AWO.B.SACATI.116 CS AWO.B.SACATI.116 Go-around climb gradient

The AFM shall contain either a weight, altitude, temperature (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]

Easy Access Rules for All-Weather Operations (CS-AWO)

SUBPART B -APPROACH AND LANDING SECTION 2 -AIRWORTHINESS CERTIFICATION OF AEROPLANES FOR OPERATIONS WITH DECISION HEIGHTS (DHs) BELOW 60 M (200 FT) AND DOWN TO 45 M (150 FT) -SPECIAL AUTHORISATION CATEGORY I (SA CAT I) OPERATIONS