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PAWAN HANS HELICOPTERS

CONTINUING AIRWORTHINESS

MANAGEMENT EXPOSITION (CAME)

Corporate Office - Pawan Hans Helicopters Ltd Corporate Office Safdarjung Airport New Delhi – 110003 Fax :91- 011-24602596 011-24611801

Western Region- Pawan Hans Helicopters Ltd Northern Region - Pawan Hans Helicopters Ltd Western Region Northern Region Juhu Airport, S.V. Road Safdarjung Airport Vile Parle (W) New Delhi – 110003 Mumbai – 400056 Fax: 011 - 24611801 Fax : 022-26117339 022-26186926

PAWAN HANS HELICOPTERS LIMITED CAME

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APPROVAL PAGE PAGE NO. i

Approval Page:

CAR M approval In Sub Part G by:

Director of Airworthiness NR (DAW, NR)

Vide Letter no: DDG/NR/MG. 005(REF. NSOP 02/1998)

Dated: 29th July 2010


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TABLE OF CONTENTS PAGE NO. ii

INTRODUCTION Page No

Approval Page i

Table Of Contents ii-iii

List of Effective Pages iv

Para wise Index v-ix

Amendment x

Distribution List xi - xii

Abbreviation Used xiii

PART 0 GENERAL PAWAN HANS ORGANISATION 0.1 Corporate Commitment by the Accountable Manager 1

0.2 General PHHL Information 2-5

0.3 Management Personnel 6-11

0.4 Management Organisation chart 12-13

0.5 Notification Procedure to the DGCA Regarding Changes to the Operator‟s Continuing Airworthiness Management Organisation

14

0.6 Continuing Airworthiness Management Exposition Amendment Procedure 14-15

0.7 Facilities 15

PART 1 CONTINUING AIRWORTHINESS MANAGEMENT PROCEDURE

1.0 Continuing Airworthiness Management Procedure 01

1.1 Aircraft Flight log Utilisation & MEL Application List 01-05

1.2 Aircraft Maintenance Program General PHHL 05-10

1.3 Time & Continuing Airworthiness Record: Responsibilities, Retention & Access 10-11

1.4 Accomplishment and control of Mandatory Requirements for Airworthiness 11-13

1.5 Analysis of the Effectiveness of the Maintenance Programme 13-14

1.6 Non-Mandatory Changes (Modification) Embodiment Policy 14-15

1.7 Major Change (Modification) Standards 15

1.8 Defect Reports 15-19

1.9 Engineering Activity 19

1.10 Reliability Programmes 19-20

1.11 Daily/Pre-flight / Relevant Inspection 20-22

1.12 Aircraft Weighing 22

1.13 Test Flight Procedure 22

1.14Sample of Documents, Tags and Forms Used 23

1.15 Leasing of Aircraft 23

1.16 General PHHL Procedures(inc Operational Approval Procedures) 23

1.17 CVR/ DFDR Readout Policy 23

1.18 Materials Auditor/ Stores Inspector 23

PART 2 QUALITY SYSTEM 2.1 Continuing Airworthiness Quality Policy, Plan and Audit Procedures 01-03

2.2 Monitoring of Continuing Airworthiness Management Activities 04

2.3 Monitoring the Effectiveness of the Maintenance Program 04

2.4 Monitoring that all maintenance is carried out by an appropriately approved Part 145 Organisation

04

2.5 Monitoring that all Contracted Maintenance is Carried Out in Accordance with the Contract, including Sub-contractors used by the Maintenance Contractor

04

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TABLE OF CONTENTS PAGE NO. iii

PART 3 CONTRACTED MAINTENANCE

3.0 Contracted Maintenance 01

3.1 Maintenance Contractor Selection Procedure 01

3.2 Detailed List of Maintenance Contractors 01

3.3 Relevant Technical Procedures Identified in the Maintenance Contract(s) 02

3.4 Aircraft Operated 02

3.5 Quality Audit of Sub Contracted CAR tasks 02

3.6 Procedure for awarding work to Sub-contractors 03

PART 4 AIRWORTHINESS REVIEW PROCEDURES 4.1 Airworthiness review staff 01-02

4.2 Airworthiness Review General PHHL Procedure 02

4.3 Review of Aircraft Records 02

4.4 Physical Survey 02

4.5 Aircraft Airworthiness Review Documentation 03-05

4.6 Recommendations to competent authorities for the issue of an ARC 05

4.7 Issuance of ARC 06-08

4.8 Airworthiness Review Records, Responsibilities, Retention & Access 08

PART 5 APPENDICES 5.1 List of Appendices –Sample of Documents 01

Appendix 1.1 - Sector Record Page/ Tech log Page/ Flight report Page(Dauphin SA365N H/C ) 02

Appendix 1.2 - Sector Record Page/ Tech log Page/ Flight report Page(Dauphin AS365N3 H/C) 03

Appendix 1.3 - Sector Record Page/ Tech log Page/ Flight report Page (MI-172 Helicopter) 04

Appendix 1.4. - Sector Record Page/ Tech log Page/ Flight report Page (Bell Helicopter) 05

Appendix 1.5 - Sector Record Page/ Tech log Page/ Flight report Page ( Ecureuil Helicopter) 06

Appendix 2. CRS 07

Appendix 3 - Audit Plan – PHHL‟s CAMO Quality System 08-10

5.2 Airworthiness Review Staff 11

5.2.1 Northern Region 11

5.2.2 Western Region 12

5.3 Appendix 4 - - List of Approved 145 Maintenance Organisation sub Contracted 13-16

5.4 NOT APPLICABLE -



5.7 Appendix 5 – Airworthiness Review Report 17-20

5.8 REVIEW CERTIFICATE -PHHL NOT AUTHORISED -

5.9 Compliance checklist- enclosed -

5.10 Appendix 6 : Details of Aircraft Managed by Organization 21

Page No

2.6 Quality Audit Personnel 05-06

2.7 Quality Audit of Aircraft 06-07

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LIST OF EFFECTIVE PAGES Page iv

Part Page

No.

Issue

No.

Rev.

No.

Date Part Page

No.

Issue

No.

Rev.

No.

Date

Approval Page i Initial 0 23/07/2010 1 18 Initial 0 23/07/2010 TOC ii Initial 1 28/06/2012 1 19 Initial 0 23/07/2010 TOC iii Initial 1 28/06/2012 1 20 Initial 0 23/07/2010 LEP iv Initial 4 28/06/2012 1 21 Initial 0 23/07/2010

Para wise Index v Initial 0 28/06/2012 1 22 Initial 0 23/07/2010 Para wise Index vi Initial 0 28/06/2012 1 23 Initial 0 23/07/2010 Para wise Index vii Initial 0 28/06/2012 2 1 Initial 0 23/07/2010 Para wise Index viii Initial 0 28/06/2012 2 2 Initial 0 23/07/2010 Para wise Index ix Initial 0 28/06/2012 2 3 Initial 0 23/07/2010

Amendment x Initial 1 28/06/2012 2 4 Initial 0 23/07/2010 Distribution List xi Initial 1 13/04/2011 2 5 Initial 0 23/07/2010 Distribution List xii Initial 2 28/06/2012 2 6 Initial 2 28/06/2012

Abbreviation xiii Initial 0 23/07/2010 2 7 Initial 0 23/07/2010 0 1 Initial 0 23/07/2010 3 1 Initial 0 23/07/2010 0 2 Initial 0 23/07/2010 3 2 Initial 2 28/06/2012 0 3 Initial 0 23/07/2010 3 3 Initial 1 13/04/2011 0 4 Initial 1 18/06/2012 4 1 Initial 0 23/07/2010 0 5 Initial 1 28/06/2012 4 2 Initial 2 13/02/2012 0 6 Initial 2 18/06/2012 4 3 Initial 0 23/07/2010 0 7 Initial 0 23/07/2010 4 4 Initial 0 23/07/2010 0 8 Initial 1 13/04/2011 4 5 Initial 0 23/07/2010 0 9 Initial 2 18/06/2012 4 6 Initial 0 23/07/2010 0 10 Initial 0 23/07/2010 4 7 Initial 1 13/02/2012 0 11 Initial 0 23/07/2010 4 8 Initial 0 23/07/2010 0 12 Initial 0 23/07/2010 5 1 Initial 1 28/06/2012 0 13 Initial 1 28/06/2012 5 2 Initial 0 23/07/2010 0 14 Initial 0 23/07/2010 5 3 Initial 1 28/06/2012 0 15 Initial 0 23/07/2010 5 4 Initial 1 28/06/2012 1 1 Initial 0 23/07/2010 5 5 Initial 1 28/06/2012 1 2 Initial 0 23/07/2010 5 6 Initial 1 28/06/2012 1 3 Initial 0 23/07/2010 5 7 Initial 0 23/07/2010 1 4 Initial 0 23/07/2010 5 8 Initial 0 23/07/2010 1 5 Initial 0 23/07/2010 5 9 Initial 1 13/02/2012 1 6 Initial 0 23/07/2010 5 10 Initial 1 13/02/2012 1 7 Initial 0 23/07/2010 5 11 Initial 1 13/02/2012 1 8 Initial 0 23/07/2010 5 12 Initial 1 28/06/2012 1 9 Initial 0 23/07/2010 5 13 Initial 0 23/07/2010 1 10 Initial 0 23/07/2010 5 14 Initial 0 23/07/2010 1 11 Initial 0 23/07/2010 5 15 Initial 0 23/07/2010 1 12 Initial 1 13/02/2012 5 16 Initial 0 23/07/2010 1 13 Initial 0 23/07/2010 5 17 Initial 0 23/07/2010 1 14 Initial 0 23/07/2010 5 18 Initial 0 23/07/2010 1 15 Initial 0 23/07/2010 5 19 Initial 0 23/07/2010 1 16 Initial 0 23/07/2010 5 20 Initial 0 23/07/2010 1 17 Initial 0 23/07/2010 5 21 Initial 2 28/06/2012

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PARA WISE INDEX Page v

INTRODUCTION Page No

Approval Page i

Table of Content ii

Table of Content iii

List of Effective Pages iv

Para wise Index v

Para wise Index vi

Para wise Index vii

Para wise Index viii

Para wise Index ix

Amendment x

Distribution List xi

Distribution List xii

Abbreviations Used xiii

PART 0 GENERAL PAWAN HANS ORGANISATION

0.1Corporate Commitment by the Accountable Manager 1

0.2 General PHHL Information 2

0.2.1 Description of the Organisation 2-3

0.2.2 Relationship with Other Organisations 3

0.2.3 Aircraft managed – Fleet composition 4

0.2.4 Type of Operation 5

0.2.5 Scope of work 5

0.3 Management Personnel 6

0.3.1 Accountable Manager 6

0.3.2 Continuing Airworthiness Manager 6

0.3.3 Quality Manager 6

0.3.4 Continuing Airworthiness Coordination – Nominated Persons 6

0.3.5 Airworthiness Review Staff 6

0.3.6 Duties and Responsibilities 6

0.3.6.1 Accountable Manager 6

0.3.6.2 Continuing Airworthiness Manager 7

0.3.6.3 Designated Quality Manager 8

0.3.6.4 CAMO Representative (North East) 8-9

0.3.7 Manpower Resources and Training Policy 9

0.3.7.1 Manpower Resources 9

0.3.7.2 Training Policy 10-11

0.4 Management Organisation Chart 12

0.4.1 General PHHL Organisation Chart 12

0.4.2 Continuing Airworthiness Management Organisation Chart 13

0.4 Notification Procedure to the DGCA Regarding Changes to the Operator‟s Continuing Airworthiness Management Arrangements / Locations / Personnel / Activities / Approval

14

0.5.1 Changes 14

0.6 Continuing Airworthiness Management Exposition Amendment Procedures 14

0.6.1 CAME Review 15

0.7 Facilities 15

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PARA WISE INDEX Page vi

PART 1 CONTINUING AIRWORTHINESS MANAGEMENT PROCEDURE Page No

1.0 Continuing Airworthiness Management Procedures 01

1.1Aircraft Flight log Utilisation and MEL Application List 01

1.1.1 The Flight log 01-02

1.1.1.1 The Flight log Contents 02-03

1.1.2 MEL Application & Approval 03-04

1.1.2.1 MEL Procedure 04

1.1.2.2 Acceptance by the Pilot 04-05

1.1.2.3 Management of the MEL Rectification Intervals (RI‟s) 05

1.1.2.4 MEL Rectification Interval expiry 05

1.2 Aircraft Maintenance Programme General PHHL 05

1.2.0.1 The Programme – Contents - Sources 05-06

1.2.0.2 Structural Inspections, Corrosion Control, Reliability and Engine Health Monitoring.

06

1.2.0.3 Mandatory Life Limitations 07

1.2.0.4 Inspection Standards 07

1.2.0.5 Maintenance Certification 07

1.2.0.6 Fuel Contamination 07

1.2.0.7 Maintenance Specific to Helicopter Operations 07

1.2.0.8 The Maintenance Programme Owner - responsibilities 08

1.2.0.9 Holders of the Maintenance Programme 08

1.2.0.10 Compliance of Maintenance Programme 08

1.2.1 Maintenance Programme Review, Development and Amendment 09

1.2.1.1 Development and Amendment 09

1.2.1.2 Maintenance Programme Meetings 09

1.2.1.3 Maintenance Programme Amendments 09

1.2.1.4 Maintenance Programme Variations 09

1.2.1.5 Variations in Excess of that Allowed by the programme 10

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

10

1.3.1 Hours and Cycles Recording 10

1.3.2 Monitoring of Maintenance Between Scheduled Maintenance 10

1.3.3 Sector Record Page Retention 10

1.3.4 Access to Continuing Airworthiness Records 11

1.3.5 Transfer of Continuing Airworthiness Records in the Event of a Sale or other Disposal of the Aircraft

11

1.3.6 Access to Continuing Airworthiness Records in the Event of an Accident/ Incident 11

1.4 Accomplishment and control of Mandatory Requirements for Airworthiness 11

1.4.1 Access to Airworthiness Directives & DGCA Requirements 11-12

1.4.2 AD, EAD & DGCA Requirement & Implementation 12

1.4.3 AD/EAD/ DGCA Requirement - Compliance Monitoring 12

1.4.4 AD/ EAD/ DGCA Requirement – Recording of AD/ DGCA Requirement Compliance

13

1.5 Analysis of the Effectiveness of the Maintenance Programme 13

1.5.1 Review Meetings 13

1.5.2 Frequency of Meetings 13-14

1.6 Non-Mandatory Changes (Modification) Embodiment Policy 14

1.6.1 Changes (Modifications) General PHHL 14

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Section Page No

1.6.2 Service Bulletins 14

1.6.3 Other Changes (Modifications) 15

1.6.4 Minor Changes (Modifications) 15

1.6.5 Recording of Changes (Modifications) 15

1.7 Major Change (Modification) Standards 15

1.8 Defect Reports 15

1.8.1 Analysis 15 & 17

Intentionally Left Blank 16

1.8.2 Review with Manufacturers and Regulatory Authorities 17

1.8.3 Deferred Defect Policy 17

1.8.4 Non Deferrable Defects Away from Base 18

1.8.5 Repetitive Defects 18

1.8.6.1 Mandatory Occurrence Reporting 18

1.8.7 Liaison Meetings 19

1.9 Engineering Activity 19

1.10 Reliability Programmes 19-20

1.11 Daily/Pre-flight / Relevant Inspection 20

1.11.1 The Pre flight Check 20

1.11.2 The Daily Inspection/Post flight Inspection 20

1.11.3 Pilot Authorisation 20-21

1.11.4 Sub-contracted Ground Handling Functions 21

1.11.5 Security of Cargo and Baggage loading 21

1.11.6 Control of Aircraft Refuelling, Quantity/Quality 21-22

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

22

1.11.8 Certificate of Airworthiness Validity & ARC Validity 22

1.12 Aircraft Weighing 22

1.13 Test Flight Procedures 22

1.14 Sample of Documents, Tags and Forms Used 23

1.15 Leasing of Aircraft 23

1.16 General PHHL Procedures(inc Operational Approval Procedures) 23

1.17 CVR / DFDR Readout Policy 23

1.18 Materials Auditor/ Stores Inspector 23

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PARA WISE INDEX Page viii

PART 2-QUALITY SYSTEM Page No

2.1 Continuing Airworthiness Quality Policy, Plan and Audit Procedures 01

2.1.1 Continuing Airworthiness Quality Policy 01

2.1.2 Quality Program 01

2.1.3 Quality Audit Procedure 02

2.1.4 Findings 02-03

2.1.5 Quality Audit Remedial Action Procedure 03

2.2 Monitoring of Continuing Airworthiness Management Activities 04

2.2.1 Quality Audit of Aircraft / Survey of Aircraft 04

2.3 Monitoring the Effectiveness of the Maintenance Program 04

2.4 Monitoring that all Maintenance is Carried Out by an Appropriately Approved Part 145 Organisation

04

2.5 Monitoring that all Contracted Maintenance is Carried Out in Accordance with the Contract, including Sub-contractors used by the Maintenance Contractor

04

2.6 Quality Audit Personnel 05

2.6.1 Name of independent auditors (NR) 06

2.6.2 Name of independent auditors (WR) 06

2.7 Quality audit of aircraft 06

2.7.1 The Annual Audit Program 07

PART 3 CONTRACTED MAINTENANCE

3.0 Contracted Maintenance 01

3.1 Maintenance Contractor Selection Procedure 01

3.1.1 Advising the DGCA of Changes to the Maintenance Support 01

3.2 Detailed List of Maintenance Contractors 01

3.3 Relevant Technical Procedures Identified in the Maintenance Contract(s) 02

3.4 Aircraft Operated 02

3.5 Quality audit of sub-contracted CAR tasks 02

3.6 Procedure for awarding work to sub-contractors 03

3.6.1 Purpose 03

3.6.2 Scope 03

3.6.3 Procedure 03

3.6.3.1 Criteria for assessment 03

3.6.4 Record Keeping 03

3.6.5 Period 03

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PARA WISE INDEX Page ix

PART 4 AIRWORTHINESS REVIEW PROCEDURES Page No

4.1 Airworthiness review staff 01-02

4.1.1 CAMO staff training 02

4.2 Airworthiness Review General PHHL Procedures 02

4.3 Review of aircraft records 02

4.4 Physical survey 02

4.5 Aircraft Airworthiness Review Documentation 03-04

4.5.1 ARC Renewal Logic 05

4.6 Recommendations to competent authorities for the issue of an ARC 05

4.7 Issuance of an ARC 06-07

4.7.1 Distribution of ARC 07

4.7.2 Airworthiness Review Certificate 08

4.8 Airworthiness review records, responsibilities, retention and access 08

PART 5 APPENDICES

5.0 Description 01

5.1 List of Appendices –Sample of Documents 01

Appendix 1.1 - Sector Record Page/ Tech log Page/ Flight report Page(Dauphin SA365N H/C )

02

Appendix 1.2 - Sector Record Page/ Tech log Page/ Flight report Page(Dauphin AS365N3 H/C)

03

Appendix 1.3 - Sector Record Page/ Tech log Page/ Flight report Page (MI-172 Helicopter)

04

Appendix 1.4. - Sector Record Page/ Tech log Page/ Flight report Page (Bell Helicopter)

05

Appendix 1.5 - Sector Record Page/ Tech log Page/ Flight report Page ( Ecureuil Helicopter)

06

Appendix 2. CRS 07

Appendix 3 - Audit Plan – PHHL‟s CAMO Quality System 08-10

5.2 Airworthiness Review Staff 11

5.2.1 Northern Region 11

5.2.2 Western Region 12

5.3 Appendix 4 - - List of Approved 145 Maintenance Organisation sub Contracted 13-16




5.7 Appendix 5 – Airworthiness Review Report 17-20

5.8 REVIEW CERTIFICATE -PHHL NOT AUTHORISED -

5.9 Compliance checklist- enclosed -

5.10 Appendix 6 : Details of Aircraft Managed by Organization 21

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AMENDMENT RECORD

AMENDMENT NO:

DATE AMENDMENT DETAILS AMENDED BY DATE OF INCLUSION

AMENDMENT PAGE NO. x

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DISTRIBUTION LIST PAGE NO. xi

1.0 Distribution list of controlled copies is given below. Controlled copy holders will receive future revisions and issues. Holder of the controlled copy will ensure that the copy is maintained up to date and is made available to the concerned staff/manager/executive of the department as and when required. 2.0 Copies are issued to any other agency other than reflected in distribution list or any personnel are considered as un-controlled. These manuals shall be current issue and revision. Un-controlled copy holder will not receive future revisions.

CONTROLLED COPY NO

HOLDER LOCATION

1. QUALITY MANAGER NR

2. QUALITY MANAGER WR

3. CMD CO

4. ACCOUNTABLE MANAGER CO

5. GENERAL MANAGER WR

6. GENERAL MANAGER NR

7. CONTINUING AIRWORTHINESS MANAGER WR

8. CONTINUING AIRWORTHINESS MANAGER NR

9. DGM LINE MAINTENANCE WR

10. DGM (PPC) NR

11. DGM (PPC) WR

12. DGCA HQTR NEW DELHI

13. REGIONAL AIRWORTHINESS OFFICE DGCA (NR) NEW DELHI

14. REGIONAL AIRWORTHINESS OFFICE DGCA (WR) MUMBAI

15. REGIONAL AIRWORTHINESS OFFICE DGCA (ER) KOLKATA

16. REGIONAL AIRWORTHINESS OFFICE DGCA (SR) CHENNAI

17. REGIONAL AIRWORTHINESS OFFICE DGCA GUWAHATI

18. REGIONAL AIRWORTHINESS OFFICE DGCA KOCHIN

19. REGIONAL AIRWORTHINESS OFFICE DGCA PATNA

20. REGIONAL AIRWORTHINESS OFFICE DGCA BHOPAL

21. TECHNICAL LIBRARY NR

22. TECHNICAL LIBRARY WR

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DISTRIBUTION LIST PAGE NO. xii

CONTROLLED COPY NO

HOLDER LOCATION

23. ENGG I/C (GUW) GUWAHATI

24. ENGG I/C (ITA) ITANAGAR

25. ENGG I/C (CHD) CHANDIGARH

26. ENGG I/C (KVT) KAVARATTI

27. ENGG I/C (PBLR) PORTBLAIR

28. ENGG I/C (BRD) BARODA

29. ENGG I/C (GTK) GANGTOK

30. ENGG I/C (RANCHI) RANCHI

31. ENGG I/C (NAZIRA) NAZIRA

32. ENGG I/C (KATRA) KATRA

33. ENGG I/C (AGT) AGARTALA

34. ENGG I/C (RAIPUR) RAIPUR

35. ENGG I/C (RANCHI) RANCHI

36. ENGG I/C (BHUVNESHWAR) BHUVNESHWAR

37. ENGG I/C (RAJAHMUNDRI) RAJAHMUNDRI

38. ENGG I/C (VIZAG) VISHAKHAPATTANAM

NOTE: Besides the above the distribution list, soft copy of the CAME in PDF read only form will be also available on the company server, accessible to any employee for reference.

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ABBREVIATIONS

PAGE NO. xiii

AAC……………..Airworthiness Advisory Circular AD ..................... Airworthiness Directive ADD ................... Acceptable Deferred Defect AMSD ................ Aircraft Maintenance Standards Department AOC .................. Air Operator's Certificate AOG .................. Aircraft on Ground AWOPS…………All Weather Operations BSI .................... British Standards Institute CA ..................... Civil Aviation CAME ................ Continuing Airworthiness Management Exposition CAMPM………….Continuing Airworthiness Management Procedure Manual C of A ................ Certificate of Airworthiness CDL ................... Configuration Deviation List CMR……………..Certificate of Maintenance Review. CRS ................... Certificate of Release to Service DGCA……………Director General of Civil Aviation ETOPS .............. Extended Range Twin Operations EAD …………… Emergency Airworthiness Directive (s) EASA ................. European Aviation Safety Agency HEMS……………Helicopter Emergency Medical Services LMM……………..Line Maintenance Manager MEL ................... Minimum Equipment List MNPS ................ Minimum Navigation Performance Service MO .................... Maintenance Organisation MOE .................. Maintenance Organisation Exposition MOR…………….Mandatory Occurrence Report MPD .................. Maintenance Planning Document MP ..................... Maintenance Programme NSOP……………Non Schedule Operators‟ Permit PCA …………….. Post holder continuing airworthiness PHHL ……………..Pawan Hans Helicopters Ltd. RAWO…………..Regional Airworthiness office RNAV……………Area Navigation SB ..................... Service Bulletin SIL ..................... Service Instruction Leaflet / Letter SMI .................... Scheduled Maintenance Inspection SRP ................... Sector Record Page


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GENERAL ORGANISATIONS PART 0

PAGE NO. 01

0.1 Corporate Commitment by the Accountable Manager

CONTINUING AIRWORTHINSS MANAGEMENT EXPOSITION This Exposition defines the organization and the procedures upon which DGCA Sub-part G approval of Pawan Hans Helicopters Limited under CAR-M is based. These procedures are approved by the undersigned and must be complied with, as applicable, in orders to ensure that all continuing airworthiness activities including maintenance for aircraft manage by Pawan Hans Helicopters Limited is carried out time to time to an approves standard It is accepted that these procedures do not override the necessity of complying with any new or amended regulation published by the DGCA from time to time where these new or amended regulations are in conflict with these procedures. DGCA will approve this organization whilst DGCA is satisfied that the procedures are being followed and work standards maintained. It is further understood that DGCA reserves the right to suspend, vary or revoke the M.A. Sub-part G continuing airworthiness management approval of the organization, as applicable, if DGCA has evidence that procedures are not followed or standards not upheld. Signed....................................................... Dated………………………...................

Accountable Manager and ................................................(quote position) ............................... For and on behalf of PAWAN HANS HELICOPTERS LTD.


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PAGE NO. 02

0.2 General PHHL Information

Pawan Hans Helicopters Limited has been established with a view to provide safe air transport services to Oil sector, operate in hilly and remote terrain, connecting inaccessible areas and to provide tourist charters for promotion of travel and tourism utilizing Dauphin SA 365 N, Dauphin AS 365 N3 & MI 172 Helicopters, Bell 206L4 , Bell 407, Dhruv and Ecureuil. 0.2.1 BACKGROUND: Pawan Hans Helicopters Ltd (PHHL) was incorporated in October 1985 as a Company under the provisions of the Companies Act, 1956 with the following objectives: Providing helicopter support services to meet the requirements of the oil sector, operating in hilly and remote terrain, connecting inaccessible area and providing tourist charters for promotion of travel and tourism. In addition undertake any other operation that may be directed / requisitioned by the Government of India. When the Company was formed, helicopter operations in civil sector were virtually non- existent and expertise in this field was very limited. Consequent upon its formation, PHHL inducted large number of helicopters in a record time and within a year of its inception the company made beginning in replacing foreign helicopter operators and by September, 1987, the Company was able to accomplish the crucial task of providing cent percent services to ONGC, thereby saving outflow of precious foreign exchange.

BROAD ORGANIZATION: The Corporate Office is located at Delhi with the two regional offices located at Mumbai and Delhi which are designated as Western Region (WR) and Northern Region (NR) respectively. The western region takes care of all helicopter operations including maintenance of helicopter in the western and southern part of India whereas Northern region takes care of the northern and Eastern part of India.

The official address of the Corporate office and two regions are as follows:

Corporate Office - Pawan Hans Helicopters Ltd

Corporate Office

Safdarjung Airport

New Delhi – 110003

Fax :91- 011-24602596

011-24611801


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PAGE NO. 03

Western Region - Pawan Hans Helicopters Ltd

Western Region

Juhu Airport, S.V. Road

Vile Parle (W)

Mumbai – 400056

Fax : 022-26117339

022-26186926

Northern Region - Pawan Hans Helicopters Ltd

Northern Region

Safdarjung Airport

New Delhi – 110003

Fax: 011 - 24611801

This Continuing Airworthiness Management Exposition has been prepared to obtain a CAR Subpart G approval as part of Pawan Hans Helicopters Limited Non Schedule Operator‟s permit. The contents relate directly to the requirements of CAR and are based on the example of Exposition contents shown in Appendix V to AMC M.A.704 Pawan Hans Helicopters Limited is approved under CAR 145 for maintenance of Helicopter being operated by the organization. Details of the current maintenance contractor are contained in Part Three of this CAME, Para. 3.2. The main operating base is New Delhi, India.

0.2.2 Relationship with Other Organisations

Pawan Hans Helicopters Limited currently operates independently of any other organisations and maintenance support is provided by PHHL Part 145 maintenance organisation.


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PAGE NO. 04

0.2.3 Aircraft Managed – Fleet Composition

The continuing airworthiness of the following aircraft types is managed by NORTHERN REGION

HELICOPTER TYPE REGN ENGINE AIRWORTHINESS REVIEW

CONTRACTED

BELL 206 L4 VT-PHA,VT-PHD, VT-PHE

ALLISON 250C-30P

√ X

BELL 407 VT-PHH,VTPHI, VTPHN,VT-PHQ,

ALLISON 250C-47B

√ X

DHRUV (ALH) VT-HAR,VT-HAN, VT-BSJ,VT-BSK, VT-BSS, VT-BSM, VT-BSP,

TM 333 2B2 √ √

ECUREUIL AS350 B3 VT-PHU, VT-PHV ARRIEL 2B1

√ X

WESTERN REGION


CONTRACTED

DAUPHIN SA 365N VT-ELB,VT-ELD, VT-ELE,VT-ELG, VT-ELI,VT-ELJ, VT-ELK,VT-ELL, VT-ELM,VT-ELN VT-ELP,VT-ELQ VT-ELR,VT-ELS, VT-ELT, VT-ENW VT-ENX.VT-ENZ

ARRIEL 1C √ X

DAUPHIN AS 365N3 VT-PHJ,VT-PHK, VT-PHL,VT-PHM VT-PHO,VT-PHR, VT-PHS, VT-PHW, VT-PHX, VT-PHY, VT-PHZ,VT-PWA, VT-PWB, VT-PWC VT-PWD, VT-PWE, VT-PWF

ARRIEL 2C √ X

MI 172 VT-PHG TV3-117M √ X

The above aircraft registration can be found in Pawan Helicopters Limited‟s current NSOP on the name of Pawan Hans except Dhruv Helicopters.

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0.2.4 Type of Operation

Pawan Hans Helicopters Limited was set up in year 1985 to provide non-schedule air transport service in all regions within India includes the following: Under Non Schedule operator Permit 2/1998, issued, by the DGCA on 16.03.1998. Pawan Hans Helicopters Limited has been established in the year of 1985 with a view to provide. a) Air transport services to Oil sector, b) A helicopter services for pilgrimage, c) Connecting inaccessible areas and to provide tourist charters d) Inter Island Services. e) Heli tourism f) VIP Operation g) Medivac 0.2.5 Scope of work

Organisation Continuing Airworthiness Management Capability:

HELICOPTER TYPE ENGINE MANAGEMENT AIRWORTHINESS REVIEW

MAINTENANCE PROGRAMME

BELL 206 L4 ALLISON 250C-30P

√ √ √

BELL 407 ALLISON 250C-47B

√ √ √

DHRUV (ALH) TM 333 2B2 √ √ X

ECUREUIL AS350 B3 ARRIEL 2B1 √ √ √

HELICOPTER TYPE ENGINE MANAGEMENT AIRWORTHINESS REVIEW

MAINTENANCE PROGRAMME

DAUPHIN SA 365N ARRIEL 1C √ √ √ DAUPHIN AS 365N3 ARRIEL 2C √ √ √

MI 172 TV3-117M √ √ √

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0.3 Management Personnel 0.3.1 Accountable Manager The duties and responsibilities associated with this post are held by Deepak Kapoor (General Manager)(Duties and Responsibilities are given in Para 0.3.6.1)

The Accountable Manager will sign the CA form 4 for approval as Accountable Manager for CAMO by DGCA.

0.3.2 Continuing Airworthiness Manager

a) Mr. S D Sharma, DGM (QC-TS)Continuing Airworthiness Manager at WR

b) Mr. Deepak Bhatnagar, Sr. Manager (ENGG) Continuing Airworthiness Manager at NR

0.3.3 Quality Manager: a) Mr. A.P.Singh, DGM (QC-TS) (Quality Manager at WR) b) SH. Vijay M. Pathiyan DGM (ENGG) (Quality Manager at NR)

NOTE: All the records for nominated / management personnel of CAMO will be retained for at

least 2 years after leaving the company.

0.3.4 Continuing Airworthiness Coordination – Nominated Persons

1. Accountable Manager CAMO 2. Post Holder of Continuing Airworthiness (PCA) 3. Quality Manager : Post Holder of Quality (PHQ)

0.3.5 Airworthiness Review Staff Pawan Hans Helicopters Limited. Is not authorised to issue / extend ARC of aircraft managed by the CAMO. Necessary recommendation for issue/extension of ARC will be prepared and submitted to DGCA local office for extension/ issuance of ARC. Detailed procedure is documented in Chapter 4.

0.3.6 Duties and Responsibilities

0.3.6.1 Accountable Manager

(a) The Accountable Manager has the overall responsibility to meet the requirements of Part-M.

(b) He is responsible to ensure that all continuing airworthiness activities can be financed and are carried out to the required standards.

(c) In particular, he is responsible for ensuring that adequate contractual arrangements exist. This includes, amongst others, provision of: facilities, material and tools, sufficient competent and qualified personnel in relation to the work to be undertaken.

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(d) All of this with a view to ensure that all due continuing airworthiness activities including maintenance is performed on time and in accordance with the applicable requirements, regulations and approved standards and that the aircraft has a valid Certificate of Airworthiness for all flights undertaken.

(e) The Accountable Manager has the financial responsibility for all Continuing Airworthiness arrangements for compliance with CAR M, CAMO policy & procedures.

0.3.6.2 Continuing Airworthiness Manager (Region)

The PCA is nominated post holder for continuing airworthiness. He will,

ensure that all maintenance is carried out on time and to an approved standard. He will act to ensure that PHHL‟s responsibilities in the following areas can be met:

a) Establishment and development of continuing airworthiness policy, including the approval of PHHL‟s maintenance programme‟s required by CAR.302.

b) Analysis of the effectiveness of the Maintenance Programme as required by CAR.A.708(b) & Appendix 1 to AMC M.A.302.

c) The relationship with the Part 145 maintenance Organization and establishment of a Maintenance standard required by CAR.A.201(h)2; d) Ensuring that the Quality System required by CAR.A.712 is effective in its application and any follow up actions required to address findings;

e) Approval, by the DGCA of Pawan Hans Helicopters Limited Flight Log, required by CAR.A.306, including any subsequent amendment thereto; f) Ensuring that PHHL‟s technical records are kept as required by CAR.A.305; g) Work planning and follow up;

h) Technical follow up;

i) Modifications and repairs (changes) are carried out to an approved standard;

j) Airworthiness Directive review and embodiment;

k) Non mandatory modification embodiment policy;

l) Rectification of all defects;


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m) Line and base maintenance;

n) That the Certificate of Airworthiness for each aircraft operated by the company remains valid in respect of

(i) The airworthiness of the Helicopter

(ii) The expiry date specified on the Certificate, and

(iii) Any other condition specified in the Certificate;

p) Reporting any occurrences of a maintenance nature to the DGCA and the aircraft manufacturers. This includes both Mandatory Occurrences and occurrences related to maintenance findings, which fall outside the Mandatory scheme.

q) The amendment and control of this Continuing Airworthiness Management Exposition.

r) Review and implementation, as appropriate, of any additional DGCA

requirements. 0.3.6.3 Designated Quality Manager (PHQ)

The Quality Manager is responsible for the following functions: a) Monitoring that all M.A. Subpart G activities are being performed in accordance with the approved procedures. b) Monitoring that all tasks of continuing airworthiness management are carried out in accordance with the concluded contracts. c) Monitoring the continued compliance with the requirements of Subpart G. d) Monitoring and amendment of the CAME and the submission of proposed amendments to DGCA. e) Ensuring that all maintenance is performed in compliance to the quality standards defined. f) Correspondence with the authority. g) Ensuring that all continuing airworthiness documentation is used properly and accordingly. h) Monitoring all company hand books. i) Performing a quality surveillance on the continuing airworthiness system) Proposing all corrective action necessary for eliminating non-compliance ensuring that these corrective actions are initiated, completed and efficient to meet the intended purpose

0.3.6.4 CAMO Representative (North East) In consultation with CAM Region ensure implementation of Continuous Airworthiness management functions for the Helicopters operating from the North eastern Region. He will ensure the following:-

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a) He will on a day-to-day basis report all significant details concerning the operation

and maintenance of helicopters in North East. b) He shall also ensure all components installed are within their stipulated life and all

inspection and modification on the helicopters and its associated systems are carried out in time.

c) Modification and repairs (changes) are carried out to an approved standard. d) He will also associate himself with daily / weekly maintenance review meetings and

send reports accordingly. e) He will liaison with local DGCA office for any airworthiness requirement as

considered necessary

0.3.7 Manpower Resources and Training Policy 0.3.7.1 Manpower Resources in CAMO

Manpower resources will be reviewed once in six months during review meetings in the light of induction of new aircraft etc. The current status of total man hours available in CAMO divisions at NR & WR is as follows:

Working Hrs in a day = 6.5 Hrs

* Working days in a year = 288

* Average working days in a month = 24

Working Hrs in a year = 1872 Hrs

*Above data is calculated for 1 person

List staff numbers and related activity:

NR WR

1 man year = 1872 hours Full Time Staff

(Number) Full Time Staff

(Number) Total Staff

Accountable Manger - - 01

Continuing Airworthiness Manager

01 01 02

Quality Manager 01 01 02

Quality Auditor/ Quality Ex / Stores Insp

04 05 09

CAMO –Tech Sec- Engineer 01 01 02

Airworthiness Review Staff 01 01 02

Continuing Airworthiness Management Staff

04 05 09

Total 12 14 27

Total Man Hours 22464 26208 50544

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PAGE NO. 10

0.3.7.2 Training Policy Training will be provided by Pawan Hans Helicopters Limited. to ensure that each member of staff is adequately trained to carry out the functions of, and satisfy the responsibilities associated with, the CAR Subpart G continuing airworthiness management functions.

Where changes occur to the organisation, its procedures, and types operated etc. The suitable continuation training will be provided, where necessary.

The Post Holder of Continuing Airworthiness (PCA) will review training needs at intervals not exceeding two years or at more frequent intervals if, and when, significant changes occur to the organisation, procedures and aircraft / helicopter types operated.

Recurrent Training: Civil Aviation Requirements Section 2, Series „L‟ Part VII, Series „L‟ Part X and Series L‟ Part XIV requires periodic refresher course for holders of AME licenses, Approvals and Certificate of Competency. Personnel mentioned above are required to undergo refresher course at least once in twenty-four months.

Post Holder of Continuing Airworthiness (PCA) & Post Holder of Quality (PHQ), will assess the requirement for Certifying Staff with respect to License renewal, currency / recency, Technological changes and any other development which in his opinion requires recurrent training shall put up for discussion with Continuing Airworthiness Manager (PCA) and Accountable Manager with relevant information and data on the basis of which the recurrent / refresher training will be decided.

The Post Holder of Continuing Airworthiness (PCA) & Post Holder of Quality (PHQ), will prepare the training syllabus to ensure that the personnel certifying the airworthiness of aircraft, engines and its components have current and updated knowledge on the following: Training will be carried out at regular intervals, taking into account of changes in:

a) CAME b) Aircraft maintenance programme c) New aircraft type and model of aircraft d) Organisation e) New equipment f) Company procedures g) DGCA regulations h) Bulletins, Airworthiness Directives, etc. i) Human Factors


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PAGE NO. 11

j) Case studies of repetitive snags, incidents, accidents due to maintenance lapse k) Good maintenance practices l ) Technical order/ technical instruction issued since last two years

m ) MMEL/MEL.

& any other relevant topics, recent technological development, He will keep Record of the DGCA updates / requirements, Regulation changes, Human factor and operational experiences of PHHL, organizational changes, technical notices etc, decide the venue, date of commencement and Instructors. He will get the concurrence of the concerned Regional Airworthiness Office for conducting training. Record of the training will be maintained by the Quality Department which includes:

i. Attendance of trainees. ii. Certificate issued by Head of Quality to the trainees. iii. Feedback from the attendees. iv. Feedback to RAWO. v. Feedback to Accountable Manager.


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PAGE NO. 12

??????????????This page contents need be changed??????????????????/

0.4 Continuing Airworthiness Management Organisation Chart

0.4.1 General PHHL Organisation Chart

GM

(OPS)

DGM

(HRD)DGM

MGR.

AIR

SAFETY

DGM

(P&A)

SECY.

STAFF

DGM

(OPS)

&

(TRG)

G.M.

P&HRD

MGR.

MATS

DGM

(OL)DGM

(ENGG)

D

DGM.

(ENGG)

T. S.

SR.MGR.

(ENGG)

O

DGM

(F&A)

D

DGM.

(F&A)

R

MGR.

(MKTG)

MKTG.

OFFICERMGR.

(PR)

DGM

(MATS)

G.M.(ENGG.)

/ACC. MGR

G.M.

(F&A)

GM

(MRKT)

CHAIRMAN & MANAGING

DIRECTOR

GM (*)

(LEGAL)

CVO(*)

(VIG)

DGM(*)

(ADMN)

DGM (*)

(CA)

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

SECY.

STAFF

NOTE : 1. (*) THESE DEPT’S ARE NOT WITHIN THE QUALITY ASSURANCE SYSTEM

2.(->->->) SHOWS ADMN. CONTROL

ORGANISATION STRUCTURE OF PHHL – CORPORATE OFFICE (CO)

BOARD OF DIRECTORS

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PAGE NO. 13

0.4.2: Continuing Airworthiness Management Organisation Chart Engineering / Planning & Tech Services Structure:


MANAGER

QUALITY MANAGER


MANAGEMENT STAFF

AIRWORTHINESS REVIEW STAFF

ACCOUNTABLE MANAGER

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PAGE NO. 14

0.5: Notification Procedure to the DGCA Regarding Changes to the Operator's Continuing Airworthiness Management Arrangements / Locations / Personnel / Activities / Approval.

The Accountable Manager will undertake to advise the DGCA of any changes with respect to:

a) The operator's name and location(s)

b) Name of the organization or change of ownership c) Location of the maintenance facilities d) Additional locations of the maintenance facility(s) e) Accountable Manager f) Person approved by DGCA. g) facilities, equipment, tools, material, procedures, work scope and certifying staff that could

affect approval h) The persons specified in Para. 0.3 of this CAME i) The operation, procedures or maintenance support arrangements as they affect the CAR Subpart

G approval. This includes the contracted maintenance support organisations, the Maintenance Programmes(s), the Flight Log, contracted person(s) in support of the Continuing Airworthiness Management/Quality system functions.

0.5.1: Changes

Any changes will be notified to the DGCA as soon as practicable, by the Accountable Manager to enable the DGCA to determine continued compliance with CAR, to approve the change prior to incorporation and to make any necessary amendments to the CA Form 14 that may be appropriate.

0.6 Continuing Airworthiness Management Exposition Amendment Procedures

The Head of Quality is responsible for reviewing the CAME and for preparing any amendments.

All amendments will be submitted to the DGCA for approval prior to their incorporation in the CAME.

Minor changes which have no impact on the organisations approval, Head of Quality of Pawan Hans Helicopters Limited will issue instructions as appropriate. Minor changes are, deputing person in case of leave/sickness of the regular post holder, transfer / change in job allocation of any of the continued airworthiness management group member, and such other matter which is ,in the opinion of the Management Personnel (Para 0.3) may consider as minor.


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PAGE NO. 15

Record of such decision will be maintained by Quality Manager and will be made available to the competent authority/ DGCA on demand.

0.6.1 CAME Review

The CAME will be reviewed by the Post Holder of Continuing Airworthiness (PCA) at intervals not

exceeding 12 months or more frequently when significant changes occur which affect the content of this CAME.

0.7: Facilities

Pawan Hans Helicopters Limited has office accommodation necessary for its operational requirement and for Continuing Airworthiness Management, Planning, Technical Services, tech. Records personnel and Quality Staff for carrying out their designated tasks in a manner that contributes to good standards. The Office Accommodation also has Technical Library with provision for document consultation.

Layout of premises:.

BLADE

SHOP

HANGER(72 MTS. X 50 MTS)

DAUPHIN

DESK

PANEL

SHOP

ENGIINE

SHOP

SOAP

LAB

TOOL

CRIP

COMPONENT REPAIR SHOP

MAIN

STORE

RADIO

SHOP

SAFETY

SHOP

BATTERY

SHOP

Q. C. OFFICE

INST.

SHOP

ELECT.

SHOP

DGM

ENGG.

STRUCTURE

BAYPROGRESS

GROUND

SUPPORTMI-172

HUT

TECH

CONTROL

PLANNING

SECTION

QCM

OFFICE

AME REST

ROOM

L

I

B

R

A

R

Y

WELDING

SHOP

T E R M A C

T

E

R

M

A

C

CVR

SHOP

1st

floor

1st

floor

1st

floor

1st

floor

1st

floor

MAJOR

MAINTENCE

O

P

E

R

A

T

I

O

N

W

S N

E

1ST FLOOR SHOP

GROUND

FLOOR SHOP

Divider of

1st & 2nd floor

PASSAGE

FRONTREAR

ENGINEERING WORKSHOP LAYOUT (PAGE-01/01) ANNEXURE – II B


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CONTINUING AIRWORTHINESS MANAGEMENT PROCEDURES

PART 1

PAGE NO. 01

1.0 Continuing Airworthiness Management Procedures This Part One defines the continuing airworthiness management procedures which PHHL uses to

ensure compliance with the continuing airworthiness aspects of CAR. Where some aspects of these functions are sub-contracted then this will be clearly defined in the text.

1.1 Aircraft Flight log Utilisation and Minimum Equipment List Application

1.1.1 The Flight log

The Flight log in use with PHHL is designed to allow recording of defects, malfunctions, and maintenance performed on the aircraft to which it applies whilst the aircraft is operating between scheduled maintenance inspections. In addition it includes maintenance information required by the operating crew and is used for recording operating information relevant to flight. It is scrutinized by the Quality Department and is preserved. The document besides recording various information contain the following information i) Aircraft nationality and registration ii) Date of flight (s) iii) Names of crewmembers. iv) Duty assignments of crewmembers. v) Place of departure.

vi) Place of arrival. vii) Time of departure. viii) Time of arrival. ix) Hours of flight. x) Incidents, observations, if any. xi) Signature of pilot in command.

The continuing airworthiness information includes: a) The operating crews observations and remarks as a result aircraft operation in service

including the aircraft, engine(s), propellers, components and system technical status; b) Defects or incidents having effect on airworthiness; c) Results of technical inspections requested by the maintenance organisation;

d) Maintenance performed by the (contracted) maintenance organisation which details: I. defect rectification action taken and associated responses to crews requests

and/or remarks; II. Scheduled maintenance inspections performed;

III. Next due scheduled maintenance inspections.


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CONTINUING AIRWORTHINESS MANAGEMENT PROCEDURES PART 1

PAGE NO. 02

IV. Where applicable, any MEL technical limitations proposed by the Maintenance Organisation

1.1.1.1 The Flight Log Contents

The flight log book is a main part of the continuing airworthiness record system. The flight log book contains the following information: Page A: This section details the owner‟s/operator‟s name, the aircraft type and Approval Number. Page B: This section contains information: 1- Aircraft Nationality, Registration No., Classification of A/C (Normal, Passenger) 2- Manufacturer, A/c Type, Operator and Owner name 3- Main Base, place of issue, date and signature Page C: This section contains the Index and the Instruction for filling of the flight log book. SECTION 1: The following details are provided in this section:

The aircraft type and registration mark

Date and place of take-off and landing

The times at which the aircraft took off and landed

The running total flying hours

Details of defect or malfunction to the aircraft affecting airworthiness or safe operation

Engine and Airframe Parameters to be recorded.

The quantity of fuel and oil uplifted

The number of landings if relevant for aircraft or aircraft component life

Section 2: This section contains

Certificate of Release to Service (CRS).

Details of maintenance carried out,

Out of phase maintenance due before the next maintenance check. Section 3:

a) This section contains Pilot Acceptance Performa current Airframe and Engine hrs. along with the S/N and Regn. Respectively

b) Details of when the next scheduled maintenance is due. c) Any out of phase component changes due before the next maintenance check. d) Hrs. available for the next maintenance.


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PAGE NO. 03

Any changes to the Flight log will be submitted to Regional Airworthiness Office, DGCA as listed in CAR for approval prior to being put into use. NOTE: Copy Flight sector page / Flight log page is as in Part 5 Appendix 1 of PHHL CAME In the event that unscheduled maintenance and/or defect rectification is required to be carried out away from main base, by another PHHL Part 145 approved maintenance organisation the organisation carrying out such maintenance will be required to issue a Certificate of Release to Service in the Flight Log, as per contracted agreement. Continuing Airworthiness Manager will ensure that copies of all Flight Log Sector Record Pages, and any other pertinent maintenance-related information, are forwarded promptly to the quality cell, to allow them to perform their planning and maintenance co-ordination functions.

1.1.2 MEL Application & Approval a) CAR Section 2, Series B part I requires that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. The Minimum Equipment List (MEL) prepare based on the MMEL issued by the State of design/manufacturer for the use and guidance of flight and ground operations personnel. The MMEL is not normally part of the required aircraft documentation and it is frequently necessary for an operator utilizing aircraft manufactured in another State to request a copy of the current MMEL and amendments as they occur, in order to develop and maintain an MEL for approval by DGCA. The MEL is not intended to provide for continued operation of the aircraft for extended periods with MEL items unserviceable. In the case of unserviceable MEL items, the PHHL make repairs at the first station where repairs or replacement can be made, but in any case repair should be accomplished at the flight termination station, since additional unserviceability may require the aircraft to be removed from service. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MEL must be operative. MEL need not include items like wings, flight controls, complete engines, landing gears etc., the airworthiness and correct functioning of which is absolutely necessary before any flight. It may also not include items like galley equipment, entertainment systems, passenger convenience equipment, which do not affect the airworthiness of an aircraft.

a) Any amendments on MMEL issued by the State of design/manufacturer

as they occur, in order to develop and maintain on MEL for approval by DGCA.


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PAGE NO. 04

When a defect occurred before departure of any aircraft and if the defect is under MEL, the same may be invoked by making an entry by an appropriately qualified or an approved certifying staff in the Flight Report Book. After invoking the MEL. The FRB/ FSR Page number to be quoted on all subsequent sectors till the rectification of the defect.

1.1.2.1 MEL procedure

Pawan Hans Helicopters Limited Minimum Equipment List (MEL) represents a listing of items of equipment, which may, under certain circumstances be unserviceable. The MEL and instructions for its use is contained within the Preamble of the approved MEL. The Preamble to the MEL defines the rectification interval of the defects. In general PHHL, the MEL items categorized as follows: Category „A‟: Items in this category shall be repaired within the time interval specified in the remarks column of the MEL. Category „B‟: Items in this category shall be repaired within three (3) consecutive calendar days, excluding the day the malfunction was recorded in the aircraft maintenance record/logbook Category „C‟: Items in this category shall be repaired within ten (10) consecutive calendar days, excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. Category „D‟: Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days, excluding the day the malfunction was recorded in the

aircraft maintenance log and/or record. MEL will be invoked by appropriately Licenced AME/ person specifically approved/ approved Basic Licence holder/ approved pilot. However, approved pilot shall invoke MEL in respect of those items only, which do not require maintenance actions/ procedures.

1.1.2.2 Acceptance by the pilot

Where the MEL item has been entered by maintenance personnel, the decision to accept the carried forward item allowed by the MEL/CDL remains the responsibility of the pilot in command.


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PAGE NO. 05

An AME will not certify the aircraft for 'Flight' or a Pilot will not accept the aircraft for flight if it is considered that it is unsafe to do so.

1.1.2.3 Management of the MEL Rectification 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) so that the defect rectification may be performed before the specified MEL limit.

1.1.2.4 MEL Rectification Interval expiry.

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

i) The Rectification Interval is extended due to non availability of spares & same approved by

the DGCA. ii) The defect has been rectified.

1.2 Aircraft Maintenance Programme – General PHHL

The purpose of this maintenance programme is to provide maintenance planning instructions

necessary for the safe operation of the aircraft.

1.2.0.1 The Programme–Sources – Contents

A. Sources The Programme is based upon the Manufacturers maintenance planning document and DGCA Approved Maintenance Programme for aircraft, which has been amended to reflect in, full the recommendations of the airframe, engine, propeller and equipment manufacturer‟s maintenance recommendations.

Contents The aircraft maintenance programs contain details, including frequency, of all maintenance to be carried out, including any specific tasks linked to the type and the specificity of operations. Maintenance of each type of helicopter shall be organized in accordance with an approved aircraft maintenance programme.


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PAGE NO. 06

The “aircraft maintenance Programme” includes the following: Scheduled maintenance tasks, the associated procedures and standard maintenance practices. The purpose of this aircraft maintenance programme is to provide maintenance planning instructions necessary for the airworthiness of the aircraft. Any aircraft will only be maintained to one approved aircraft maintenance programme at any given time.

The Approved Maintenance Programmes for PHHL aircraft are as follows: PHHL Maintenance Programme Reference: 1. PHHL/MP/DN 2. PHHL/MP/DN3 3. PHHL/MP/MI 172 4. PHHL/MP/Bell 206L4 5. PHHL/MP/Bell 407 6. PHHL/MP/DHRUV (ALH) 7. PHHL/MP/ ECUREUIL AS350 B3

NOTE: more detail on the subjects to be considered as part of the approved Maintenance

Programmes, where appropriate as given in AMC M.A.302. 1.2.0.2 Structural PHHL Inspections, Corrosion Control, Reliability and Engine Health

Monitoring

Due to the size and level of complexity of the aircraft operated by Pawan Hans, there are no specific requirements for a Structure inspection, Corrosion Control, Reliability, and Engine Health Monitoring Programmes as part of the manufacturer‟s maintenance Recommendations. Pawan Hans‟s Aircraft Maintenance Programme based on manufacture‟s recommendation is duly approved by DGCA.


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PAGE NO. 07

1.2.0.3 Mandatory Life Limitations Mandatory Life Limitations are those imposed by the manufacturers or DGCA. A listing of

these is provided in Aircraft Maintenance Programme in TBO / SLL section, approved by DGCA.

1.2.0.4 Inspection Standards The Inspection Standards applicable are those given by the manufacturers of the airframe,

engine, main rotor and equipment and detailed in approved Aircraft maintenance Programme. Other Inspection Standards will be adopted if and when these are promulgated by DGCA.

1.2.0.5 Maintenance Certification All maintenance above the pre-flight level shall be certified by authorised persons through

the issuance of a Certificate of Release to Service as applicable to aircraft on the Indian register and as per PHHL Part 145.

1.2.0.6 Fuel Contamination

Fuel contamination checks are addressed in Part 1 of this CAME Para. 1.11.6. Also, the Daily Check/Pre-flight inspection includes a fuel water drain sample to be carried out prior to the first flight of the day.

1.2.0.7 Maintenance Specific to Helicopter Operations

The Maintenance Program contains the necessary tasks required to ensure continued compliance with additional special authorizations / Approvals:

Equipment necessary for Off-shore operation:

Helicopter Emergency Medical Service (HEMS) Rescue hoist Cargo Sling


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1.2.0.8 The Maintenance Programme Owner – responsibilities

The Maintenance Programme has been produced by PHHL who is the owner of the programme and is responsible for its development in accordance with CAR.A.708 (b). If the Maintenance Organisation has produced the maintenance programme, then the Programme will still have to be submitted to the DGCA via PHHL for approval. In this case the DGCA will have the access to the Maintenance Programme.

1.2.0.9 Holders of the Maintenance Programme

A copy of the Maintenance Programme will be held by;

a) Quality Manager of Pawan Hans Helicopters Ltd. (Original) b) PHHL Part 145 maintenance organisations. c) The DGCA, Regional Airworthiness Office d) Continuing Airworthiness Manager of PHHL

1.2.0.10 Compliance of Maintenance Program

1. A maintenance program will be based upon the maintenance review board (MRB) report where applicable, the maintenance planning document (MPD), the relevant chapters of the maintenance manual or any other maintenance data containing information on scheduling published in any other technical document. Furthermore, maintenance program will also take into account any maintenance data containing information on scheduling for aircraft components. 1. Instructions issued by DGCA for all types of aircraft either specific to an aircraft or

generic are to be complied by Pawan Hans

NOTE: Details of procedure for compliance of Maintenance program are described in Pawan Hans MOE.


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1.2.1 Maintenance Programme Review, Development and Amendment 1.2.1.1 Development and Amendment Development and amendment of the Maintenance Programme is the product of PHHL‟s

actions in monitoring the effectiveness of the Programme (see Paragraph 1.5), this together with the recommendations received from the Part 145 maintenance organisations(s), and PHHL‟s response to continued airworthiness information published by the manufacturers of aircraft, engines, Main Rotor and equipment in the form of Service Bulletins (SB), Service Information Letters (SIL),

Maintenance program will be revised atleast annually & if required necessary amendment will be submitted to DGCA for approval.

1.2.1.2 Maintenance Programme Meetings

Maintenance program Review Meetings will be held by PHHL‟s PCA. Following member will participate in meeting.

Accountable Manager (PHHL)

Post Holder Continued Airworthiness.

Head of Quality /Quality Assurance Manager – CAMO

PHHL Part145 Organisation Representatives. Time / Date / Venue of such meetings will be intimated to DGCA office, for their

association, if required by them. Records / Minutes of meeting of such meeting will be maintained and circulated by the

PCA to the concern.

1.2.1.3 Maintenance Programme Amendments

Where changes are identified as being necessary, and agreed between the PCA of PHHL and PHHL Part 145 organisation, these will be submitted by the PCA to the DGCA Office as an amendment to maintenance program.

1.2.1.4 Maintenance Programme Variations

Any variations to the Maintenance Programme within the accepted deviations in AMM

shall be utilized with prior concurrence of DGCA. These variations will be within the guidelines defined in the programme. These variations will only be requested when circumstances arise which could not reasonably have been anticipated by PHHL. Acceptable reasons would be, say, the aircraft being unable to return on time to the maintenance base due to weather or an AOG situation down the line.


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1.2.1.5 Variations in Excess of that allowed by Programme

Any requests for variations to the Maintenance Programme outside the limitations given in 1.2.1.4 will be submitted by the Head of Quality of PHHL to the DGCA following consultation, and agreement with the Part 145 Maintenance organisation for approval. These variations will only be sought in very exceptional circumstances.

1.3 Time and Continuing Airworthiness Records: Responsibilities, Retention and

Access. 1.3.1 Hours and Cycles Recording Continuing Airworthiness records, including hours and cycles recording for PHHL‟s

helicopters are the responsibility of PHHL.These records include:

a) The aircraft Log Books for Airframe, Engine(s) b) Modification records. c) Inspection records (Inspections Schedules, Work Orders etc). d) Component life records. e) Sector record pages (second copy). f) Overhaul records g) Repair records. h) Airworthiness Directive/Airworthiness Notice compliance records.

i) Certificate of Release to Service for completed maintenance. j) Mass and Balance reports for each Aircraft. k) A status of service life limit components (including component life imitation,

total no. of Hrs/cycles/calendar time)

1.3.2 Monitoring of Maintenance Between Scheduled Maintenance Based upon the maintenance programme PHHL generates a short term forecast of maintenance inspection/items which fall during the period between the last base maintenance i.e. out of face forecast. These items will be monitored by the Quality Manager through the record of daily flying recorded in Flight Log pages

1.3.3 Sector Record Page Retention Copies of the Flight Log Pages are retained in PHHL for a period of 36 months from the

date of the last entry. The maintenance contractor retains all other maintenance records, on behalf of PHHL, for the periods prescribed in M.A.305.

Colour coding for sector recode page is as follows: 1. White – To be kept with Q.C.cell (contracted 145) 2. Yellow – To be provided to Engineering / Tech. Cell (PHHL)


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1.3.4 Access to Continuing Airworthiness Records

All of the records may be accessed by PHHL at any reasonable time and remain the property of PHHL at all times. Access to the records by duly authorized members of the DGCA will be arranged where this is necessary

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

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

PHHL is required to transfer the records to the new owner or operator of the aircraft. All records will be made available by PHHL for transfer to the new Owner/operator.

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

In the event of an accident or serious incident the Quality Manager, will hold the records secure until requested by the Directorate of Air safety, DGCA.

NOTE; It is necessary that any computer based records systems if used by PHHL or MO, such system will also be held by Quality Manager.

1.4 Accomplishment and Control of Mandatory Requirements for Airworthiness (including

Airworthiness Directives, Emergency Airworthiness Directives & DGCA Requirements) 1.4.1 Access to Airworthiness Directives & DGCA Requirements The PHHL is responsible for the accomplishment of all applicable airworthiness

directives‟ (CAR.A.708) and DGCA generic requirements. The following mandatory requirements for Airworthiness Directives (AD) & DGCA

requirement publications as applicable to the aircraft operated are subscribed to, and held by the PHHL Part 145 maintenance organisation on behalf of PHHL:


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a) State of Design Airworthiness Directives b) DGCA published Airworthiness Directives c) DGCA published Emergency Airworthiness Directives d) Manufacture‟s Service Bulletins /Service Information Letter

Airworthiness Manager will visit websites of Manufactures, regulatory authorities of the states of manufacture, DGCA INDIA, OEMs/Component Manufactures every fortnight for mandatory publications. He will compile a report & submit to Quality Manager for further action.

1.4.2 AD, EAD & DGCA Requirement and Implementation

PHHL Part 145 maintenance organisation will be advised by Airworthiness Manager of

PHHL of any AD‟s, EAD‟s or DGCA Requirement, or revisions thereto, which affect PHHL‟s aircraft, engines, rotor or equipment at the earliest possible opportunity with a view to establishing compliance, but no later than date of compliance mentioned in the document. The necessary actions will be agreed between the PCA, PHHL and the Part 145 Maintenance organisation to schedule the compliance with the AD / DGCA Requirement at the first reasonable maintenance inspection within the AD/ DGCA Requirements in required compliance time. In the case where an EAD has been issued the responsible manager of Maintenance Organization shall to take all reasonable steps immediately and ensure affected aircraft do not fly until the task(s) detailed in the EAD has been accomplished. Where necessary, and required by the AD/DGCA Requirement, Repetitive Inspections will be introduced until full compliance is achieved.

The maintenance organisation will be notified of any emergency airworthiness directives or EAD‟s on receipt.

1.4.3 AD/EAD/DGCA Requirement Control - Compliance Monitoring

Airworthiness Directive, Emergency Conformity Information and Generic Requirement

compliance monitoring is the responsibility of PHHL. The Continuing Airworthiness Manager will review this monitoring at the Liaison Meetings indicated in Para. 1.2.1.2/1.5.1. Compliance with AD/DGCA requirement will be verified by the Head of Quality / Quality Manager as part of PHHL‟s quality system.

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1.4.4 AD/EAD/DGCA Requirement Control - Recording of AD/GR Compliance The method of compliance and when such compliance was achieved will be recorded in the

aircraft airworthiness records (Log Books) by the contracted Part 145 maintenance organisation. For AD/DGCA Requirements with a repetitive inspection content then each and every inspection will be recorded on completion in the aircraft airworthiness records. A CRS will be issued every time compliance with an AD/EAD/DGCA Requirement is established.

1.5 Analysis of the Effectiveness of the Maintenance Programme Pawan Hans Helicopters Limited remains responsible for this subject. The Quality Manager /

Continuing Airworthiness Manager (PCA) will analyse and monitor the effectiveness of the Maintenance Programme through regular Liaison Meetings with Part 145 Maintenance organisation.

1.5.1 Review Meetings

These meetings will address the following areas:

a) The Maintenance Programme content. b) The effect on the Maintenance Programme of any ADs, Modifications or

repairs. c) Changes to the operation, which may affect the Maintenance Programme. d) Maintenance findings. e) Other defect reports i.e. air turn-backs, spares reliability, technical

delays, technical incidents, repetitive defects and pilot reports. f) Quality monitoring product samples (aircraft surveys). g) Changes to the manufacturer's maintenance guidance material, Service

Bulletins Service Letters etc. and how these affect the Maintenance Programme.

h) Other Quality System findings as they impinge upon the Maintenance Programme.

Where appropriate and necessary, amendments to the Maintenance Programme will be promulgated by the PCA for submission to the DGCA Regional Office as an amendment.

1.5.2 Frequency of Meetings

Review meetings will be held at a minimum of six monthly intervals and the results of any meeting recorded with any actions required allocated to the responsible person.


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Accountable Manager will hold the Review meeting at least twice in a year at an interval of six months or as and when considered necessary. This meeting will be attended by Head of Quality / Quality Assurance Manager and any one whose involvement and input is necessary. The agenda for the meeting will be circulated in advance so that concerned attendees can prepare and contribute for the continuing airworthiness of Pawan Hans aircraft in a cost effective manner maintaining high standard. Review meeting will be conducted for each type of aircraft in our fleet & these meeting can be clubbed if required. Agenda for the meeting will be related to effectiveness of the Maintenance Programme, Continuing Airworthiness Compliances, Issues related to maintenance support from Pawan Hans vis-à-vis Maintenance Organization, Repetitive defects, MEL/CDL Releases / actions taken, Compliance of SB/ADs, Issues of mutual concerns. Record of such meetings will be kept by Continuing Airworthiness Manager and circulated to attendees, Accountable Manager of Pawan Hans and all concerned.

1.6 Non-Mandatory Changes (Modification) Embodiment Policy

1.6.1 Changes (Modifications) General PHHL Non-mandatory changes (modifications) will normally take the form of manufacturer's Service

Bulletins, or will be derived from them. Any other changes (i.e. those not covered by a manufacturer's Bulletin) will be initiated by the PCA, Head of Quality/ Quality Assurance Manager in consultation with the Part 145 Maintenance organisation.

1.6.2 Service Bulletins

All manufacturers‟ Service Bulletins applicable to the aircraft operated by PHHL will be

reviewed in the first instance by the post holder continuing airworthiness for applicability. Where compliance with the Service Bulletins' may be seen as beneficial to PHHL then the Part 145 organisation will be advised. All relevant SBs will be discussed during the Review Meetings.


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1.6.3 Other Changes (Modifications)

For all changes (modifications) other than those introduced by Manufacturer‟s SBs' i.e. those proposed by PHHL or Part 145 maintenance organisation for operational advantage or other reasons then these will be subject to the current DGCA change procedures. In the first instance the Regional Office will be consulted for advice with an outline of the proposed change with a view to ascertaining whether or not a change is deemed to be classified as „Major‟ or „Minor‟.

1.6.4 Minor Changes (Modifications) All minor changes will be agreed by the PCA before submission either to a suitably

approved Design Organisation or to DGCA. Where application is made to DGCA the PCA will be responsible for raising and submitting the Minor change approval application.

1.6.5 Recording of Changes (Modifications)

Incorporation of all non-mandatory changes, whether introduced through Service Bulletins

or by DGCA Approved Minor/Major change, are to be recorded in the aircraft's airworthiness records.

1.7 Major Change (Modification) Standards

All Major Changes will be raised through a suitably approved Design Organisation and submitted to DGCA by PHHL. The approval of the change will be by DGCA and will need to be recorded and held in the aircraft's airworthiness records.

1.8 Defect Reports

All defects occurring on PHHL‟s aircraft will be subject to review and analysis for their effect upon airworthiness and the safe operation of the aircraft.

1.8.1 Analysis

Flight Log Sector Record pages are examined at regular intervals by PHHL to provide

information concerning defects occurring, Pilot's reports, maintenance actions and defects of a repetitive nature.

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

PHHL maintenance organisation which may have airworthiness or operational implications.


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The continuing airworthiness manager of PHHL will assess the findings as necessary and

any action required agreed before implementation; implementation may take the form of a Maintenance Programme amendment or modification action.

1.8.2 Review with Manufacturers and Regulatory Authorities

Quality Manger may be required by the Maintenance Contract to liaise with the manufacturer(s) and the DGCA all matters concerning the airworthiness of PHHL Helicopters. The PHHL continuing airworthiness manager is to be advised when such action is necessary and will take action required to ensure the continued airworthiness of the aircraft.

1.8.3 Deferred Defect Policy

PHHL will seek to ensure by Safety Management System practices that the minimum number of open Deferred Defects exist. All open Deferred Defects will be monitored by the Engineer (Planning and Tech.Services) / Head of Quality in consultation with the Part 145 maintenance organisation to ensure earliest rectification and subsequent closure. All defects that are subject to defer PHHL action will be as per the Minimum Equipment List and its guidelines for use, which are given in the Preamble of the approved MEL.

Defects such as cracks and structural defects that are not addressed in the MEL may only

be deferred after agreement with the Type Certificate holder and that the defect is not of a safety concern, such defects shall be intimated to DGCA.

When a Deferred Defect is raised the Continuing Airworthiness Manager (LMM) will

consult with the Part 145 maintenance organisation with a view to arranging the earliest possible rectification action to be taken. This will involve the pre- allocation of down time, spares, personnel, tooling etc. as appropriate.

A Certificate of Release to Service will be issued in the Flight log upon clearance of any

Deferred Defects.


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1.8.4 Non Deferrable Defects Away from Base Where defects occur that are not listed in the MEL then the following actions must be

taken:

a) The Quality Manager and/or the Part 145 Maintenance organisation should be consulted with a view to establishing the extent of the defect and the rectification action required.

b) The Part 145 maintenance organisation will ascertain if there is a suitably approved Part 145 organisation, with the appropriate ratings on their Schedule of Approval in proximity to the AOG aircraft. Suitable contractual action will be taken to have the defect rectified, and duly certified by that organisation.

c) Where no suitably approved Part 145 maintenance organisation is available then action will be taken to position a member of the contracted Part 145 maintenance organisation's certifying staff, together with the necessary spares, tooling, and technical publications to rectify and certify the defect.

1.8.5 Repetitive Defects

Repetitive Defects means a defect in an aircraft (including its components and Systems) which recurs, in spite of rectification attempt, on the same aircraft. The Flight Log is monitored by the Continuing Airworthiness Manager to identify these defects as and when they arise. Remedial action will be taken with consultation with Quality Manager.

1.8.6 Mandatory Occurrence Reporting.

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

A Sub Part B clause M.A.202 will be reported to the DGCA within 72 hours as required.

1.8.6.1 All occurrences, which have maintenance implications, will be analysed by the Continuing Airworthiness Manager (PCA) in consultation with the Part 145 maintenance organisation. Any MORs raised by the contracted Part 145 maintenance organisation on PHHL‟s aircraft will also be advised to the Continuing Airworthiness Manager. Both organisations will hold copies of any MORs that have been raised that affect maintenance.

NOTE: Detailed procedure of occurrence reporting is laid down in Pawan Hans‟s CAME.


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1.8.7 Liaison Meetings

Liaison Meetings, in addition to those identified in Para. 1.5.1, will be held between Pawan Hans‟s Continuing Airworthiness Manager, the Part 145 maintenance organisation, the Quality Manager and any other interested parties to discuss airworthiness, quality and MOR issues. The frequency of these meetings will not be less than every six months or more frequently if operational circumstances and maintenance findings warrant it.

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

Programme/Management meeting identified in Para. 1.5.1. All of the 'formal' meetings will be recorded and minuted. All actions required in response to maintenance findings, follow up actions, audit corrective actions etc. will be duly allocated with respect to responsibility. Minutes of these meetings will be held by the Continuing Airworthiness Manager and the Part 145 maintenance organisation. The minutes will be made available on request to any duly authorised member of the DGCA.

1.9 Engineering Activity Where applicable the development and submission of changes (modification and repairs) for

approval by the agency will be coordinated by Continuing Airworthiness Manager as the person responsible for design changes.

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

Each application will be submitted to DGCA accompanied by a data pack, which provides technical justification for approval of the change.

1.10 Reliability Programs

1. Reliability programs will be developed for aircraft maintenance programmes based upon maintenance steering group (MSG) logic or those that include condition monitored components or that do not contain overhaul time periods for all significant system components.

2. Reliability programmes will not be developed for aircraft not considered as large aircraft or that contain overhaul time periods for all significant aircraft system components.

3. The purpose of a reliability program is to ensure that the aircraft maintenance program tasks are effective and their periodicity is adequate.

4. The reliability program may result in the escalation or deletion of a maintenance task, as well as the de-escalation or addition of a maintenance task


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5. A reliability program provides an appropriate means of monitoring the effectiveness of the maintenance program.

6. Appendix 1 to AMC M.A.302 and M.B.301 (d) gives further guidance.

1.11 Daily / Pre-flight / Relevant Inspections The preparation of the aircraft for flight is the responsibility of. Pawan Hans‟s engineering prior to first flight of the day. Daily inspection / relevant inspection as per CAMO approved

maintenance program will be carried out and Certificate of Release to Service issued by the operating pilot only where they are authorised to do so.

This inspection to be certified by the maintenance organisation's engineering staff, where they are available and they are authorised to do so.

1.11.1 The Pre-Flight Check

The preparation of the aircraft for flight is the responsibility of Pawan Hans‟s Pilot. Pre-flight/Turn around Check will be done prior to every flight by the pilot. For Pawan Hans Helicopters Limited aircraft: this check is defined in the flight manual.

NOTE: The pre-flight/Turn Around inspection does not require a Certificate of Release to Service and may be carried out by the Pilot without further Part 145 authorisation as this is in privileges of licence. 1.11.2 The Daily Inspection /Post Flight Inspection

Daily Inspection / After last flight inspection where ever applicable on Pawan Hans Fleet This Inspection schedule contains all items of inspection in accordance with Chapter 5 of AMM. of concerned aircraft and duly approved by Continuing Airworthiness Manager .

1.11.3 Pilot Authorisation

Pilot's certifying the Pre-Flight Inspection/Daily Inspection and/or other short term maintenance requirements must be duly authorised by the contacted Part 145 maintenance organisations' Quality Manager or by DGCA. Authorisation will be subject to the provision of suitable initial and continuation training 'on the job' with the Part 145 maintenance organisation. (Reference AMC 145.A.30 (j)(4))


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NOTE: The authorisation of any member of PHHL remains the Prerogative of the DGCA / Quality Manager 145 and may be withdrawn or suspended at any time.

The Pilots, when duly authorised, will be given an authorisation Document. The authorisation will

require the Pilots to quote their individual Authorisation Number issued by DGCA or by CAR 145 organisation.

Tasks for which Pawan Hans Pilot‟s are currently authorised are as follows: a) Pre Flight Check b) *Daily Inspection/Post flight Inspection * (may or may not be applicable from pilot to pilot) Guidance to Flight Crews on preparing the aircraft for flight is also contained in the Operations Manual Chapter 1.

1.11.4 Sub-Contracted Ground Handling Functions

Since Pawan Hans is non-scheduled operator as due to the size and nature of the Pawan Hans operation at outstation ground handling functions will be made by the agency available there at airport on case to case bases. In main base Pawan Hans is providing the services.

1.11.5 Security of Cargo and Baggage loading

The security of cargo and baggage loading is the responsibility of the pilot. Cargo and baggage will only be carried on board the aircraft in those are as specifically designed to do so and in accordance with the limitations quoted in the Flight Manual and Weight and Centre of Gravity Schedule. Further guidance to crews on this subject is contained in the Operations Manual Section A clause 9.7 Loading and securing of items in aeroplane.

1.11.6 Control of Aircraft Refuelling Quantity/Quality

The responsibility for aircraft refuelling lies with the operating Pilot at outstation whereas it is the responsibility of the engineering personal at main base and at detachments. This includes responsibility for the right quantity of fuel being carried on board for the intended flight and the


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specification and quality of the fuel taken on board. Further guidance to the Pawan Hans‟s crews on this subject is provided in the Operations Manual Chapter -8.

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

The control of snow, ice, dust and sand contamination before flight is the responsibility of the Pilot. He/she will take whatever steps they consider necessary to ensure the aircraft is free from such contamination before flight. Further guidance on this subject is contained in the Operations Manual Chapter -14.

1.11.8 Certificate of Airworthiness and Airworthiness Review Certificate Validity

Continuing Airworthiness Manger will monitor the continued validity of the Certificate of Airworthiness and Airworthiness Review Certificate. Arrangements will be made by the organisation in order that the Airworthiness Review Certificate can be issued, extended or a recommendation to reissue made to the DGCA at the prescribed periods. Monitoring of this validity is catered for by use of monitoring by a wall board or computer programme etc.

1.12 Aircraft Weighing

Aircraft weighing is performed at Pawan Hans approved maintenance organisation. The Continuing Airworthiness Manager in consultation with the Part 145 maintenance organisation will maintain a record of each aircraft operated. Re-weighing will be carried out at intervals not exceeding Five years, as & when required by relevant CAR section.

1.13 Test Flight Procedures

Test flights are only required as specified by the aircraft manufacturer and are included in the maintenance programme for instance after a particularly extensive maintenance check or major modification affecting the aircraft performance that cannot be checked on ground.

If the Certificate of Airworthiness is invalid due to modification or maintenance action, an authorised person must issue a Flight Release Certificate and a Test flight is carried out in accordance with CAR Sec 2, T part II before the Test flight is allowed to take place.


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1.14 Sample of Documents and Forms Used The examples of all documents and forms used by PHHL are given in Continuing Airworthiness

Management Procedure Manual. 1.15 Leasing of Aircraft

Not applicable at present. 1.16 General PHHL Procedures (Inc Operational Approval Procedures)

Information and reference to operational approvals and associated procedures are given in PHHL Operation Manual.

1.17 CVR / DFDR Read out Policy

As per CAR Sec 2 I part V & VI every aircraft is required to be fitted with FDR/DFDR, CVR Operational checks and evaluation of recordings from the flight data and cockpit voice recorder systems shall be conducted as per the manufacturer‟s recommendations to ensure the continued serviceability of the recorders. Proper records shall be maintained by Continuing Airworthiness Manager/Q.C.Cell for the readouts and evaluation carried out for each serial number of the FDR installed on the aircraft which should be authenticated by the Quality Manager for satisfactory recording and for completion of the specified duration of the DFDR/ FDR / CVR and preserved for a period of 30

days.

1.18 Material Auditors / Stores Inspector:

The Material Auditors / Stores Inspector are responsible for the inspection of all incoming material to Pawan Hans‟s Stores. They ensure that all materials conform to stipulated standards and are accompanied with proper documentation.

NOTE: Detailed procedure defining responsibility of Stores Inspectors is defined in Pawan Hans‟s MOE.


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2.1 Continuing Airworthiness Quality Policy, Plan and Audit Procedures This Part 2 of Pawan Hans Helicopters Limited CAME defines the continuing airworthiness

quality policy, planning and procedures to meet the requirements of CAR Subpart G. It forms part of Pawan Hans‟s Quality System required as per DGCA regulations.

2.1.1 Continuing Airworthiness Quality Policy

The Quality System and associated Quality Assurance Programme enables monitoring of Pawan Hans compliance with DGCA requirement & CAR M, the Operations Manual, Continuing Airworthiness Management Exposition and any other standards specified by Pawan Hans, to ensure safe operations and airworthy aircraft.

2.1.2 Quality Programme

The Quality Programme will be developed by the Quality Manager in liaison with the Post

Holder Continuing Airworthiness. The Quality Manager will implement an audit programme which during a twelve month period will address the whole continuing airworthiness management activity and all of the aspects of CAR which have a bearing on the continuing airworthiness arrangements of PHHL.

(This includes the audit of Pawan Hans 145 organisations & any sub-contracting activity) Additional audits are required to be carried out: A) Whenever corrective action has to be performed before the next scheduled audit. B) When maintenance procedure are newly established or revised C) Upon exchange of the nominated post holders referred to in part 0.3 D) Before subcontracting of Airworthiness management activities take place.

The Quality Programme will also address those aspects of the individual aircraft's continuing airworthiness, which would have been covered by the DGCA requirement of Maintenance Review.

The Quality Programme will also incorporate Surveys of the aircraft operated by Pawan

Hans. The Quality Programme forms Appendix 1 to this Part 2 of the CAME is held by Pawan Hans‟s Quality Manager.


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2.1.3 Quality Audit Procedure

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

particular event/action/document etc. in order to verify whether established operational and continuing airworthiness procedures and requirements are followed during the accomplishment of that event. This with a view to ensuring that the required standard is being achieved.

Every audit is undertaken by a quality auditor as part of the over PHHL audit Programme

and will be the subject of an audit report. Before distribution, the preliminary conclusions will be advised to the person(s) in charge of the areas subject to audit. The quality auditor and the persons responsible for the areas/subjects audited will determine and agree together the corrective actions to be taken. This will also define the time allowed for corrective actions to be implemented. The corrective action should be determined taking into account the root cause of the finding, such that the corrective action may be carried out in a fashion that will prevent possible re-occurrence of the finding.

The audit reports are distributed to the following persons

a) The person responsible for the audited areas/department b) The Accountable Manager of PHHL c) The Continuing Airworthiness Manager d) The Part 145 maintenance organisation. e) Quality Manager NOTE also that as a minimum, it would be recommended that at least two audits per annum are

performed. These should preferably occur just before any scheduled Liaison Meeting so that the necessary actions can be agreed with all parties present.

The Part 145 maintenance organisation will be responsible for any findings/concerns that affect the contracted Part 145 maintenance organisation and ensuring that appropriate corrective action measures are implemented.

2.1.4 Findings

(a) A level 1 finding is any significant non-compliance with CAR-M requirements which lowers the safety standard and hazards seriously the flight safety.

(b) A level 2 finding is any non-compliance with the CAR-M requirements which could lower the safety standard and possibly hazard the flight safety.


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(c) After receipt of notification of findings a closing date is to be identified mutually by the auditor & auditee, also a corrective action plan is defined by the auditee.

2.1.5 Quality Audit Remedial Action Procedure

o The QM monitors the remedial actions and their compliance. o The remedial actions are taken by the concerned person. o The QM agrees time for correction with the Continuing Airworthiness Manager. o He shall check if every corrective action has been applied in due course and shall record

the corrective actions in his audit reports in the appropriate box. o The audit report shall show by whom the corrective action was carried out and when the

QM made the check. o If no corrective or insufficient action has been taken, the QM shall inform the CAM

accordingly. All the non-conformities raised during Audit are identified and segregated. All "CAF" are evaluated and analyzed by Regional Quality Manager along with the departmental Heads to arrest the potential causes of non-conformities.

Departmental Heads initiate the correction action to rectify the deficiencies observed during the Audit.

All the CAFs along with corrective and preventive action taken are submitted to the Regional Quality Manager for acceptance and effective control of non-conformity.

All non-conformities connected with maintenance work are reviewed and disposed off by the AME I/C at the Sub-base and at region same are disposed off by departmental Heads. In case of disposition of any non-conformity is beyond the capacity of the departmental or necessary action. Any non-conformity which needs evaluation and review by DGCA is disposed off only after obtaining due clearance from DGCA.

FOLLOW UP AUDIT: A follow up monitoring actions is decided by the Regional Quality Manager / his

representative to verify that the corrective and preventive actions are implemented and the CAF is signed as satisfactory and closed. In case of unsatisfactory result, a fresh CAF is issued and the process is repeated.


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2.2 Monitoring of the Operators Continuing Airworthiness Management Activities The Audit Plan includes an assessment of the Continuing Airworthiness Management activities

against the procedures defined in the CAME and in particular the ability of the Continuing Airworthiness Coordinator‟s ability to discharge their responsibilities effectively with respect to CAR.

2.2.1 Quality Audit of Aircraft / Survey of Aircraft

During time Helicopters is in major / minor inspection, survey of aircraft may be carried out by CAMO Quality auditor in form of spot check / product audit any discrepancies NOTED will form a level of finding & same will be notified to concern persons in 145 organisations.

2.3 Monitoring of the Effectiveness of the Maintenance Programme The Audit Plan as carried out by Quality Manager includes a review of the effectiveness of the

Maintenance Programme. This review will critically analyse the findings and actions taken as a result of Para. 1.5 of this CAME.

NOTE: Detailed procedure for above is defined in Pawan Hans‟s CAME

2.4 Monitoring that all Maintenance is Carried Out by an Appropriately Approved Part 145

Organisation Pawan Hans Helicopters Limited is approved under CAR 145 to carry out maintenance of

Helicopter.The Annual Audit Plan includes Part 145 maintenance organisation's activity approval granted by the DGCA is relevant to the maintenance being performed on the aircraft operated by Pawan Hans.

Any feed back information requiring amendments to the maintenance contracts for aircraft,

engines or components should be reviewed and the contracts amended accordingly. 2.5 Monitoring that all Contracted Maintenance is Carried Out in Accordance with the

Contract, including Sub-contractors used by the Maintenance Contractor The Audit Programme will include a review of all maintenance provided to Pawan Hans by the

contracted Part 145 maintenance organisation, including sub-contractors if any. This review will assess all of the contracted maintenance is carried out in accordance with the Maintenance Contract.


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QUALITY SYSTEMS

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2.6 Quality Audit Personnel Qualification

a. All personnel involved in the Audit process will be trained for the appropriate Audit training, such as Audit technique and appropriate method of reporting and recording as per the part of Quality Audit system.

b. Senior person of the Company having at least 10 years of maintenance and operational

experience in the company may be nominated to carry out Quality Audit.

c. The Quality auditors should have AME License or such other equivalent qualification issued by a competent authority in Aircraft Maintenance or pertinent experience in continued airworthiness management

d. The Auditor should not have any day to day involvement in the area of maintenance or

operational activities that is to be audited. Auditors will have freedom to access to all work area, files and records.

e. The Auditors must be able to conduct Audit in accordance with Quality Audit Personnel and

report and record all finding and discrepancies to enable them to be dealt with close loop process.

f. All personnel involved in the Audit process will be trained for the appropriate Audit training,

such as Audit technique and appropriate method of reporting and recording as per the part of Quality Audit system.

g. Where persons act as a part time auditor, it will be emphasized that this person must not be

directly involved in the activity he/she audits.

Training:

The quality audit personal shall be trained in a manner to fulfill the required knowledge to perform quality audit checks. The quality auditor must be trained for the following as minimum.

1) CAR-M 2) Quality management 3) Audit technique 4) Technical expertise on the subject audited


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2.6.1 Independent Auditors (NR):

The following personnel have been appointed as independent auditors taking the qualification and experience into account as specified in Part II Para 2.6.

a) Mr. Ajay Singh (Sr. Manager, Engg) b) Mr. Yash Pal (Engr-D)

2.6.2 Independent Auditors (WR):

The following personnel have been appointed as independent auditors taking the qualification and experience into account as specified in Part II Para 2.6.

a) Mr. P M Gupte DGM (Line Maint) WR b) Mr. P K Sen Sr Manager (Engg) WR

2.7 Quality Audit of Aircraft The purpose of quality audit of Aircraft is to ensure that all required Continuing

Airworthiness task are performed on the Aircraft and shall not be considered as periodic Airworthiness review of the Aircraft.

a. Quality audit of Aircraft are tools to have a feedback on quality level of the

Organization to the management

b. The quality audits of the Aircraft do not affect the airworthiness review certificate but are submitted to the airworthiness manager for necessary corrective action.

c. Audit of aircraft shall be carried out along with Line Maintenance / Detachment Audit as per the procedure described in Chapter „Quality Audit of Organization Procedures‟, Part 3, Section 3.1.

PHHL shall carry out „Quality audit‟ of aircraft as per detailed procedures in Continuing Airworthiness Management Procedure Manual.

To accomplish this, the auditor must consider all processes that contribute to PHHL‟s

ability to issue CRS to the aircraft. The audit shall cover at least:-

1) Certifying Staff and Manpower used 2) The applicable Maintenance Data, work instructions (inspection schedules / work

cards etc.) and procedures used 3) Demonstrate compliance with the Approved Maintenance Program used. 4) Tooling & Equipment utilized 5) Spares and Material used 6) Facility used 7) Compliance with approved procedures; 8) Contracted maintenance is carried out in accordance with the contract; 9) Continued compliance with CAR.

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2.7.1 The Audit Program

The prime objective of Quality Department is to ensure, the organization is in compliance with Regulatory Requirements, Company Procedures, and Airworthiness to ensure that they comply with Engineering Procedures and remain within the scope of the terms of approval and requirements of DGCA as published.

This is ensured by means of a Quality Audit Program and continual monitoring of the effectiveness of Maintenance Department activities to achieve the above.

The area required to be audited are as follows:

- CAMO Procedures - Maintenance Program Development, Compliance & Amendment Procedures - AD / SB Recording Procedure - CVR/ DFDR Read out/ Record Procedures - Occurrence Reporting Procedures - Records up keeping - Contracted 145 Organisation

NOTE: Detailed Audit Plan is included in Appendix 3 of Part 5 Appendices of this CAME. Employees:

Qualification, experience and Job descriptions of all staff are held on file with the respective sectional manager who also has responsibility for the upkeep of these job descriptions.

All employees are required:

To carry out activities only in accordance with their skills, qualifications and authorizations as specified in the applicable organizational documentation.

To immediately report potential risks or errors or defects that occur, to the responsible sectional manager and to notify the responsible offices via the recording and reporting systems provided for this purpose.


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CONTRACTED MAINTENANCE PART 3

PAGE NO. 01

3.0 Contracted Maintenance Presently PHHL is approved under CAR 145 to carry out maintenance on Helicopters

being operated and does not have any maintenance arrangement with any maintenance organization. In case any maintenance is outsource to a contractor the selection procedure describe in Para 3.1 of this section shall be applied.

3.1 Maintenance Contractor Selection Procedure

Before any contract is signed with a maintenance organisation the Continuing

Airworthiness Manager will verify that: a) The maintenance organisation is appropriately approved in accordance with Part

145, and has the necessary qualified manpower, facilities, tooling, technical documentation etc. This verification to take into account any engine, propeller, or component maintenance capability that may be required (though this may be available through sub-contract to other suitably approved Part 145 MOs.)

b) It will be confirmed that the maintenance organisation has adequate capacity to

undertake the proposed maintenance support. Where this includes aspects of the continuing airworthiness management then experience will be criteria to be considered.

b) The draft Maintenance Contract will be reviewed and agreed by both parties with a

view to ensuring that each has the ability to discharge their responsibilities with respect to CAR M

3.1.1 Advising the DGCA of Changes to the Maintenance Support

The DGCA Regional Airworthiness Office and Flight Operations Department of PHHL will

be advised of any proposed continuing airworthiness management arrangements in writing giving the notice required by CAR Subpart G.

Changes to the nominated Maintenance Contractor will be advised to DGCA Regional

Office giving the 30 days notice. Part 0.5 of this CAME also refers.

3.2 Detailed List of Maintenance Contractors

The current Part 145 Maintenance Contractors is nil.:


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PAGE NO. 02

3.3 . Relevant Technical Procedures Identified in the Maintenance Contract(s)

NOT APPLICABLE

3.4 Aircraft Operated

Pawan Hans Helicopters Limited currently operates the following aircraft

NORTHER REGION HELICOPTER TYPE REGN

BELL 206 L4 VT-PHA,VT-PHD,VT-PHE BELL 407 VT-PHH,VTPHI, VTPHN,VT-PHQ,

DHRUV (ALH) VT-HAR,VT-HAN, VT-BSJ,VT-BSK, VT-BSS, VT-BSM, VT-BSP,

AS350 ECUREUIL B3 VT-PHU,VT-PHV

WESTERN REGION

HELICOPTER TYPE REGN

DAUPHIN SA 365N VT-ELB,VT-ELD,VT-ELE,VT-ELG,VT-ELI,VT-ELJ, VT-ELK,VT-ELL,VT-ELM,VT-ELN,VT-ELP,VT-ELQ VT-ELR,VT-ELS,VT-ELT, VT-ENW,VT-ENX.VT-ENZ

DAUPHIN AS 365N3 VT-PHJ,VT-PHK,VT-PHL,VT-PHM,VT-PHO,VT-PHR, VT-PHS,VT-PHW, VT-PHX, VT-PHY, VT-PHZ, VT-PWA, VT-PWB, VT-PWC, VT-PWD, VT-PWE, VT-PWF,

MI 172 VT-PHG

3.5 Quality audit of sub-contracted CAR tasks The Quality audit will ensure that the continuing airworthiness functions sub-contracted out, has taken care of

Compliance with approved procedures;

Contracted continuing airworthiness functions are carried out in accordance with the contract;

Continued compliance with CAR M

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PAGE NO. 03

3.6 PROCEDURE FOR AWARDING WORK TO SUB-CONTRACTORS

3.6.1 PURPOSE The purpose of this procedure is to establish a uniform and consistent method for servicing / repair / testing of helicopter components / rotables / engines by approved repair agencies. 3.6.2 SCOPE The scope of this procedure extends to servicing / repair / testing carried out by repair agencies approved abroad as well as within the country by regulatory body of the country of repair agency / DGCA for which servicing / repair / testing facilities do not exist within Pawan Hans Helicopters or cases where Pawan Hans lacks the resources / expertise for the said repair works. 3.6.3 PROCEDURE 3.6.3.1 Criteria for assessment and selection of sub-contractors for repair / servicing / testing of helicopters including engine covers following features.

a) Previous experience of sub-contractors for similar type of repair in case of new sub-contractor

b) Comparable repair change for similar components c) Authorisation for carrying out repair by the regulatory body of the country of repair

agency / DGCA d) Whether the sub-contractor is an authorised repair / service centre of original

equipment manufacturer. e) Previously demonstrated performance in terms of turn-around time, quality and

response time in case of already existing repair agencies. f) Awarding of contract will be through an internal tender processing governed by the

existing company tendering policy. 3.6.4 In cases where the sub-contractors does not meet the selection criteria as given in 3.6.3.1 the QM or the representative shall ensure that the sub-contractors meets the following requirements to ensure observance of airworthiness standards.

a) A record keeping system pertaining to incoming certificates, test, calibrations, specifications and inspection performed during various stages of processing, identification method and inspection before release of item by the sub-contractor

b) A duly qualified person to ensure that quality of processed part is maintained till the final stages of the process.

3.6.5 Based on above factors a maintenance and repairs contract is entered into for a specified period or for a specified component. Generally the contract is for one year which may be extendable on yearly basis based upon performance of the repair agency.

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AIRWORTHINESS REVIEW PROCEDURES (M.A.710) PART 4

PAGE NO. 01

Airworthiness review of aircraft operated under PHHL as a CAMO organisation will be carried out by DGCA. Recommendation with appropriate application to issue & for extension of Airworthiness Review Certificate (ARC) will be made to DGCA Office at least 10 days prior to date of expiry of ARC.

When the aircraft has remained within a controlled environment, the extension of the validity of the airworthiness review certificate does not require an airworthiness review but only a verification of the continuous compliance with M.A.902 (b)., This verification of compliance will be done by PHHL‟s Airworthiness Review Staff, & recommendation to extend the validity of ARC will be made to DGCA, with all supporting documents.

4.1 Airworthiness review staff

Qualification and experience required for Airworthiness Review Staff will be as follows:

The Airworthiness Review personnel shall meet the following requirements:

a. He/She shall have an appropriate category of AME licence. He/She must have Diploma in Engineering in appropriate branch. OR He/She must have Degree in Engineering in appropriate branch b. Shall have at least 10 years Practical experience in maintenance and certification

of Helicopter out of which. c. He/She must hold position as a Manager in PHHL Engineering Organization

NOTE:

1. PHHL Airworthiness review staff, acceptable to the competent authority, should have conducted or associated with a full airworthiness review under supervision prior to their nomination as Airworthiness Review Staff

2. If the airworthiness review personnel do not hold license on type issued by DGCA for

the aircraft being physically surveyed, a suitably type rated licensed engineer should be utilised to assist with this part of the review.

3. PHHL will retain records of airworthiness staff for a period of 2 years after the person

has left the employment of PHHL


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PAGE NO. 02

4. For carrying out Airworthiness review of PHHL Aircraft .an Airworthiness Review Cell will be formed within the Quality Department. qualified certifying staff assisted by a group The staff will ensure all compliance of the requirements such as inspections due, components due and AD, SB compliance etc. The minimum qualifications required for issue of the approval to the airworthiness review personnel are as per the guide lines

given at M.A.707. 4.1.1 CAMO Staff training

Training for CAMO personnel will be conducted once every six months on regulation, latest CAR, CAR M and CAR 145 requirements procedure and trends. This training will be recorded and a copy of the minutes, be circulated to all post holders.

4.2 Airworthiness Review General PHHL Procedures The Airworthiness review on all Aircraft is carried out annually. The various date of the

ARA (Annual Review of Airworthiness) of the Aircraft is staggered for effective compliance the review. After carrying out the review as per a schedule, prepared and approved separately by the Continuing Airworthiness Manager, a log book entry is made on the white pages of the Aircraft log book.

4.3 Review of aircraft records All the maintenance records are monitored separately by the Quality Cell. Certain Aircraft

are monitored separately by contracted Maintenance agency, for which a separate contract exists. These records can be accessed at time & as when required. The information available through these agencies is considered only as an advisory nature.

4.4 Physical Survey Physical checking and confirming of the Aircraft and its documents are necessary to keep

the high standard of Airworthiness. The personnel deputed by PCA will carryout such task with particular attention to Part 4, para 4.7 (b) and should have thorough knowledge of the same. The physical survey shall also assess the material state of the helicopter and check for leaks, corrosion, cracks, chafing of cables and interference of pipelines / hoses installed etc. A register will be maintained covering the date of audit, registration and the type of Aircraft.

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4.5 Aircraft airworthiness review Documentation

The recommendation sent to DGCA in a format of form & will contain the items described as follows; (a) General PHHL information

- M.A. Subpart G organisation information – (Approval Copy) - Owner/lessee information - Date and place the document review and the aircraft survey were carried out - Period and place the aircraft can be seen if required by DGCA (b) Aircraft information - Registration - Type - Manufacturer - Serial number - Flight manual current reference - Weight Schedule and centre of gravity data - Approved Maintenance programme Reference

(c) Documents accompanying the recommendation - Copy of registration papers - Copy of the owners request for a new airworthiness review certificate

(d) Aircraft status - Aircraft total time and cycles - List of persons or organisation carried out continuing airworthiness activities including

maintenance tasks on the aircraft and its components since the last airworthiness review certificate (In last 12 Months)

(e) Aircraft survey - A precise list of the areas of the aircraft that were surveyed and their status


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PAGE NO. 04

(f) Findings - A list of all the findings made during the airworthiness review with the corrective action

carried out (g) Maintenance - A copy of the work packages requested by the subpart G organisation including details of any bridging check to ensure all the necessary maintenance has been carried out. NOTE: The above requirement will be complied only when it is new issue of ARC of

aircraft & is may or may not be carried out on time of extension, as decided by PCA. (h) Statement

A statement signed by the airworthiness review staff recommending the issue of an airworthiness review certificate. The statement will confirm that the aircraft in its current configuration complies with the following: - Airworthiness directives up to the latest published issue, and; - Type certificate datasheet, and; - Maintenance programme, and; - Component service life limitations, and; - The valid weight and centre of gravity schedule reflecting the current configuration of the aircraft, and; - For all modifications and repairs, and; - The current flight manual including supplements, and; - Operational requirements.

(i) Aircraft Test flight

- A copy of the Test flight report, as per requirement laid down in CAR Sec 2, series T part II or when new aircraft‟s ARC issued.


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PAGE NO. 05

4.5.1 ARC Renewal Logic

4.6 Recommendation to competent authorities for the issue of Airworthiness Review

Certificates (DGCA Form 15a)

PHHL will make a recommendation report along with application as per CAR Sec 2 series F part III appendix I along with prescribe fee to DGCA. Document as required will be attached with application.

The application is made by the authorized person of PHHL Continuing Airworthiness Manager Region addressed to Director General PHHL of Civil Aviation (DGCA).

Aircraft in controlled

environment for more than

12 month?

YES

ARC Renewal Logic

ARC already extended more than

Twice ?

CAMO recommends to DGCA for issue

of new ARC

NO

NO

YES

CAMO recommends DGCA for extension (does not require an airworthiness review but only a verification of the continuous

compliance)

CAMO show compliance & recommends to DGCA

to Issue NEW ARC


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PAGE NO. 06

4.7 Issuance of Airworthiness Review Certificates (CA Form 15a)

Airworthiness review To satisfy the requirement for an M.A.902 airworthiness review of an aircraft, a full Documented review of the aircraft records shall be carried out by PHHL in order to be satisfied that:

1 airframe, engine and propeller flying hours and associated flight cycles have been properly recorded, and;

2 the flight manual is applicable to the aircraft configuration and reflects the latest revision

status, and; 3 all the maintenance due on the aircraft according to the approved maintenance programme

has been carried out, and; 4 all known defects have been corrected or, when applicable, carried forward in a controlled

manner, and; 5 all applicable airworthiness directives have been applied and properly registered, 6 all modifications and repairs applied to the aircraft have been registered and are approved

according to CAR 21 or equipment, and; 7 all service life limited components installed on the aircraft are properly identified, registered

and have not exceeded their approved service life limit, and; 8 all maintenance has been released in accordance with this Part of CAR , and; 9 the current mass and balance statement reflects the configuration of the aircraft and is valid,

and; 10 The aircraft complies with the latest revision of its type design approved/ accepted by the

DGCA. a) The approved PHHL airworthiness review staff shall carry out a physical survey (if

required) of the aircraft. For this survey, airworthiness review staff not appropriately qualified to the licensing requirements shall be assisted by such qualified personnel.

b) through the physical survey of the aircraft, the airworthiness review staff shall ensure that: i. all required markings and placards are properly installed, and; ii. the aircraft complies with its approved flight manual, and; iii. the aircraft configuration complies with the approved documentation, and; iv. no evident defect can be found that has not been addressed according to

M.A.403, and; v. No inconsistencies can be found between the aircraft and the paragraph (a)

documented review of records.

c) By derogation to M.A.902 (a) the airworthiness review can be anticipated by a maximum

period of 90 days without loss of continuity of the airworthiness review pattern, to allow

the physical survey for review to take place during a maintenance check.


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PAGE NO. 07

d) An M.A.902 airworthiness review certificate (CA Form 15b) or a recommendation is

issued by appropriately authorized M.A.707 airworthiness review staff on behalf of the

approved continuing airworthiness management organization (PHHL) when satisfied that

the airworthiness review has been properly carried out.

e) A recommendation report for issue/extension airworthiness review certificate along with

copy of ARC in case of extension will be sent to Regional Airworthiness Office, DGCA,

and India 10 days prior to the date of expiry of ARC.

f) Airworthiness review tasks shall not be sub-contracted.

g) Should the outcome of the airworthiness review be inconclusive, the Regional

Airworthiness Offic, DGCA will be informed; informed assigning reason there to.

4.7.1 Distribution of AIRWORTHINESS REVIEW CERTIFICATE (CA Form 15A/15B)

1. Aircraft Records – Original copy 2. Quality Manager(Region) 3. Continuing Airworthiness Manager (Region) 4. copy to DGCA (RAWO)

The condition under which the ARC may be extended

1. Any Natural calamity beyond control of PHHL 2. Aircraft under going Major Maintenance /Major Repair/ Major Modification(s). 3. Aircraft grounded due to technical reason/Incident at a station other than station

where ARA can be undertaken. 4. An airworthiness review certificate cannot be issued nor extended if there is evidence

or reason to believe that the aircraft is not airworthy.

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4.7.2 AIRWORTHINESS REVIEW CERTIFICATE To ensure the validity of the aircraft airworthiness review certificate and its continuing airworthiness records an audit & review will be carried out at least once in a year from the date of issue the previous ARC. This will be included as part of Quality audit conducted by quality auditor on CAMO process & records. 4.8 Airworthiness review records, responsibilities, retention and access

Airworthiness Review Records will be kept in Quality Cell in the Engineering Department.

The Records will be accessible only to the authorised personnel i.e. Quality Manager, Continuing Airworthiness Manager, Accountable Manager or any person authorised

These documents will be provided to DGAC Official for scrutiny as and when required by them.

Engineer/Planning and Technical Services will be responsible for the record keeping.


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PART 5-APPENDICES-SAMPLE OF DOCUMENT

PART 5

PAGE NO. 01

PART DESCRIPTION APPENDIX

5.1 Sector Record Page/Flight– Dauphin SA365N

Sector Record Page/Flight – Dauphin AS365N3

Sector Record Page/Flight – MI-172

Sector Record Page/Flight – BELL

Sector Record Page/Flight –Ecureuil

Certificate of Released to Service

Audit Plan

Appendix -1.1

Appendix -1.2

Appendix -1.3

Appendix -1.4

Appendix -1.5

Appendix-2

Appendix-3

5.2 List of Airworthiness Review Staff

5.3 List of Sub-Contractor Appendix -4

5.4 Not Applicable

5.5 Not Applicable

5.6 Not Applicable

5.7 Airworthiness Review Report Appendix -5

5.8 Review Certificate

5.9 Compliance Checklist (Enclosed)

5.10 Details of Aircraft Managed by the Organisation Appendix -6

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APPENDIX 1.1

5.1 Sector Record Page / Tech log /Flight Report Page A. Dauphin SA365N Helicopter


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APPENDICES

PART 5

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5.1 Sector Record Page / Tech log /Flight Report Page B. Dauphin AS365N3 Helicopter

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5.1 Sector Record Page / Tech log /Flight Report Page APPENDIX 1.3 C. MI-172 Helicopter

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APPENDIX 1.4 5.1 Sector Record Page / Tech log /Flight Report Page

D. Bell Helicopter

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APPENDIX 1.5

5.1 Sector Record Page / Tech log /Flight Report Page E. Ecureuil Helicopter

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APPENDICES

PART 5

PAGE NO. 7

5.1


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5.1 APPENDIX 3 CAMO Quality System – Audit Plan

Weeks→

January 1 2 3 4

February 1 2 3 4

March 1 2 3 4

April 1 2 3 4

May 1 2 3 4

June 1 2 3 4

July 1 2 3 4

Aug 1 2 3 4

September 1 2 3 4

October 1 2 3 4

November 1 2 3 4

December 1 2 3 4

Group 1 I 2 3 4 5 6

Group 1 II 2 3 4 5 6

Group 1 III 2 3 4 5 6

Group 1 IV 2 3 4 5

Group-I : 1) Line Maintenance Group-II : 1) Engine Bay Group-III : 1) Radio Shop Group-IV : 1) Main Store 2) Major Maintenance 2) C R S 2) Electrical Shop 2) POL Store 3) Tool Crib 3) MRB Shop 3) Instrument Shop 3) Progress Cell 4) Ground Equipment 4) Safety Shop 4) Booster Pump Overhaul Shop 5) CAMO Procedures 5) Synthetic Panel Shop 5) Battery charging Room 6) SOAP Lab 6) CVR/DFDR Readout Sh


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5.1

CAMO Procedures audit – biannually

S/N Ref. Description Jan Feb Mar Apr May Jun Jul Aug Sept Oct Nov Dec

1. M.A. 201 Responsibilities

M.A. 703 Extent of approval

M.A. 715 Continued validity of approval

M.A. 705 Facility

M.A. 706 Personnel

2. M.A. 801 Aircraft certificate of release to service

M.A. 802 Component certificate of release to service

M.A. 803 Pilot-owner authorization service

M.A. 903 Transfer of aircraft registration within India

3. M.A. 501 Installation

M.A. 502 Component maintenance

M.A. 503 Service life limited components

M.A. 504 Control of unserviceable components

4. M.A. 401 Maintenance data

M.A. 402 Performance of maintenance

M.A. 403 Aircraft defects

M.A. 202 Occurrence reporting

Audit Cycle 1st Audit Cycle 2ND Audit Cycle

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5.1

CAMO Procedures audit – biannually

S/N Ref. Description Jan Feb Mar Apr May Jun Jul Aug Sept Oct Nov Dec

5. M.A. 301 Continuing airworthiness tasks

M.A. 302 Maintenance programme

M.A. 303 Airworthiness directives

M.A. 304 Data for modifications and repairs

6. M.A. 305 Aircraft continuing airworthiness record system

M.A. 306 Operator‟s technical log system

M.A. 307 Transfer of aircraft continuing airworthiness records

M.A. 714 Record keeping

M.A. 709 Documentation

7. M.A. 704 Review of CAME

M.A. 708 Continuing airworthiness management

M.A. 707 Airworthiness review staff

M.A. 710 Airworthiness review

M.A. 713 Changes to the approved CAMO

8. M.A. 711 Privileges of the CAMO

M.A. 712 Quality system

M.A. 901 Aircraft airworthiness review

M.A. 902 Validity of the airworthiness review certificate

M.A. 904 Airworthiness review of aircraft imported into India

Audit Cycle 1st Audit Cycle 2ND Audit Cycle

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5.2 LIST OF AIRWORTHINESS REVIEW STAFF 5.2.1 NORTHERN REGION

AIRWORTHINESS REVIEW STAFF AIRWORTHINESS REVIEW AUTHORISATION REFERENCE

NAME BELL 407 BELL 206L4 AS 350 B3 DHRUV ALH

SUNIL KUMAR √ x x x

SUVOJIT ROY √ √ x x

PYARE LAL √ √ x x

ADRISH RAY √ √ x x

SATNAM SINGH √ √ x x

N. A SIDDIQUI √ x x x

BINOD SAHU x √ x x

ASHOK KUMAR DANG x x √ x

ILANGOVAN P x x x √

RITESH S. HEJMADY x x x √

SHRINIWASAN K x x x √

JEEVAN PRAKASH BEHERA x x x √

SUBRATO CHANDA x x x √

SUNIL JUNEJA x x x √

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PART 5

PAGE NO. 12

5.2.2 WESTERN REGION

AIRWORTHINESS REVIEW STAFF AIRWORTHINESS REVIEW AUTHORISATION REFERENCE

NAME DAUPHIN SA

365 N

DAUPHIN AS 365 N3

MI-172

V C KATOCH x x √

A ASOKAN

√ √ x

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APPENDICES

PART 5

PAGE NO. 13

5.3 APPENDIX 4 List of sub-contractors as per AMC M.A.201 (h)1 and M.A.711(a)3

Pawan Hans Helicopters Limited sub contracts certain task to other approved competent agencies for fulfilment of the same.

Before awarding any contact to any such agencies, Head of Quality/ Quality Assurance Manager or his deputed personnel will audit the organisation for confirming its ability to complete the assignment.

Record of such audit will be maintained by Quality cell. On the basis of the report PHHL will award such task periodically.

An annual audit will be carried out on such organisation for its continued acceptance. Presently following organisations are in the list of Subcontractors.

S/N Supplier Name & Address Repairs/Calibration

11. Brenco Aerospace Pvt. Ltd., 171-173 Fairbairn Road Sunshine 3020 Victoria Australia

Repair/Overhaul of engine components of the Turbomeca Arriel 8

12. M/s Kazan Helicopters, 4200085, Kazan, Russia.

MI-172 H/C & Spares.

13. General Director, Spetstenhno Export, Subsidiary of the State Co. Ukrespets Exports, Ukraine-254119, 36, Deotyarivska Str Kylv.

MI-172 H/C Spares.

14. M/S Singapore Precision Pte Ltd. Singapore. Repair & Overhaul of Nose Wheel, Main Wheel, Brake, Restrictor, Locking System, Actuating Jack, Drag strut jack, Auxiliary leg, Main Landing Gear.

15. M/S Curtis Wright Accessory Services, USA Servo Control

16. M/S Goodrich Control Systems, Pte .Ltd, Singapore. Tail Rotor Actuator, Main Rotor Actuator

17. M/S Sagem (M/S Sfim & M/S Aviac Technologies are merged with M/S Sagem) France.

Accelerometer, Control Box, Amplifier Box, Air data Generator, Actuator, Trim Actuator, Computer coupler, Gyro Compass


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5.3

S/N Supplier Name & Address Repair/Calibration

18. M/S Aviabaltika Aviation Ltd , Lithuania. MI-172 H/C Spares

19. M/S Klimov Corporation , Russia. MI-172 H/C Spares Engine

20. M/S Helisota Ltd, Lithuania. MI-172 H/C Spares MGB‟s Cooler Warning Unit

21. M/S The State Enterprise Kharkiv Machinary Plant, Ukraine

MI-172 H/C Spares Fuel Control Unit.

22. M/S Spare Russia Repair/Overhaul & brand new spares of MI-172 H/C Spares (not yet received any Repair contract)

23. M/s Air Works India (P) Ltd. Santacruz (E), Mumbai-49.

H/C Spares/Tools

24. M/s Max Aerospace & aviation Ltd. Malkani Chambers, Vile Parle (E), Mumbai

CVR

25 M/s Aplab Ltd. Deodhar Cenet,424, Marol Maroshi Road, Andheri (E), B13 Mumbai 400059.

D.C. Regulator

26. M/s Instrulab Abu Illan II GSI Road, Santacruz, Madras.

HSI, Gyro Compass, Calibration of instruments

27. M/s BOC India Ltd. Godrej Soaps Complex, 3rd Floor, Vikroli, Mumbai 79.

Argon Gas Cylinder

28. M/s Air India Santacruz, Mumbai.

Starter Generator, Voltage Regulator.

29 M/s Kamal Carpets 9th Patanural Chal, Paliram Road, Andheri(W)

Seat Cover

30 M/s Aretic India Sales 3/9 TV Industrial Estate, Worli, Mumbai.

Ball Bearing

31 M/s B.F.Goodrich Aerospate, Aircraft Eva.System 5th Main Ind.Suburban, 2nd Stage Yashwanttrar, Bangalore.

Helium Cylinder

32 M/s Hindustan Aeronautics Ltd. HAL, PO, Hyderabad.

Strobex, Balancer


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5.3


33 M/s ERTL Limited Plot No. F.7/8, M.I.D.C. Area, Opp. SEEPZ, Andheri (E), Mumbai 93.

Vernier, Micrometer

34 M/s Arial Service Private Ltd. Juhu Airport, Vile Parle (W), Mumbai

GPS 150

35 M/s Control Services 205, Shakti Chambers, 172, Samuel Street, Masjid Bandar 09.

Glass Rotameter

36 M/s Blue Star Ltd. Unit No.1, Prabhadevi Ind. Estate, Vir Savarkar Marg, Prabhadevi.

Radar Test Set

37. M/s Million Air Mumbai.

H/C Spares/Tools

38. M/s Indemar Ltd. Juhu Airport, Mumbai

H/C Spares/Tools

39. M/s Phillips India Ltd. Annie Besant Road, Worli, Mumbai

Philips Oscilloscope

40. Varian India Pvt. Ltd. 2nd Floor, CC chambers, Saki Vihar Road, Powai, Mumbai-72.

Service and Maintenance of Analytical Instrument.

41. Cali-Labs Pvt. Ltd. HX-21, E-7 Area Colony BHOPAL-462016

Air/Oxygen/Nitrogen Pressure Gauges

42. JOST‟S Engineering Company Ltd, Great Social Building, Sir Phirozeshah Metha Road, MUMBAI – 400001.

Engine Vibration Meter

43. Off Shore Testing Inspection Service (India) Pvt Ltd, W-347, Pawane, Thane Belapur Road, Navi Mumbai-400703

Calibration of Measuring & Test Equipment & NDT.

44. Aero Oil Pvt .Ltd., 2, Leela Apartments, Yari Road, Versova Andheri(W), Mumbai-400 061

Storage and distribution of aviation lubricants, greases, aviation sealants.


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5.3


45. Air Works India Engg. Pvt. Ltd., Mumbai International Airport Mumbai- 400 029

To carry out Non Destructive test on various aircraft parts. To carry out testing of a/c furnishing material.

46. Bombay Flying club Juhu Aerodrome, Vile Parle(E) Mumbai – 400 056

Overhaul, testing, modification, repair & calibration of instruments. Calibration/testing and check of mater gauges and instruments viz. Landing compass, pressure & suction gauge, torque wrench, tensiometer, ammeter and voltmeter.

47. Indrox Chemicals Ltd. Nirlon House, 254B, Dr. Annie Besant Road, Worli, Mumbai –400 025

Storage and distribution of products trade named INDROX manufactured by M/s Chemitall-Rai India Ltd.

48. Loctite India Ltd. 38, Marol Co-0p.Ind. Estate, M.V. Road,Sakinaka Andheri(E), Mumbai – 400 059

Manufacture of Loctite products as per relevant MIL/ASTM specifications.

49. Hyderabad Batteries Ltd. Lalgudi Malakpet, Shameer pet Mandal R.R District., Hyderabad

Manufacture of Ni-Cd batteries.

50. Instrulab No.11 GST Road, Tambaram, Sanatorium Chennai

Overhaul of instrument installed on aircraft upto 15000 Kg AUW Overhaul of electrical equipment on aircraft upto 15000Kg.

51. Veesem Raytech Aerospace Ltd. Chelekere, Ring Road, Banaswadi Post Bangalore

Repair, overhaul and modification of types of DERs/SSDFRs of Fairchild Repair , Overhaul and modification of CVRs/ Control units of Fairchild

52. Bell Helicopter Textron, U.S.A. and its Directory


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PART 5

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5.7 APPENDIX 5 Airworthiness Review Report PHHL will not significantly change the format or content of the CAME Airworthiness

Review Report version. It is acceptable for example to insert a company logo or produce an electronic version for ease of printing.

PHHL CONTINUING AIRWORTHINESS MANAGEMENT EXPOSITION

AIRWORTHINESS REVIEW REPORT

NOTE: A COPY OF THIS REPORT TO BE RETAINED IN THE AIRCRAFT RECORDS.

ORGANISATION NAME APPROVAL REFERENCE NUMBER

1. AIRCRAFT DETAILS

Registration ………………………………

Type, Designation and Series ………………………/…………………/………………………..

Serial No. ………………/………………

Current Flight Hours/Cycles ………………/………………

Hours/Cycles at 31 December ………………/………………

Engine Type (1)…………………(2)….………..………(3)……………………..(4)……………….

Serial No (1)…………………(2)….………..………(3)……………………..(4)……………….

Hours/Cycles (1)…………………(2)….………..………(3)……………………..(4)……………….

Propeller (1)…………………(2)….………..………(3)……………………..(4)……………….

Serial No (1)…………………(2)….………..………(3)……………………..(4)……………….

Hours/Cycles (1)…………………(2)….………..………(3)……………………..(4)……………….

Hub Pt/No (1)…………………(2)….………..………(3)……………………..(4)……………….

Blade Pt/No (1)…………………(2)….………..………(3)……………………..(4)……………….

AIRWORTHINESS REVIEW PERIOD


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CAR.A.710 AIRWORTHINESSREVIEW DETAILS

1.1. ight Manual/Pilots Handbook Issue and Revision: ……………………………..

Is this the correct document for the current aircraft configuration YES NO

1.2. Maintenance Programme Approval Reference ………………………………………………………………………….

All scheduled maintenance required by the referenced programme has been carried out YES NO

1.3. All known defects have been corrected or deferred in accordance with an approved procedure:

YES NO

1.4. All applicable airworthiness directives have been incorporated

YES NO

Quote documents assessed: -

CAA CAP 747 Issue No / Amendment No

……………………………../…………………………………………..

Aircraft State of Design Airworthiness Directives

Bi-weekly/AD No./Issue no./Date ………………../……………………/…………….…./……………….

Engine State of Design Airworthiness Directives


Propeller State of Design Airworthiness Directives


Equipment State of Design Airworthiness Directives


Published EASA Airworthiness Directives


From (Last Review) Date, Aircraft Hours/Cycles …………………………………/…………………………………

To Date, Aircraft Hours/Cycles ………………………………/………………………………..


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1.5. Confirm all modifications and repairs have been approved in accordance with Part 21

YES NO

1.6. All installed life limited components have been recorded and have not exceeded their approved service life

YES NO

1.7. All maintenance accomplished within this airworthiness review period has been released to service iaw M.A.801

YES NO

3. PHYSICAL SURVEY OF AIRCRAFT

1.11. Survey Report Reference No (Copy of survey report to be attached to this airworthiness review report)

…………………………………………………………………………………….

1.8. The Mass and Balance Statement is correct for the current aircraft configuration

Provide reference/issue/revision/date of statement Date aircraft was last weighed

YES NO

…………………………/…………………………/……………………. …………………………………………………………………………..

1.9. The aircraft, in its current configuration, complies with the type design approved by EASA

Provide reference/issue/revision/date of the latest EASA approved or accepted Type Certificate Data Sheet

YES NO

…………………………/…………………………/……………………..

1.10. Aircraft Documentation reviewed: All documents reviewed are available, current and complete

Registration YES NO

Certificate of Airworthiness YES NO

Radio License YES NO

Technical/Journey Log (as applicable) YES NO

Airframe Logbook YES NO

Engine Logbook(s) YES NO

Propeller Logbook(s) YES NO

Modification Logbook YES NO

NOTE: An unsatisfactory answer to any of the questions 2.1 to 2.10 will mean a recommendation may not be made. Details of any NO answers should be listed in Section 4 with details of the corrective actions taken.


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1.12. Date and location where survey undertaken

…………………………………………………………………………………….

1.13. All known defects and problems found during the survey have been appropriately addressed

YES NO

NOTE: Answering NO will mean a recommendation may not be made until the identified problems and defects have been appropriately addressed.

2. DEFECTS AS REPORTED IN SECTION 2 All defects must be rectified before a recommendation can be made.

REF DEFECT RECTIFICATION/ACTIONS

3. RECOMMENDATION FOR THE ISSUE OF AN AIRWORTHINESS REVIEW CERTIFICATE

3.1. This is to certify that all of the above records have been reviewed for the period DDMMYYYY- DDMMYYYY plus a physical survey of the aircraft undertaken DDMMYYYY and the aircraft G-XXXX _________ was/was not* found to be fully in compliance with all of the applicable requirements of CAR. On this basis it is/is not* recommended that an Airworthiness Review Certificate be issued in accordance with M.A.901. * Delete as applicable

NOTE: If the result of the full airworthiness review is unsatisfactory or inconclusive then this form, along with all necessary supporting data should be sent to the CAA in order to satisfy the requirements of M.A.710(h)

Signed ……………………………………………………………………………

Authorisation No ……………………………………………………………………………

Company Approval No ……………………………………………………………………………

Date …………………………………………………………………………….

A copy of this report shall be provided to the aircraft owner and a copy to be retained in the aircraft

records.


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APPENDICES

PART 5

PAGE NO. 21

5.10 APPENDIX 6

NORTHERN REGION


CONTRACTED

BELL 206 L4 VT-PHA,VT-PHD, VT-PHE

ALLISON 250C30P

√ X

BELL 407 VT-PHH,VTPHI, VT-PHN,VT-PHQ,

ALLISON 250C47B

√ X

DHRUV VT-HAR,VT-HAN, VT-BSJ,VT-BSK, VT-BSS, VT-BSM, VT-BSP,

TM 333 2B2 √ √

ECUREUIL AS350 B3 VT-PHU, VT-PHV ARRIEL 2B1

√ X

WESTERN REGION


CONTRACTED

DAUPHIN SA 365N VT-ELB,VT-ELD, VT-ELE,VT-ELG, VT-ELI,VT-ELJ, VT-ELK,VT-ELL, VT-ELM,VT-ELN VT-ELP,VT-ELQ VT-ELR,VT-ELS, VT-ELT, VT-ENW VT-ENX.VT-ENZ

ARRIEL 1C √ X

DAUPHIN AS 365N3 VT-PHJ,VT-PHK, VT-PHL,VT-PHM VT-PHO,VT-PHR, VT-PHS,VT-PHW, VT-PHX, VT-PHY, VT-PHZ, VT-PWA, VT-PWB, VT-PWC, VT-PWD, VT-PWE, VT-PWF.

ARRIEL 2C √ X

MI 172 VT-PHG TV3-117M √ X

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