AMC 25.149(e) Minimum control speed

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ED Decision 2003/2/RM

During determination of V_MCG, engine failure recognition should be provided by:

a. The pilot feeling a distinct change in the directional tracking characteristics of the aeroplane, or

b. The pilot seeing a directional divergence of the aeroplane with respect to the view outside the aeroplane.

Source-Title: AMC 25.149(e) Minimum control speed

Erulesid: ERULES-1963177438-8277 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 17 October, 2003

Entryintoforcedate: 17 October, 2003

Regulatorysource: ED Decision 2003/2/RM Navigate

Regulatorysubject: CS-25

Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)

Parentir: CS 25.149 Minimum control speed

Origin: EASA

Category: EAR