Explore the intricacies of jet fuel management in '5 Level Volume 3'. This quiz assesses knowledge on JP-8 fuel composition, its behavior under different conditions, and crucial aspects of fuel control in jet engines. Essential for learners in aerospace and mechanical engineering.
T5 amplifier.
Unified control.
Afterburner fuel control.
CENC
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Soft metal construction; these seals can be damaged easily.
Soft metal construction; they are sharp and can cut your hand.
Hard metal construction; they are sharp and can cut your hand.
Hard metal construction; these seals can damage the bearing races.
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Aeration.
Induction.
Convection.
Compression.
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Wear metals.
Friction metals.
Precious metals.
Transformation metals.
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Static.
Electronics.
Mutual induction.
Electromagnetic induction.
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Has a constant polarity; AC changes direction at regular intervals.
Fluctuates from negative to positive values; AC stays at a constant positive value.
Differs from AC only in the way current is used; otherwise there is no real difference.
Is produced directly from a generator; AC is produced by an alternator after the generator.
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Act as the basic engine tailpipe.
Control engine discharge pressure.
Aid in control of engine oil pressure.
Help to control pressure and N2 speed.
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Gasoline and kerosene.
Gasoline and diesel fuel.
Diesel fuel and kerosene.
Diesel fuel and aviation gasoline.
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A green flag pops out of the filter.
Fuel pressure from the fuel pump is low.
A differential pressure indicator is actuated.
There is no way to tell without disassembling the filter.
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Fuel pump.
Fuel pump controller.
Signature elimination probe.
DEEC.
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Air/oil.
Fuel.
Hydraulic.
Pneumatic
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1 and 2.
1 and 3.
2 and 3.
2 and 4.
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Accelerates the rate of wear, decreasing the production of wear metal particles.
Accelerates the rate of wear, increasing the production of wear metal particles.
Slows the rate of wear, decreasing the production of wear metal particles.
Slows the rate of wear, increasing the production of wear metal particles.
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Alumel.
Chromel.
Both alumel and chromel.
None of these.
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Oil pressure transmitter.
Engine Diagnostic Unit.
Fan turbine Inlet Temperature.
Augmentor Nozzle positioning indicator.
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Flameout.
Turbine seizure.
Compressor shift.
Overtemperature.
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Oil
Fuel.
Ram air.
Hydraulic fluid.
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1/25 inch.
1/250 inch.
1/2,500 inch.
1/25,000 inch.
Secondary fan airflow as a coolant.
Secondary fan airflow as an oil heater.
Primary core engine airflow as a coolant.
Primary core engine airflow as an oil heater.
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Insufficient oil collection.
Contaminated samples.
A minor stomach ache.
Paralysis or death.
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Piston-type starter
Pneumatic-type starter.
Small gas turbine engine.
Cartridge-pneumatic starter.
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Compressor stall.
Variable nozzle closes.
Decrease in exhaust gas temperature.
Increase in RPM.
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Torch igniter and hot streak.
Hot streak and fuel injection.
Pilot burner ring and hot streak.
Torch igniter and pilot burner ring.
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MFC.
DEEC
Stator generator
Throttle quadrant.
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Adjust and reseal the component.
Keep the component in service to meet the mission.
Forward the component to the authorized depot for reflow and resealing.
Continue to keep the component in service if it is documented as a red diagonal on Form 781A, Hydromechanical Fuel Control.
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Replaced.
Die marked.
Safety sealed and/or lockwired.
Treated with a thread locking compound.
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AFP, AFC, fuel/oil cooler, P&D, and fuel nozzles.
MFC, fuel/oil cooler, P&D, and fuel nozzles.
AFC, AFP, fuel/oil cooler, P&D, and fuel nozzles.
Fuel/oil cooler, P&D, MFC, and fuel nozzles.
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Dispose of any portion not immediately used.
Store remaining portion immediately after use.
Dispose of any portion not used within 60 days.
Store remaining portion in clearly marked containers.
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Base commander.
Unit commander.
Program manager.
Unit safety officer.
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Compressor.
Combustion.
Augmentor.
Turbine
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Option1
Option2
Option3
Option4
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Fuel nozzle
P&D valve.
N2 sensor
Tt 2.5 sensor.
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AC high-voltage.
DC high-voltage.
Continuity.
Polarity.
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JP–4 for 60 minutes
PD–680 for 30 minutes.
Kerosene for 60 minutes.
Engine lubricating oil for 30 minutes.
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Check for large particles.
Check the drain operation.
Drain off uncirculated oil.
Drain off water and sludge.
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Manually.
Electrically.
Hydraulically.
By spring pressure.
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Through a heat exchanger.
Out the turbine case bleed holes.
Into the gas stream to exit the engine.
Back to the compressor to be used again.
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DEC.
CEDU.
FADEC
CEDU and FADEC.
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Pneumatic.
Fuel injection.
Hydromechanical.
Electrohydromechanical.
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Control the oil poppet valve.
Direct oil around the fuel filter.
Control oil exiting from the cooler.
Direct oil around or through the cooler.
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More oil sampling.
More engine removals.
Less unnecessary maintenance.
Less wear metal found in the oil.
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Wobbler control.
Pump and motor unit.
Variable pump wobbler.
Frequency and load controller.
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Ring cowl.
Fan inlet guide vane flaps.
Variable exhaust nozzle flaps.
C-D duct.
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Allows airflow in only one direction.
Bleeds off air before it enters the engine.
Prevents airflow from entering the engine.
Bleeds off air after it has entered the engine.
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Two
Three
Four
Five
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Unified.
Combined
Bimechanical.
Electrosecondary.
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Check.
Relief.
Bypass.
Pressurizing.
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Air pressure
Oil pressure
Spring pressure.
Hydraulic pressure.
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