The '2A852 CDC Volume 4' quiz assesses knowledge on navigation systems in military aviation, focusing on components like the digital controller and magnetic azimuth detector. It evaluates understanding of system errors, modes, and compensations crucial for accurate navigation.
Fuel consumption by each engine in pounds.
Fuel consumption by each engine in ounces.
Oil consumption by each engine in pounds
Oil consumption by each engine in ounces
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Pilot only
Copilot only.
Pilot and copilot.
Pilot and navigator
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Acceleration.
Wind speed.
Laser beam.
Frequency.
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An electrical connector
A pair of tubes
Shock mounts.
An amplifier.
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Atmosphere
Case
Fuel
Oil
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Engine fuel flow rate in pounds per hour
Engine fuel flow rate in ounces per hour.
Engine fuel used in pounds.
Engine fuel used in ounces
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Zero torque
Positive torque.
Negative torque
Feedback torque.
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Greater attitude changes during aircraft roll.
Smaller attitude changes during aircraft roll.
Greater attitude changes during aircraft pitch.
Smaller attitude changes during aircraft pitch
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Dim switch
Flap test switch.
Test reset switch.
Weight-on-wheels test switch.
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Lo-Z
Hi-Z.
Kapton
Thermocouple.
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Power
Monitor
Intercom
Transmitter
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Horizontal situation indicator (HSI) lubber line.
Attitude director indicator (ADI) command bars
Horizontal situation indicator (HSI) compass card.
Attitude director indicator (ADI) speed deviation scale.
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Battery
Accelerometer.
Ring laser gyro
Synchro repeater
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Engine fan blade passing by the magnetic field of the N1 tachometer transmitter.
Engine fan blade passing by the magnetic field of the N2 tachometer transmitter.
Engine fan blade passing by the limit index of the N1 tachometer transmitter
Engine fan blade passing by the limit index of the N2 tachometer transmitter
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Power level.
Fluid level
Amplifier
Torquer.
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Tripod
Aircraft
Compass rose
Magnetic field monitor
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Oil
Fuel
Series
Parallel
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0.1
1.0
2.0
4.1
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DG mode
RGA mode.
MAG mode
AUTO mode.
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Airborne alignment
Gyro compass alignment
Inertial navigation system initialization (INS INIT).
Global positioning system initialization (GPS INIT).
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Global positioning system only.
Pure inertial
Stored heading
Blended solution.
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0 to 1.999 milliohms.
0 to 19.99 milliohms.
19 to 199.9 milliohms.
199 to 1999 milliohms.
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Approach speed.
Approach track
Ground speed
Ground track.
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0 to 150.
0 to 200
15 to 100
15 to 200.
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Pints.
Quarts
Gallons
Pounds.
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Coarse adjustments of simulation values.
Fine adjustments of simulation values
Coarse adjustments of power values.
Fine adjustments of ground values
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Rotation of the Earth, and geographic longitude.
Rotation of the Earth, and geographic latitude
Aircraft attitude, and geographic longitude
Aircraft attitude, and geographic latitude
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Magnetic azimuth detector or remote magnetic compensator.
Remote magnetic compensator or digital controller
Magnetic azimuth detector or digital controller
Compass controller or compass amplifier
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Five monitored dual navigation systems has a discrepancy
Seven monitored dual navigation systems has a discrepancy.
Five monitored dual navigation systems is operating correctly
Seven monitored dual navigation systems is operating correctly.
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Global positioning
Flight director
Autopilot.
Compass.
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Meridian convergence error
Transmission error.
Coriolis error.
Index error
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4 seconds
4 minutes
20 seconds
20 minutes
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Synchro receiver.
Bourdon tube.
Sector gear.
Rotor.
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90 degrees out-of-phase with each other
180 degrees out-of-phase with each other.
270 degrees out-of-phase with each other.
360 degrees out-of-phase with each other
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Increases and current decreases
Increases and current increases
Decreases and current increases
Decreases and current decreases.
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Compass
Autopilot.
Flight director
Digital air data.
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2
6
8
20
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Built-in display illumination
Resistance range setting
LAMP switch.
TEST switch
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Accelerometers.
Ring laser gyros
Synchro repeaters
Control/annunciator panel.
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10
90
100
270
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RGA computer
RGA control panel.
RGA interface logic unit
Longitudinal accelerometer
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Rotation go-around (RGA).
Navigation/localizer (NAV/LOC).
Approach manual (APPR MAN).
Approach automatic (APPR AUTO).
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Magnets.
Aneroids
Dual bellows
Bourdon tubes.
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Total fuel quantity indicator
Fuel quantity indicator
Compensator probe
Tank probe
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Remote heading slew switch
Pitch command control
Heading slew controls
Rate-of-turn indicator
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Wings-level dive attitude of 7 degrees
Wings-level dive attitude of 8 degrees.
Wings-level climb attitude of 7 degrees.
Wings-level climb attitude of 8 degrees.
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100 foot altitude trip voltage.
200 foot altitude trip voltage.
300 foot altitude trip voltage
500 foot altitude trip voltage.
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0 to 1000 degrees Celsius
20 to 975 degrees Celsius
0 to 1000 degrees Fahrenheit
70 to 975 degrees Fahrenheit.
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