Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CAT.POL.H.410 En-route
Available versions for ERULES-1963177438-12903
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)
From
Air Operations Rev... (Mar 2026)
Air Operations (96... (Feb 2025)
Air Operations (96... (Sep 2023)
From section
To
Air Operations Rev... (Mar 2026)
Air Operations (96... (Feb 2025)
Air Operations (96... (Sep 2023)
To section
No visible text changes
0 removals
0 additions
View
Rich
Plain
Sync scrolling
Share
From
Show details
Hide details
To
Show details
Hide details
Version
Show side by side
CAT.POL.H.410 En-route Regulation (EU) No 965/2012 (a) The helicopter shall be able, with all engines operating within the maximum continuous power conditions, to continue along its intended route or to a planned diversion without flying at any point below the appropriate minimum flight altitude. (b) Except as provided in [CAT.POL.H.420](#_DxCrossRefBm318085275), in the event of an engine failure the helicopter shall be able to perform a safe forced landing.
CAT.POL.H.410 En-route Regulation (EU) No 965/2012 (a) The helicopter shall be able, with all engines operating within the maximum continuous power conditions, to continue along its intended route or to a planned diversion without flying at any point below the appropriate minimum flight altitude. (b) Except as provided in [CAT.POL.H.420](#_DxCrossRefBm927677639), in the event of an engine failure the helicopter shall be able to perform a safe forced landing.
#### CAT.POL.H.410 En-route *Regulation (EU) No 965/2012* (a) The helicopter shall be able, with all engines operating within the maximum continuous power conditions, to continue along its intended route or to a planned diversion without flying at any point below the appropriate minimum flight altitude. (b) Except as provided in [CAT.POL.H.420](#_DxCrossRefBm523087148), in the event of an engine failure the helicopter shall be able to perform a safe forced landing.