CAT.POL.H.220 Landing

• Regulation (EU) No 965/2012 found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Feb 2025)

CAT.POL.H.220 Landing Regulation (EU) No 965/2012 (a) The landing mass of the helicopter at the estimated time of landing shall not exceed the maximum mass specified in the AFM for the procedure to be used. (b) In the event of the critical engine failure being recognised at any point at or before the landing decision point (LDP), it is possible either to land and stop within the FATO, or to perform a balked landing and clear all obstacles in the flight path by a vertical margin of 10,7 m (35 ft). Only obstacles as specified in [CAT.POL.H.110](#_DxCrossRefBm927678855) have to be considered. (c) In the event of the critical engine failure being recognised at any point at or after the LDP, it is possible to: (1) clear all obstacles in the approach path; and (2) land and stop within the FATO. (d) When showing compliance with (a) to (c), account shall be taken of the appropriate parameters of [CAT.POL.H.105(c)](#_DxCrossRefBm927678853) for the estimated time of landing at the destination aerodrome or operating site, or any alternate if required. (e) That part of the landing from the LDP to touchdown shall be conducted in sight of the surface. CAT.POL.H.220 Landing Regulation (EU) No 965/2012 (a) The landing mass of the helicopter at the estimated time of landing shall not exceed the maximum mass specified in the AFM for the procedure to be used. (b) In the event of the critical engine failure being recognised at any point at or before the landing decision point (LDP), it is possible either to land and stop within the FATO, or to perform a balked landing and clear all obstacles in the flight path by a vertical margin of 10,7 m (35 ft). Only obstacles as specified in [CAT.POL.H.110](#_DxCrossRefBm318086475) have to be considered. (c) In the event of the critical engine failure being recognised at any point at or after the LDP, it is possible to: (1) clear all obstacles in the approach path; and (2) land and stop within the FATO. (d) When showing compliance with (a) to (c), account shall be taken of the appropriate parameters of [CAT.POL.H.105(c)](#_DxCrossRefBm318086473) for the estimated time of landing at the destination aerodrome or operating site, or any alternate if required. (e) That part of the landing from the LDP to touchdown shall be conducted in sight of the surface. #### CAT.POL.H.220 Landing *Regulation (EU) No 965/2012* (a) The landing mass of the helicopter at the estimated time of landing shall not exceed the maximum mass specified in the AFM for the procedure to be used. (b) In the event of the critical engine failure being recognised at any point at or before the landing decision point (LDP), it is possible either to land and stop within the FATO, or to perform a balked landing and clear all obstacles in the flight path by a vertical margin of 10,7 m (35 ft). Only obstacles as specified in [CAT.POL.H.110](#_DxCrossRefBm523088411) have to be considered. (c) In the event of the critical engine failure being recognised at any point at or after the LDP, it is possible to: (1) clear all obstacles in the approach path; and (2) land and stop within the FATO. (d) When showing compliance with (a) to (c), account shall be taken of the appropriate parameters of [CAT.POL.H.105(c)](#_DxCrossRefBm523088409) for the estimated time of landing at the destination aerodrome or operating site, or any alternate if required. (e) That part of the landing from the LDP to touchdown shall be conducted in sight of the surface.