Navigate / EASA
Ask question Discover more Add to collection

CS-E 680  Inclination and Gyroscopic Load Effects

ED Decision 2007/015/R

(See AMC E 680)

It must be demonstrated that the effects of inclination on Engine running are not seriously detrimental and that the Engine is designed to withstand the gyroscopic loads resulting from normal flight manoeuvres.

[Amdt. No.: E/1]
Details
Source-Title: CS-E 680 Inclination and Gyroscopic Load Effects
Erulesid: ERULES-1963177438-8885 Compare versions
Domain: Initial airworthiness
Amendedby: Amendment 1
Applicabilitydate: 10 December, 2007
Entryintoforcedate: 10 December, 2007
Regulatorysource: ED Decision 2007/015/R Navigate
Regulatorysubject: CS-E
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR
Related sections: