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AMC 25.351 Yaw manoeuvre conditions

ED Decision 2013/010/R

The physical limitations of the aircraft from the cockpit yaw control device to the control surface deflection, such as control stops position, maximum power and displacement rate of the servo controls, and control law limiters, may be taken into account.

[Amdt 25/13]
Details
Source-Title: AMC 25.351 Yaw manoeuvre conditions
Erulesid: ERULES-1963177438-9770 Compare versions
Domain: Initial airworthiness
Amendedby: Amendment 13
Applicabilitydate: 14 June, 2013
Entryintoforcedate: 14 June, 2013
Regulatorysource: ED Decision 2013/010/R Navigate
Regulatorysubject: CS-25
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 25.351 Yaw manoeuvre conditions
Origin: EASA
Category: EAR