14 CFR 29.483 - One-wheel landing conditions.

Regulations last checked for updates: May 19, 2024

Title 14 - Aeronautics and Space last revised: May 07, 2024

View all text of Subpart C [§ 29.301 - § 29.573]

§ 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.

authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704

source: Docket No. 5084, 29 FR 16150, Dec. 3, 1964, unless otherwise noted.

cite as: 14 CFR 29.483