Code of Federal Regulations
For single-engine helicopters and multiengine helicopters that do not meet the Category A engine isolation requirements of Part 29 of this chapter, the minimum rate of descent airspeed and the best angle-of-glide airspeed must be determined in autorotation at--
(a) Maximum weight; and
(b) Rotor speed(s) selected by the applicant.
Amdt. 27-44, Eff. 3/31/08
This section was added by Amendment 27-21.
Notice of Proposed Rulemaking Actions:
Notice of Proposed Rulemaking. Notice No. 82-12; Issued on 04/29/82.
Final Rule Actions:
Final Rule. Docket No. 23266; Issued on 08/14/84.
Final Rule. Docket No. 2006-25414; Issued on 2/20/08