IRImplementing rule
AWO.B.SACATI.111CS AWO.B.SACATI.111 Installed equipment
(See AMC AWO.B.SACATI.111)
The approach guidance system shall include the following:
- (a) two separate navigation receivers or demonstrated equivalent devices with a display of the selected deviation information at each pilot's station; - (b) a flight guidance system (or an alternative that provides for equivalent performance and safety) with displays at each pilot's station; - (c) a radio altimeter (or other device capable of providing for equivalent performance and integrity level) with displays at each pilot's station of: - (1) height above terrain; and - (2) the selected decision height (DH); - (d) clear visual indication at each pilot's s tation (e.g. an alert light) when the aircraft reaches the preselected DH appropriate to the approach; - (e) automatic or flight director go-around system or any other attitude indicators that can achieve the required performance, accuracy and function; - (f) audible warnings of automatic pilot failure (for automatic approach) (refer to CS 25.1329); - (g) an automatic throttle/thrust system, where necessary (see CS AWO.B.CATII.106); - (h) an appropriate alerting system; and - (i) an alert of excess deviation from the required approach path, at each pilot's station .
[Issue: CS-AWO/2]
ED Decision 2022/007/R
The recognition of the decision height (DH) shall be made by means of height measured by a radio altimeter or another system that provides height above terrain with equivalent performance, accuracy, integrity, availability, level of independence, and dissimilarity.
[Issue: CS-AWO/2]
IR · AWO.B.SACATI.111 — CS-AWO · CS-AWO Easy Access Rules · EAR revision 14 Aug 2026