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Sec. 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.

Previous: Sec. 27.479 - Level landing conditions.
Next: Sec. 27.483 - One-wheel landing conditions.

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