Navigate / EASA
Ask question Discover more Add to collection
AMC3 23.2120 Climb requirements

ED Decision 2023/002/R

CS-VLA Amdt 1

CS-VLA 65 ‘Climbs’: All engines operating

Remarks

To demonstrate compliance with CS 23.2120, the climb gradient should be determined, using F3179M 20 ‘Standard Specification for Performance of Aircraft’.
Details
Source-Title: AMC3 23.2120 Climb requirements View latest amendments
Erulesid: ERULES-1963177438-6993 Compare versions
Domain: Initial airworthiness
Amendedby: CS-23 Amendment 6 and AMC ＆ GM to CS-23 Issue 4
Applicabilitydate: 8 March, 2023
Entryintoforcedate: 8 March, 2023
Regulatorysource: ED Decision 2023/002/R Navigate
Regulatorysubject: CS-23
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 23.2120 Climb requirements
Origin: EASA
Category: EAR