CONTINUING AIRWORTHINESS REQUIREMENTS – PART M 2(41)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

F) ENGINES 
20-Cleaning and Lubrication not requiring disassembly other than removal of non-structural items such as cover plates, cowlings and fairings.  Yes  N/A  N/A 
21-Cowling-removal and re-fitment not requiring removal of the propeller  Yes  N/A  N/A 
22-Fuel and oil strainers and/or filter elements – Removal, cleaning and/or replacement  Yes  N/A  N/A 
23-Batteries – replacing and servicing (excluding servicing of Ni-Cd batteries).  Yes  N/A  N/A 
24-Propeller Spinner – removal and installation for inspection.  Yes  N/A  N/A 
25-Powerplant – Removal or installation of powerplant unit including engine and propeller.  Yes  N/A  N/A 
26-Engine-Chip detectors – remove, check and replace.  Yes  N/A  N/A 
27-Ignition Spark Plug – removal or installation and adjustment including gap clearance.  Yes  N/A  N/A 
28-Coolant fluid – replenishment.  Yes  N/A  N/A 

ED 2008/013/R
257

ED 2008/013/R
29- Engine Controls – minor adjustments of non-flight or propulsion controls whose operation is not critical for any phase of flight.  Yes  N/A  N/A 
30- Engine instruments – removal and replacement.  Yes  N/A  N/A 
31- Lubrication oil – changing or replenishment of engine oil and gearbox fluid.  Yes  N/A  N/A 
32- Fuel lines – replacement of prefabricated hoses with self- sealing couplings.  Yes  N/A  N/A 
33- Air filters (if installed) – removal, cleaning and replacement.  Yes  N/A  N/A 

Appendices to AMC’s

 

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 main-tenance 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 pro-gramme 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 applica-ble and acceptable to the competent authority of registry.
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 mainte-nance 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.
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：CONTINUING AIRWORTHINESS REQUIREMENTS – PART M 2(41)