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CAT.POL.H.415 Landing
Available versions for ERULES-1963177438-12906
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)
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CAT.POL.H.415 Landing Regulation (EU) No 965/2012 (a) The landing mass of the helicopter at the estimated time of landing shall be the lower of: (1) the maximum certified landing mass; or (2) the maximum landing 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 landing mass 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.415 Landing Regulation (EU) No 965/2012 (a) The landing mass of the helicopter at the estimated time of landing shall be the lower of: (1) the maximum certified landing mass; or (2) the maximum landing 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 landing mass 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.415 Landing *Regulation (EU) No 965/2012* (a) The landing mass of the helicopter at the estimated time of landing shall be the lower of: (1) the maximum certified landing mass; or (2) the maximum landing 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 landing mass 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.