This quiz from Volume 4 - 2014 2A651S CDC evaluates knowledge on aircraft and engine troubleshooting, focusing on practices, systems, and components like EDU and DCU in the F100-PW-220 engine. It is designed to enhance understanding of aircraft maintenance procedures.
Checking the applicable trouble areas.
Understanding the function of each engine unit.
Inspecting other areas after isolating trouble between points.
Performing easy checks, then going to more difficult checks.
Rate this question:
Fix-it diagrams.
Power plant charts.
Mechanical drawings.
Troubleshooting charts.
Rate this question:
Be a 7-level.
Have at least five years experience.
Complete college courses in troubleshooting techniques.
Understand the function of each unit within each system.
Rate this question:
DCU.
GSU.
EAU.
EDU.
Rate this question:
DCU.
EAU.
Mn test system.
SCS.
Rate this question:
Be small in size.
Use digital readout.
Use analog readout.
Cheap to manufacture.
Rate this question:
If an engine should be removed from an aircraft.
If the engine should be sent to the test cell.
The meaning of the instrument readings.
What tools are required for maintenance.
Rate this question:
Electrical valve to the indicator.
Metal tubing for electron flow.
Radio frequency transmitter.
Transmitter and indicator.
Rate this question:
Combustion inlet.
Fan turbine inlet.
Turbine inlet.
Exhaust gas.
Rate this question:
A resistor.
A turbine inlet.
A control valve.
An exhaust duct.
Rate this question:
Steel and iron.
Steel and alumel.
Iron and chromel.
Alumel and chromel.
Rate this question:
Transmitter and a float valve.
Control valve and a float valve.
Transmitter and a fuel-flow indicator.
Control valve and a fuel-flow transcriber.
Rate this question:
Pounds per hour.
Gallons per hour.
Pounds per minute.
Gallons per minute.
Rate this question:
Gyro
Transmitter.
Hydraulic unit.
Synchronous unit.
Rate this question:
Indicator.
Fuse panel.
Transformer.
Thermocouple.
Rate this question:
Fuel control.
Combustion case.
Engine turbine section.
Engine accessory section.
Rate this question:
Engine speed.
Transformer speed.
Speed of the electrical magnet.
Speed of the alternating magnet.
Rate this question:
Rheostat.
Rectifier.
Transducer.
Transformer.
Rate this question:
One gold contact.
Two silver contacts.
Three bronze contacts.
Four copper contacts.
Rate this question:
Only the TEST switch.
Both TEST and NORMAL switches.
Only the TEST WARNING ON switch.
Both TEST ON and TEST OFF switches.
Rate this question:
EPR.
RPM.
EGT.
TIT.
Rate this question:
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).
Rate this question:
Electrically.
Mechanically.
Hydraulically.
Through tubing.
Rate this question:
Aircraft transformer.
Engine transformer.
Aircraft transmitter.
Engine transmitter.
Rate this question:
The EGT parameter for transit speeds.
The accuracy check switch during adjustment.
Digital or analog readings for the EGT indicator.
Individual thermocouple inputs or an average of these inputs.
Rate this question:
Fuel control.
Flow turbines.
Flow cascades.
Fuel-oil coolers.
Rate this question:
–100 to +1,000 °F.
–75 to +1,400 °F.
–50 to +1,600 °F.
–25 to +1,800 °F.
Rate this question:
Forced.
Transient.
Unbalanced.
Externally excited.
Rate this question:
Forced.
Transient.
Unbalanced.
Externally excited.
Rate this question:
Forced.
Transient.
Resonance.
Externally excited.
Rate this question:
Mils.
Phase lags.
Cycles per second.
Phases per second.
Rate this question:
Velocity.
Phase log.
Displacement accelerometer.
Piezoelectric accelerometer.
Rate this question:
Test cell technical order.
Intermediate maintenance manual.
Organizational maintenance manual.
Methods and procedures maintenance manual.
Rate this question:
A horn alarm.
Flashing red lights.
A buzzer sounding.
A flashing channel indicator LED.
Rate this question:
Bushings.
Brackets.
Bearings.
Bulkheads.
Rate this question:
Engine trim.
Fan rotor trim balance.
Low-pressure turbine rotor trim balance.
High-pressure turbine rotor trim balance.
Rate this question:
The flight-line JG.
AFI 36-2903.
The intermediate maintenance TO.
AFOSH STD 91-100.
Rate this question:
Hydraulic and mechanical.
Hydraulic and electronic.
Manual and mechanical.
Manual and electronic.
Rate this question:
Inlet side of the oil pump and the vent system.
Output side of the main oil pump and the vent system.
Scavenge pump and the inlet side of oil pressure pump.
Bearing jets and the output side of the oil scavenge pump.
Rate this question:
FTIT.
TIT.
EGT.
IGT.
Rate this question:
ON.
OFF.
START.
MANUAL.
Rate this question:
2.
4.
6.
8.
Rate this question:
Prevents aircraft inlet damage.
Prevents engine turbine wheel damage.
Ensures the noise suppressor will be operational for the next aircraft.
Ensures that the noise suppressor is not damaged by improper engine shutdown procedures.
Rate this question:
Air inlet modules.
Observation ports.
Air exhaust modules.
High-grade steel panels.
Rate this question:
Flexible soft metal filled with noise reduction material.
Cylinder-type tubing filled with noise reduction material.
Small panel modules filled with noise reduction material.
Panels and air cooling ports filled with noise reduction material.
Rate this question:
Red streamers.
And its forms.
Flight station.
Forms.
Rate this question:
Tailhook connects to the engine.
Wheel chocks restrain the engine.
The thrust stand slides into position on tracks.
Engines can be run while on the ALC 3000 trailer.
Rate this question:
Engine being tested.
Concrete deterioration.
Fire suppression system.
Engine tie-down assemblies.
Rate this question:
Quiz Review Timeline (Updated): Mar 21, 2023 +
Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.
Wait!
Here's an interesting quiz for you.