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AMC E 690 Engine bleed

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

AMCAcceptable means of compliance

AMC E 690 Engine bleed

For reducing test complexity, and for improved flexibility needed to attain the key parameters (speed, temperature and torque) during the 2-hour test of CS-E 740(c)(3)(iii), maximum air bleed for Engine and aircraft services need not be used if the applicant can show by test or analysis based on test that the Engine's ability to meet the strip examination specifications of CS-E 740(h)(2) is not enhanced. The analysis should include The effect of the bleed air extraction to the Engine secondary air system which provides cooling air to various Engine components, The thermodynamic cycle effects of bleed (e.g., gas generator speed to output shaft speed changes).

[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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