This pretest assesses knowledge of the C-5 aircraft's control systems, including aileron cable systems, roll control, elevator control, and pilot assistance mechanisms.
Centering device.
Override bungee.
Mix box.
Flaps.
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Lift increases.
Lift decreases.
Airspeed increases.
Airspeed decreases.
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Swash plate.
Foot pedals.
Rudder.
Cyclic.
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Variable flap drive roller carriages.
Variable slat drive roller carriages.
Telescoping ballscrew actuators.
Telescoping slat drive limiters.
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Switches to channel B and remains engaged.
Remains in channel A with reduced accuracy.
Remains in channel A and disengages the system.
Switches to channel B and disengages the system.
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Step-down transformer.
Torque synchro.
Gear train.
Lever.
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A solenoid-operated shutoff valve (SOV), hydraulic pressure switch (HPS), electrohydraulic valve (EHV), and linear variable differential transformer (LVDT).
An SOV, automatic throttle system, EHV, and LVDT.
A pressure data converter, HPS, EHV, and LVDT.
And SOV, HPS, EHV, and pilot assist cable servo.
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Spring.
Servo.
Cable.
Beam.
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Two power sources to the trim actuator.
Power and ground to the trim actuator.
A discrete pulse to the yaw computer.
Two grounds to the yaw damper.
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Single channel failure protected.
Fail-operational and fail-safe.
Fail-operational only.
Fail-safe only.
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Very-high frequency control panel.
Inertial navigation system.
Master caution.
Autopilot.
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Maintenance.
Continuous.
Postflight.
Preflight.
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Ailerons.
Rudder pedals.
Force transducer.
Ailerons and spoilers.
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Degrees; 0-60.
Degrees; 0-100.
Percentage; 0-60.
Percentage; 0-100.
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Dual power relays.
Power and ground.
Backup battery power.
Bipolar synchro transmitters.
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95; 80.
75; 60.
50; 40.
20; 15.
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Yoke.
Cyclic.
Collective.
Foot pedals.
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53 degrees, 55 minutes (').
56 degrees, 37'.
57 degrees, 57'.
61 degrees, 57'.
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Symmetrically by the pilot control stick only.
Asymmetrically by the pilot control stick only.
Asymmetrically by the co-pilot control stick only.
Symmetrically by the pilot and co-pilot control sticks.
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High-pass.
Low-pass.
Greenfield.
Body-bend.
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Aileron.
Elevator.
Dutch roll.
Trim stabilizer.
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Turn knob.
Pitch wheel.
Air control unit sensor.
Angular accelerometer.
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Attitude hold.
Altitude hold.
Dutch roll damping.
Divergence control.
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The GLIDE SLOPE CAP annunciator goes out.
ALT HOLD or MACH HOLD are engaged.
The GLIDE SLOPE beam is captured.
The localizer beam is captured.
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Pilot assist cable servo.
Centering spring.
Bob weight.
Cable.
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Roll axis is engaged.
Yaw axis is engaged.
Pitch axis is engaged.
Lateral axis is engaged.
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Parity.
Polarity.
Amplitude.
Frequency.
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1 - 1 1/2 minutes.
2 - 3 minutes.
5 - 10 minutes.
More than 10 minutes.
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Weight-on-wheels.
Forward relay unit.
Digital remote unit.
System control unit.
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Synchro.
Solenoid switch.
Variable resistor.
Control transformer.
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Trim actuator.
Jackscrew assembly.
Surface control assembly.
Drum and bracket assembly.
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Rotary variable displacement transducers (RVDT) in the hydraulic actuators.
Linear variable displacement transducers (LVDT) in the hydraulic actuators.
RVDTs in the integrated flight control module.
LVDTs in the integrated flight control module.
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Switch.
Spring.
Valve.
Cam.
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Slats in or left/right main gear must be uplocked.
Slats in and left/right main gear must be uplocked.
Flaps out or left/right main gear must be downlocked.
Flaps out and left/right main gear must be downlocked.
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Aileron.
Trim tab.
Elevator.
Stabilizer.
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Variable feel unit.
Centering spring.
Bob weight.
Cable.
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DOWN, T/O 40, T/O AND APP, and LANDING.
DOWN, T/O 80, T/O AND APP, and LANDING.
UP, T/O 40, T/O AND APP, and LANDING.
UP, T/O 80, T/O AND APP, and LANDING.
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With one bellcrank and two push-pull rods.
Through two bellcranks and push-pull rods.
With tension regulator bungees and bellcranks.
To one another with idler arms and push-pull rods.
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Cam.
Brake.
Bellcrank.
Output shaft.
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0.
1.
2.
3.
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A shaker signal.
An axis hardover.
An FCS shutdown.
An axis disengagement.
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Processor.
Control panel.
Flight controller.
Status/test panel.
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ALT HOLD.
LOCALIZER.
MACH HOLD.
GLIDE SLOPE.
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Engages into the mode the pilot has selected.
Causes the F/D to switch to the A/P mode.
Automatically disengaged the F/D mode.
Engages into the same mode as the F/D.
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HOV.
HOV/RA.
RAD/ALT.
BAR/ALT.
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Slats.
Flaps.
Spoilers.
Speedbrakes.
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The position of the travel limit switches.
Whether the brake is engages or disengaged.
The signal from the proximity switch assemblies.
Which power control assembly relay is energized or deenergized.
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Wing camber control.
Vertical lift distribution.
Spiral divergence control.
Roll coriolis compensation.
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Quiz Review Timeline (Updated): Mar 22, 2023 +
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