Miscellaneous Flashcards
ICING CONDITIONS
(In Visible Moisture and OAT Below +5C) What equipment must be ON, operative and utilized?
- Engine/propeller anti-ice systems
- Pitot heat/SAS heat
- Windshield heat
- Wing/empennage deice boots
- Continuous ignition system
The oxygen system includes a ______ oxygen supply cylinder.
49 cubic foot
Normal oxygen cylinder pressure is between ____ and ____ psi.
1600 and 1850
The NATO code for JP-8 is _____.
F-34
What is the minimum crew?
2 pilots
Starter limitations are:
30 sec on / 60 sec off (2 cycles)
30 sec on / 15 min off
Max continuous load for each generator is:
300 amps
Minimum oil pressure above 23,000 feet is:
50 psi
Max starting current from an external power source:
1,000 amps
Max fuel imbalance when fueling in gallons:
125 gal
Icing inhibitor fule additive:
MIL-L-27686E
Useable fuel quantity in gallons and liters:
648 gal
2453 liters
Max fuel imbalance for take-off, landing and normal flight:
200 pounds
Max shaft horsepower takeoff and continuous:
1,100 takeoff
1,000 continuous
Mixing oil types is allowed (T/F)
False
Engine/propeller system total oil quantity:
7.1 US quarts
Oil specification:
MIL-L-23699B (Type II)
Full reverse speed is limited to below _____ knots.
90
Takeoff with fuel transfer pump caution light(s) is:
prohibited
Autopilot/yaw damper use during fuel balancing is:
prohibited
G-limits Flaps Up
3.02 to -1.21
G-limits Flaps Down
2.00 to zero
During single engine taxi operations, nose wheel steering must be:
on