Hawker 800 XP, Pilot Training Manual

Page: 263 / 504

1. The powerplant classification on Hawker-
800 XP series airplane is:
A. Free-spool turbofan
B. Reverse-flow turbofan
C. Two-spool turbofan
D. Single-spool turbojet
2. When the airplane is static on a standard
day at sea level, each engine develops:
A. 4,660 pounds of thrust
B. 3,000 equivalent shaft horsepower
C. 3,700 pounds of thrust
D. 4,300 pounds of thrust at 98% N
2
3. The primary overspeed rpm-limiting de-
vice on the 731 series engine is the:
A. N
1
ultimate overspeed sensor
B. PT
2
T
T2
limiter
C. N
2
ultimate overspeed sensor
D. Mechanical governor in FCU
4. The maximum HP rotor (N
2
) overspeed
is:
A. 100% for 5 minutes
B. 103% for 5 seconds
C. 105% continuous
D. 101% momentary
5. The maximum oil pressure for power at
or above idle rpm without a time limit is:
A. 55 psi
B. 25 psi
C. 38 psi
D. 46 psi
6. The maximum interturbine temperature
for engine starting or relight is:
A. 924° C over 30,000 feet for 10 seconds
B. 952° C until stabilized at idle rpm
C. 996° C for 10 seconds or 5 seconds in
excess of 996° C
D. 995° for the first 5 minutes of operation
7. The maximum transient oil pressure per-
missible is:
A. 55 psi for 3 minutes
B. 38 psi for takeoff, climb, and maxi-
mum continuous
C. 55 psi for all operations under 25,000
feet
D. 25 psi for a maximum of 3 minutes
8. If the MWS reverser annunciator illumi-
nates during the deploy cycle it indicates:
A. T/R’s are not deployed
B. Rudder bias not inhibited
C. Throttles are above idle
D. Auto stow cycle activated
9. To facilitate an accurate setting of climb
power:
A. MWS annunciator comes on
B. APR light goes out
C. A green light in ITT indicator lights
D. APR green light illuminates
10. The APR system is available:
A. To both engines at all times
B. If the engine sync system is on
C. When both computers are functioning
D. To t h e e n g i n e w i t h a n o p e r a t iv e
computer
Revision 1.02 7-39
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP PILOT TRAINING MANUAL
FlightSafety
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