CS 29.71 Helicopter angle of glide: Category B

• ED Decision 2003/16/RM found in: CS-29 Amdt 10 - Large Rotercraft (Jan 2023)

CS 29.71 Helicopter angle of glide: Category B ED Decision 2003/16/RM For each Category B helicopter, except multi-engine helicopters meeting the requirements of [CS 29.67(b)](#_DxCrossRefBm1513259334) 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. CS 29.71 Helicopter angle of glide: Category B ED Decision 2003/16/RM For each Category B helicopter, except multi-engine helicopters meeting the requirements of [CS 29.67(b)](#_DxCrossRefBm1178331715) 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. #### CS 29.71 Helicopter angle of glide: Category B *ED Decision 2003/16/RM* For each Category B helicopter, except multi-engine helicopters meeting the requirements of [CS 29.67(b)](#_DxCrossRefBm1685772180) 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.