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AMC E 660 Fuel Pump Tests (Turbine Engines for Aeroplanes)

Engines (CS-E) · CS-E · EAR revision 7 Dec 2023

AMCAcceptable means of compliance

AMC E 660 Fuel Pump Tests (Turbine Engines for Aeroplanes)

When testing equipment susceptible to cavitation erosion (e.g. Engine fuel pumps) the possibility of such erosion being relieved by dissolved air in the test fluid should be considered and, if appropriate, some testing should be carried out with fuel at the most critical temperature and pressure with regard to cavitation erosion and having the minimum amount of air in solution that is likely to occur during normal operating conditions.

[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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