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AMC 25.121(a)(1) Climb: One-engine-inoperative

ED Decision 2003/2/RM

A ‘power operating condition’ more critical than that existing at the time when retraction of the landing gear is begun would occur, for example, if water injection were discontinued prior to reaching the point at which the landing gear is fully retracted.

Details
Source-Title: AMC 25.121(a)(1) Climb: One-engine-inoperative
Erulesid: ERULES-1963177438-8196 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