14 CFR 27.483

§ 27.483 One-wheel landing conditions.

United States · 14 CFR — Aeronautics and Space · Status: effective

Cite this

Citation: 14 CFR 27.483, § 27.483 One-wheel landing conditions, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54467
Permanent ID: ys:prov:54467@1
SHA-256: 264801002dedc3a7a1ab43a0e44797533bdb6b7600948d65705c15b566b5939e

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Full text

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 § 27.479(b)(1); and (b) The unbalanced external loads must be reacted by rotorcraft inertia.

Legislative history

This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.