§ 27.67. Climb: one engine inoperative.

135 words·~1 min read·/us/cfr/t14/s§ 27.67·

A research copy — for the controlling text, always check the official state or federal source. Not legal advice.

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. (Secs. 313(a), 601, 603, 604, and 605 of the Federal Aviation Act of 1958 (49 U.S.C. 1354(a), 1421, 1423, 1424, and 1425); and sec. 6(c) of the Dept. of Transportation Act (49 U.S.C. 1655(c))) [Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as amended by Amdt. 27-23, 53 FR 34210, Sept. 2, 1988]

Connections2 off-index

2 references not yet in our index

49 USC 1354(a)
49 USC 1655(c)

Citation graph

cites case law

§ 27.67

Climb: one engine inoperative.

Cite49 USC 1354(a)

Cite49 USC 1655(c)

Cites 2Cited by 0 across 0 sources