§ 29.483 - One-wheel landing conditions.

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§ 29.483 One-wheel landing conditions.

For the one-wheel landing condition, the rotorcraft is assumed to be in the level attitude and to contact the ground on one aft wheel. In this attitude -

(a) The vertical load must be the same as that obtained on that side under § 29.479(b)(1); and

(b) The unbalanced external loads must be reacted by rotorcraft inertia.

                    
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§ 29.483 - One-wheel landing conditions.

§ 29.483 One-wheel landing conditions.