Aircraft Power Plant And Engine Quiz
- 1.After reviewing the aircraft/engine forms, where should you begin troubleshooting?
- A.
Discuss problem with other journeymen in the shop
- B.
Check each part of every system.
- C.
Examine the most complex unit.
- D.
Observe gauge indications.
- 2.All of the options listed below are proper troubleshooting practices except...
- A.
Checking the applicable trouble areas
- B.
Understanding the function of each engine unit
- C.
Performing easy checks, then going to more difficult checks
- D.
Inspecting other areas after isolating the trouble between points
- 3.Aircraft power plant and engine intermediate technical orders (TO) contain information on troubleshooting. This information is presented in the form of
- A.
Fix-it diagrams
- B.
Power plant charts
- C.
Mechanical drawings
- D.
Troubleshooting charts
- 4.To become an expert troubleshooter, you must
- A.
Be a 7-level
- B.
Have at least 5 years experience
- C.
Attend college courses in troubleshooting techniques
- D.
Understand the function of each unit within each system
- 5.The F100-PW-220 engine monitoring system component that acquires faultdata from the digital electronic engine control (DEEC) and logs the faults with the time of their occurrence is the
- A.
Data collection unit (DCU)
- B.
Ground station unit (GSU)
- C.
Engine analyzer unit (EAU)
- D.
Engine diagnostic unit (EDU)
- 6.An understanding of trhe operating principles of engine instruments will help you decide
- A.
If an engine should be removed from an air craft
- B.
If the engine should be sent to test cell
- C.
The meanings of instrument readings
- D.
What tools are required for maintenance
- 7.Most engine monitering gauges and instruments require some type of
- A.
Electrical valve to the indicator
- B.
Metal tubing for electron flow
- C.
Radio frequency transmitter
- D.
Transmitter and indicator
- 8.Which jet engine temperature is not measured?
- A.
Exhaust gas
- B.
Turbine inlet
- C.
Combustion inlet
- D.
Fan turbine inlet
- 9.A typical jet exhaust gas temperature (EGT) indicating system contains thermocouples, leads, an indicator, and
- A.
A resistor
- B.
A turbine inlet
- C.
A control valve
- D.
An exhaust duct
- 10.The engine fuel-flow indicating system of most jet powered aircraft contains a fuel-flow
- A.
Transmitter and float valve
- B.
Control valve and a float valve
- C.
Transmitter and a fuel flow indicator
- D.
Control valve and a fuel flow indicator
- 11.The fuel system component of a jet engine that operates by using a water wheel concept is the
- A.
Fuel-flow transmitter
- B.
Fuel-flow indicator
- C.
Fuel-flow transmitter
- D.
Fuel remaining counter
- 12.The fue-flow indicator indicates the rate of fuel flow as
- A.
Pounds per hour
- B.
Gallons per hour
- C.
Pounds per minute
- D.
Gallons per second
- 13.Two units that work together to indicate that the oil system is operating correctly are the oil pressure
- A.
Transmitter and indicator
- B.
Relief valve and indicator
- C.
Relief valve and transmitter
- D.
Synchronous unit and indicator
- 14.The oil pressure indicator recieves an electrical signal from the
- A.
Gyro
- B.
Transmitter
- C.
Hydraulic unit
- D.
Synchronous unit
- 15.The two primary units of the tachometer indicating system are the tachometer generator and tachometer
- A.
Indicator
- B.
Fuse panel
- C.
Transformer
- D.
Thermocouple
- 16.The N2 tachometer generator is usually driven from the tachometer drive located on the
- A.
Engine accessory section
- B.
Engine turbine section
- C.
Combustion case
- D.
Fuel control
- 17.The tachometer indicator is
- A.
An electric direct-drive type instrument
- B.
An electric-magnetic-drag-type instrument
- C.
A mechanical direct-drive-type instrument
- D.
A mechanical-magnetic-drag-type instrument
- 18.The exhaust nozzle position indicating system found on engines with afterburners is important because it
- A.
Helps the pilot determine engine power
- B.
Helps the pilot determine fuel consumption
- C.
Gives the pilot indications of electrical failures
- D.
Aids the pilot in selection of proper altitude levels
- 19.On engines with afterburners, the possition of the exhaust nozzle is converted into an electrical signal by a
- A.
Rheostat
- B.
Rectifier
- C.
Transducer
- D.
Transformer
- 20.One type of overheat detector unit used on aircraft engines consists of a hollow stainless steel tube that covers
- A.
One gold contact
- B.
Two silver contacts
- C.
Three bronze contacts
- D.
Four copper contacts
Related Topics
Recent Quizzes
Featured Quizzes
Popular Topics
Back to top