This quiz, titled '2A656 VOL 3 URE (2013)', assesses knowledge on AC power systems in aerospace contexts, focusing on components like CSDs, GCUs, and GLCs. It evaluates understanding of generator operations, load control, and emergency power management, crucial for professionals in aerospace electrical engineering.
135 [±3] VAC.
125 [±3] VAC.
115 [±2] VAC.
105 [±2] VAC.
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Both the electrical and hydraulic systems.
The electrical system.
The hydraulic system.
The bleed air system.
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Take meter readings.
Limit the malfunction.
Define the discrepancy.
Perform operational check of the system.
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Emergency power disconnect relay (EPDR).
Emergency power interlock relay (EPIR).
Emergency generator test switch (EGTS).
Power fail relay (PFR).
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Ohms check the switch.
Voltage check the switch.
Perform an operational check.
Turn in all tools and test equipment.
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115 VAC, 60 hertz.
208 VAC, 60 hertz.
115 VAC, 400 hertz.
208 VAC, 400 hertz.
Repair the defective item.
Bench-check any new parts.
Perform an operational check.
Replace any malfunctioning part.
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Soft iron.
Aluminum.
Malleable tin.
INCONEL®.
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Data bus controller.
Parallel data bus.
Remote terminal.
Serial data bus.
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Turn off inoperative systems.
Give wind and speed crosswind data.
Tell the pilot how much fuel is left in the main tank.
Transfer data between an aircraft system and the data bus controller (DBC).
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Floodlights.
Instrument.
Warning.
Utility.
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Load controller.
Underspeed switch.
Constant speed drive.
Generator control unit.
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10 to 12 VDC.
26 to 31 VDC.
32 to 36 VDC.
52 to 56 VDC.
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Extinguishes.
Remains illuminated.
Flashes on and off briefly.
Remains on throughout the full cycle of the ailerons.
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Open, hold, and land.
Open, hold, and retract.
Open, release, and retract.
Actuate, hold, and retract.
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Emergency DC bus.
Right main DC bus.
Essential DC bus.
Isolated DC bus.
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In the air.
In the air, with gear fully retracted.
In the air, with gear down and locked.
On the ground, with weight on the wheels.
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Learn normal system operation.
Define the discrepancy.
Limit the malfunction.
Take meter readings.
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The pilot valve.
A pressure switch.
Centrifugal switch.
The ON-OFF switch in the cockpit.
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No. 1 transformer rectifier (TR).
No. 2 TR.
Standby battery relay.
Normal battery relay.
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Scissors assembly
Steer control valve.
Hydraulic linear actuator.
NWS A/R DISC MSL step switch.
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Review the technical order (TO).
Disconnect the power.
Analyze the malfunction.
Check for continuity.
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90 VAC from A phase.
90 VAC from C phase.
93 VAC from A phase.
93 VAC from C phase.
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Up (left wing up).
Up (left wing down).
Down (right wing up).
Down (right wing down).
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½ gpm.
1 gpm.
2 gpm.
3 gpm.
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Locked wheel circuit.
Brake indicator driver.
Touchdown protection.
Pressure bias modulation.
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Current input.
Voltage input.
Current output.
Voltage output.
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Infinity.
5 ohms.
50 ohms.
500 ohms.
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Sunlight.
Light emitted from flashlights.
Signals with a frequency between 7 and 60 Hz.
Signals with a frequency between 60 and 160 Hz.
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Ramp opens first.
Door opens first.
Ramp and door open at the same time.
The door will open, but the ramp will remain closed.
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Bus protection panel (BPP).
Auxiliary power unit (APU).
APU/external power contactor (AEPC).
APU/external power disconnect contactor (AEDC).
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Bus tie connector (BTC).
Bus protection panel (BPP).
APU/external power contactor (AEPC).
APU/external power disconnect contactor (AEDC).
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Flasher.
Anti-collision.
Both anti-collision and flasher.
Both anti-collision and landing light
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Lockout relay (LOR).
Bus protection panel (BPP).
APU/external power contactor (AEPC).
APU external power disconnect contactor (AEDC).
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10 hertz (Hz).
100 Hz.
200 Hz
400 Hz.
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Open relay will energize.
Open relay will de-energize.
Position relay will energize.
Position relay will de-energize.
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Power for the horn silence relay.
A ground for the horn silence relay.
A lock-out circuit for the horn silence relay.
An open circuit for the horn silence switch.
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Extended forward and downward.
Form a slot between the flap and the wing.
Increases the chamber or curvature of the wing.
Lowers the trailing edge to about 40° below its retracted (UP) position.
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Crossfeed.
Fire shutoff.
Interconnect.
Fuel-level control.
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A photoconductive cell.
An iron fireman switch.
A FENWAL® switch.
A continuous cable.
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The shutter closes.
The fault is corrected.
The reset circuit is energized.
Another system fault is detected.
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Limit switches.
Touchdown relays.
Control handle solenoids.
Up-lock and down-lock cylinder sending units.
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GEN terminal is greater than the indicator terminal.
GEN terminal is less than the battery terminal.
GEN terminal is greater than the SW terminal.
BAT terminal is less than the SW terminal.
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Two.
Three.
Four.
Five.
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Manual system.
Autopilot system.
Hydraulic system.
Electric power system.
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Perform an operational check.
Limit the malfunction.
Take meter readings.
Replace a bad pump.
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Door is in the fully up position.
Ramp is in the fully up position
Door is in the fully down position.
Ramp is in the fully down position.
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Control stick grip trim switch.
Aileron trim control switch.
Trim selector switch.
Auxiliary trim switch.
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