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AMC 25.121(b)(1)(i) Climb: One-engine-inoperative

ED Decision 2007/010/R

A ‘power operating condition’ more critical than that existing at the time the landing gear is fully retracted would occur, for example, if water injection were discontinued prior to reaching a gross height of 122 m (400 ft).

[Amdt 25/3]
Details
Source-Title: AMC 25.121(b)(1)(i) Climb: One-engine-inoperative View latest amendments
Erulesid: ERULES-1963177438-9489 Compare versions
Domain: Initial airworthiness
Amendedby: Amendment 3
Applicabilitydate: 19 September, 2007
Entryintoforcedate: 19 September, 2007
Regulatorysource: ED Decision 2007/010/R 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