2a353: Fighter Aircraft Maintenance Journeyman

153 Questions | Total Attempts: 449

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Aircraft Maintenance Quizzes & Trivia

In the air force the aircrafts need to be in top shape in case they are called to action, this is ensured by aircraft maintenance personnel. Are you on the road to becoming a fighter aircraft maintenance journeyman and are looking for revision material? Look no further as the quiz is designed for that purpose. Give it a try.


Questions and Answers
  • 1. 
    The number of positions on the function switch of the AN/PSM-37 multimeter is....
    • A. 

      2

    • B. 

      3

    • C. 

      5

    • D. 

      7

  • 2. 
    To measure current flow, you connect an AN/PSM-37 multimeter in....
    • A. 

      Series in the circuit

    • B. 

      Parallel in the circuit

    • C. 

      Series with the component

    • D. 

      Parallel with the component

  • 3. 
    The symbol entered on the forms if an aircrft exceeds the PDM cycle by 90 days and an extension is not granted is a.....
    • A. 

      Red x

    • B. 

      Red dash

    • C. 

      Red diagonal

    • D. 

      Black signature

  • 4. 
    The AF IMT 2691 is used to .....
    • A. 

      Serve as a receipt document

    • B. 

      Serve as a shipping document

    • C. 

      Transfer aircraft -21 equipment

    • D. 

      Account for aircraft -21 equipment

  • 5. 
    On the F-15 aircraft, what is the useable pressure range for the LOX system?
    • A. 

      35-70 psi

    • B. 

      55-90 psi

    • C. 

      75-100 psi

    • D. 

      95-120 psi

  • 6. 
    On the F-15 aircraft, what component contains the logic circuits for the overheat/fire detection system?
    • A. 

      BIT panel

    • B. 

      Flashing relay

    • C. 

      Control panel

    • D. 

      Controllers

  • 7. 
    The F-100 engine gearbox module is attached to the.....
    • A. 

      Compressor intermediate case

    • B. 

      Fan inlet case assembly

    • C. 

      Rear turbine case

    • D. 

      N1 section

  • 8. 
    The function of the F-100 Electronic Engine Control (EEC) is to....
    • A. 

      Provide histroy data storage

    • B. 

      Trim the convergent exhaust nozzle

    • C. 

      Send signals to the cockpit indicators

    • D. 

      Supervise the trim of the UFC and CIVV

  • 9. 
    The F-100 engine exhaust nozzle position transmitter is driven by......
    • A. 

      The convergent exhaust nozzle control

    • B. 

      115-VAC power

    • C. 

      26-VAC power

    • D. 

      An air motor

  • 10. 
    How many air/oil coolers are there on the -229 engine?
    • A. 

      3

    • B. 

      4

    • C. 

      9

    • D. 

      NONE

  • 11. 
    On the F-15, the Mach blocking solenoid locks the diffuser ramp in the DOWN position by.....
    • A. 

      Energizing the shutoff valve

    • B. 

      Closing the rate limiter valve

    • C. 

      Opening the rate limiter valve

    • D. 

      Deenergizing the shutoff valve

  • 12. 
    On the F-15, which JFS fuel filter component acts like a jet pump?
    • A. 

      Bypass valve

    • B. 

      Fuel accumulator

    • C. 

      Fuel shutoff valve

    • D. 

      Fluid-flow restrictor

  • 13. 
    On the F-15, what airframe mounted accessory drive switch is commonly called the 50% switch?
    • A. 

      Two-speed switch assembly

    • B. 

      Oil pump and start cut-out

    • C. 

      Power turbine overspeed

    • D. 

      Right decoupler position

  • 14. 
    On the F-15 aircraft, the airframe mounted accessory drive component that takes the input from the pawl carrier assembly and transmits the rotational force to the power takeoff drive shaft for engine starting is the......
    • A. 

      Layshaft

    • B. 

      Face gear

    • C. 

      Gear trian

    • D. 

      Pinion gear

  • 15. 
    On the F-15, the JFS start handle input is transmitted to the JFS start control manifold by......
    • A. 

      A torque link

    • B. 

      A cable assembly

    • C. 

      A hydraulic signal

    • D. 

      An electrical signal

  • 16. 
    The light for a borescope is transmitted by the......
    • A. 

      Lens

    • B. 

      Probe

    • C. 

      View finder

    • D. 

      Fiber optic cables

  • 17. 
    On the ignition test set, what monitors the output of energy?
    • A. 

      Stored energy meter

    • B. 

      Potentiometer

    • C. 

      Toggle switch

    • D. 

      Rotary meter

  • 18. 
    What supplies power to the engin ignition system durning an ignition test?
    • A. 

      Electronic scaler

    • B. 

      Ligh-off detector

    • C. 

      Electronic trasmitter

    • D. 

      Alternator simulator output

  • 19. 
    On the F-15, at what pressure differential does the utility thermal control valve allow fluid to bypass the heat exhanger?
    • A. 

      32.5 psid

    • B. 

      42.5 psid

    • C. 

      52.5 psid

    • D. 

      62.5 psid

  • 20. 
    When a hydraulic leak occurs in the utility system on an F-15 aircraft, how does circuit A shut off?
    • A. 

      Pneumatically

    • B. 

      Hydraulically

    • C. 

      Mechanically

    • D. 

      Electrically

  • 21. 
    On the F-15, what holds the aileron switching valve in the primary position?
    • A. 

      Normal PC system pressure

    • B. 

      Normal utility system pressure

    • C. 

      Backup utility system pressure

    • D. 

      Backup PC system pressure

  • 22. 
    On the F-15 aircraft, how long does utility system non-reservoir level-sensing maintain pressure if the aircraft develops a leak in the utility hydraulic system?
    • A. 

      Until the circuit A and B shutoff valves open.

    • B. 

      Until the circuit A and B shutoff valves close

    • C. 

      As long as there is hydraulic fluid left in the utility reservoir

    • D. 

      As long as there is hydraulic fluid left in the power control backup system

  • 23. 
    On the F-15, what hydraulic indication component uses a Bourdon tube? 
    • A. 

      Pressure transmitter

    • B. 

      Pump pressure switch

    • C. 

      Over-temperature indicator

    • D. 

      Temperature volume indicator

  • 24. 
    On the F-15, how many over-temperature indicators are there in the hydraulic system?
    • A. 

      One per PC reseroir and two for the utility reservoir

    • B. 

      Two per PC reservoir and one for the utility reservoir

    • C. 

      Two per reservoir

    • D. 

      One per reservoir

  • 25. 
    On the F-15, the control stick consists of a stick grip and.......
    • A. 

      Control system damper

    • B. 

      Force transducer

    • C. 

      Ratio changer

    • D. 

      Torque tube

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