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AMC E 140  Test - Engine configuration

ED Decision 2009/018/R

For turbine engines, if the power turbine accessory drives are not loaded, the equivalent power should be added as required by CS-E 140(d)(1) to the required power at the output drive so that the power turbine rotor assembly is operated at or above the same level as it would be if the power turbine accessory drives were loaded.

[Amdt. No.: E/1]

[Amdt. No.: E/2]
Details
Source-Title: AMC E 140 Test - Engine configuration
Erulesid: ERULES-1963177438-9039 Compare versions
Domain: Initial airworthiness
Amendedby: Amendment 2
Applicabilitydate: 18 December, 2009
Entryintoforcedate: 18 December, 2009
Regulatorysource: ED Decision 2009/018/R Navigate
Regulatorysubject: CS-E
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS-E 140 Tests - Engine Configuration
Origin: EASA
Category: EAR