2a353 Volume 2 Aircraft

89 Questions | Total Attempts: 340

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Aircraft Quizzes & Trivia

Questions and Answers
  • 1. 
    On the F-15 aircraft, what is the usable pressure rage for the LOX system?
    • A. 

      35-70 psi

    • B. 

      55-90 psi

    • C. 

      75-100 psi

    • D. 

      95-120 psi

  • 2. 
    On the F-15 aircraft, what can the maintainer or aircrew use to check the oxygen indication system?
    • A. 

      Oxygen test switch

    • B. 

      Oxygen quantity switch

    • C. 

      Oxygen pressure test switch

    • D. 

      Oxygen regulator test switch

  • 3. 
    On the F-15 aircraft, the product gas in the MSOGS that does not go to the console-mounted regulators
    • A. 

      Returns to the molecular sieve beds for processing

    • B. 

      Ports to the regenerative heat exchanger

    • C. 

      Stores in the backup oxygen supply

    • D. 

      Dumps overboard

  • 4. 
    How does the windshield anti-ice valve operate on the F-15 aircraft?
    • A. 

      Manually

    • B. 

      Electrically

    • C. 

      Hydraulically

    • D. 

      Pneumatically

  • 5. 
    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

  • 6. 
    On the F-15 aircraft, what part of the AB burn-through system does the BIT control panel test?
    • A. 

      Responders

    • B. 

      Switches

    • C. 

      Sensors

    • D. 

      None

  • 7. 
    On the F-100 engine, what is the benefit of the modular construction concept?
    • A. 

      Prevents engine vibration

    • B. 

      Modular construction decreases the weight of the engine

    • C. 

      Allows depot maintenance to ship each module separately

    • D. 

      Allows for removal and replacement of sections of the engine that are bad

  • 8. 
    On the F-15 aircraft, aircraft intake air is prevented from getting into the engine bay area by
    • A. 

      A bellmouth seal

    • B. 

      A peripheral seal

    • C. 

      The primary ram air inlet duct

    • D. 

      The secondary ram air inlet duct

  • 9. 
    On the F-100 engine, the tips of the FTIT sensors protude into the
    • A. 

      1st-stage nozzle guide vanes

    • B. 

      2nd-stage nozzle guide vanes

    • C. 

      3rd-stage nozzle guide vanes

    • D. 

      4th-stage nozzle guide vanes

  • 10. 
    The function of the F-100 electronic engine control is to
    • A. 

      Provide history data storage

    • B. 

      Trim the convergent exhaust nozzle

    • C. 

      Send signals to the cockpit indicators

    • D. 

      Supervise the trim of the UFC and CIVV

  • 11. 
    If the outputs from the F-100 electronic engine control deenergize, the engine is trimmed by the
    • A. 

      MFC

    • B. 

      UFC

    • C. 

      EDU

    • D. 

      Electrohydraulic servo valve

  • 12. 
    On the F-100 engine, what reduces the fuel flow during engine start
    • A. 

      MFC

    • B. 

      Fuel flow transmitters

    • C. 

      Fuel derichment valve

    • D. 

      Fuel depressurizing and dump valve

  • 13. 
    The F-100 engine exhaust nozzle postion transmitter is driven by
    • A. 

      The convergent exhaust nozzle control

    • B. 

      115-VAC power

    • C. 

      26-VAC power

    • D. 

      An air motor

  • 14. 
    How many air/oil coolers are there on the -229 engine?
    • A. 

      Three

    • B. 

      Four

    • C. 

      Nine

    • D. 

      None

  • 15. 
    When taking a JOAP sample, how much oil should be drained into a container proir ro filling the sample bottle?
    • A. 

      None

    • B. 

      One pint

    • C. 

      Enough to fill the bottle

    • D. 

      Enough to wash out any sediment trapped in the drain valve

  • 16. 
    On the F-15 aircraft, which ramp is the last ramp in the air inductin system?
    • A. 

      Diffuser

    • B. 

      Third

    • C. 

      Second

    • D. 

      First

  • 17. 
    On the F-15 aircraft, what does the air induction system use to get rid of the friction air riding on the surface of the ramps?
    • A. 

      Oblique shock waves

    • B. 

      Normal shock waves

    • C. 

      Bleed air holes

    • D. 

      Bypass door

  • 18. 
    On the F-15 aircraft, what is the air that retards along the surface of the aircraft while the aircraft is in flight called?
    • A. 

      Mach tuck air

    • B. 

      Boundary layer air

    • C. 

      Normal shock wave

    • D. 

      Oblique shock wave

  • 19. 
    On the F-15 aircraft, what type of shock wave begins to form at transsonic airspeed?
    • A. 

      Induced

    • B. 

      Oblique

    • C. 

      Parasite

    • D. 

      Normal

  • 20. 
    On the F-15 aircraft, 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

  • 21. 
    On the F-15 aircraft, which JFS fuel filter component acts like a jet pump?
    • A. 

      Bypass valve

    • B. 

      Fuel accumulator

    • C. 

      Fuel shutoff valve

    • D. 

      Fluid-flow restrictor

  • 22. 
    On the F-15 aircraft, the purpose of the central gearbox right decoupler position switch is to
    • A. 

      Allow limited-duty-mode operation

    • B. 

      Prevent limited-duty-mode operation

    • C. 

      Sense the position of the clutch control valve

    • D. 

      Prevent both decouplers from extending at the same time

  • 23. 
    On the F-15 aircraft, what airframe-mounted accessory drive switch is commonly called the 50 percent switch?
    • A. 

      Two-speed switch assembly

    • B. 

      Oil pump and starter cutout

    • C. 

      Power turbine overspeed

    • D. 

      Right decoupler position

  • 24. 
    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 train

    • D. 

      Pinion gear

  • 25. 
    On the F-15 aircraft, the F-100 engine start cycle begins in the
    • A. 

      Cockpit

    • B. 

      Start manifold

    • C. 

      Hydraulic components

    • D. 

      Fuel and ignition components

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