Learjet 20 Series Pilot Training Manual page 335

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1.
Pitot and static drain valves are
located:
A. In the nose wheel well
B. On the skin below the entrance door
C. On the nose section near the nose
gear wheel well doors
D. On the nose section at the lower cen-
terline
2.
The pilot's pitot system supplies im-
pact pressure to the:
A. Mach overspeed switch and
Mach/airspeed indicator
B. Cabin pressure controller and
Mach/airspeed indicator
C. Mach/airspeed indicator and autopi-
lot controller
D. Mach/airspeed indicator
3.
An alternate static source is selectable
for the:
A. Autopilot altitude controller
B. Pilot's flight instruments only
C. Mach airspeed overspeed switch
D. Copilot's flight instruments only
4.
When the FC 110 manual pitch com-
mand (thumbwheel) is operated, it will
disengage:
A. The altitude hold mode
B. All available modes
C. The heading and altitude hold
modes
D. The heading mode
5.
In accordance with the AFM supple-
ments, the FC 110 must be:
A. Engaged when flying at speeds
above Mach .78 or .79
B. Disengaged before using the spoilers
C. Flown with altitude hold off in se-
vere turbulence
16-18
LEARJET 20 SERIES PILOT TRAINING MANUAL
QUESTIONS
FOR TRAINING PURPOSES ONLY
D. Operated as outlined in A, B, or C
6.
The basic attitude reference mode is
energized when:
A. AC and DC power is applied to the
airplane.
B. The AUTO PILOT engage button is
depressed.
C. The TEST switch is depressed.
D. Both A and B above
7.
When using autopilot back course
mode, the:
A. Reciprocal of the front course must
be set in the HSI course window.
B. Glide-slope receiver signal is cap-
tured.
C. Published inbound (front) course
must be set in the HSI course win-
dow.
D. Both B and C are correct.
8.
To control the airplane in the pitch
axis, the autopilot uses the:
A. Pitch servo only
B. Pitch servo and trim tabs on the
elevators
C. Horizontal stabilizer trim actuator
only
D. Pitch servo and emergency pitch trim
motor
9.
When the pedestal disconnect lever is
depressed and held, it will
A. Completely disengage the autopilot
B. Disengage the pitch and roll axes
while the lever is depressed
C. Disengage the pitch axis while the
lever is depressed
D. Disengage the roll axis while the lever
is depressed
FlightSafety
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