§29.71 Helicopter angle of glide: Category B.

[For each category B helicopter, except multiengine helicopters meeting the requirements of Sec. 29.67(b) and the powerplant installation requirements of category A, the steady angle of glide must be determined in autorotation-- (a) At the forward speed for minimum rate of descent as selected by the applicant; (b) At the forward speed for best glide angle; (c) At maximum weight; and (d) At the rotor speed or speeds selected by the applicant.]