14 CFR 27.67

§ 27.67 Climb: one engine inoperative.

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

Cite this

Citation: 14 CFR 27.67, § 27.67 Climb: one engine inoperative, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54426
Permanent ID: ys:prov:54426@1
SHA-256: 77ec8478eb1186f13b2b9598bbd6b5a660dff0705073c833c000d3841731f75c

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Full text

For multiengine helicopters, the steady rate of climb (or descent), at Vy (or at the speed for minimum rate of descent), must be determined with— (a) Maximum weight; (b) The critical engine inoperative and the remaining engines at either— (1) Maximum continuous power and, for helicopters for which certification for the use of 30-minute OEI power is requested, at 30-minute OEI power; or (2) Continuous OEI power for helicopters for which certification for the use of continuous OEI power is requested.

Legislative history

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