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Aircraft Maintenance Program (CA10)

AIRCRAFT MAINTENANCE PROGRAM (AMP CA10) PUBLISHED BY

SAMCO B.V. Maastricht - the Netherlands

Copy no.:

This manual is published by SAMCO and is the property of SAMCO Aircraft Maintenance bv. It may not be reproduced in whole or in part or otherwise disclosed without prior consent from the SAMCO Accountable Manager.

Revision: 11 1-7-2015

Title Page Page 1 of 2

Aircraft Maintenance Program (CA10)

PREAMBLE This baseline Aircraft Maintenance Program (AMP), prescribes the minimum requirements necessary for maintaining F28 mk100 type aircraft in an airworthy condition as well as Fly Away Storage. In addition to the accomplishment of the maintenance actions prescribed in this AMP, compliance shall also be established with all appropriate mandatory requirements issued by the CAA-NL and by the recognized aviation authority of the Aircraft Type Certificate Holder, Engine Type Certificate Holder and all installed equipment, where applicable. Nothing in this AMP is to be construed as absolving SAMCO from maintaining the aircraft, to which it refers, in an airworthy condition. This AMP is intended to be used by the SAMCO Continued Airworthiness Management Organisation as a Baseline for maintaining the aircraft to which it refers in an airworthy condition. This AMP has been prepared and published by: SAMCO Aircraft Maintenance Horsterweg 19 6199 AC Maastricht - Aachen Airport The Netherlands Phone: +31-43-3587 900 Fax: +31-43-3650 143 Email: [email protected]

Revision: 00 12-11-2009

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Aircraft Maintenance Program (CA10)

HOLDERS LIST Manual No. 1. 2. 3.

Revision: 11 1-7-2015

Function/department Location SAMCO, Continuous Airworthiness Department Maastricht Airport, The Netherlands CAA-NL Hoofddorp, The Netherlands CAA Romania Bucharest, Romania

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Aircraft Maintenance Program (CA10)

REVISION RECORD Revision No. 00 01 02

Date 12-11-2009 01-08-2010 03-01-2011

03

01-06-2011

Revision details Initial issue MRB revision 013 Removal of compass swing, Addition of 3 aircraft serial numbers Addition of aircraft serial numbers 11410, 11420. EASA AD 2011-0046 Implementation of Fokker reports SE-473 iss 8, SE-623 iss 7, SE-672 iss 2. Implementation of Fokker TR 13-001, 13-002, 13-003 of MPR rev 13 Airworthiness Directives that affect the baseline program

04 05 06

30-08-2011 01-11-2011 15-05-2012

Added Inspection tasks from damage and repair mappings Addition of aircraft serial number 11493 Addition of aircraft serial number 11494 MPD revisions 14 and MRB revisions 14 EASA AD 2012-0049 Implementation of Fokker reports SE-473 iss 9, SE-623 iss 8, SE-672 iss 3. Implementation of Fokker MPD TL 14-001 Airworthiness Directives that affect the baseline program

07

07-08-2012

08

01-02-2013

Addition of aircraft serial numbers 11444 and 11477, MRB TL 14-001 Implementation of EASA AD 2012-0204 Engine – Low pressure compressor disc assembly life limitation EASA AD 2013-0004 Implementation of Fokker reports SE-473 iss 10 and SE-623 iss 10.

09

01-08-2013

Implementation of MPD TL 14-002 Addition of aircraft serial numbers 11308 and 11313 EASA AD 2013-0036 Implementation of Fokker report SE-672 iss 4. Implementation of ALI SE-623 iss 11 Implementation of MRB TL 14-002

10

Implementation of MPD TL 14-003 Chapter 4 (Permitted variations) revised to be in compliance with MD NL-2011-001 EASA AD 2014-0157 Implementation of Fokker reports SE-473 iss 10, SE-623 iss 12 and SE-672 iss 4

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Aircraft Maintenance Program (CA10)

EASA AD 2014-0224 Implementation of Fokker reports SE-473 iss 10, SE-623 iss 13 and SE-672 iss 4 Implementation of ALI SE-623 iss 12 & 13 Implementation of MRB revision 15 Implementation of MRB TL 15-001 Implementation of MPD revision 15 Implementation of MPD TL 15-001 Implementation of MPD TL 15-002 Introduction of Appendix G – Optional tasks

11

Revision: 11 1-7-2015

1-7-2015

Deletion of PH-CXF, PH-CXN Addition of Fokker Engineering Report SE-743 – Continuous Fly-Away Storage Program Addition of aircraft serial number 11493 (YR-CRY)

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TERMINOLOGY AND DEFINITIONS Airworthiness Directive: An ‘airworthiness directive’ means a document issued or adopted by the EASA which mandates actions to be performed on an aircraft to restore an acceptable level of safety, when evidence shows that the safety level of this aircraft may otherwise be compromised Authority: The competent body responsible for the safety of civil aviation. Baseline AMP: An Aircraft Maintenance Program which is used as the basic document. It is amended in its contents to incorporate (temporary) revisions to the AMP source documents (refer to Chapter 2) as well as effectivity related issues regarding customised approved maintenance data and its applicability regarding aircraft serial numbers under contract with the SAMCO CAMO. Continuous Airworthiness Management Organisation: The Part M subpart G approved organisation responsible for the maintenance management of aircraft within its approved scope of work. Inspection: Means the examination of an aircraft/aircraft component to establish conformity with an approved standard. Private Operator / Owner: Means the owner of the aircraft or the operator who operates the aircraft non-commercially.

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Aircraft Maintenance Program (CA10)

ABBREVIATIONS The following abbreviations may be found throughout the manual: AD AFM AMC AMM AMP APU ATA AWL CAA-NL CAMO CMM EASA ECTM EMM EN EO FW GWL HS JAA JAR MAREP MD MME MOE MPD MRB MSN PIREP RR SB SIL SL SLL STC TBI TBO TC TCCA TCDS TSHSI TSN TSO TSR

Revision: 10 10-10-2014

Airworthiness Directive Aircraft Flight Manual Acceptable Means of Compliance Aircraft Maintenance Manual Aircraft Maintenance Program Auxiliary Power Unit Air Transport Association Airworthiness Limitation Civil Aviation Authority – The Netherlands Continued Airworthiness Management Organisation Component Maintenance Manual European Aviation Safety Agency Engine Condition Trend Monitoring Engine Maintenance Manual Engineering Notice Engineering Order Fixed Wing Goedkeuring Wijziging Luchtvaartuig Hamilton Sundstrand Joint Aviation Authority Joint Aviation Regulations Maintenance Reports Maintenance Directive Maintenance Management Exposition Maintenance Organization Exposition Maintenance Planning Document Maintenance Review Board Document Manufacturer Serial Number Pilot Flight Report Rolls Royce Service Bulletin Service Information Letter Service Letter Safe life Limitation Supplemental Type Certificate Time Between Inspection Time Between Overhaul Type Certificate Transport Canada Civil Aviation Type Certificate Data Sheet Time Since Hot Section Inspection Time Since New Time Since Overhaul Time Since Repair

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Aircraft Maintenance Program (CA10)

REFERENCE MATERIAL The following documents are used as reference material for this Manual:  

SAMCO Continued Airworthiness Management Exposition, latest approved revision. EASA Part M (EC regulation 2042/2003 Annex I as amended).

Revision: 09 06-08-2013

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CROSS REFERENCE LIST This document follows the guidelines for Maintenance Programs as stated in AMC M.A.302 and Appendix 1 to AMC M.A.302. Reference M.A.302(a) M.A.302(b) M.A.302(c) M.A.302(d) M.A.302(e) M.A.302(f) M.A.302(g) 1 1.1 1.1.1 1.1.2 1.1.3 1.1.4 1.1.5 1.1.6 1.1.7 1.1.8 1.1.9 1.1.10 1.1.11 1.1.12 1.1.13 1.1.14 1.1.15 1.1.16 1.1.17 1.1.18 1.1.19 1.1.20 2 2.1 2.2 2.3 3 3.1 4 5 5.1 5.2

Revision: 10 10-10-2014

Description EASA Part M.A. Aircraft Maintenance Programme Aircraft Maintenance Programme – Direct Approval of Aircraft Maintenance Programme – Indirect Approval of Aircraft Maintenance Programme – Compliance Aircraft Maintenance Programme – Details Aircraft Maintenance Programme – Reliability Programme Aircraft Maintenance Programme – Periodic Reviews Appendix I to AMC M.A.302 and AMC M.B.301(b) General Requirements Maintenance Program Requirements Aircraft Details Operator Details Maintenance Program Reference Identification Statement of Operator Contents and List of Effective Pages Utilization Escalations Amendment Records Preflight Maintenance Tasks Intervals and Frequencies Component Maintenance Ageing Aircraft Requirements and Sampling Programs Structural Maintenance Program Critical Design Configuration Control Limitations Structural Program Validity Overhaul and Replacement Periods Mandatory Tasks Reliability Report Type Certificate Holder’s Maintenance Instructions Maintenance Task Identification Program Basis Maintenance Review Board Report Newly Type Certificated Aircraft Previously Approved Maintenance Programs Amendments Amendment Procedure Permitted Variations to Maintenance Periods Periodic Review of Maintenance Program Contents Contents of Review Period of Review

AMP PREAMBLE PREAMBLE & 3 3 1&2 8 6 5 1 1.1 1.1.1 1.1.2 1.1.3 1.1.4 1.1.5 1.1.6 1.1.7 1.1.8 1.1.9 1.1.10 1.1.11 1.1.12 1.1.13 1.1.14 1.1.15 1.1.16 1.1.17 1.1.18 1.1.19 1.1.20 2 2.1 2.2 2.3 3 3.1 4 5 5 5

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Reference 6 6.1 6.2 6.3 6.4 6.5 6.6

Revision: 00 12-11-2009

Description Appendix I to AMC M.A.302 and AMC M.B.301(b) Reliability Program Applicability Applicability to small fleet(s) Engineering Judgment Contracted Maintenance Reliability Program Pooling Arrangements

AMP 6 6 6 6 6 6 6

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TABLE OF CONTENTS PREAMBLE...................................................................................................................................................................... 1 HOLDERS LIST ............................................................................................................................................................... 1 REVISION RECORD ...................................................................................................................................................... 1 LIST OF EFFECTIVE PAGES....................................................................................................................................... 1 TERMINOLOGY AND DEFINITIONS ........................................................................................................................ 1 ABBREVIATIONS ........................................................................................................................................................... 1 REFERENCE MATERIAL ............................................................................................................................................. 1 CROSS REFERENCE LIST ........................................................................................................................................... 1 TABLE OF CONTENTS ................................................................................................................................................. 1 1.

MAINTENANCE PROGRAM ................................................................................................................................ 1 1.1 MAINTENANCE PROGRAM REQUIREMENTS ........................................................................................... 1 1.1.1 Aircraft Details ........................................................................................................................................... 1 1.1.2 Private Operator details ............................................................................................................................. 2 1.1.3 Maintenance Program Reference Identification ......................................................................................... 2 1.1.4 Statement of operator .................................................................................................................................. 3 1.1.5 Contents and List of Effective Pages........................................................................................................... 4 1.1.6 Utilization ................................................................................................................................................... 4 1.1.7 Escalations .................................................................................................................................................. 4 1.1.8 Amendment Records.................................................................................................................................... 4 1.1.9 Pre-Flight Maintenance Tasks .................................................................................................................... 4 1.1.10 Intervals and Frequencies........................................................................................................................... 4 1.1.11 Component Maintenance ............................................................................................................................ 5 1.1.12 Ageing Aircraft Requirements and Sampling Programs ............................................................................. 6 1.1.13 Structural Maintenance Program ............................................................................................................... 6 1.1.14 Critical Design Configuration Control Limitations .................................................................................... 6 1.1.15 Structural Program Validity ....................................................................................................................... 6 1.1.16 Overhauls and Replacement Periods .......................................................................................................... 6 1.1.17 Mandatory Tasks......................................................................................................................................... 6 1.1.18 Reliability Report ........................................................................................................................................ 6 1.1.19 Type Certificate Holder’s Maintenance Instructions .................................................................................. 7 1.1.20 Maintenance Task Identification ................................................................................................................. 8 1.1.21 Engine Health Monitoring Data ................................................................................................................. 8

2.

PROGRAM BASIS ................................................................................................................................................... 1 2.1 MAINTENANCE REVIEW BOARD DOCUMENT ......................................................................................... 1 2.1.1 Fokker 70/100 (Fokker) Publications ......................................................................................................... 1 2.1.2 Rolls Royce (Tay Engine) Publications....................................................................................................... 1 2.1.3 APU Publications ....................................................................................................................................... 1 2.1.4 Airworthiness Directives ............................................................................................................................. 1 2.1.5 Other ........................................................................................................................................................... 1 2.2 NEWLY TYPE CERTIFICATED AIRCRAFT .............................................................................................................. 1 2.3 PREVIOUSLY APPROVED MAINTENANCE PROGRAMS ......................................................................... 1 2.4 MAINTENANCE STANDARDS ...................................................................................................................... 2 2.5 MANDATORY REQUIREMENTS FOR AMENDMENT ................................................................................................. 2

3.

AMENDMENTS ....................................................................................................................................................... 1 3.1

AMENDMENT PROCEDURE - REVISIONS ............................................................................................................... 1

4.

PERMITTED VARIATIONS TO MAINTENANCE PERIODS ......................................................................... 1

5.

PERIODIC REVIEW OF MAINTENANCE PROGRAM CONTENTS ............................................................ 1

6.

RELIABILITY PROGRAM .................................................................................................................................... 1

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7.

AIRCRAFT MODIFICATION AND REPAIR STATUS ..................................................................................... 1

8.

MAINTENANCE PROGRAM TASK LISTING .................................................................................................. 1

APPENDIX A – MAINTENANCE TASK LISTING .................................................................................................... 1 APPENDIX B – COMPONENT MAINTENANCE ...................................................................................................... 1 APPENDIX C – UNSCHEDULED MAINTENANCE TASKS AFTER COMPONENT REMOVAL .................... 1 APPENDIX D – AIRWORTHINESS DIRECTIVES .................................................................................................... 1 APPENDIX E – PRE FLIGHT AND DAILY INSPECTIONS .................................................................................... 1 APPENDIX F – FLY AWAY STORAGE ...................................................................................................................... 1 APPENDIX G – OPTIONAL TASKS ............................................................................................................................ 1 APPENDIX H – NOT APPLICABLE MAINTENANCE TASKS ............................................................................... 1

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1. MAINTENANCE PROGRAM 1.1 MAINTENANCE PROGRAM REQUIREMENTS 1.1.1 Aircraft Details This AMP is from its baseline applicable for F28 mk100 aircraft, all MSN, as it is derived from the source documents (refer to Chapter 2) and the Fly Away Storage and Pre-flight requirements.

Aircraft Engine

Manufacturer Fokker Rolls Royce

Type/Model F28-100 RR Tay 620-15 or 650-15

Registration -all-

MSN -all-all-

Maintenance Task effectivity requirements will allow the incorporation of serialized maintenance requirements as produced by the Type Certificate holders. The following aircraft MSN have been checked for effectivity and are maintained in accordance with this AMP: Aircraft type

MSN

Registration

Start date

PH-LXG

Customer / Owner MASS JET LEASE AERO CENTURY AERO CENTURY AERO CENTURY AFT

01-08-2010

Cancellation date 05-05-2011

Fokker 100

11322

PH-LNE

Fokker 100

11333

PH-CXN

03-01-2011

19-08-2014

Fokker 100

11337

PH-CXP

03-01-2011

10-05-2012

Fokker 100

11303

PH-CXF

03-01-2011

01-11-2014

Fokker 100

11420

01-01-2011

14-01-2013

Fokker 100

11410

PH-KXR

AFT

01-01-2011

06-03-2013

Fokker 100

11493

PH-ABW

EADS

06-09-2011

29-09-2011

Fokker 100

11494

PH-ABX

EADS

01-11-2011

16-02-2012

Fokker 100

11444

PH-OFL

Air Batumi

02-07-2012

18-07-2012

Fokker 100

11477

PH-OFN

Air Batumi

01-08-2012

08-11-2012

Fokker 100

11308

PH-CXH

09-07-2013

Fokker 100

11313

PH-CXK

Fokker 100

11493

YR-CRY

AERO CENTURY AERO CENTURY ASKAN Holding Ltd

09-07-2013 1-7-2015

Not applicable tasks for each of the above mentioned aircraft are listed in appendix G.

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Aircraft Maintenance Program (CA10)

1.1.2 Private Operator details This Aircraft Maintenance Program may be applied to any Private Operator contracting their Part M, subpart G responsibilities to SAMCO.

1.1.3 Maintenance Program Reference Identification The AMP bears reference identification number: CA10 This reference identification is listed in the page headers of all AMP sections. The current revision number and revision date of this AMP is listed in the Revision Index. Each section bears its current revision number and revision date in the footer of the page. The List of Effective Pages lists the applicable revision number and date for the sections for the current revision number.

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Aircraft Maintenance Program (CA10)

A Certificate of Airworthiness inspection report will be submitted at intervals not exceeding 12 months commencing on the date of validation of the Certificate of Airworthiness. If the aircraft is un-airworthy at the time when the inspection should be completed, the interval may be extended until the aircraft is again airworthy. The Fly Away Storage consists of tasks contained in the Aircraft Maintenance Manual as well as Fokker Engineering Report SE-743 and one pre-flight inspection (refer to section 1.1.9). After performing the AMM Storage Preparations inspection, the 7-days and 14-days inspections recur for a period with a maximum of 18 weeks. Following this 18 week period the aircraft will become subject to the conditions of Fokker Report SE-743, which can be used for a period of 2 years. Thereafter the aircraft has to be re-activated. The inspections are identified by a section number, as listed below and can be found in Appendix F.            

CA10.CR.12 - Storage Preparations CA10.CR.13 - 7-Days Inspection (Weekly) CA10.CR.14 - 14-Days Inspection (Bi-Weekly) CA10.CR.15 - Return to Service CA10.CR.16 – Preparations to put the aircraft in Continuous Fly-Away storage CA10.CR.17 – Additional Maintenance Practices after one year Continuous Fly-Away storage CA10.CR.18 – Weekly Continuous Fly-Away storage Inspection CA10.CR.19 – Bi-Weekly Continuous Fly-Away storage Inspection CA10.CR.20 – Six Weekly Continuous Fly-Away storage Inspection (Optional) CA10.CR.21 – Re-activation after Continuous Fly-Away storage CA10.CR.22 – Perform additional maintenance requirements following Continuous Fly-Away storage CA10.CR.50 – Verify no tasks are overdue at re-activation

MRB task compliance shall be checked during the Return to Service inspection in order to assure that Maintenance Tasks for operational aircraft are not overdue after the storage period. Task CA10.CR.50 has been created for this purpose.

1.1.10.1 Engine Maintenance Program The 14-days inspection requires engine runs at least every 14-days. The RR Tay engines will be maintained on an on-condition maintenance program. The maintenance requirements for engines maintained on an on-condition maintenance program are included in Section 8 appendix A of this CMP. 1.1.10.2 APU Maintenance Program Specific APU Maintenance is not required during the Fly Away Storage. Inlets and Outlets are covered by protective covers. 1.1.10.3 Unscheduled Maintenance after component removal Unscheduled maintenance task which are to be performed prior, during or after a component removal are listed in section 8 Appendix C.

1.1.11 Component Maintenance The periods at which items as appropriate, should be checked, cleaned, lubricated, replenished, adjusted and tested are incorporated and given in section 8 Appendix A.

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1.1.12 Ageing Aircraft Requirements and Sampling Programs 1.1.12.1 Ageing Aircraft Requirements The specific structural inspections are incorporated in the tasks in this AMP. 1.1.12.2 Sampling Programs There are no sampling programs incorporated in this AMP.

1.1.13 Structural Maintenance Program 1.1.13.1 Specific Structural Inspections The baseline AMP will be amended with any specific structural inspections for the aircraft serial numbers under contract with the SAMCO CAMO. 1.1.13.2 Corrosion Control Program Reference: • MRB, Section 03 Fokker Services has not issued a separate Corrosion Prevention & Control Program (CPCP) document for the Fokker 100, the basic CPCP inspections are covered in the structure section of the MRB document and controls corrosion to Level 1 or better.

1.1.14 Critical Design Configuration Control Limitations Reference: • Fokker Services Report SE-672 All maintenance tasks identified as having a CDCCL are contained in the AMM. No CDCCL is applied to scheduled maintenance tasks.

1.1.15 Structural Program Validity The F28Mk100 structural program is based on a design life of 90,000 flights.

1.1.16 Overhauls and Replacement Periods The periods at which items as appropriate should be overhauled and discarded (life-limited), and as such require replacement, are given in section 8 Appendix B.

1.1.17 Mandatory Tasks All tasks incorporated in this AMP are considered to be mandatory, since no permitted variations are allowed as per AMP section 4. Section 8 Appendix D comprises the applicable recurring Airworthiness Directives that affect maintenance: - F100 Airframe Airworthiness Directives (EASA) - RR Tay Engine Airworthiness Directives (EASA)

1.1.18 Reliability Report Refer to AMP section 6.

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1.1.19 Type Certificate Holder’s Maintenance Instructions The practices and procedures to satisfy the AMP will be performed to the standards specified in the Type Certificate Holder’s Maintenance Instructions, e.g. Maintenance Manuals, Structural Repair Manuals, NonDestructive Testing Manual, etc.

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1.1.20 Maintenance Task Identification The tasks in this AMP have been derived from the Aircraft Maintenance Manual instructions and numbered CA10.XXXX.YY, where X is a section number and YY is a sequence number. Tasks that evaluate from the MRB and/or MPD will remain numbered as in the MRB/MPD in order to track compliance. All maintenance tasks are listed in Appendix A of section 8, including its identification number and definition of the accomplishment.

1.1.21 Engine Health Monitoring Data During the Fly Away Storage, engine maintenance and engine runs are carried out according to the requirements in the AMM and EMM. Engine Health Monitoring is not possible during these runs as far as ECTM is concerned.

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Aircraft Maintenance Program (CA10)

2. PROGRAM BASIS 2.1 MAINTENANCE REVIEW BOARD DOCUMENT The AMP is based upon the Fokker 70/100 Maintenance Review Board Document, and the associated sections of the engine and Component Maintenance Manuals. The following publications are considered the source documents for the AMP:

2.1.1 Fokker 70/100 (Fokker) Publications        

Fokker 70/100 Aircraft Maintenance Manual chapter 10 - Parking, Mooring, Storage and Return to Service revision date 01 June 2015. Fokker 70/100 Maintenance Review Board Document, Revision 015 dated 31 December 2013 and MRB TL 15-001 date 15 February 2014. Fokker 70/100 Maintenance Planning Document, Revision 015 dated 15 February 2014, MPD TL 15-001 date 2 June 2014, MPD TL 15-002 date 25 August 2014 and MPD TL 15-003 date 19 January 2015. Airworthiness Limitations items and safe life items, MRB Appendix 1 Fokker Services Report SE-623 issue 13, 25 August 2014 Certification Maintenance Requirements, MRB Appendix 1 Fokker Services Report SE-473 issue 10, 23 October 2012. Fuel Airworthiness Limitation Items and Critical Design Configuration Control Limitations, MRB Appendix 1 Fokker Services Report SE-672 issue 5, 11 December 2014. Fokker Engineering Report SE-743, latest revision Fokker 70/100 Service Letter #176

2.1.2 Rolls Royce (Tay Engine) Publications 

CH 05 Time Limits Manual for RR Tay Series, issue date 15 June 2011.

2.1.3 APU Publications 

Not applicable.

2.1.4 Airworthiness Directives  

Refer to Appendix D of section 8 for a list of all repetitive Airworthiness Directives (AD’s). MD NL-2011-001 (One-time variations to maintenance intervals)

2.1.5 Other   

DRM 11308 d.d. 04 February 2013 DRM 11313 d.d. 09 January 2013 DRM 11493 d.d. 1-7-2015

2.2 NEWLY TYPE CERTIFICATED AIRCRAFT This section does not apply to this AMP since the aircraft is a previously Type Certificated aircraft.

2.3 PREVIOUSLY APPROVED MAINTENANCE PROGRAMS The issue of this AMP is based on SAMCO CAMO AMP CA10 Revision 0, which has been previously approved by the Dutch CAA (ILenT).

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Aircraft Maintenance Program (CA10)

2.4 MAINTENANCE STANDARDS All maintenance is performed by qualified personnel, following the methods, standards and instructions specified in the approved maintenance data. All maintenance is performed using tools, equipment and material as specified in the approved maintenance data.

2.5 MANDATORY REQUIREMENTS FOR AMENDMENT This AMP has been amended to fulfill the requirements of the following Airworthiness Directives      

MD NL-2011-001 (One-time variation to maintenance intervals) AD EASA-2012-0204 AD EASA-2014-0224 AD EASA-2015-0027 AD EASA-2015-0032 AD EASA-2015-0056

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Aircraft Maintenance Program (CA10)

3. AMENDMENTS The AMP is subject to amendment when found necessary. The procedures detailed below describe the amendment procedure of the AMP. An amendment to the AMP can be either a revision or a temporary revision. A revision is used when several changes to the AMP are required. A temporary revision may be used to incorporate a single change in the AMP, principally containing one amended section. The AMP requires amendment to incorporate and apply Fly Away Storage requirements to a new aircraft serial number or to remove them from the AMP. In this case the new MSN will be checked against effectivity requirements set forth in the Maintenance Manual. Any further required changes to the AMP will also be incorporated. SAMCO will be responsible for the approval of the initial (baseline) AMP and subsequent amendments (if required) by CAA-NL, acting on behalf of the EASA.

3.1 AMENDMENT PROCEDURE - REVISIONS Revisions to this Aircraft Maintenance Program are subject to the requirements of CAME section 2.2.2 and require direct or in-direct approval as per CAME 2.2.3 (direct approval) or CAME 2.2.4 (in-direct approval). In case of a revision, the revised sections of the AMP will be issued under a new revision number and revision date. The following sections will in any case be part of the revision package:  Amendment Sheet  List of Effective Pages  Applicable revised sections The Continued Airworthiness Manager will sign the Amendment Sheet and LEP to approve contents of the revision on behalf of the SAMCO CAMO. The revision package will then be distributed by SAMCO to the AMP holders as listed in the Holder’s List.

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Aircraft Maintenance Program (CA10)

4. PERMITTED VARIATIONS TO MAINTENANCE PERIODS Reference:

MD NL-2011-001 Fokker Service Letter Fokker 70/100 #176

A permitted variation may not be used as a maintenance planning tool, but as an exceptional means to allow operation for a limited period of time until the required maintenance is performed. An unforeseen workload peak in the maintenance organization, an unforeseen unavailability of staff, an unforeseen delay in parts provisioning, an unforeseen unavailability or unserviceability of a required tool or equipment, may be seen as an acceptable reason for requesting a permitted variation. Contrary to an amendment (i.e., escalation or de-escalation of a task), a permitted variation applies to a unique aircraft for a unique occasion. A variation shall not be applied if there is evidence or reason to believe that this could endanger flight safety. A variation shall be requested by means of CAME Form C2.2.06 (Maintenance Extension Request). The request has to be approved by the SAMCO CAMO Manager. In case the variation will fall outside the scope of this section, approval from the (State of Registry) authority is required. The maximum permitted one-time variation of a maintenance task interval is as indicated in following table: Nature of task (a) Tasks controlled by flight hours (b) Tasks controlled by calendar time, with an interval of: - 1 year or less - More than 1 year, but not exceeding 3 years - More than 3 years (c) Tasks controlled by landings / cycles (d) Fatigue and damage tolerance tasks (e) Tasks controlled by more than one limit

Permitted variation 10%, with a maximum of 500 flight hours

-

10% or 1 month, whichever is lesser 2 months

- 3 months 10%, with a maximum of 250 landings / cycles 5% The more restrictive shall be applied

The above variations do not apply to: -

Life limitations (Safe Life Items / Retirement Life / Discard) Initial compliance of recurring Airworthiness Directives and one time Airworthiness Directives AMP tasks which have been classified as mandatory by the TC holder, EASA or the authority of the state of registration. Certification Maintenance requirements, unless specified otherwise in the MRB/ALS report and agreed by the authority Fuel Airworthiness Limitation Items (Fuel ALI’s) resulting from the Fuel Tank Safety Assessment as laid down in the MRB Restoration with work scope category “Overhaul”.

After a variation has been applied, the maintenance task next due is calculated as if the last compliance was at the original due date (so without the variation being applied).

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Aircraft Maintenance Program (CA10)

5. PERIODIC REVIEW OF MAINTENANCE PROGRAM CONTENTS The aircraft maintenance program is subject to an annual review for continued validity in order to ensure that the CMP reflects the current Type Certificate holder’s recommendations, revisions to the MRB Report. The review for the Fly Away Storage Maintenance Program is focussed on changes in the Aircraft Maintenance Manual chapter 10 and Fokker Engineering Report SE-743..

In case of recurring requirements originating from (Emergency) Airworthiness Directives, the Aircraft Maintenance Program must be amended ASAP.

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Aircraft Maintenance Program (CA10)

6. RELIABILITY PROGRAM Fly Away Storage is resulting from Maintenance Manual tasks and therefore not requiring any Reliability Reporting from MSG-3 analysis. Due to the nature and the intention of this maintenance program, gathering of Reliability data would be minimal.

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Aircraft Maintenance Program (CA10)

7. AIRCRAFT MODIFICATION AND REPAIR STATUS The modification and repair status of the aircraft have an effect on the maintenance schedule. While some modifications or repairs eliminate the need for an inspection or other periodic maintenance actions, other modifications or repairs initiate a recurring inspection or other periodic maintenance action. The effectivity of the maintenance tasks for specific aircraft serial numbers will be checked and amended when required.

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Section 7 Page 1 of 2

Aircraft Maintenance Program (CA10)

8. MAINTENANCE PROGRAM TASK LISTING The following is a list of all required maintenance actions derived from the documents listed in the program basis of chapter 2. A detailed list containing all maintenance tasks, including any company requirements, is listed in Appendix A. A detailed list containing the required component maintenance is given in Appendix B. A detailed list containing all unscheduled maintenance tasks after component removal, is given in Appendix C. All Airworthiness Directives affecting maintenance, which require repetitive inspections, are listed in Appendix D. The Pre-Flight Inspection requirements are listed in Appendix E.  CA10.10.01 - Pre-Flight Inspection The Fly Away Storage requirements are listed in Appendix F.  CA10.20.01 - Storage Preparations  CA10.30.01 - 7-Days Inspection  CA10.30.02 - 14-Days Inspection  CA10.40.01 - Return to Service Optional Maintenance tasks are listed in Appendix G. Appendix H lists all not applicable tasks for the aircraft subjected to this maintenance programme.

Revision: 10 10-10-2014

Section 8 Page 1 of 2