§25.477 Landing gear arrangement

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

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

CS 25.479 to 25.485 apply to aeroplanes with conventional arrangements of main and nose gears, or main and tail gears, when normal operating techniques are used.

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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