CAT.POL.H.405 Take-off

• 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 (Sep 2023)

CAT.POL.H.405 Take-off Regulation (EU) No 965/2012 (a) The take-off mass shall be the lower of: (1) the MCTOM; or (2) the maximum take-off mass specified for a hover in ground effect with all engines operating at take-off power, or if conditions are such that a hover in ground effect is not likely to be established, the take-off mass specified for a hover out of ground effect with all engines operating at take-off power. (b) Except as provided in [CAT.POL.H.400(b)](#_DxCrossRefBm318086518), in the event of an engine failure the helicopter shall be able to perform a safe forced landing. CAT.POL.H.405 Take-off Regulation (EU) No 965/2012 (a) The take-off mass shall be the lower of: (1) the MCTOM; or (2) the maximum take-off mass specified for a hover in ground effect with all engines operating at take-off power, or if conditions are such that a hover in ground effect is not likely to be established, the take-off mass specified for a hover out of ground effect with all engines operating at take-off power. (b) Except as provided in [CAT.POL.H.400(b)](#_DxCrossRefBm927678898), in the event of an engine failure the helicopter shall be able to perform a safe forced landing. #### CAT.POL.H.405 Take-off *Regulation (EU) No 965/2012* (a) The take-off mass shall be the lower of: (1) the MCTOM; or (2) the maximum take-off mass specified for a hover in ground effect with all engines operating at take-off power, or if conditions are such that a hover in ground effect is not likely to be established, the take-off mass specified for a hover out of ground effect with all engines operating at take-off power. (b) Except as provided in [CAT.POL.H.400(b)](#_DxCrossRefBm523088454), in the event of an engine failure the helicopter shall be able to perform a safe forced landing.