Hawker 800 XP, Pilot Training Manual

Page: 197 / 504

1. All fuel annunciators and contents indi-
cators are supplied from bus bar(s):
A. PE and/or BATT 1
B. PS1 and PS2
C. PE and XE
D. A and B
2. The number of water drains in the fuel
system is:
A. Two
B. Three
C. Four
D. Five
3. When the ventral tank contains fuel, a
low VMO horn will sound whenever air-
plane speed exceeds:
A. 270 KIAS
B. 280 KIAS
C. 292 KIAS
D. 320 KIAS
4. Total usable fuel capacity is:
A. 9,300 pounds
B. 9,440 pounds
C. 9,640 pounds
D. 10,000 pounds
5. The maximum lateral imbalance permit-
ted is:
A. 250 pounds
B. 500 pounds
C. 750 pounds
D. 1,000 pounds
6. With both boost pumps inoperative:
A. Leave the AUX FUEL TRANSFER
lever open.
B. Fuel will gravity transfer.
C. Both A and B
D. Ventral tank fuel cannot be trans-
ferred.
7. If the ventral tank is to be used in flight,
it must be full, and each wing must con-
tain more than:
A. 3,300 pounds of fuel
B. 1,000 pounds of fuel
C. 3,450 pounds of fuel
D. 2,000 pounds of fuel
8. The aircraft fuel system accepts a maxi-
mum refueling supply pressure of:
A. 25 psi
B. 45 psi
C. 50 psi
D. 55 psi
5-11
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP PILOT TRAINING MANUAL
FlightSafety
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QUESTIONS