Explore key aspects of aircraft systems with the MHAFB CDC 2A051T Vol. 1 quiz. Covering topics like aerial navigation, ILS, TACAN, and VOR systems, this quiz assesses understanding of directional guidance and operational principles essential for aviation professionals.
Antenna
Speaker
Amplifier
Microphone
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CALL
HOT-MIC
EXTERNAL
INTERPHONE
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Active
Passive
Geosynchronous
Nongeosynchronous
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Left wing down
Right wing down
Nose up, nose down
Nose left, nose right
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Noise
Distortion
Modulation
Heterodyning
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29 (0-29)
29 (01-29)
30 (00-29)
30 (01-30)
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Size
Value
Resolution
Consistency
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30 Hz reference and 30 Hz variable signals
30 Hz reference and 9960 Hz FM signals
30 Hz variable and 9960 Hz FM signals
90 Hz and 150 Hz modulated signals
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2.2500 to 3.9997 MHz
22.500 to 39.997 MHz
225.000 to 399.975 MHz
2250.00 to 3999.75 MHz
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AM only
AM and FM
Pulse and AM
Pulse and FM
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Carrier only
Upper sideband only
Lower sideband only
Carrier and one sideband
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Used for noise reduction
Primarily used to prevent shock
Connected close to each line replaceable unit
Completes the path for current back to the power source
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Circuit breakers are closed
Station rotary select is set to operate
Monitor panel pushbutton is engaged
Set control master switch is depressed
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Preassigned
Assigned randomly
Assigned on the basis of current need and priorities
Are assigned on the basis of current location of the aircraft
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Roll and yaw
Pitch and yaw
Pitch and roll
Yaw and direction
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Rockets
Missiles
Nuclear bombs
Conventional bombs
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Removes the sidebands
Removes the center frequency
Filters, amplifies, and up converts.
Down converts, amplifies, and up converts
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Cause a Doppler shift
Enhance radar returns
Confuse radar operators
Jam a specific frequency
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Bend
Radical
Articulated
Reverse mount
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Time of day
Aircraft identification
Have-quick synchronization
Correction for in-flight internal navigation system (INS) alignment
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225 MHz
234 MHz
243 MHz
325 MHz
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Lateral
Vertical
Horizontal
Longitudinal
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Ailerons
Twin ruddrs
Stabilators
Flaperons
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Stick
Throttle
Rudder pedals
Integrated servo actuator
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A way to interface multiple aircraft systems
A method of communication between analog aircraft systems
The concept of time-sharing communication lines on the aircraft
The procedure of transmitting many digital signals over a single pair of wires
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Manual
Computed
Automatic
Manual computed
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Airborne interrogator-receiver and a surface beacon (UHF range)
Airborne interrogator-receiver and a surface beacon (VHF range)
Airborne beacon and surface interrogator-receiver (HF range)
Airborne beacon and surface interrogator-receiver (LF range)
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Computer
Integrator
Stabilized platform
Performance monitor
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One altitude
Two altitudes
Six altitudes
Seven altitudes
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Allow the transmission of the center frequency and carrier signal from one antenna
Match the impedance of the antenna to the selected frequency
Compensate for the degree of atmospheric ionization
Allow the use of multiple antennas
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Wings
Rudders
Flaperons
Elevators
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Pulsed
Modulated
Unmodulated
Stationary
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0.25 degrees off glide path
2.5 degrees off glide path
0.6 degrees off glide path
6.0 degrees off glide path
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Index
Coriolis
Hard iron
Transmission
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75-bits per second (bps)
300 bps
33.6-kilobits per second (Kbps)
56 Kbps
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Echo frequency
Local oscillator "beat" frequency
Sum of the echo frequency and local oscillator "beat" frequency
Difference between the echo frequency and the local oscillator "beat" frequency
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8,000 pounds
8,355 pounds
10,000 pounds
10,355 pounds
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Analog and digital
Motion and velocity
Electrical and mechanical
Acceleration and directional
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Target is approaching the set
Target is moving parallel to the set
Distance between the target and set is decreasing
Distance between the target and set is increasing
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Operator
Main computer
Backup computer
Interface unit
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Microwave landing system (MLS) back azimuth transmitter
MLS approach azimuth transmitter
Glide slope
Localizer
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Time
Distance
Direction
Distance and time
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Mode 1
Mode 2
Mode 3/A
Mode 4
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Between the chord line and true heading
Between the chord line and the direction of relative wind
Of elevation between the aircraft pitch line and the target
Beween the aircraft pitch line and the surface of the earth
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Two pure platinum sensing elements
A stabilized gyroscope that detects aircraft angle
Two synchros that align the probe tip with the airstream
A movable sensing element that routes air into two synchro cavities
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Digital and analog information alternating on the MUX system
Avionics systems processing digital information at different times
All information that has to be processed takes turens on the same communication line
A method of controlling the amount of time each avionics system can communicate on a MUX line
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Concurrently
Consecutively
Asynchronously
Monosynchronously
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Way the load exits the aircraft
Type of cargo parachute used
Rate of decent of the load
Type of platform used
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Quiz Review Timeline (Updated): Mar 21, 2023 +
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