(b)
Aircraft information
- aircraft assigned registration
- state of manufacturer
- previous registration
- export certificate number
- TC and TC data sheet numbers
- noise and emissions TC and TC data sheet numbers
- comparison of prior maintenance programme with the proposed new maintenance programme.
Rev 0, dated 2nd March, 2010
(c) Documents accompanying the recommendation
-
copy of the application, and;
-original export certificate, and;
-
copy of the approvals of the flight manual and its supplements, and;
- list of ADs incorporated up to the latest published issue, and;
- proposed new maintenance programme, and;
- status of all service life limited components, and;
- the valid weight and centre of gravity schedule reflecting the current configuration of the
aircraft, and;
-approval reference for all modifications and repairs.
(d) 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.
(e) Aircraft check flight
-a copy of the check flight report
Rev 0, dated 2nd March, 2010
Section 2 CAR M
Appendix I to AMC M.A.302 and AMC M.B.301 (b) Content of the maintenance programme
1 General requirements
1.1 The maintenance programme should contain the following basic information.
1.1.1 The type/model and registration number of the aircraft, engines and, where applicable,
auxiliary power units and propellers
1.1.2 The name and address of the owner, operator or M.A Subpart G approved organisation
managing the aircraft airworthiness.
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 M.A 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 the DGCA.
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.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：CONTINUING AIRWORTHINESS REQUIREMENTS CAR -M(75)
