CS 29.85 Balked landing: Category A

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

CS 29.85 Balked landing: Category A ED Decision 2003/16/RM For Category A rotorcraft, the balked landing path with the critical engine inoperative must be established so that: (a) The transition from each stage of the manoeuvre to the next stage can be made smoothly and safely; (b) From the LDP on the approach path selected by the applicant, a safe climbout can be made at speeds allowing compliance with the climb requirements of [CS 29.67(a)(1) and (2)](#_DxCrossRefBm1513259334); and (c) The rotorcraft does not descend below 4.6 m (15 ft) above the landing surface. For elevated heliport operations, descent may be below the level of the landing surface provided the deck edge clearance of [CS 29.60](#_DxCrossRefBm1513259349) is maintained and the descent (loss of height) below the landing surface is determined. CS 29.85 Balked landing: Category A ED Decision 2003/16/RM For Category A rotorcraft, the balked landing path with the critical engine inoperative must be established so that: (a) The transition from each stage of the manoeuvre to the next stage can be made smoothly and safely; (b) From the LDP on the approach path selected by the applicant, a safe climbout can be made at speeds allowing compliance with the climb requirements of [CS 29.67(a)(1) and (2)](#_DxCrossRefBm1178331715); and (c) The rotorcraft does not descend below 4.6 m (15 ft) above the landing surface. For elevated heliport operations, descent may be below the level of the landing surface provided the deck edge clearance of [CS 29.60](#_DxCrossRefBm1178331730) is maintained and the descent (loss of height) below the landing surface is determined. #### CS 29.85 Balked landing: Category A *ED Decision 2003/16/RM* For Category A rotorcraft, the balked landing path with the critical engine inoperative must be established so that: (a) The transition from each stage of the manoeuvre to the next stage can be made smoothly and safely; (b) From the LDP on the approach path selected by the applicant, a safe climbout can be made at speeds allowing compliance with the climb requirements of [CS 29.67(a)(1) and (2)](#_DxCrossRefBm1685772180); and (c) The rotorcraft does not descend below 4.6 m (15 ft) above the landing surface. For elevated heliport operations, descent may be below the level of the landing surface provided the deck edge clearance of [CS 29.60](#_DxCrossRefBm1685772195) is maintained and the descent (loss of height) below the landing surface is determined.