This quiz, titled '2A533A Volume 5: Avionics System!', assesses knowledge on the manual control and built-in test functionalities of steerable television systems in military avionics. It is designed for learners aiming to understand operational protocols and troubleshooting of avionics equipment.
Sun
Moon
Earths Surface
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Sensor unit
Video post processor
Video distribution unit
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Auto turns it on
Auto turns it off
Changes the color of the light displayed
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Illustrate the external connections
Show the input on the right
Flow from left to right
Flow from right to left
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Shutter
Flash Protector
Control Module
Image-gating unit
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2 volts were applied
5 volts were applied
-2 volts were applied
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Have no danger of overcharging
Complete the charge cycle and the T/S shuts down
Overcharge and must be replaced
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Display of fiducial marks
Closing of the camera shutter
Display of fiducial marks and preamp noise
Closing of the shutter and preamp noise on the display
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Servo control unit and video distribution unit (VDU)
Symbol signal generator and radar scan converter
VDU and symbol signal generator
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Diluted
Reflected
Refracted
Absorbed
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Distance to fault measurements
Disturbance measurements
Continuity tests
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LL
ILLUM
ELEC-A
ELEC-B
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CAL ADJ
RANGE HOLD
CAL FACTOR %
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Gain and Light Level
Gain and Light Emission
Sensitivity and light level
Sensitivity and light emission
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LL, HL, and ILLUM
LL and HL
ELEC-A
ELEC-B
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Reset the mode switch to OFF and back to STBY
Reset the mode switch to STBY and back to OPR
Cycle the built-in test switch from NORM to ELEC-B and back
Do nothing because the fault is noted and cleared in 2 minutes
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Iris
Video automatic gain
Image intensifier exposure
Sensor photocathode voltage
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Has frequency
Has wavelength
Is caused by molecular friction.
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Focal plan array
Gimbal assembly
Signal data converter
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Alphabetic and Numeric
Cross-reference and numeric
Alphanumeric and Alphabetic
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Magnetic
Electrostatic
Magnetic and Electrostatic
Electrostatic and Mechanical
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Video saturation disapperas and the system reverts to ALC FULL mode
The system enters ALC FULL MODE
The system reverts to STBY mode
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Preflight tests
BIT ELEC-B
Front-to-rear tests
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The nature of the controlling medium
The manner in which IR is processed
That visible light can be refracted while IR cannot
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Gimble Assembly
FLIR control panel
Signal data converter
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Short
Open
Frayed cable
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DELETE
SELECT
ENTER
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Properly married with the power sensor
Set to match the line voltage you are using
Adjusted to the freq range to be measured
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Aircraft
Power unit
Parking ramp
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Current
Voltage
Distance
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TEST and RF
TEST and monitor
CONFIDENCE and RF
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72 Hours
48 Hours
24 Hours
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Controls system gain
Turns on the camera assembly
Protects the camera tube assembly
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Neutralize
Stabilize
Climb to -1.000 mW
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36 inch 50 ohm cable
36 inch 25 ohm cable
12 inch 50 ohm cable
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1 + 2
1, 2, 3/A and 4
1, 2, 3/A and C
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Relative decibels (dBR)
Referenced decibels (dBm)
Measured decibels (dBM)
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-1.000 milliwatts (mW)
1.00 mW
-1.000 Watts (W)
1.00 W
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1
2
3
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LL
ILLUM
ELEC-A
ELEC-B
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Comprehensive system checks of the MLS components
GO/NO-GO functions of the cockpit controls
GO/NO-GO verification of the installed MLS receivers
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Oscilloscope
Power meter
Time domain reflectometer
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MODE
DB REF
RANGE HOLD
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102 NM
125 NM
132 NM
146 NM
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0 - 1 hour
1 - 2 hours
2 - 3 hours
3 - 4 hours
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Make RF power level calibrations
Remove and install the system antenna
Install the MLS test batteries
Make RF signal Adjustments
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12 Hours
36 Hours
24 Hours
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ELEC-A; Camera assembly
ElEC-B; Camera Assembly
ELEC-A; Camera electronics
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Quiz Review Timeline (Updated): Jan 13, 2023 +
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