Autofeather conditions
Hot Battery Bus (singularly powered)
Hot Battery Bus (dual powered)
Right Squat Switch
Flight hour meter Operation of some functions of AHRS/GPS/DCU inhibited Radar stby after 60 secs Transponder stby Landing gear circuit inop, j hook extends Engine lip boot heat right side Stall heat 28V to 14V Stall warning deactivated
Left Squat Switch
Left engine inlet lip heat inop
Electric heater works in ground max
Ambient air solenoid to close
Pressurization controls