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§29.481 Tail-down landing conditions.

14 CFR 29 · Strength Requirements · Ground Loads · at 29-59 (current)

Text in force at 29-59: from 29-0, effective 1 Feb 1965.

(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.

29 FR 16150 · Source

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