§29.477 Landing gear arrangement

CS-29 · Subpart C — Strength Requirements · at CS29-12 (current)

Text in force at CS29-12: from CS29-0, effective 14 Nov 2003.

Paragraphs C S 29.235, 29.479 to 29.485, and 29.493 apply to landing gear wi th two wheels aft, and one or m ore wheel s forward, of t he cent re of gravity.

ED Decision 2003/016/RM · Source

Version history

Version	Effective	Published
CS29-0	14 Nov 2003	ED Decision 2003/016/RM

Rulemaking for CS29-0

easa decision ED Decision 2003/016/RM source

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