This quiz assesses skills in aircraft engine troubleshooting, focusing on practical scenarios and technical order guidance. It targets understanding gauge indications, prioritizing repairs, and utilizing engine monitoring systems. Essential for learners aiming to excel in aircraft maintenance.
Individuals assigned
Civil engineer squadron
Equipment maintenance squadron
Aerospace ground equipment (AGE) flight
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Troubleshooting charts.
Mechanical drawings
Power plant charts
Fix-it diagrams
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Go back and check engine forms again
Replace all if 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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Engine start system (ESS)
Engine monitoring system (EMS)
Supervisory control system (SCS)
Supervisory monitoring system (SMS)
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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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Resistor
Turbine inlet
Control valve
Exhaust duct
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Velocity
Phase log
Displacement accelorometer
Piezolectric accelorometer
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At an unnoticeable level
Directly into the inlet, within +/- 45 degrees
At a 90 degree angle to the engine exhaust
Directly into the exhaust, within +/- 45 degrees
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Trips and engine no-go flag
Turns on cokcpit lights to warn the pilot
Trips and engine monitoring unit (EMS) maintenance flag
Accommodates the fault and sends the fault code to the engine diagnostic unit (EDU)
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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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Special
Calender
Acceptance
Time replacement item
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Data collection unit (DCU)
Engine analyzer unit (EAU)
Match number (Mn) test system
Supervisory control system (SCS)
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Electrical valve to the indicator
Metal tubing for electron flow
Radio frequency transmitter
Transmitter and indicator
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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 die to shutdown
Eliminate items that could cause inaccurate readings
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Examine most complex unit.
Observe guage indications.
Check each part of every system
Discuss problem with other journeyman in the shop.
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If an engine should be removed from an aircraft
If the engine should be sent to test cell
The meanings of the intrument readings
What tools are required for maintenance
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1.000 inch
0.100 inch
0.010 inch
0.001 inch
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Bushings
Brackets
Bearings
Blades
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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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Ingestion of bolts
Formation of ice
Ingestion of rocks
Failure of internal parts
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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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Transient vibration
Partial loss of lubrication
Complete loss of lubrication
Stall condition over temperature
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Small in size
Analog readout
Digital readout
Cheap to manufacture
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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 damage
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By cargo straps
From a cradle mount
By a tailhook adapter
On a model 4100 trailer
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Fuel control
Turbine area
Inlet to the oil pump
Inlet to the fuel pump
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Start up
Starter motoring
During engine coast down
During fuel-flow indication
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Test cell run procedures
Unit serial number listings
Periodic inspection checklists
Monthly requirements listings
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Periodic
Preflight
Thruflight
End of runway
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Gyro
Transmitter
Hydraulic unit
Synchronous unit
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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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Engine oil
Atmosphere
Hydraulic fluid
Pneumatic system
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Steel and iron
Steel and alumel
Iron and chromel
Alumel and chromel
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Rheostat
Recitifier
Transducer
Transformer
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Daily
Hourly
Weekly
Monthly
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Restricted air inlet
Rapid throttle movement
A restricted turbine nozzle
Malfuctioning variable geometry system
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Provide an exact 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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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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Exhaust gas
Turbine inlet
Combustion inlet
Fan turbine inlet
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Relief valve and indicator
Transmitter and indicator
Relief valve and transmitter
Synchronous unit and indicator
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Engine speed
Transformer speed
Speed of the electrical magnet
Speed of the alternating magnet
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1 rpm
2 rpm
3 rpm
4 rpm
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-100 to +1,000
-75 to +1,400
-50 to +1,600
-25 to +1,800
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Mils
Phase lags
Cycles per second
Phases per second
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