AMC 25.121(a) Climb: One-engine-inoperative

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ED Decision 2003/2/RM

The configuration of the landing gear used in showing compliance with the climb requirements of CS 25.121(a) may be that finally achieved following ‘gear down’ selection.

Details

Source-Title: AMC 25.121(a) Climb: One-engine-inoperative

Erulesid: ERULES-1963177438-8192 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 25.121 Climb: one-engine-inoperative

Origin: EASA

Category: EAR