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AMC E 680  Inclination and Gyroscopic Load Effects

ED Decision 2007/015/R

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]
Details
Source-Title: AMC E 680 Inclination and Gyroscopic Load Effects
Erulesid: ERULES-1963177438-8952 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: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS-E 680 Inclination and Gyroscopic Load Effects
Origin: EASA
Category: EAR