This quiz for 2A652 (AGE Journeyman) Volume 3, Edit Code 6 assesses knowledge on converting electrical energy to mechanical energy, motor inertia, torque, and induction motor operations. It's designed for learners aiming to master practical applications in aerospace ground equipment.
Voltage check.
Continuity test.
Visual inspection.
Current measurement.
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Correct defective components only.
Rigid maintenance schedules.
Periodic overhaul schedule.
Preventive maintenance.
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Historical record.
Maintenance record.
Troubleshooting chart.
Illustrated parts breakdown.
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Wattage.
Horsepower.
Rotational force.
Opposition to applied voltage.
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Blockage of airflow.
Lube system malfunctions.
Slipping belts on the blower.
Abrasion by foreign particles.
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Retorque the engine-mount bolts.
Drain moisture from fuel system.
Perform a preoperational check.
Perform a periodic inspection.
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Excessive exhaust gas temperature.
Maladjusted rate adjustment screw.
Ruptured actuator diaphragm.
Defective relief valve.
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Direct current (DC) generator.
Single-phase generator.
Two-phase generator.
Three-phase generator.
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Only minor repairs.
Any needed repairs.
A periodic inspection.
An operation inspection.
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Unit under test (UUT).
Load bank generators.
External batteries.
Facility power.
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Connects the batteries together.
Protects the exciter field circuit.
Allows two generators to be paralleled.
Allows for quick warm-up of the batteries.
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After equipment is placed on the ready line.
After maintenance.
Once a week.
Once a day.
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Leakage.
Excess heat.
Hairline cracks.
Foreign objects.
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The load is automatically removed and the cooling cycle begins.
The load bank will start the load test over again.
The load bank will automatically shuts down.
The display will show results of the load test.
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Fuel gravity system.
Fuel transfer system.
Low fuel level safety circuit.
Manually operated switch to change tanks.
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Chamber 2 pressure.
Chamber 4 pressure.
The rate adjustment screw.
The dual-ball selector valve.
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Flow chart.
Wiring diagram.
Schematic diagram.
Reference designation list.
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Aerospace ground equipment (AGE) generator sets only.
Alternating current (AC) power supplies only.
Direct current (DC) power supplies only.
AC and DC power supplies.
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Blowing off with 5 pounds per square inch (psi) uncontaminated air.
Blowing off with 15 psi uncontaminated air.
Scrubbing with soap and water.
Steam cleaning.
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Protects the generator electrical system against damage resulting from an overload, overvoltage, undervoltage, and over/underfrequency.
Protects the aircraft electrical system against damage resulting from an overload, overvoltage, undervoltage, and over/underfrequency.
Senses fault conditions, stopping the generator.
Senses fault conditions, stopping the engine.
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5 minutes.
10 minutes.
15 minutes.
20 minutes.
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Resolder them until they have been bench checked.
Cut them, but remove the wiring completely intact.
Resolder them until all wiring has been replaced with new wires.
Cut them unless there is sufficient length remaining for resoldering.
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Fuel atomizer.
Main fuel pump.
Combustion chamber.
Fuel air mixture valve.
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Excessive engine revolutions per minute (rpm).
Excessive engine exhaust temperature.
Oil that enters the airflow system.
Fuel mixing with the airflow.
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Its operating 5 times faster than a car engine.
Noise, intense heat, and electrical shock.
Excessive carbon monoxide buildup.
Turbine wheel disintegration.
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Pressure sufficient for bleed operations.
Air filter sufficient for operations.
Pressure sufficient for operations.
Air filter needs to be changed.
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20 degrees apart.
30 degrees apart.
90 degrees apart.
120 degrees apart.
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Radiator cap.
Thermostat.
Water pump.
Radiator.
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EMF, relative motion, and magnetic field.
Magnet, lines of force, and relative motion.
Magnetic field, a conductor, and relative motion.
Counter-electromotive force (CEMF), a conductor, and magnetic field.
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Safety interlock.
EF line fuse.
Start switch.
Stop switch.
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Air inlets for blockage.
Wiring for secure mounting.
Maintenance panels for corrosion.
Interior air vents for secure mounting.
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Alternating current (AC) generator.
Fuel pump and control unit.
Tachometer generator.
Starter motor.
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Atomizer.
Drain valve.
Pneumatic control device.
Acceleration limiter valve.
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Cooling fans blowing into prevailing wind.
Cooling fans blowing not into prevailing wind.
Load bank close to generator to eliminate line drop.
Load bank as far as possible from generator for cooling.
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From 0 to 35 percent.
From 35 to 95 percent.
From 95 to 100 percent.
Anytime during operation.
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Overvoltage.
Out-of-phase.
Undervoltage.
Fault.
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At the last minute.
With the defective part removed.
Before final reassembly of the enclosure.
As soon as you replace the defective part.
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Fuel atomizer.
Combustor can.
Mixer assembly.
Plenum chamber.
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Alternating current (AC).
Direct current (DC).
Pulsating AC.
Pulsating DC.
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Turning the start switch OFF, then ON.
Turning the master switch OFF, then ON.
De-energizing the low-level lockout relay.
De-energizing the low-level warning switch.
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Cooling.
Sealing.
Cleaning.
Reducing friction.
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Overspeed actuator.
Fuel shutoff switch.
35 percent centrifugal switch.
110 percent centrifugal switch.
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Battery charging resistor.
Battery charging diode.
Voltage regulator.
Charging shunt.
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Opens the magneto circuit.
Energizes the shutdown solenoid.
De-energizes the engine run/idle circuit.
Puts the fuel rack in the NO-FUEL position.
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Decreased because of the increased internal operating temperature of the engine.
Increased because of the better mixing of the fuel with the air charge.
Used more efficiently and horsepower is increased.
Used more efficiently and horsepower is decreased.
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Mechanical linkage.
Actuator diaphragm.
Rate adjustment screw.
Actuator return spring.
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Sudden rumbling noises after 35 percent.
A decrease in vibration after 35 percent.
Smooth and quiet acceleration.
Burping.
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35 percent switch has closed.
95 percent switch has closed.
110 percent switch has opened.
BLEED AIR ON switch is closed.
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