§27.477 Landing gear arrangement

CS-27 · Subpart C — Strength Requirements · at CS27-10 (current)

Text in force at CS27-10: from CS27-0, effective 14 Nov 2003.

Paragraphs CS 27.235, 27.479 to 27.485, and CS 27.493 apply to landing gear with two wheels aft, and one or more wheels forward, of the centre of gravity.

ED Decision 2003/015/RM · Source

Version history

Version	Effective	Published
CS27-0	14 Nov 2003	ED Decision 2003/015/RM

Rulemaking for CS27-0

easa decision ED Decision 2003/015/RM source

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