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

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