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Subpart C continuing airworthiness - Coggle Diagram
Subpart C continuing airworthiness
pre flight inspection
Accomplishment of preflight inspection inspect for any defect or damage affecting safe operation for large aircraft or aircraft using commercial air transport.
walk around type inspection for aircraft inspect emergency equipment for condition including obvious signs of wear damage and leakage
technical log to ensure that the intended flight is not adversely affected by any defects and does not require any maintenance actions shown in the maintenance statement which is overdue all will become due during the flight.
airworthiness task
control fluids gases, uplifted prior to a flight are of the correct specificatian free from contamination and correctly recorded
control that all doors are securely fastened
Control surface and landing gear locks, pitot/static covers engine aperture blanks have been removed.
All aircrafts external surfaces and engines are free from ice, snow, sand, dust etc. assessments confirm and results of condition have been applied on it and no fluid residues could endanger flight safety.
Oil and hydraulic fluid uplift and tire inflation may be considered as part of preflight inspection. Requires additional maintenance action by the approved maintenance organisation or certifying staff as appropriate
The CAMO managing the continuing airworthiness of aircraft established work according to a policy which assesses non mandatory information of aircraft, information such as service bulletins, service letters and other information that is produced for aircraft components by approved design organisation
The CAMO managing the continuing airworthiness of aircraft have a system to analyse effectiveness of maintenance program.
aircraft maintenance programme
Maintenance of each aircraft organised in accordance with aircraft maintenance program
aircraft maintenance program approved by competent authority
aircraft is managed by continuing airworthiness management organisation approved in accordance with section A subpart G, or where there's a limited contract between the owner and this organisation in accordance with point.
indirect approval procedure shall be established by continuing airworthiness management organisation. Management exposition approved by competent authority responsible for continuing airworthiness.
aircraft maintenance program must establish compliance with instructions issued by competent authority and instructions for continuing airworthiness issued by holders off the type certificate.
Data of modification/repairs
Damage will be assessed, modifications and repairs carried out by data approved by Agency or approved Part‑21 design organisation, as appropriate.
operator obligation
Detailed maintenance records in respect of aircraft and service life limited components fitted information contained is superseded can you information equivalent in scope and detail.
Total time in service of aircraft at least 12 months after aircraft or components has been permanently withdrawn from service.
details of engine propeller and other components vital to flight safety at least 12 months after they have been permanently withdrawn,
operator technical log system
Information about each flight necessary to ensure continued flight safety
current aircraft certificate of release to service
current mission statement giving the aircraft maintenance status and out of face maintenance next to accept that the competent authority agreed to the maintenance statement
aircraft technical log system amendment shall be approved by competent authority
operators shall ensure that aircraft technical logs is retained for 36 months after the date of the last entry