---
title: "AWO.B.CATII.119 CS AWO.B.CATII.119 General — CS-AWO · Avioverse"
description: "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…"
url: "https://avioverse.aero/regulations/easa/cs-awo/subpart-b/awo-b-catii-119"
---

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

All Weather Operations (CS-AWO) · CS-AWO · EAR revision 14 Aug 2026

IR Implementing rule

## 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]

IR · AWO.B.CATII.119 — CS-AWO · ED Decision 2022/007/R · CS-AWO Easy Access Rules · EAR revision 14 Aug 2026

[All rules in SUBPART B -APPROACH AND LANDING](https://avioverse.aero/regulations/easa/cs-awo/subpart-b)

Consolidated from the EASA Easy Access Rules (revision 14 Aug 2026, extracted 13 Oct 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.