shall be deferred only withthe approval of CAA or Type Certificate Holder and that the defect is not ofa safety concern.

When a Deferred Defect is raised, the Head of CAMO shall consult with the IASL Approved Maintenance Organisation with a view to arranging the earliest possiblerectification action to be taken. This will involve the pre-allocation of down time,

spares, personnel, tooling etc. as appropriate.

A CRS shall be issued in the Technical Log upon clearance of any DeferredDefects.






1.8.3.1 Non-Airworthiness Defects

Non-Airworthiness defects are defects that would not affect theairworthiness of aircraft. The following list provides some of the typicalnon-airworthiness defects which could be deferred under this procedure.

Unserviceable Reading Light/Cabin Light

Missing Ash Tray Cover

Damaged Seat Arm Rest Cap/Cover

Unserviceable Air Scoop/Vent

Unserviceable Buffet Overhead Light

Missing Seat Track Cover

Unserviceable Coffee Maker/Oven

Seat Back Recline feature Unserviceable

Unserviceable IFE/IFE Display

Water Tap in Lavatory Unserviceable

Missing screws within maintenance data limits

Unserviceable Window Blinds

Unserviceable Tray Table

Unserviceable Headphone Jack Point

Unserviceable Overhead Bin Door

Poor condition of Curtain, Seat Cover/Seat Pocket

Missing paints that do not require maintenance action in accordancewith maintenance data

Missing coating in the cabin panels

The scope of this procedure covers only defects which are similar innature to the defects listed above.

It is the responsibility of the Certifying Staff to determine whether anaircraft defect would affect the airworthiness of aircraft.

Non-Airworthiness defects shall be deferred in accordance with thefollowing procedure.

a) Issue a Non-Airworthiness Defect ‘Item No’ and update the ‘Non- Airworthiness Deferred Item Log’ in the Technical Log. This numberbegins at 001 and terminates at 999, and again begins at 001.

b) The entry in the ‘Corrective Action’ column of the TLP should beannotated ‘Non-Airworthiness Defect deferred in accordance withCAME, NAW-DD Item No …..’ This entry may be made by theoperating crew (only at Out Stations with approval of a Certifying Staff)or maintenance personnel.

c) No Certificate of Release to Service is to be issued for the Non- Airworthiness Defect until the defect has been cleared on asubsequent TLP.

d) The IASL Approved Maintenance Organisation shall maintain a list ofall outstanding Non-Airworthiness deferred defects. This list shall bedistributed daily to Head of Engineering, Head of CAMO, ManagerMaintenance, Head of Safety and Quality.






1.8.3.2 Acceptance by the Pilot

Where the Non-Airworthiness defect has been deferred by maintenancepersonnel, the decision to accept the deferred defect remains theresponsibility of the pilot in command. This acceptance of any opendeferred defects is indicated by his/her signature on the TLP in the ‘Pre-Flight Performed & Aircraft is fit for intended Flight’ block.

1.8.3.3 Management of the Non-Airworthiness Defect Rectification Interval

The time limit for the non-airworthiness defect rectification shall notexceed 30 calendar days. This interval may only be extended underexceptional circumstances with prior approval of Head of Safety andQuality.

IASL CAMO shall ensure that all deferred Non-Airworthiness defects arerectified as soon as possible and within the rectification interval.

1.8.4 Non Deferrable Defects Away from Base

Where defects occur that are not listed in the MEL, then the following actions mustbe taken:

a) IASL AMO shall consult with the Head of CAMO with a view toestablishing the extent of the defect and the rectification action required.

b) IASL AMO shall ascertain if there is a suitably approved maintenanceorganisation with the appropriate ratings on their schedule of approvalin close proximity to the AOG aircraft. Suitable contractual action shallbe taken to have the defect rectified and duly certified by thatorganisation.

c) Where no suitably approved maintenance organisation is available thenaction shall be taken to position certifying staff of IASL AMO or asuitably approved maintenance organisation, together with thenecessary spares, tooling, technical publications to rectify and certifythe defect.

d) IASL CAMO may also submit an application to CAA in accordance withSubpart P requirements of MCAR-21 for a Permit to Fly to ferry theaircraft to the base for rectification action.

1.8.5 Repetitive Defects

Repetitive Defects are those defects re-occurring e.g. on three occasions betweenscheduled Maintenance Inspections. The Technical Log is monitored by the Headof CAMO to identify these defects as and when they arise. Remedial action shallbe taken by Head of CAMO in consultation with IASL Approved MaintenanceOrganisation.






1.8.6 Mandatory Occurrence Reporting

All occurrences that fall within the reporting criteria defined in MCAR-M.A.202 andMCAR-12 shall be reported to the CAA within 72 hours from the time of theoccurrence.

All occurrences shall be reported in accordance with the requirements of Chapter11 of IASL Safety Management Manual

All such occurrences shall be reported to Head of Safety and Quality using Q-Pulse Software as soon as practicable but in any case within 24 hours from thetime of the occurrence. If Q-Pulse Software is not accessible, the occurrence shallbe reported to Head of Safety and Quality by submitting paper copy of occurrencereport.

IASL CAMO shall inform Head of Safety and Quality as soon as possible toenable him to analyse and to file the occurrence report to the TC/STC holder(s)and CAA within 72 hours of identifying any condition of the aircraft or componentthat has resulted or may result in an unsafe condition that hazards seriously the

flight safety.

All occurrence reports, which have maintenance implications, shall be provided toHead of CAMO by Head of Safety and Quality. Head of CAMO shall analyse suchreports in consultation with IASL AMO and take immediate corrective actions toprevent recurrence of occurrences.

1.8.7 Liaison Meetings

Airworthiness, quality and MOR issues will be discussed during the liaisonmeetings held in accordance with Para 1.5.

All of the 'formal' meetings shall be recorded and minuted. All actions required in

response to maintenance findings, follow up actions, audit corrective actions etc.shall be duly allocated with respect to responsibility. Minutes of these meetingsshall be held by Head of CAMO. The minutes shall be made available on requestto any duly authorised member of the CAA.






1.9 Engineering Activity

Where applicable the development of changes (modification and repairs) for approvalby the CAA shall be coordinated by Head of CAMO as the person responsible fordesign changes.

Application for the approval of such changes shall be made on the appropriate CAA

application form.

Each application shall be submitted to CAA by Head of Safety and Quality,accompanied by supporting documents, which provides technical justification forapproval of the change and in accordance with the requirements given in Para 1.6.4and 1.7.






1.10 Reliability Programmes

The reliability programme for each type of aircraft operated by IASL is given in Approved Maintenance Programme (AMP) for that type of aircraft.

A320/A321 ETOPS Reliability Programme requirements are given in Part 7 of ETOPSManual.

IASL CAMO shall prepare a monthly reliability reports and distribute the report for theprevious month to Head of Engineering, Head of Safety and Quality, IASL AMO andCAA before 10th day of every month.

Reliability statistics shall be discussed during the liaison meetings as referred in Para1.5.1.






1.11 Pre-Flight Inspections

The preparation of the aircraft for flight is the responsibility of the IASL ApprovedMaintenance Organisation.

Pre-flight inspection is intended to mean all of the actions necessary to ensure that theaircraft is fit to make the intended flight.

Prior to every flight, a pre-flight inspection shall be performed and signed in the AircraftTechnical Log. Pre-flight inspections may be performed by IASL AMO but are generallycarried out by the flight crew. The pre-flight inspection does not require a Certificate ofRelease to Service and may be carried out by the flight crew without a certificationauthorisation from IASL AMO.

1.11.1 The Pre-Flight Inspection

The pre-flight inspection checklists for DHC-8-200/300 and DHC-6 aircraft aregiven in Part 5 of this CAME. Pre-flight inspection checks for A320 and A321aircraft has been incorporated into Transit Check and it is a requirement to

perform Transit Check by IASL AMO prior to every flight.

The pre-flight inspections shall be performed in accordance with the pre-flightinspection checklist. IASL CAMO is responsible for ensuring that pre-flightinspection checklists remain concurrent with respect to the evolution of FlightManuals and Maintenance Programmes.

1.11.2 The Daily Check

The Daily Check will be performed on DHC-6, DHC-8, A320 and A321 Aircraft inaccordance with the requirements of AMP.

1.11.3 Pilot Author isation

Training Captain shall ensure that appropriate training is provided to all Captainsfor carrying the pre-flight inspection using the checklists mentioned under Para1.11.1. All Captains who have completed pre-flight training are considered to beauthorised to carry out pre-flight inspections.

1.11.4 Sub-Contracted Ground Handling Functions

Head of Ground Operations is responsible for all ground handling functions.

IASL has established offices and appointed a Station Manager at all stations toensure ground handling functions are performed in accordance with therequirements of Ground Operations Manual.

IASL has appointed Ground Handling Agents for the performance of groundhandling functions and they are listed in Chapter 2 of Ground Operations Manual.

1.11.5 Security of Cargo and Baggage Loading

The security of cargo and baggage loading is the responsibility of Head of GroundOperations and operating crew. Cargo and baggage shall only be carried onboardthe aircraft in those areas specifically designed to do so in accordance with the






limitations quoted in the Flight Manual and the requirements of Ground OperationsManual (GOM) listed below:

GOM Reference Description

Chapter 6 Baggage Handling

Chapter 7 Aircraft Handling

Chapter 8 Load Control

Chapter 9 Dangerous Goods

Chapter 11 Cargo Handling

Chapter 12 Security

For further guidance, refer to Para 8.1.9, Para 8.2 and Para 8.10 of OperationsManual Part A.

1.11.6 Control of Ai rcraft Refueling Quantity/Quality

The responsibility for aircraft refueling lies with the operating crew. The operatingcrew shall ensure that the right quantity, specification and quality of fuel beingcarried on board for the intended flight.

Before refueling, the operating crew shall ensure that the refuelling vehiclecontains the correct grade of fuel, as shown at the refuelling points on the aircraft.The AMP contain tasks that guarantee that filling points are clearly marked toindicate the fluid to be used and these markings maintained in a legible condition.

Precautions shall be taken to provide a path to earth for any static electricitywhich may be present or which may build up as a result of the fuel flow. Theaircraft and the refuelling vehicle shall be earthed to a point which is known to besatisfactory and the earthing wire on the refuelling pipe shall be connected to theearth point provided on the aircraft before connecting the refuelling pipe orremoving the tank filler cap. The earthing wire shall remain in position until afterthe refuelling pipe is disconnected or the tank filler cap is replaced, as

appropriate. When draining fuel into buckets, containers or tanks, these shall bebonded to the aircraft and/or the refuelling vehicle. No radio or radar equipmentshall be operated while refueling or defueling is taking place and only thoseelectrical circuits essential to these operations shall be switched on.

A fuel system contamination check shall be carried out in accordance with the AMP. A small quantity of fuel shall be drained into a glass jar and checked for thepresence of water, sediment and microbiological contamination. Also, the colourof the fuel shall be checked to ensure that Jet A has not been mixed with AviationGasoline.

In addition, a fuel contamination check shall be carried out by the operating crewif fuel is obtained from sources whose integrity in respect of fuel grade and quality

is in doubt. In case of doubt, the operating crew shall inform IASL AMO ofsuspected fuel. Flight may not be continued unless jointly released by the Headof Engineering and the IASL AMO. For relevant procedures, refer to CAME Part1.8.

For further guidance, refer to Para 8.1.8 and Para 8.2.1 of Operations ManualPart A.






1.11.7 Control of Snow, Ice, Dust and Sand Contamination to an ApprovedStandard

The control of snow, ice, dust and sand contamination before flight is theresponsibility of the operating crew. Operating crew shall take whatever stepsthey consider necessary to ensure the aircraft is free from such contaminationbefore flight.

De-icing/Anti-icing on A320/A321 aircraft shall be performed in accordance withSOP321.

For further guidance, refer to Para 8.2.4 and 8.3.8 of Operations Manual Part A.

1.11.8 Certificate of Airworthiness and Airworthiness Review Certifi cate Validity

Head of CAMO shall monitor the continued validity of Certificate of Airworthinessand Airworthiness Review Certificate (ARC).

If the aircraft remained within a controlled environment, IASL CAMO may extend

twice the validity of ARC for a period of one year each time. An ARC shall not beextended if the organisation is aware or has reason to believe that the aircraft isunairworthy.

Head of CAMO shall submit application to Head of Safety and Quality forextending the validity of ARC at least 30 days prior to expiry date. ARC shall beextended by an Airworthiness Review Staff following a full documented review ofthe aircraft and physical survey of the aircraft.

If IASL CAMO has extended twice the validity of ARC following issue of ARC byCAA, Head of Safety and Quality shall submit application to CAA at least 30 daysprior to expiry date of ARC for issue of new ARC.






1.12 Aircraft Weighing

DHC-6 and DHC-8 aircraft weighing is performed by IASL Approved MaintenanceOrganisation and A320/A321 aircraft weighing is performed by a suitably approvedmaintenance organisation. Head of CAMO shall prepare and maintain a Mass andBalance report for each aircraft operated. It is the responsibility of the Head of CAMO toensure that the Mass and Balance report reflects the current configuration of the aircraft.

Re-weighing of aircraft shall be carried out at intervals specified in the AMP andrecommended by the Type Certificate holder or the CAA. In addition, aircraft shall be re-weighed if the effect of changes, repairs and painting on the mass and balance is notaccurately known.

1.12.1 Weighing

The aircraft shall be in the condition as specified in Type Certificate holder’smaintenance data, or the aircraft weight & balance manual, or the CAArequirements, as applicable. Fluids, such as engine oil or fuel, shall be partially orcompletely drained and equipment positioned at its normal operational location.The equipment and other items of load such as fluid in the tanks shall berecorded. Instructions supplied by the relevant aircraft Type Certificate holder onlevelling procedures and the positioning of equipment shall be carefully followedand adhered to.

Weighing is carried out inside a closed hangar. The aircraft shall be positioned inthe hangar several hours before weighing so that it can assume an eventemperature and be free from moisture. If weighing in the open is unavoidable, itshall be carried out on a firm level site when wind force is at a minimum with theaircraft completely dry (i.e. not affected by dew) and several readings shall betaken at each reaction point to obtain a reliable average figure.

All weighing apparatus shall be checked, adjusted and certified either by theequipment manufacturer, or by an appropriately approved organisation within 2years or within a time period defined by the equipment manufacturer, whicheveris less. Weighing apparatus accuracy is satisfactory, if for a scale/cell load below2000 kg, the accuracy is within +/- .1%. For a scale/cell load from 2000 kg to 20000 kg, the accuracy should be within +/- 20 kg. The zero indication will bechecked for accuracy before any weighing is commenced.

1.12.2 Mass and Centre of Gravity Calculation

For weighing aircraft, IASL CAMO shall issue a work package with WeighingRecord form and the weighing is carried out by IASL AMO or a suitably approvedmaintenance organisation and certified by a maintenance Certifying Staff.

Based on the weighing record, IASL CAMO prepares a Basic Weight ChangeRecord. IASL CAMO shall forward a copy of Basic Weight Change Record torelevant Chief Pilot and it is the responsibility of Chief Pilot to prepare OperatingWeight Empty (OWE) for each configuration of aircraft.

Basic Weight Change Record and OWE shall be inserted in the Weight andBalance Manual kept onboard the aircraft and IASL CAMO Library.






1.12.3 Change in Basic Mass

When an item of basic equipment is added, removed or repositioned in anaircraft, or a modification, repair and painting carried out and the changes tomass and balance is not accurately known, IASL CAMO shall issue a workpackage with Weighing Record form and the weighing is carried out by IASL AMO or a suitably approved maintenance organisation and certified by amaintenance Certifying Staff. Based on the weighing record, IASL CAMO shallraise a new Basic Weight Change Record.

If the change to mass and balance is accurately known, in order to find the newbasic mass and moment of the aircraft, the mass and moment of the equipmentadded or removed shall be entered on the existing Basic Weight Change Record.

Based on the new or revised Basic Weight Change Record provided by IASLCAMO, Chief Pilot shall amend Operating Weight Empty (OWE) for eachconfiguration of aircraft.

New or revised Basic Weight Change Record and OWE shall be inserted in theWeight and Balance Manual kept onboard the aircraft and IASL CAMO Library.






1.13 Check Flight Procedures

Check flights are required under the following circumstances.

a) Specified by the aircraft manufacturer, for instance after a particularly extensivemaintenance check or major modification affecting the aircraft performance thatcannot be checked on the ground

b) Prior to issue of Certificate of Airworthiness

c) Subsequent to an engine change on a twin-engined aircraft

d) If deemed necessary by IASL AMO

Check flights shall be coordinated between IASL CAMO, IASL AMO and IASL FlightOperations.

1.13.1 Certification before Check Flight

IASL Approved Maintenance Organisation shall inspect aircraft, engines andequipment to determine whether aircraft is fit for flight.

On satisfactory completion of physical inspection and the documentation,including Certificate of Release to Service for the maintenance works performedon the aircraft, a ‘Certificate for Fitness for Flight’ shall be issued by IASL AMO. A sample of ‘Certificate for Fitness for Flight’ is given in Chapter 5 of this CAME.

1.13.2 Check Flight

Check flights shall be performed by IASL pilots in accordance with TypeCertificate holder’s check flight schedule or a schedule established by IASLFlight Operations and acceptable to IASL AMO and IASL CAMO.

To ensure that appropriate levels of safety are maintained, check flights shall beconducted by pilots who have satisfactory experience with the appropriate checkflight schedule, and have received adequate familiarisation of check flighttechniques and safety precautions. Director Flight Operations shall ensurecompliance with this requirement and assign pilots for check flights.

It is necessary that the pilot concerned fully understands the significance andintent of the tests, as well as the techniques used to minimise the risk associatedwith some tests.

IASL Check flights will only be performed by pilots listed as qualified by theDirector Flight Operations

On completion of the Check Flight the Commander shall complete the “FlightTest Certificate”. The Certificate shall include any defects arising from the CheckFlight and the same shall be entered in the Technical Log. Depending on theperformance of the Check Flight the Commander may request a further CheckFlight.

Check flight records shall be retained in accordance with CAME Part 1.3procedures.






1.13.3 Release to Service

Prior to the aircraft being placed into operation, all reported defects after themaintenance check flight must be rectified and the aircraft released to service byIASL AMO or suitably approved maintenance organisation in accordance withthe procedures described in CAME Part 1.1 and the requirements of MCAR-145.






1.14 Sample of Documents , Tags and Forms Used

The examples of documents and forms used by IASL CAMO are given in Part 5 of thisCAME.






1.15 Maintenance Data

Head of CAMO is responsible for provision, updating and control of maintenanceinstructions. Head of CAMO shall prepare a list of all applicable maintenance data,which are required to be maintained by IASL CAMO. The list shall be approved byHead of Safety and Quality and the list shall include the following details.

Publication Reference

Name of the Publication

Author of the Publication

Medium of Publication (Soft Copy or Hard Copy)

Status of Subscription Service

Location of the Publications

Frequency of revision status checks for ensuring that the publication is up-to-date

Applicable maintenance data is:

any applicable requirement, procedure, standard or information issued by CAA

any applicable Airworthiness Directive

applicable instructions for continuing airworthiness, issued by type certificateholders, supplementary type certificate holders and any other organisation thatpublishes such data in accordance with MCAR-21

Any applicable standard, such as but not limited to, maintenance standardpractices recognised by CAA as a good standard for maintenance

any applicable data issued in accordance with MCAR-145.45(d)

IASL CAMO is responsible for supplying maintenance data to IASL ApprovedMaintenance Organisation.

All applicable maintenance data shall be controlled and marked as such. Anyuncontrolled documents shall be labeled accordingly.

IASL CAMO shall ensure all applicable maintenance data are kept up-to-date and shallmaintain a publication inventory showing the revision status of all publications.

Manual Change Request form (Form/SQD/15) shall be used by IASL CAMO staff tonotify Head of Safety and Quality of any inaccurate, incomplete or ambiguousprocedure, practice, information or maintenance instructions found in the maintenance

data.






1.16 Documents to be carried onboard the Aircraft

The following up-to-date documents shall be carried onboard the aircraft in theCertificate File on each flight.

Documents Respons ible Person

Certificate of Registration (original copy) CAMO Staff

Certificate of Airworthiness (original copy) CAMO Staff Airworthiness Review Certificate (HSQ certified true copy) CAMO Staff

Insurance Certificate (HSQ certified true copy) CAMO Staff

Noise Certificate (original copy) CAMO Staff

Radio Licence (original copy) CAMO Staff

Maintenance Statement (includes CRS) CAMO Staff

Air Operator Certificate and Operations Specifications(CAA certified true copy)

Chief Pilot

A list of weight and balance licence holders Chief Pilot

A list of important contact details Chief Pilot

Appendix 1 to Chapter 11 (Mandatory OccurrenceReporting) of Safety Management Manual

Chief Pilot

Occurrence Report for Flight Crew (FORM/SQD/6) Chief Pilot

Occurrence Report for Flight Attendant (FORM/SQD/7) Chief PilotMedical Occurrence Report for Flight Attendant(FORM/SQD/11)

Chief Pilot

Hazard Report for all Staff (FORM/SQD/10) Chief Pilot

Platform Discrepancy Report (FORM/SQD/18) DHC-6 Chief Pilot

The following up-to-date manuals/logs/documents shall be carried onboard the aircrafton each flight.

Documents A320 A321

DHC-8 DHC-6 ResponsiblePerson

Technical Log x x x CAMO Staff

Cabin Log x x CAMO Staff

Operating Data Manual x CAMO Staff Aircraft Flight Manual x x CAMO Staff

Weight and Balance Manual x x x CAMO Staff

Quick Reference Handbook x x x CAMO Staff

FCOM x CAMO Staff

Minimum Equipment List (MEL) x x x Chief Pilot

Configuration Deviation List (CDL) x Chief Pilot

Part A of Flight Operations Manual x x x Chief Pilot

Part B of Flight Operations Manual x x x Chief Pilot

Part C of Flight Operations Manual x x x Chief Pilot

Cabin Crew Operating Manual(CCOM)

x Chief Pilot

Flight Deck Normal Checklist x x x Chief Pilot

Speed Card x x Chief Pilot

Airspeed Limitations Card x Chief Pilot

ICAO 9481 – Emergency ResponseGuide for Aircraft Incidents InvolvingDangerous Goods

x x Chief Pilot

Cabin Checklist / EmergencyProcedure

x x Cabin Crew inCharge

Flight Attendant Manual x x x Cabin Crew inCharge

Passenger Safety Card x x x Cabin Services






1.17 Extended Range Twin Engine Operations (ETOPS)

CAA has granted approval to IASL to operate A320 and A321 aircraft, over routes thatcontain a point further than 60 minutes but not exceeding the diversion times specified inthe table below at the approved one-engine inoperative cruise speed in accordance withETOPS procedures contained in the following manuals:

ETOPS Manual

OM Part A, Part B, Part C and Part D

A320/A321 MEL

A320/A321 AMP

Aircraft Type Diversion Time

A320 90 minutes

A321 90 minutes

IASL CAMO shall comply with the procedures included in the ETOPS Manual and across-reference of the procedures are given below.

AMC 20-6Reference

Subject ETOPS ManualReference

Appendix 8, 4(a) General description of ETOPS procedures Part 0, Part 1,Part 2

Appendix 8, 4(b) ETOPS maintenance programme developmentand amendment

Part 4.1

Appendix 8, 4(c) ETOPS reliability programme procedures

Appendix 8, 4(c)(1) Engine/APU oil consumption monitoring Part 9

Appendix 8, 4(c)(2) Engine/APU oil analysis Part 9

Appendix 8, 4(c)(3) Engine condition monitoring Part 10

Appendix 8, 4(c)(4) APU in-flight start programme Part 7.4

Appendix 8, 4(c)(5) Verification programme after maintenance Part 11

Appendix 8, 4(c)(6) Failures, malfunctions and defect reporting Part 7.2, 7.3,

Part 12 Appendix 8, 4(c)(7) Propulsion system monitoring/reporting Part 8.1

Appendix 8, 4(c)(8) ETOPS significant systems reliability Part 5, Part7.2(e)

Appendix 8, 4(d) Parts and configuration control programme Part 3

Appendix 8, 4(e) Maintenance procedures that includeprocedures to preclude identical errors beingapplied to multiple similar elements in anyETOPS significant system

Part 4.3, Appendix 1

Appendix 8, 4(f) Interface procedures with the ETOPSmaintenance contractor, including the operatorETOPS procedures that involve the

maintenance organisation and the specificrequirements of the contract

Part 4.2, 4.4,4.5, 4.6Part 13

Appendix 8, 4(g) Procedures to establish and control thecompetence of the personnel involved in thecontinuing airworthiness and maintenance ofthe ETOPS fleet

Part 14




PART 2 – QUALITY SYSTEM


PART 2

QUALITY SYSTEM






2.1 Continuing Airworthiness Quality Policy, Plan and Audit Procedures

This Part defines the continuing airworthiness quality policy, planning and proceduresto meet the requirements of MCAR-M Subpart G.

2.1.1 Continuing Airwor thiness Quality Policy

IASL has established an integrated Safety and Quality Management System,which covers the safety and quality requirements of the following approvalsheld by IASL:

Approval Type Approval No

Air Operator Certificate (AOC) 007

CAMO Approval MV.MG.001

MCAR-145 Approval MV.145.031

Aerodrome Certificate – Dharavandhoo Airport ADC/06/2012

Aerodrome Certificate – Ifuru Airport ADC/09/2015

Certificate of Authorisation – Thimarafushi Airport MCAA-AD-A006

The integrated Safety and Quality Management System is administered bySafety and Quality Department. Head of Safety and Quality is the designatedQuality Manager and Safety Manager for all the above approvals held byIASL, including IASL CAMO.

Safety Management System (SMS) procedures are contained in the SafetyManagement Manual.

Quality Management System (QMS) procedures for IASL CAMO aredescribed in Part 2 of this CAME. For QMS procedures of IASL AMO, refer toPart 3 of MOE.

IASL has established a common Safety and Quality Policy and it is given inChapter 4 of Safety Management Manual.

By its commitment to quality, the Accountable Manager (AM) through theresponsibility for Head of Safety and Quality of IASL, define and describe thequality goals and policies. Therefore the AM has the overall responsibility ofthe IASL QMS.

The QMS shall include a feedback system of the audit results to Head ofEngineering and AM.

The objectives of the QMS are:

Incorporate aviation safety management into all operational andmaintenance activities

Identify and eliminate potentially hazardous conditions

Ensure overall compliance with MCAR-M regulation and this CAME

Ensure that adequate procedures are in place and, the requiredstandards of continuing airworthiness management are achieved andmaintained






Ensure that contacted maintenance activities are carried out to therequired standards

To maintain compliance with MCAR-M and CAME, IASL Head of Safety andQuality (HSQ) shall monitor compliance of policies, procedures and operatinginstructions. The HSQ has an independent position in the organisation andreports directly to the AM. The HSQ shall not have any involvement in thedaily continuing airworthiness activities of the CAMO.

2.1.2 Quality Assurance Programme

The Quality Assurance Programme shall be developed by Head of Safety andQuality in liaison with Head of Engineering and Head of CAMO. The Head ofSafety and Quality shall implement an audit plan which during a twelve monthperiod will address all continuing airworthiness management activities and allof the aspects of MCAR-M which have a bearing on the continuingairworthiness arrangements of IASL, including sub-contracted activities.

The Quality Assurance Programme consists of:

Audit planning

Audits and inspections

Classification of findings

Initiation of corrective actions

Monitoring the implementation of corrective actions

Management review

Audits are performed on a sampling basis to verify all aspects of continuingairworthiness management activities of IASL CAMO, including samplesurveys of aircraft and those aspects of the individual aircraft’s continuingairworthiness. The auditor will not only check the main elements of the qualitysystem, but also check the work performed against the applicable

requirements and processes.

The quality audit plan is held by Head of Safety and Quality on Q-PulseSoftware. The annual audit plan for next year shall be sent, before 31st December of current year, to the Accountable Manager, Head of Engineeringand Head of CAMO.

2.1.3 Quality Audit Procedure

The primary purpose of the audit(s) shall be to observe, in an objectivefashion, a particular event/action/document etc. in order to verify whetherestablished operational and continuing airworthiness procedures and

requirements are followed during the accomplishment of a specific event witha view to ensuring that the required standard is being achieved.

2.1.3.1 Selection of Auditors

a) Every audit is undertaken by an audit team lead by a Lead Auditoror a single quality auditor (Lead Auditor) as part of the overall auditplan.






b) The auditors shall not have any day-to-day involvement in the areaof the activity which is to be audited. Independent audit of QMS ofIASL CAMO may be performed by an auditor who is not involvedin auditing CAMO activities.

c) Auditors report directly to Head of Safety and Quality.

2.1.3.2 Audit Notification

a) The selected auditor or audit team leader (lead auditor) shallinform the auditee of the audit date(s) and audit areas at least 5days prior to the audit.

b) For the purpose of carrying our spot checks or randominspections, Head of Safety and Quality may decide whether priornotification is not required for a particular audit.

2.1.3.3 Audi t Process

a) Audit preparation by auditor/audit team shall involve:

Studying the scope of the audit

Reviewing previous audit records

Reviewing changes in regulatory requirements, managementand activities of the organisation as well as negative trends

Collecting as much information as possible in the audit area(s)

Preparing and familiarising with audit checklists in accordancewith the following requirements:

Audit checklists are established in Q-Pulse Software and eachchecklist item shall be verified during audits and updated in Q-Pulse.

Audit checklists shall ensure to achieve the primary purpose ofthe audits given in this procedure and coverage of theapplicable MCAR-M requirements as well as all the relevantprocedures described in this CAME. To ensure traceability ofindividual audit questions to the respective regulatory andinternal requirements, the corresponding references shall be

listed in the audit checklists.






b) The following structure is recommended for use during audits.

c) Lead Auditor shall prepare an audit report on Q-Pulse Software.The audit report shall include at least the following information.

Audit scope

Audit date(s)

Name of auditor(s) and auditee(s)

Audit findings

Observations

d) Audit findings or non-compliances will be categorised as follows:

Level 1 – Means a critical non-compliance and is justified if:

Procedure is missing and may affect safety of operation;

Total lack of mastering the procedures, which consequentlymay be detrimental to the safety of operation;

The mastering of the procedures presents shortcomingsand the procedure itself is not adequate.






Level 2 – Means a major shortcoming more localised and is justified if:

The procedure is missing but is not detrimental to safety ofoperation;

The procedure established represents shortcomings butthey are not critical to safety.

Level 3 – Means a minor shortcoming and is justified if:

Putting in place a new procedure or instruction to clarify theexisting system;

The procedure is valid itself but minor shortcomings maybe corrected to clarify the procedure.

e) Lead Auditor shall discuss the audit findings and observations withHead of Engineering and Auditees, and finalise the audit report onQ-Pulse Software within 5 working days from the date ofcompletion of the audit.

f) The audit reports are distributed to the following persons:

The person responsible for the audited area

Accountable Manager

Head of Engineering

Head of CAMO

2.1.4 Quality Audit Remedial Act ion Procedure

a) Once the audit report has been accepted, auditee shall enter proposedcorrective action with target date under ‘Root cause and Corrective Actions’ stage of the Finding Form in Q-Pulse Software within 7 workingdays from the date of completion of the audit report on Q-Pulse Software.

The corrective action plan should be determined taking into account theroot cause of the finding, such that the corrective action may be carriedout in a fashion that will prevent possible re-occurrence of the finding.

b) The corrective action plan shall be acceptable to Lead Auditor and Headof Safety and Quality.

c) The maximum time allowed for taking corrective actions to differentcategories of audit findings are as follows:

Audit Finding Category Time Limit

Level 1 Immediate corrective action shall betaken

Level 2 Initial time allowed for completion ofcorrection action shall not exceed 3months. If the auditee requests formore time, Lead Auditor may give anextension not exceeding 2 months,provided that a safety assessmenthas been carried out to ensure thatthe safety risks are at an acceptablelevel and there are valid reasons forthe extension






Level 3 As defined in the corrective actionplan

d) The auditee is responsible for ensuring that appropriate corrective actionmeasures are implemented in accordance with the corrective action plan.

e) It is the responsibility of the Accountable Manager to allocate sufficientresources for the implementation of corrective actions.

f) Lead Auditor shall regularly check the status of all open findings andverify that appropriate corrective actions have been implemented and thatthe corrective actions have re-established compliance with the applicablerequirements.

g) In case, the Lead Auditor has concluded that the auditee has failed totake appropriate corrective actions within the given deadline, this shall bereported in writing to Head of Engineering before the case(s) is referred tothe Accountable Manager by Head of Safety and Quality. If the Head ofEngineering also fails to ensure completion of appropriate correctiveactions, it will be responsibility of the Accountable Manager to ensure

immediate corrective action is taken.

h) When all findings have been closed, the Lead Auditor shall close the auditreport.

2.1.5 Audi t Records

Audit reports shall be retained for a period of 5 years.

2.1.6 Management Review

The Accountable Manager shall hold a management review meeting withHead of Safety and Quality and Head of Engineering at least every six

months.

a) The management review shall consider:

The results of quality inspections, audits and any other indicators

The overall effectiveness of the management organisation inachieving stated objectives

b) Management review shall identify and correct trends, and prevent, wherepossible, further non-conformities.

c) Conclusions, actions and recommendations made as a result of

management review shall be submitted in writing to the responsibleperson for corrective action. Head of Safety and Quality shall monitor theimplementation of required corrective actions.






2.2 Monitoring of Continuing Airworthiness Management Activ ities

The Quality Audit Plan includes an assessment of the Continuing AirworthinessManagement activities against the procedures defined in the CAME and in particularthe ability of the maintenance management personnel to discharge theirresponsibilities effectively with respect to MCAR-M.

The periodical audits of IASL CAMO’s continuing airworthiness management activitiesshall be performed by IASL Safety and Quality Department and as determined by Headof Safety and Quality.

Compliance with CAME and MCAR-M requirements shall be verified by auditing ofprocedures, resources, methods and forms.






2.3 Monitoring of the Effectiveness of the Maintenance Programme

The HSQ shall have an oversight of the implemented AMPs and their effectiveness.The Quality Audit Plan as carried out by the Head of Safety and Quality includes areview of the effectiveness of the AMP. This review will critically analyse the findingsand actions taken as a result of Para. 1.5 of this CAME. If required, HSQ shall adviseIASL CAMO to make required improvements to the AMPs.

In order to satisfy the responsibility for the effectiveness of AMPs, the Head ofEngineering shall attend the periodical liaison meetings referenced in CAME Part 1.5.HSQ shall also participate in such meetings; monitor the process and performance ofIASL CAMO and IASL AMO.

IASL CAMO shall ensure that AMPs maintain the inherent safety and reliability ofaircraft operated by IASL.






2.4 Monitoring that all Maintenance is carried out by an appropriately ApprovedMCAR-145 Organisation

The Quality Audit Plan includes verification that the contracted MCAR-145maintenance organisation's approval granted by CAA or approvals held by contractedmaintenance organisations acceptable to CAA are relevant to the maintenance beingperformed on the aircraft operated by IASL. This verification shall critically analyseapproval schedule of contracted maintenance organisations, including IASL AMO andshall provide evidence that the scope of approval and privileges of all the contractedmaintenance organisations correspond with the current scope of maintenance activitiesrequired by IASL.

In addition, annual audits of IASL AMO performed by the Safety and QualityDepartment shall verify whether IASL AMO has adequate facilities, personnel,equipment, tools, material, maintenance data, safety and quality procedures, andcapacity to undertake the maintenance support required by IASL CAMO.

In the case of maintenance to be contracted to a third party MCAR-145 maintenanceorganisation or a suitably approved maintenance organisation, IASL CAMO shall notify

HSQ of such arrangements sufficiently in advance. HSQ shall liaise with themaintenance organisation and ensure compliance with procedures given in Part 2 ofthis CAME.

Any feedback information requiring amendments to the maintenance contracts foraircraft, engines or components should be reviewed and the contracts amendedaccordingly.






2.5 Monitoring that all Contracted Maintenance is carried out in accordance with theContract, including Sub-contractors used by the Maintenance Contractor

Audit of all contracted maintenance activities is included in the Quality Audit Plan.This audit will assess whether only organisations listed in the ‘List of ApprovedContractors’ and ‘List of Approved Sub-Contractors’ in Part 5 of this CAME are used byIASL CAMO for contracted maintenance and contracted maintenance activities arecarried out in accordance with the maintenance contracts.

The ultimate responsibility for the maintenance services provided by contractedmaintenance organisations, including sub-contractors, remains with IASL CAMO andHead of Engineering.

The Quality Audit Plan shall ensure that all organisations listed in the ‘List of ApprovedSub-Contractors’ are audited once every year.

Head of Safety and Quality shall ensure that IASL CAMO only uses sub-contractorslisted on CAMO Approval Certificate (CAA Form 14).






2.6 Quality Audit Personnel

Accountable Manager shall ensure that always sufficient suitably qualified, trained andexperienced quality personnel are available to ensure compliance with therequirements of Quality Management System of IASL CAMO.

Audits of IASL CAMO and contractors in accordance with the annual audit plan arecarried out by quality personnel of IASL Safety and Quality Department. IASL does nothave any contracted quality personnel.

All quality audit personnel shall meet the following basic criteria:

a) Completed basic AME Course or aeronautical degree or equivalentb) Two years of continuing airworthiness experiencec) Completed induction training and continuation training in accordance with the

requirements of Para 0.3.6.2d) Completed SMS training in accordance with the requirements of Safety

Management Manuale) Completed aircraft type training at least to a level equivalent to MCAR-66

Appendix III Level 1 general familiarization. Each auditor should have undergoneat least one type training course on a type operated by IASL. Between all theauditors, completed type training should cover all the types operated by IASL.

f) Completed initial audit training.g) Auditors shall undergo quality related continuation training once every 2 years.h) Completed three audits under the supervision of a qualified auditor.

Quality audit personnel are authorised to perform quality audits upon meeting theabove criteria and completion of satisfactory competency assessment in accordancewith Para 2.6.1 of this CAME.

Quality audit personnel must not be directly involved in the activity they have beenasked to audit.

Records of Audit Personnel shall be kept by Head of Safety and Quality.

2.6.1 Competence Assessment

Competency assessment of quality audit personnel shall be performed inaccordance with the requirements given below:

Job Title Responsible person forconducting the assessment

Airworthiness Inspectors Head of Safety and Quality

Head of Safety and Quality Accountable Manager

The initial competency assessment of each staff shall be performed within 6months of joining the organisation. Following satisfactory completion of initialcompetency assessment, additional competency assessments shall be carriedout once every two years.

If a staff receives an unsatisfactory result in competency assessment, followingactions shall be taken based on the performance of the staff:

Work performed by the staff to be closely supervised by a competent staff






Assist the staff to comply with the required standards and arrange to carryout a competency assessment of the staff within a reasonable time period

For each job title, Head of Safety and Quality shall prepare a Competency Assessment Check Sheet and it shall include the requirements given in thefollowing table:

H e a d o f S a f e t y

a n d Q u a l i t y

A i r w o r t h i n e s s

I n s p e c t o r

Knowledge of quality system and auditing techniques; planning,conducting and reporting

X X

Knowledge of human factors, human performance andlimitations

X X

Knowledge of organisation capabilities, privileges and limitations X X

Knowledge of MCAR-M, MCAR-145 and any other relevantregulations

X X

Knowledge of IASL MOE, IASL CAME, SMM, AMPs, officiallyrecognised standards and procedures

X X

Knowledge of safety management system and occurrencereporting system

X X

Knowledge of investigation techniques X X

Knowledge of safety risks linked to the working environment X X

Knowledge on CDCCL when relevant X XKnowledge on EWIS when relevant X XUnderstanding of professional integrity, behaviour andattitude towards safety

X X

Understanding of conditions for ensuring continuing

airworthiness of aircraft and components

X X

Understanding of his/her own human performance andlimitations

X X

Understanding of personnel authorisations and limitations ofmaintenance organisations

X X

Understanding critical task X X Ability to consider human performance and limitations X X Ability to identify and rectify existing and potential unsafeconditions

X X

Ability to promote the safety and quality policy X X Ability to understand work packages, task cards and refer to anduse applicable maintenance data

X X

Ability to use information systems and software X X Ability to identify required tooling, equipment and spare parts forplanned maintenance

X X

Ability to identify applicable Airworthiness Directives, ServiceBulletins and implementation procedures

X X

Ability to draft procedures, manuals and review for compliance withapplicable regulatory requirements

X X

Ability to prepare investigation reports X X Adequate communication and literacy skills X XTeamwork, decision-making and leadership skills X XResources management and planning skills X






2.7 CAMO Personnel

2.7.1 Competency Assessment of CAMO Personnel

Competency assessment of IASL CAMO staff shall be performed in accordancewith the requirements given below:


Planner Head of CAMO

Technical Service Engineer Head of CAMO

Head of CAMO Head of Engineering

Head of Engineering Accountable Manager

The initial competency assessment of each staff shall be performed within 6months of joining the organisation. Following satisfactory completion of initialcompetency assessment, additional competency assessments shall be carriedout once every two years.




For each job title, CAMO shall prepare a Competency Assessment Check Sheetand it shall include the requirements given in the following table:

H e a d o f

E n g i n e e r i n g

H e a d o f C A M

O

T e c h n i c a l

S e r v i c e E n g i n e e r

P l a n n e r

Knowledge of human factors, human performanceand limitations

X X X X

Knowledge of logistics processes X X X X

Knowledge of organisation capabilities, privilegesand limitations

X X X X

Knowledge of MCAR-M, MCAR-145 and any otherrelevant regulations

X X X X

Knowledge of IASL MOE, SMM, AMPs, IASL CAMEand procedures

X X X X

Knowledge of occurrence reporting system andunderstanding of the importance of reportingoccurrences, incorrect maintenance data andexisting or potential defects

X X X X

Knowledge of safety risks linked to the workingenvironment

X X X X






H

e a d o f

E

n g i n e e r i n g

H

e a d o f C A M O

T

e c h n i c a l

S

e r v i c e E n g i n e e r

P

l a n n e r

Knowledge on CDCCL when relevant X X X XKnowledge on EWIS when relevant X X X XUnderstanding of professional integrity, behaviour andattitude towards safety

X X X X

Understanding of conditions for ensuring continuingairworthiness of aircraft and components

X X X X

Understanding of his/her own human performance andlimitations

X X X X

Understanding of personnel authorisations andlimitations of maintenance organisations

X X X X

Understanding critical task X X X X Ability to use AMP, compile and control completed work

packages

X X X

Ability to consider human performance and limitations X X X X Ability to determine required maintenance qualificationsfor task performance

X X X

Ability to identify approved maintenance contractorsand subcontractors, and co-ordinate contractedmaintenance activities

X X X X

Ability to identify and properly plan performance ofcritical task

X X X

Ability to prioritise tasks and report discrepancies X X X Ability to promote the safety and quality policy X X X Ability to properly process component replacements X X X Ability to properly record work accomplished and

manage continuing airworthiness recordsX X X

Ability to split complex maintenance tasks into clearstages

X X X

Ability to use maintenance data andinformation/software systems required for continuingairworthiness activities

X X X X

Ability to prepare maintenance program and analyseeffectiveness of the maintenance program

X X

Ability to identify required tooling, equipment and spareparts for planned maintenance

X X X X

Ability to identify applicable Airworthiness Directives,Service Bulletins and implementation procedures

X X X X

Knowledge of approved modifications and repairs and

able to prepare documentation for approval ofmodifications and repairs

X X

Adequate communication and literacy skills X X X XResources management and production planning skills X X X XTeamwork, decision-making and leadership skills X X X Ability to meet safety and quality targets X X






2.7.2 Issuing of Approval Stamp to CAMO Personnel

Head of CAMO shall arrange to assess competency of CAMO personnel within 6months of joining IASL CAMO and send completed Staff Competency Assessment Check Sheet to Head of Safety and Quality for issue of approvalstamp.

Head of Safety and Quality shall issue an approval stamp to CAMO personnelmeeting the following criteria. The approval stamp is required to workindependently and wherever signature of CAMO personnel is required oncontinuing airworthiness records, the approval stamp shall be used by CAMOpersonnel.

a) Meets basic qualification requirements for the job given in SOP201.

b) Successfully completed induction training and continuation training inaccordance with Para 0.3.5.2 of this CAME.

c) Recommendation issued by Head of CAMO on Competency Assessment

Check Sheet.

d) Pass an assessment conducted by Head of Safety and Quality. This isintended to assess the knowledge of the applicant on applicable regulationsincluding MCAR-M and MCAR-145, CAME, SOP’s and any other relevantareas.

In order to maintain the validity of the approval, Head of CAMO shall arrange toassess competency of CAMO personnel once every two years and sendcompleted ‘Competency Assessment Check Sheet’ to Head of Safety andQuality.






2.8 Training Personnel

2.8.1 Competency Assessment of Training Personnel

Competency assessment of IASL training staff shall be performed in accordancewith the requirements given below:


Head of Technical Training Head of Engineering

Instructors Head of Technical Training

The initial competency assessment of each staff shall be performed within 6months of joining the organisation or prior to appointment as an Instructor.Following satisfactory completion of initial competency assessment, additionalcompetency assessments shall be carried out once every two years.




For each job title, Head of Technical Training shall prepare a Competency Assessment Check Sheet and it shall include the requirements given in thefollowing table:

H e a d o f T e

c h n i c a l

T r a i n i n g

I n s t r u c t o r

Knowledge of human factors, human performance and limitations X X

Knowledge of safety management system X X

Knowledge of organisation capabilities, privileges and limitations X X

Knowledge of IASL MOE, IASL CAME, SMM, AMPs andprocedures

X X

Knowledge of occurrence reporting system and understanding ofthe importance of reporting occurrences, incorrect maintenancedata and existing or potential defects

X X

Knowledge of safety risks linked to the working environment X X

Knowledge on CDCCL and EWIS when relevant X X

Detailed knowledge of training subject X XUnderstanding of professional integrity, behaviour and attitudetowards safety

X X

Understanding of conditions for ensuring continuing airworthiness ofaircraft and components

X X

Understanding of his/her own human performance and limitations X XUnderstanding of personnel authorisations and limitations ofmaintenance organisations

X X






H e a d o f T e c h n i c a l

T r a i n

i n g

I n s t r u c t o r

Understanding critical tasks X X Ability to promote the safety and quality policy X X Ability to understand work packages, task cards, and refer to and useapplicable maintenance data

X X

Ability to identify required tooling, equipment and spare parts forplanned maintenance

X X

Ability to use information systems and software X X Ability to identify applicable Airworthiness Directives, Service Bulletinsand implementation procedures

X X

Ability to create course outlines for training programmes X X

Ability to apply principles of adult learning X X Ability to implement common instructional methods and aids X X Ability to recognise and manage classroom problems X X Ability to assess learners and provide feedback X X Ability to identify and overcome barriers to the transfer of learning X X Ability to demonstrate effective instruction and facilitation X X Adequate communication and literacy skills X XResources management and planning skills X XTeamwork, decision-making and leadership skills X X Ability to select the best training activities to improve the safety andquality standards of the organisation and effectiveness of training

X

Ability to carry out training needs assessment X Ability to implement the annual training programme X

Ability to meet safety and quality targets X




PART 3 – CONTRACTED MAINTENANCE


PART 3

CONTRACTED MAINTENANCE






3.0 Contracted Maintenance

This Part applies to maintenance contracts of IASL CAMO that include basemaintenance, line maintenance and engine shop maintenance and componentmaintenance, as applicable, whilst installed on aircraft. Both the scope of work andassignment of responsibilities should be clear and unambiguous with sufficient detail toensure that no misunderstanding could arise between the parties concerned.

All maintenance details in the contract must at least address those main points asspecified in the current Appendix XI to AMC to MCAR-M.708(c).

In the event that no valid maintenance contract is available for particular linemaintenance tasks (scheduled or unscheduled), the applicable MCAR-145 organisationmay be given the order to carry out the tasks by means of a formal work order issued byIASL CAMO.

In the event that no valid maintenance contract is available for particular componentmaintenance tasks (scheduled or unscheduled), the applicable maintenanceorganisation may be given the order to carry out the tasks by means of a formal work

order issued by IASL CAMO.

Aircraft and components shall only be sent for maintenance to contractors which arelisted under Para 5.1.24.

3.1 Maintenance Contractor Selection Procedure

a) Before any maintenance organisation is selected or a contract is signed with amaintenance organisation, Head of Engineering shall verify that:

i) Maintenance organisation has the necessary qualified manpower, facilities,tooling, technical documentation etc. This verification to take into account anyengine, propeller, or component maintenance capability that may be required

(though this may be available through sub-contract to other suitably approvedmaintenance organisation)

ii) In case of base maintenance and scheduled line maintenance of aircraft, andmaintenance of components listed below, whether the maintenance organisationis appropriately approved in accordance with MCAR-145 or the maintenanceorganisation is owned (fully or partially) by the Original Equipment Manufacturer(OEM).

Engines

APU

Propellers

Landing Gear

For all other maintenance, the maintenance organisation shall be OEM (includesorganisations owned by OEM) and/or shall hold an approval from any of thefollowing national aviation authorities.

CAA (MCAR 145 Approval)

EASA or EASA member country (EASA145 Approval)

FAA (FAR 145 Approval)

Transport Canada (TCCA)






iii) It shall be confirmed that the maintenance organisation has adequate capacity toundertake the proposed maintenance support. Where this includes aspects ofcontinuing airworthiness management then experience shall form part of thecriteria to be considered.

iv) The Maintenance Contract meets the requirements of MCAR-M.

v) In case of base maintenance and scheduled line maintenance of aircraft, theMaintenance Contract includes a requirement for the Maintenance Contractor toreport to IASL, of any identified condition of the aircraft that hazards seriously theflight safety.

vi) The Maintenance Contract shall be reviewed and agreed by both parties with aview to ensuring that each has the ability to discharge their responsibilities withrespect to MCAR-M.

vii) A visit of a representative of IASL CAMO and/or audit by IASL CAMO QualitySystem may be part of the selection procedures to assure compliance withMCAR-145 and IASL CAMO requirements.

b) Head of Engineering shall consult Head of Safety and Quality and obtain his writtenagreement before signing the contract.

c) Once the selection process has been completed and agreement(s) executed, Headof Engineering shall forward the details of the selected maintenance organisation,including a copy of maintenance contract, MOE and approval certificates to Head ofSafety and Quality for his records. Head of Engineering shall be responsible formaintaining original copies of Maintenance Contracts.

d) Once the internal selection process has been completed, Head of Safety and Qualityshall amend CAME Para 5.1.24 (List of Approved Contractors) and obtain CAA Approval for the CAME Amendment.

e) Once the selection process is over, Head of Procurement and Logistics shall manageall contracted maintenance as per the terms and conditions of the executedcontract(s).

3.1.1 Advising the CAA of Changes to the Maintenance Support

The CAA will be advised of any proposed continuing airworthiness managementarrangements in writing giving the notice required by MCAR-M Subpart G.

Changes to nominated Maintenance Contractors for base maintenance andscheduled line maintenance of aircraft, shall be advised to CAA in writing giving 10calendar days notice. In the case of arrangements for unscheduled line or base

maintenance, CAA shall be notified as soon as possible.

Prior to establishing base maintenance, schedule maintenance and enginemaintenance contracts and contracts with sub-contractors, IASL CAMO shallobtain CAA approval for technical contents of the contract. Once the contract hasbeen executed, Head of Safety and Quality shall provide a copy of the technicalcontents of the contract to CAA.






3.2 Detailed List of Maintenance Contractors

This list is given under CAME Para 5.1.24.

3.3 Relevant Technical Procedures identified in the Maintenance Contract(s)

The relevant maintenance procedures are included in the Maintenance Contracts.

3.4 Quality Aud it of Aircraft

Following completion of base maintenance activities by a contracted maintenanceorganisation, Head of CAMO or other representative appointed by Head of Engineeringshall verify the following on IASL Form:

a) All maintenance have been carried out by or through a maintenance organisationlisted in the ‘List of Approved Contractors’.

b) Check the work performed as indicated on the Certificate of Release to Service(CRS) or in the document referenced by the CRS against the contents of the

work order and ensure that all work, which has been ordered has beenperformed.

c) Check the CRS for proper completion, e.g. the maintenance organisation's nameis the same as on the work order, the organisation's approval number is indicatedand any references to a work order, maintenance program and inspection reportare correct and that the aircraft details (type, serial number and registration,aircraft hours, cycles and the date) are entered and correct.

d) Any Deferred Defect items which were ordered but not performed or defectfindings that could not be closed shall be checked against the approved MEL forthe aircraft and entered on the Deferred Defect log.

e) Check for any structural repairs performed during the maintenance visit, therepair status (permanent or temporary), their validity and their approval (SRM orother maintenance data).

f) Check any Airworthiness Directives performed during the maintenance visit forincorporation in accordance with the selected means of compliance (inspection ormodification) as stated in the work order.

g) Check aircraft physically for obvious conditions.

h) For every serialised component installed: Part Number, Serial Number and CRSis available.

i) All relevant maintenance records have been signed off/stamped and completelyreceived from the Maintenance Organisation.

j) CRS issued by the Maintenance Organisation received prior to first flight aftermaintenance.

If the above items are acceptable, the assigned person may proceed with acceptance ofthe aircraft by signing for acceptance on IASL Form.






If in doubt, or if any of the items found unacceptable, the assigned person shall consultthe Head of Engineering in order to obtain his (temporary) acceptance or to requestcorrective action by the maintenance organisation.

When the aircraft has been accepted, the completed IASL Form must be sent to theHead of Engineering and Head of CAMO. The Head of CAMO shall perform any of thefollowing follow-up actions as applicable:

Check or prepare a new maintenance statement, which shall indicate when thenext base maintenance event will be due (date, flight hours and/or flight cycles,as applicable)

Ensure that all open acceptance items which were accepted temporarily areclosed

Ensure that all maintenance records are updated

Ensure that components (including life Iimited parts) records are up dated

Ensure AD and SB records are updated

Ensure that the Deferred Defect list is updated

Ensure that recurrent maintenance requirements are re-scheduled for nextcompliance

After the Head of CAMO has ensured that all items have been satisfactory performed, heshall sign the IASL Form for closure and file it with the aircraft records.

Head of Safety and Quality shall monitor contracted maintenance in accordance withPara 2.5 of this CAME.




PART 4 – AIRWORTHINSS REVIEW PROCEDURES


PART 4

AIRWORTHINESS REVIEW PROCEDURES




PART 4 – AIRWORTHINSS REVIEW PROCEDURES


4.0 Introduction

IASL CAMO is not approved by CAA to perform airworthiness reviews.

IASL CAMO has been approved by CAA to extend the validity of Airworthiness ReviewCertificate (ARC) in accordance with the procedure given in Para 1.11.8 of this CAME.

Prior to extending the validity of ARC, a full documented review of aircraft records andphysical survey of aircraft is performed by Airworthiness Review Staff listed in Para0.3.5 of this CAME in accordance with IASL SOP-SQ 006, with a view of obtaining CAAapproval for performing airworthiness reviews in accordance with requirements ofMCAR-M.710.




PART 5 – APPENDICES


PART 5

APPENDICES






5.1 Sample Documents

5.1.1 Technical Log Book

5.1.1.1 Cover Page






5.1.1.2 Notice to Flight and Maintenance Crew






5.1.1.3 Notice to Fligh t and Maintenance Crew Log Transfer Record






5.1.1.4 Deferred Items Log






5.1.1.5 Deferred Items Log Transfer Record






5.1.1.6 Non-Airworth iness Deferred Items Log






5.1.1.7 Non-Airworth iness Deferred Items Log Transfer Record






5.1.1.8 Technical Log Page

5.1.1.8.1 DHC-8 and DHC-6 Aircraft






5.1.1.8.2 A320 and A321 Aircraft






5.1.2 DHC-8-200/300 Pre-Fligh t Checklist






5.1.3 Non Destructive Test Report






5.1.4 Engineering Delay Report






5.1.5 Airw orth iness Review Report (reserved)

5.1.6 AD/SB Compl iance Form






5.1.7 CAA Concess ion Request Form






5.1.8 In-House Concession Request Form






5.1.9 Purchase Order






5.1.10 Repair Order






5.1.11 Compass Swing Record






5.1.12 Pre-Weighing Check L ist (DHC-8 Aircraft)






5.1.13 Weighing Record (DHC-8 Airc raft)






5.1.14 Basic Weight Change Record






5.1.15 CAA Form 1






5.1.16 EASA Form 1






5.1.17 FAA Form 8130-3






5.1.18 Work Package

5.1.18.1 Work Package Sheet (Cover Page)






5.1.18.2 Task Card






5.1.18.3 Maintenance Statement






5.1.19 Non-Routine Task Card (NRTC)






5.1.20 Removal / Installation Record Card






5.1.21 Certif icate of Fitness for Flight






5.1.22 Flight Test Certificate






5.1.23 List o f Airworthiness Review Staff

Refer to CAME 0.3.3.






5.1.24 List of Approved Contractors

Name of the Contractor Address Maintenance Arrangements Aircraft & Component MROB. V

EindhovenThe Netherlands

Maintenance of A320 and DHC-8Wheels and Brakes

Aircraft MaintenanceSriLankan Airlines

KatunayakeSri Lanka

A320 aircraft maintenance, repairand management of A320

components

Air Works India Engineering HosurIndia

A320 aircraft maintenance, repairand management of A320components

AMETEK Singapore Repair and management ofaircraft components

Aventure Aviation GeorgiaUSA

Repair and management ofaircraft components

Fokker Services AN Oude MeerThe Netherlands


GKN Aerospace TrollhattenSweden

HSI and Overhaul of PW123Engines

Global AerospaceCorporation

OntarioCanada


Hamilton SundstrandCorporation

MaastrichtThe Netherlands

CaliforniaUSA

DHC-8 propeller maintenance

DHC-8 APU maintenance

Honeywell Aerospace Various Locations Repair and management ofaircraft components

Kenn Borek Air CalgaryCanada

Repair and maintenance of DHC-6 components

Lufthansa Technik HamburgGermany

Repair and management of A320components

Messier Services SAFRANGroup

Singapore DHC-8 landing gear maintenance

MSI Aircraft MaintenanceServices

RusselsheimGermany


MTU Maintenance Zhuhai ZhuhaiChina

Repair and maintenance of CFM56-5B engines and enginecomponents

NedAero Components B.V ZevenaarThe Netherlands


Pratt & Whitney Canada Singapore HSI and Overhaul of PW123Engines

Prime Turbines BudenheimGermany

Repair and maintenance of DHC-8 fuel nozzles

Revima APU Caudebec-en-cauxFrance

DHC-8 APU maintenance

Rockwell Collins Various Locations Repair and maintenance of

avionic componentsRuag Aerospace MunichGermany


ST Aerospace Engineering Singapore NDT tasks

Vector Aerospace EngineServices

PEICanada

Repair and maintenance of PT6-27 engines and enginecomponents

W H Brennan & Co Singapore Repair and management of life jackets






5.1.25 List o f Approved Sub-Contractors

Name of the Sub-Contractor

Address Maintenance Arrangements

Danish Engine Trend Analysing (DETA)

Sindal, Denmark ECTM of PW123Engines

CFM International - ECTM of CFM56-5BEngines

Head of Engineering is responsible for maintaining original copies of contracts signedbetween IASL and Sub-Contractors.






5.1.26 Contracts with Approved Maintenance Organisations

All the contracts with Approved Maintenance Organizations are held with Head ofEngineering. The contracts would be available to CAA authorised personnel uponrequest.

Head of Safety and Quality shall provide a copy of the technical contents of contracts

to CAA.






5.1.27 Manual Change Request






5.1.28 DHC-6 Pre-Flight Checkl ist

CAME - Amnd 10 - Approved

Documents

Transcript of CAME - Amnd 10 - Approved