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1.1.3 The reference, the date of issue and issue number of the approved maintenance programme.
1.1.4 A statement signed by the owner, operator or MCAR-M Subpart G approved organisation managing  the aircraft  airworthiness  to the  effect  that the specified aircraft will  be maintained to the programme and that the programme will be reviewed and updated as required.

1.1.5 Contents/list of effective pages and their revision status of the document.
1.1.6 Check  periods, which reflect the  anticipated  utilisation of the aircraft. Such utilisation  should be stated and include a tolerance of not more than 25%. Where utilisation cannot be anticipated, calendar time limits should also be included.
1.1.7 Procedures for the escalation of established check periods, where applicable and acceptable to CAD.
1.1.8 Provision to record the date and reference of approved amendments incorporated in the maintenance programme.
1.1.9 Details of pre-flight maintenance tasks that are accomplished by maintenance staff.
1.1.10 The tasks and the periods (intervals/frequencies) at which each part of the aircraft, engines, APU’s, propellers, components, accessories, equipment, instruments, electrical and  radio apparatus, together with the associated systems  and installations should be inspected. This should include the type and degree of inspection required.
1.1.11 The  periods at which components  should be checked, cleaned, lubricated, replenished, adjusted and tested.
1.1.12 If   applicable  details  of  ageing  aircraft  system  requirements  together  with any specified sampling programmes.
1.1.13 If applicable details of specific structural maintenance programmes where issued by the type certificate holder including but not limited to:
(a)
Maintenance  of structural Integrity by damage Tolerance and Supplemental Structural Inspection Programmes (SSID).

(b)
Structural maintenance programmes resulting  from the SB review performed by the TC holder.

(c)
Corrosion prevention and control.

(d)
Repair Assessment.

(e)
Widespread Fatigue Damage

1.1.14 If applicable, details of Critical Design Configuration Control Limitations together with appropriate procedures.
1.1.15 If  applicable  a statement  of the limit  of validity in terms  of total flight cycles/calendar date/flight hours for the structural programme in 1.1.13.
1.1.16 The  periods at which overhauls and/or replacements  by new or overhauled components should be made.
1.1.17 A cross-reference to other documents approved by the type certificate issuing authority which contain the details of   maintenance  tasks  related to mandatory  life   limitations,   Certification Maintenance Requirements (CMR’s) and ADs.
Note: To prevent inadvertent variations to such tasks or intervals these items should not be included in the main portion of the maintenance programme document, or any planning control system, without specific identification of their mandatory status.
1.1.18 Details of, or cross-reference to, any required reliability programme  or statistical methods of continuous Surveillance.
1.1.19 A statement that practices and procedures to satisfy the programme should be to the standards specified in the TC holder’s Maintenance Instructions. In the case of approved practices and procedures that differ, the statement should refer to them.
1.1.20 Each maintenance task quoted should be defined in a definition section of the programme.
2.  Programme basis
2.1 An  owner or an MCAR-M Subpart G approved organisation’s  aircraft maintenance programme should normally be based upon the MRB report, where applicable, and the TC holder’s maintenance planning document or Chapter 5 of the maintenance manual, (i.e. the manufacturer’s recommended maintenance programme).
　
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