LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 1/11 MAINTENANCE PROGRAMME

Programme Owner’s Name

LX-??? and/or

Aircraft Manufacturer

Aircraft Type

Maintenance Programme

This programme belongs to: Owner’s/CAMO/Operator’s name Address LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 2/11 MAINTENANCE PROGRAMME

CHAPTER 0: INTRODUCTION.

TABLE OF CONTENT

CHAPTER 0: INTRODUCTION...... 2 CHAPTER 1: GENERAL INSTRUCTIONS...... 5 CHAPTER 2: MAINTENANCE PERIODICITY...... 8 CHAPTER 3: COMPONENTS MAINTENANCE...... 10 CHAPTER 4: SPECIAL INSPECTIONS...... 10 CHAPTER 5: RUN-UP AND TEST FLIGHT PROCEDURE...... 10 CHAPTER 6: MAINTENANCE OPERATIONS...... 10 APPENDIXES...... 11 LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 3/11 MAINTENANCE PROGRAMME

LIST OF EFFECTIVE PAGES

Page N° Ed./Rev. Date Page N° Ed./Rev. Date ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? ??? LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 4/11 MAINTENANCE PROGRAMME

RECORDS OF REVISIONS

Edition/ Approval ref. Date Reason of revision Inserted by Date Revision and date

DISTRIBUTION LIST

Copy N° Holder Name Address

1 Owner’s Name Owner’s address

2 CAMO/Operator’s Name CAMO/Operator’s Address Direction de l’Aviation Civile 4, rue Lou Hemmer 3 de Luxembourg L-1748 Luxembourg Contracted Maintenance 4 Maintenance Organisation Address organisation 5 ??? ???

6 ??? ??? LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 5/11 MAINTENANCE PROGRAMME

CHAPTER 1: GENERAL INSTRUCTIONS.

OWNER’S/CAMO/OPERATOR’S STATEMENT

I undersigned, Owner’s/CAMO/Operator’s Nominated Post Holder’s Name, responsible for continuing airworthiness, certify that aircraft listed in this document are maintained according to the instructions contained in this manual, and that this programme will be up-dated in close connection with operational needs, maintenance requirements and manufacturer’s Maintenance Manual recommendations. This manual will be reviewed at least annually in order to keep it current in the light of operating experience. I declare that practices and procedures aimed to satisfy the manual requirements are the ones issued in the manufacturer’s/Type Certificate Holder’s Maintenance Manuals as well as ICAO, EASA and/or DAC Luxembourg.

Date: ???

Signature:

MAINTENANCE DEFINITION

Aircraft maintenance is defined as periodic, preventive or corrective actions enabling the aircraft and its components to be operated safely. The different types of inspections are established in order to keep the aircraft and its components in an airworthy condition as described in the manufacturers’/Type Certificate Holders’ publication and the relevant Civil Aviation Authorities requirements. The different types of actions can be defined as follow:  Inspections: visual examination or functional check of aircraft, components or systems in order to ensure that they are still in airworthy condition.  Scheduled components replacement: replacement of components having a pre-determined service life or life limit.  Rectification of defects: correction of abnormalities resulting in the unserviceability of aircraft or aircraft systems discovered during aircraft operation. Periodic inspections can be tracked by means of aircraft operating flight hours or landings, engine flight hours or cycles, or calendar time.

AIRCRAFT YEARLY UTILISATION

This Maintenance Programme is established based on an estimated yearly utilisation of ??? hours and ??? landings. This annual rate may vary by 25% without affecting the content of this document. LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 6/11 MAINTENANCE PROGRAMME

MAINTENANCE DATA

The following maintenance data were used for the development of this manual.

Manufacturer Publication Reference or P/N Revision status and approval date.

Airframe Manufacturer/ Type ??? ??? Certificate Holder Engine Manufacturer/ Type ??? ??? Certificate Holder Propeller Manufacturer/ Type ??? ??? Certificate Holder

AIRCRAFT CONCERNED

This Maintenance Programme is applicable to all aircraft listed in the table here below.

Engine Propeller APU Registration Aircraft Aircraft Aircraft Manufacturer Manufacturer Manufacturer Mark Manufacturer Type S/N and Type and Type and Type

??? ??? ??? ??? ??? ??? ???

??? ??? ??? ??? ??? ??? ???

??? ??? ??? ??? ??? ??? ???

LIST OF MODIFICATIONS/STC’S INCORPORATED

The following modifications and/or Supplemental Type Certificates are incorporated in the aircraft.

Mod./STC Mod./STC Aircraft Flight Maintenance Mod./STC Description reference Holder Manual Supplement Manual Supplement

??? ??? ??? ??? ???

??? ??? ??? ??? ???

??? ??? ??? ??? ???

MAINTENANCE STANDARD LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 7/11 MAINTENANCE PROGRAMME

Aircraft, engine, propeller and appliance maintenance is always performed in accordance with the latest manufacturers’/Type Certificate Holders’ maintenance publications by an appropriately approved Part 145 organisation, Part M Subpart F organisation, Part 66 Certifying staff (except for complex maintenance tasks identified in this manual), DAC Luxembourg accepted organisation/technician, or the pilot-owner (only for maintenance tasks identified in this manual).

PRE-FLIGHT INSPECTION

There is no item part of the pre-flight inspection that may be considered as maintenance action. Refer to applicable Aircraft Flight Manual/Pilot Operating Handbook for pre-flight description. Pre-flight inspection includes various visual inspections such as, but not limited to:  Walk-around inspection of the aircraft and its emergency equipments for obvious wear, damage or leak.  Review of aircraft Journey Log or Technical Logbook for any outstanding deferred defect or overdue maintenance action that may affect the intended flight.  Control of consumable or fluids necessary for the intended flight.  Control that all doors and access panels are properly closed and secured.  Control that control surface and landing gear locks, pitot-static and engine covers are removed.  Control that aircraft external surfaces and engines are free from ice, snow, sand, dust or residue of de- icing/anti-icing fluid having been previously applied on it. Any defect discovered during the pre-flight inspection will need to be rectified by appropriately qualified technical personnel or deferred in accordance with approved data.

REVISION PROCEDURE

This Maintenance Programme must be reviewed as least annually to ensure that it stills reflect the latest Manufacturers’ maintenance publications and procedures. In case of those data were amended during that period or modifications, STC’s or repairs having an impact on continuing airworthiness have been incorporated, this Maintenance Programme must be revised in the shortest delay.

RELIABILITY PROGRAMME

There is no reliability programme incorporated in this manual.

ESCALATION PROCEDURE

There is no escalation procedure applicable. LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 8/11 MAINTENANCE PROGRAMME

CHAPTER 2: MAINTENANCE PERIODICITY.

AIRFRAME MAINTENANCE INTERVALS

Airframe manufacturer’s maintenance intervals are defined as described here below:

Airframe inspections types and intervals:  Type of inspection, interval.  Type of inspection, interval.  Type of inspection, interval.

In the case of inspections tracked by more than one interval (ex: hours and cycles, months and hours, etc), inspection will be due at the first limit reached.

COMPONENTS AND APPLIANCES MAINTENANCE INTERVALS

For engine, propeller or any other components having their own inspection intervals, time between overhaul or life limitations, as described in manufacturers’ publications, refer to attached Cardex in Chapter 3 of this manual. In the case of components tracked by more than one interval (ex: hours and cycles, months and hours, etc), inspection will be due at the first limit reached.

DAC LUXEMBOURG MAINTENANCE REQUIREMENTS

If not already covered by one of the above mentioned inspection, the following maintenance actions must be carried out as follow:  Pitot and static system test (including altimeter, airspeed indicator, vertical speed indicator and stand- by instruments check for accuracy) every 24 months.  Transponder test every 24 months.  Compass and Stand-by compass calibration every 24 months.  Avionic global test every 24 months.  First aid kit inspection for content and expiry date of the products every 12 months.  Portable fire extinguisher weighing every 12 months and life expiry date.  Aircraft weighing every 60 months or after complete painting, interior refurbishment, or modification/repair affecting the aircraft weight and balance data.

PERMITTED VARIATIONS

Unless otherwise specified in the manufacturers’/Type Certificates Holders’ publications, the following policy will apply. In certain unexpected circumstances due to operational requirements, it is permitted to extend the maintenance intervals here above specified without exceeding the following limitations:  Inspections tracked by hours: 10% of the interval value but not more than 10 hours.  Inspections tracked by landings: 10% of the interval value but not more than 10 landings.  Inspections tracked by calendar time: . Inspection interval is less than 12 months: 10% of the interval value but not more than 1 month. . Inspection interval is equal to or more than 12 months: not more than 1 month. LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 9/11 MAINTENANCE PROGRAMME

Permitted variations to maintenance intervals do not apply to inspections mandated by Airworthiness Directives, Life Limited Components, Certification Maintenance Requirements, and Airworthiness Limitations.

Permitted variations to maintenance interval are not cumulative. Ex: if a 100 Hours inspection is due at 100 A/C hours and is performed at 110 A/C hours, next 100 Hours inspection will be due at 200 A/C hours. In the case of inspections tracked by more than one interval (ex: hours and cycles, months and hours, etc), permitted variations are non cumulative and inspection will be due at the first limit reached.

Any other excedence of defined interval is subject to DAC Luxembourg approval and must be requested in advance by use of appropriate form in order to ensure that inspections intervals will not be overrun. LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 10/11 MAINTENANCE PROGRAMME

CHAPTER 3: COMPONENTS MAINTENANCE.

List in this section all components (type and Part Number) that shall undergo maintenance activity at defined interval. CHAPTER 4: SPECIAL INSPECTIONS

TYPE OF SPECIAL INSPECTIONS

The aircraft will undergo special inspection after occurrence of the following unexpected events:  Runway exceedence during take off or landing.  Hard or over-weight landing.  Lightning strike.  Propeller strike.  Bird strike.  Flight in hailstorm.  Flight in heavy turbulence.  Flight through sand or volcanic ashes.  Aircraft’s limitations exceedence.

CHAPTER 5: RUN-UP AND TEST FLIGHT PROCEDURE

CHAPTER 6: MAINTENANCE OPERATIONS LX-??? and/or Edition N°? PROGRAMME AIRCRAFT MANUFACTURER Revision N°? OWNER’S NAME AIRCRAFT TYPE Page 11/11 MAINTENANCE PROGRAMME

APPENDIXES

APPENDIX I

L ist of acronyms:  A/C: Aircraft.  AD: Airworthiness Directive.  AFM: Aircraft Flight Manual.  ALI: Airworthiness Limitation Item.  AMM: Aircraft Maintenance Manual.  ATA: Air Transport Association.  CAMO: Continuing Airworthiness Management Organisation.  Cy: Cycle.  DACL: Direction de l’Aviation Civile de Luxembourg  DGAC: Direction Générale de l’Aviation Civile:  EASA: European Aviation Safety Agency.  FAA: Federal Aviation Administration.  Hrs: Hours.  ICAO: International Civil Aviation Organisation.  Ldg: Landing  Mod: Modification.  MP: Maintenance Programme.  NDT: Non Destructive Testing.  O/C: On Condition.  OVH: Overhaul.  POH: Pilot Operating Handbook.  S/N: Serial Number.  SB: Service Bulletin.  SL: Service Letter.  STC: Supplemental Type Certificate.  TBO: Time Between Overhaul.  TCDS: Type Certificate Data Sheet.  TCH: Type Certificate Holder.  W&B: Weight and Balance.