General Limitations Flashcards
Max turbulent air speed
280 KIAS or M .75 (whichever is lower)
Max relief differential pressure
8.7 PSI
Max negative differential pressure
-0.5 PSI
Max differential pressure for taxi, takeoff and landing
0.1 PSI
Min cabin altitude in MANUAL mode
-1,500 ft
Normal minimum autopilot altitude
600 AGL
Min autopilot altitude for visual and non-precision approaches
400 AGL
Min autopilot altitude for precision approaches
80 AGL
Min altitude for true north operations
10,000 ft
Min RVR for rolling takeoff when HGS guidance is used
1200 RVR
Min autopilot altitude during an “A” mode approach with the HGS
650 ft
Max time on ground with DC power only
5 min (to protect CRT displays)
Max airpseed with ADG deployed
Vmo/Mmo
Max altitude for SLATS/FLAPS operation
15,000 ft (enroute use of slats/flaps prohibited)
Min altitude for use of flight spoilers
300 AGL
Min engine fuel temperature for takeoff
5 C
Bulk Fuel Takeoff Limit [Jet A]
-30 C
Bulk Fuel Freezing Point [Jet A]
-40 C
Takeoff with a fuel load in excess of 500 lbs in the centre tank is not permitted unless:
-Each main wing tank is above 4400 lbs; or
-Each wing tank is above 2000 lbs and the allowable zero fuel weight is reduced by the weight of the fuel in the centre tank in excess of 500 lbs
Prolonged ground operation with any hydraulic system operating should be avoided when ambient temperatures are greater than ___
40 C
Normal hydraulic system pressure
2800 to 3200 PSI
Normal hydraulic system quantity
45% to 85%
Max Landing Gear Speed [Retraction]
200 KIAS
Min brake cooling time between landing or rejected takeoff and subsequent takeoff
15 min