AWO.B.CATII.119 CS AWO.B.CATII.119 General

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]

ED Decision 2022/007/R

The system shall be designed so that no selection or changes of switch settings (other than system disengagement) need be made manually below a height of 150 m (500 ft) in the absence of a failure.

[Issue: CS-AWO/2]