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Engines (CS-E) · CS-E · EAR revision 7 Dec 2023
AMCAcceptable means of compliance
Normally inclination and gyroscopic load effects will be proved during flight testing but in certain cases some supplementary running or rig testing, to an agreed schedule, may be required before flight tests can be permitted.
[Amdt. No.: E/1]
AMC — CS-E · ED Decision 2007/015/R · CS-E Easy Access Rules · EAR revision 7 Dec 2023
All rules in SUBPART E – TURBINE ENGINES: TYPE SUBSTANTIATION
Consolidated from the EASA Easy Access Rules (revision 7 Dec 2023, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.
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