CS 29.83 Landing: Category B

• ED Decision 2003/16/RM found in: CS-29 Amdt 10 machine readable xml file
• ED Decision 2003/16/RM found in: EAR for CS-29 Amendment 11

CS 29.83 Landing: Category B ED Decision 2003/16/RM (a) For each Category B rotorcraft, the horizontal distance required to land and come to a complete stop (or to a speed of approximately 5.6km/h (3 knots) for water landings) from a point 15m (50 ft) above the landing surface must be determined with: (1) Speeds appropriate to the type of rotorcraft and chosen by the applicant to avoid the critical areas of the height-velocity envelope established under CS 29.87 ; and (2) The approach and landing made with power on and within approved limits. (b) Each multi-engine Category B rotorcraft that meets the powerplant installation requirements for Category A must meet the requirements of: (1) CS 29.79 and 29.81 ; or (2) Sub-paragraph (a). (c) It must be possible to make a safe landing on a prepared landing surface if complete power failure occurs during normal cruise. CS 29.83 Landing: Category B ED Decision 2003/16/RM (a) For each Category B rotorcraft, the horizontal distance required to land and come to a complete stop (or to a speed of approximately 5.6km/h (3 knots) for water landings) from a point 15m (50 ft) above the landing surface must be determined with: (1) Speeds appropriate to the type of rotorcraft and chosen by the applicant to avoid the critical areas of the height-velocity envelope established under CS 29.87 ; and (2) The approach and landing made with power on and within approved limits. (b) Each multi-engine Category B rotorcraft that meets the powerplant installation requirements for Category A must meet the requirements of: (1) CS 29.79 and 29.81 ; or (2) Sub-paragraph (a). (c) It must be possible to make a safe landing on a prepared landing surface if complete power failure occurs during normal cruise.