NATOPS Flashcards
1
Q
Autofeather conditions
A
- AUTOFEATHER swich in ARM
- both power levers in position that would normally correspond to 90 +/- 2% N1 or greater
- torque drops on one engine below 200 +/- 40 lb.ft
2
Q
Hot Battery Bus (singularly powered)
A
- LH/RH Fire Extinguishers
- Baggage door light
- Threshold light
- Spar cover light
- Aft dome light
- Cabin door observer light
3
Q
Hot Battery Bus (dual powered)
A
- LH/RH boost pumps
- LH/RH firewall shut-off valves
- Crossfeed valve and crossfeed annunciator light
4
Q
Right Squat Switch
A
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
5
Q
Left Squat Switch
A
Left engine inlet lip heat inop
Electric heater works in ground max
Ambient air solenoid to close
Pressurization controls