2a352 H F-16 Avionics

11 Questions | Total Attempts: 74

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Avionics Quizzes & Trivia

URE QUIZ FOR FIRST SET OF 2A352 CDC'S


Questions and Answers
  • 1. 
    1. (001) On the F–16 aircraft, fuselage station zero (FS 0.0) is located
    • A. 

      AT THE AFT END OF THE NOSE RADOME

    • B. 

      AT THE FORWARD END OF THE NOSE RADOME

    • C. 

      5.0 INCHES AFT OF THE FORWARD END OF THE NOSE RADOME

    • D. 

      5.0 INCHES FORWARD OF THE FORWARD END OF THE NOSE RADOME

  • 2. 
    2. (001) On the F-16 aircraft, waterline 65.0 (WL 65.0) is ocated 65.0 inches in which direction from waterline 0.0?
    • A. 

      AFT

    • B. 

      ABOVE

    • C. 

      BELOW

    • D. 

      FORWARD

  • 3. 
    3. (001) When should worn door/panel fasteners be replaced?
    • A. 

      IMMEDIATELY

    • B. 

      BEFORE THE AIRCRAFT TAXIS

    • C. 

      WHEN SHEET METAL SHOP SEES FIT

    • D. 

      THE NEXT TIME YOU PERFORM MAINTENANCE UNDER THAT DOOR/PANEL

  • 4. 
    4. (001) Which of the following structures is not part of the empennage group?
    • A. 

      WINGS

    • B. 

      RUDDER

    • C. 

      VENTRAL FINS

    • D. 

      HORIZONTAL STABILIZERS

  • 5. 
    5. (001) The leading edge flaps for the F-16 are located on the
    • A. 

      WING ASSEMBLY

    • B. 

      EMPENNAGE GROUP

    • C. 

      FUSELAGE ASSEMBLY

    • D. 

      HORIZONTAL STABILIZERS

  • 6. 
    6. (002) On the F-16 installing the emergency power unit (EPU) safety pin will
    • A. 

      Not prevent the firing of the EPU in flight

    • B. 

      Prevent the accidental firing of the EPU only in flight

    • C. 

      Not prevent the firing of the EPUif the external source shuts down

    • D. 

      Prevent the accidental firing of the EPU during ground maintenance

  • 7. 
    7. (002) To operate the aircraft primary flight controls, the F–16 hydraulic systems provide hydraulic pressure at approximately
    • A. 

      1,100 psi

    • B. 

      2,100 psi

    • C. 

      3,100 psi

    • D. 

      4,100 psi

  • 8. 
    8. (002) At aircraft altitudes between 8,000 feet and 23,000 feet, the F–16 cabin pressure is regulated to
    • A. 

      The 8,000 foot air pressure

    • B. 

      The 23,000 foot air pressure

    • C. 

      Ambient (outside) air pressure

    • D. 

      5 psi above ambient (outside) air pressure

  • 9. 
    9. (002) The digital flight control system uses what means to transfer inputs to the control surfaces?
    • A. 

      Control cables

    • B. 

      Full fly-by-wire

    • C. 

      Mechanical linkage

    • D. 

      A combination of control cables and electrical wire

  • 10. 
    10. (002) Artificial feel in the digital flight control system is provided by beams and coil springs
    • A. 

      Internal to the handgrip assembly

    • B. 

      Internal to the transducer assembly

    • C. 

      External to the handgrip assembly

    • D. 

      External to the transducer assembly

  • 11. 
    11. (002) In addition to rudder control, the rudder pedals are also used to generate
    • A. 

      Brake command signals only

    • B. 

      Nosewheel steering signals only

    • C. 

      Brake command and nosewheel steering signals

    • D. 

      Anti-skid command and nosewheel steering signals

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