IRImplementing rule
AWO.B.CATII.116CS AWO.B.CATII.116 Go-around climb gradient
The AFM shall contain either a WAT limit corresponding to a gross climb gradient of 2.5 %, with the critical engine failed and with the speed and configuration used for go-around, or the information necessary to construct a go-around gross flight path with an engine failure at the start of the go-around from the DH.
[Issue: CS-AWO/2]
IR · AWO.B.CATII.116 — CS-AWO · ED Decision 2022/007/R · CS-AWO Easy Access Rules · EAR revision 14 Aug 2026