§ 27.481 - Tail-down landing conditions.

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§ 27.481 Tail-down landing conditions.

(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.

                    
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§ 27.481 - Tail-down landing conditions.

§ 27.481 Tail-down landing conditions.