15-30
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP
PILOT TRAINING MANUAL
FlightSafety
international
1.
The servo tab on the left aileron:
A. Aids the aileron in moving to a desired
position
B. Prevents the aileron from moving to
a selected position too rapidly
C. Functions as a trim tab
D. A and C
2.
The elevator trim tabs can be actuated:
A
Mechanically
B. Electrically
C. Mechanically and electrically
D. By servo action of the geared tabs
3.
The purpose of the rudder bias system
is:
A. To boost rudder operation in turbu-
lence
B. To automatically counteract asym-
metrical thrust due to engine failure
C. To actuate the rudder trim tab in the
event an engine fails
D. None of the above
4.
If takeoff is attempted with the aileron/el-
evator gust lock engaged:
A. The gust lock automatically disen-
gages.
B. A warning horn sounds.
C. Neither throttle can be advanced for
full power.
D. Only one throttle can be advanced to
full power.
5.
The guard is removed from a pitch trim
switch:
A. When trim cannot be accomplished
using both elements of the switch
B. During testing, to assure that trim-
ming can be accomplished with one
element of the switch
C. The guard must not be removed under
any circumstance.
D. During testing, to ascertain that trim-
ming cannot be accomplished with
one element of the switch
6.
The flight control surfaces that are hy-
draulically actuated are:
A. All primary flight control surfaces
B. Flaps and airbrakes
C. Flaps only
D. Airbrakes only
7.
Asymmetrical flap operation is prevented
by:
A. A synchronizing cable arrangement
that shuts off the flap unit cutoff valve,
stopping the flaps
B. A synchronizing cable arrangement
that mechanically connects both flap
segments, forcing them to move in
unison
C. A flow divider in the flap control unit
D. Nothing prevents asymmetrical op-
eration; it can occur.
8.
The purpose of lift dump is:
A. To decrease lift in flight
B. To increase drag and decrease lift on
the ground
C. To increase drag in flight
D. None of the above
QUESTIONS
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