IRImplementing rule
AWO.B.CATII.111CS AWO.B.CATII.111 Installed equipment
The approach guidance system shall include:
- (a) two xLS receivers with a display of the selected deviation infor mation at each pilot's station;
- (b) a n automatic approach coupler or a flight director system with display at each pilot's station (or an alternative system capable of providing for equivalent performance and safety);
- (c) a radio altimeter with displays at each pilot's station of:
- (1) radio altitude, and
- (2) the selected DH (e.g. an index on an analogue scale or a digital indication);
- (d) c lear visual indication at each pilot's station (e.g. an alert light) when the aeroplane reaches the pre-selected decision height appropriate to the approach;
- (e) automatic or flight director go-around system or acceptable attitude indicators;
- (f) audible warning of automatic pilot failure (for automatic approach);
- (g) an automatic throttle/thrust system when required by CS AWO.B.CATII.106;
- (h) an appropriate equipment failure warning system; and
ED Decision 2022/007/R
The approach system shall cause no sustained nuisance oscillations or undue attitude changes or control activity as a result of configuration or power changes or any other disturbance to be expected in normal operation.
[Issue: CS-AWO/2]
IR · AWO.B.CATII.111 — CS-AWO · CS-AWO Easy Access Rules · EAR revision 14 Aug 2026