This quiz, titled '2a651 edition2 volume 5', assesses skills in aircraft engine troubleshooting. It focuses on practical scenarios like observing gauge indications, prioritizing unit repairs, and using troubleshooting charts, aiming to enhance expertise in understanding aircraft systems.
If an engine should be removed from an aircraft.
If the engine should be sent to the test cell.
The meanings of the instrument readings.
What tools are required for maintenance.
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Transmitter and a float valve.
Control valve and a float valve.
Transmitter and a fuel-flow indicator.
Control valve and a fuel-flow transcriber.
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Eliminate items that could possibly cause foreign object damage (FOD).
Assure that the instrumentation is working properly.
Prevent wasted maintenance hours due to shutdown.
Eliminate items that could cause inaccurate readings.
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Individuals assigned.
Civil engineer squadron.
Equipment maintenance squadron.
Aerospace ground equipment (AGE) flight.
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Be a 7-level.
Have at least 5 years experience.
Attend college courses in troubleshooting techniques.
Understand the function of each unit within each system.
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Electrical valve to the indicator.
Metal tubing for electron flow.
Radio frequency transmitter.
Transmitter and indicator.
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Resistor.
Turbine inlet.
Control valve
Exhaust duct.
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Only the TEST switch
Both TEST and NORMAL switches
Only the TEST WARNING ON switch.
Both TEST ON and TEST OFF switches.
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Type these items.
Check past records.
Enter these only after test is complete.
Verify these numbers on the engine data plate.
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A restricted air inlet.
Rapid throttle movement.
A restricted turbine nozzle.
Malfunctioning variable geometry system.
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Examine most complex unit.
Observe gauge indications.
Check each part of every system.
Discuss problem with other journeymen in the shop.
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Go back and check engine forms again.
Replace all the units suspected to be at fault.
Try to repair the more complex unit on the spot.
Examine the unit that requires the least amount of time to replace.
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Small in size.
Analog readout
Digital readout.
Cheap to manufacture.
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Steel and iron.
Steel and alumel.
Iron and chromel.
Alumel and chromel.
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Indicator
Fuse panel.
Transformer.
Thermocouple.
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Provide an exact revolutions per minute (rpm) indication.
Indicate the amplitude of the overall vibration.
Display the frequency of the overall engine.
Allow selection of the necessary filter.
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Test cell oil formulas.
Base engine manager’s office.
Applicable engine publications.
Periodic checklist for the engine.
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Troubleshooting charts.
Mechanical drawings.
Power plant charts.
Fix-it diagrams.
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Engine start system (ESS).
Engine monitoring system (EMS).
Supervisory control system (SCS).
Supervisory monitoring system (SMS).
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Velocity.
Phase log.
Displacement accelerometer.
Piezoelectric accelerometer.
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Near the bleed area.
To the rear exhaust area.
Against the aircraft fuselage.
Forward of the bleed exhaust area.
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Tailhook connects to the engine.
Wheel chocks restrain the engine.
The thrust stand slides into position on tracks.
Engines are run while on the ALC 3000 trailer.
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Ingestion of bolts.
Formation of ice.
Ingestion of rocks.
Failure of internal parts.
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Start-up.
Starter motoring.
During engine coast down.
During fuel-flow indication.
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Daily
Hourly
Weekly
Monthly
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Periodic.
Preflight.
Thruflight.
End-of-runway.
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Forced.
Transient.
Resonance.
Externally excited.
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A horn alarm.
Flashing red lights.
The sound of a buzzer.
Flashing channel indicator light emitting diode (LED).
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At an unnoticeable level
Directly into the inlet, within 45.
At a 90ï‚° angle to the engine exhaust.
Directly into the exhaust, within 45.
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Fuel control.
Turbine area.
Inlet to the oil pump.
Inlet to the fuel pump.
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Engine speed.
Transformer speed.
Speed of the electrical magnet.
Speed of the alternating magnet.
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Transient vibration
Partial loss of lubrication.
Complete loss of lubrication.
Stall condition over temperature.
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Data collection unit (DCU).
Engine analyzer unit (EAU).
Mach number (Mn) test system.
Supervisory control system (SCS).
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Interface operational.
Bleed schedule.
Dry motoring.
Wet motoring
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Fixed.
Portable.
Both fixed and portable.
None.
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Nicks.
Dents
Blends.
Scratches.
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Total (t) pressure (P) at flange 2 (2).
Total (t) pressure (P) at station 2 (2).
Temperature (t) and pressure (P) at flange 2 (2).
Temperature (t) and pressure (P) at station 2 (2).
For training practice.
In aircraft that have been washed.
That have been involved in an incident or a mishap.
That have severe foreign object damage (FOD) damage.
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By cargo straps.
From a cradle mount
By a tailhook adapter.
On the model 4100 trailer.
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A damaged aft bearing oil seal.
An underserviced oil system.
Leaking external oil lines.
A loose aft roller bearing.
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Ignition exciter.
Oil pressure pump.
Thrust reverser pump.
Variable stator vanes.
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Exhaust gas.
Turbine inlet.
Combustion inlet.
Fan turbine inlet.
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A mechanical magnetic-drag-type instrument.
An electric magnetic-drag-type instrument.
A mechanical direct-drive-type instrument.
An electric direct-drive type instrument.
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Bushings.
Brackets.
Bearings.
Blades.
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Red streamers.
And its forms.
Flight station.
Forms.
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Control cab
Thrust trailer
Miscellaneous equipment kit.
Hydraulically operated pylon mount cradle.
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Test cell run procedures.
Unit serial number listings.
Periodic inspection checklists.
Monthly requirements listings.
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Gyro
Transmitter.
Hydraulic unit.
Synchronous unit.
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Quiz Review Timeline (Updated): Dec 14, 2023 +
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