|
|
Advertisement Sec. 27.71 - Glide performance. 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. 27-21, 49 FR 44433, Nov. 6, 1984]
Previous: Sec. 27.67 - Climb: one engine inoperative.
|
