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On the basis of EASA Part-M, an airline has to regularly prove the reliability of its aircraft to the Aviation Authority in the form of a Reliability Program.
Select the desired departments as required, e.g.:
- Engine Condition Trend Monitoring (ECTM)
- On Condition Maintenance early diagnosis of system errors, piloting, decreasing unscheduled maintenance, supply optimization
- Periodic Engine Performence Test - issuing a data protocol
- Cruise Recordsheet Data - input and analysis of data
- Onboard Recording System - recording of data in an Engine Monitoring Unit (EMU), replacement of the storage medium/update
- Periodic transmission of engine data through on-board communication systems - fully automatic data download via data link
- Request of current parameters for online system analysis
- System Build, VHF Data Link, System Representation, Data Downlink Definition, Trouble Shooting Support, Engine Manufacture Support
- Description of system types: ECTM, ECM, EHM, GSS, ODM, etc.
- System diagnosis case study V2500 / A320
- Parameter variation, e.g., in SVA open schedule, compressor VBV open schedule, with loss of turbine efficiency, etc.
- Determination of EGT margin