§29.481 Tail-down landing conditions

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

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

(a) The rotorcraft is assumed to be in the maximum nose-up attitude allowing ground clearance by each part of the rotorcraft. (b) In this attitude, ground loads are assumed to act perpendicular to the ground.

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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