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AMC 25.701(d)  Flap and slat interconnection

ED Decision 2019/013/R

FAA Advisory Circular AC 25-14 High Lift and Drag Devices, dated 5-4-88, incorporated in FAA Advisory Circular AC 25-22, Certification of Transport Airplane Mechanical Systems, dated 14 March 2000, is accepted by EASA as providing acceptable means of compliance with CS 25.701(d).

[Amdt No: 25/23]
Details
Source-Title: AMC 25.701(d) Flap and slat interconnection
Erulesid: ERULES-1963177438-8477 Compare versions
Domain: Initial airworthiness
Amendedby: Amendment 23
Applicabilitydate: 17 July, 2019
Entryintoforcedate: 17 July, 2019
Regulatorysource: ED Decision 2019/013/R Navigate
Regulatorysubject: CS-25
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 25.701 Flap and slat interconnection
Origin: EASA
Category: EAR