§25.457 Wing-flaps

CS-25 · Subpart C — Structure · at CS25-28 (current)

Text in force at CS25-28: from CS25-0, effective 17 Oct 2003.

Wing flaps, their operating mechanisms, and their supporting structures must be designed for critical loads occurring in the conditions prescribed in CS 25.345, accounting for the loads occurring during transition from one wing-flap position and airspeed to another.

ED Decision 2003/002/RM · Source

Version history

Version	Effective	Published
CS25-0	17 Oct 2003	ED Decision 2003/002/RM

Rulemaking for CS25-0

easa decision ED Decision 2003/002/RM source

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