---
kind: "section"
citation: "14 C.F.R. § 29.483"
title: "14"
number: "29.483"
heading: "One-wheel landing conditions."
url: "https://uscodex.org/cfr/14/29.483"
---

# §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)](/cfr/14/29.479.md?p=b-1); and
- (b) The unbalanced external loads must be reacted by rotorcraft inertia.

## Notes

### Authority

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

### Source

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