CS 27.71 Glide performance

• ED Decision 2003/15/RM found in: CS-27 Amdt 10 - Small Rotorcraft (Feb 2023)

CS 27.71 Glide performance ED Decision 2003/15/RM For single-engine helicopters and multi-engine helicopters that do not meet the category A engine isolation requirements of CS-27, 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. CS 27.71 Glide performance ED Decision 2003/15/RM For single-engine helicopters and multi-engine helicopters that do not meet the category A engine isolation requirements of CS-27, 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.