2a352h Volume 2 Ure's

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2a352h Volume 2 Ure

2a352h volume 2 ure's 


Questions and Answers
  • 1. 
    What  is supercruise? 
    • A. 

      Flight above 60,000 ft

    • B. 

      Supersonic flight over mach 2.0

    • C. 

      Supersonic flight above 60,000 ft

    • D. 

      Supersonic flight without afterburners

  • 2. 
    On the F-22 aircraft, fuselage station zero (FS 0.0) is located 
    • A. 

      At the aft end of the integrated forebody

    • B. 

      5.0 inches aft of the integrated forebody

    • C. 

      169.77 inches forward of the integrated forebody

    • D. 

      5.0 inches forward of the forward end of the integrated forebody

  • 3. 
    The starting point for the buttock line is BL 0.0, what does this represent? 
    • A. 

      The aircraft's parallel plane

    • B. 

      The aircraft's horizontal plane

    • C. 

      The aircraft's vertical centerline

    • D. 

      The aircraft's horizontal centerline

  • 4. 
    What is the primary reference in determining panel and door numbers? 
    • A. 

      System number

    • B. 

      Fuselage station number

    • C. 

      Structural zones and areas

    • D. 

      Left or right side of aircraft

  • 5. 
    How far can the F-22 main weapons bay doors be opened for weapons loading? 
    • A. 

      90 degrees

    • B. 

      105 degrees

    • C. 

      110 degrees

    • D. 

      125 degrees

  • 6. 
     How can the electronic warfare/infrared counter measures (EW/IRCM) doors be opened for ground maintenance?
    • A. 

      By the portable maintenance aid or from the cockpit

    • B. 

      By using the maintainer vehicle interface panel or from the cockpit

    • C. 

      By the portabe maintenance aid or using the maintainer vehicle interface panel

    • D. 

      From the portabe maintenance aid only

  • 7. 
    Form in place sealed panels must be opened with what type of tools? 
    • A. 

      Ceramic

    • B. 

      Nonmetallic

    • C. 

      Plastic

    • D. 

      Tungsten

  • 8. 
     How many external weapons stations does the F-22 have?
    • A. 

      4

    • B. 

      6

    • C. 

      8

    • D. 

      10

  • 9. 
    What structures comprise the fuselage section? 
    • A. 

      Engine air inlet, rudder, vertical stabilizers, and wings

    • B. 

      Forward fuselage, center fuselage, aft fuselage, and wings

    • C. 

      Forward fuselage, rudder, engine inlet ducts, and aft fuselage

    • D. 

      Forward fuselage, engine inlet ducts, center fuselage, and aft fuselage

  • 10. 
    The ailerons for the F-22 are located on the 
    • A. 

      Wing assembly

    • B. 

      Empennage group

    • C. 

      Fuselage assembly

    • D. 

      Horizontal stabilizers

  • 11. 
     The F-22 cockpit is the first baseline (by design) cockpit compatible with
    • A. 

      Infrared binoculars

    • B. 

      A JHMCS

    • C. 

      Night vision goggles

    • D. 

      An infrared detecting pilot helmet

  • 12. 
    On the F-22, the AUX COMM panel is located 
    • A. 

      On the left console

    • B. 

      On the right console

    • C. 

      On the throttle grip

    • D. 

      Between the pilot's legs

  • 13. 
    To operate, the ECS uses 
    • A. 

      Ram air, bleed air, and electrical power

    • B. 

      Ram air, bleed air, and compressed air

    • C. 

      Ram air, compressed air, and electrical power

    • D. 

      Bleed air, compressed air, and electrical power

  • 14. 
     Which function (subsystem) of the fire protection system monitos the high prssure bleed air ducts that contain air over 500 degrees F?
    • A. 

      Thermal overheat

    • B. 

      Optical fire detection

    • C. 

      Fire protection modules

    • D. 

      Fire extinguishing agent

  • 15. 
    What is the primary fuel grade used on the F-22? 
    • A. 

      JP-4

    • B. 

      JP-5

    • C. 

      JP-8

    • D. 

      Jet A

  • 16. 
    Both hydraulic systems on the F-22 utilize two variable delivery pumps that operate at 
    • A. 

      27 gpm

    • B. 

      40 gpm

    • C. 

      55 gpm

    • D. 

      72 gpm

  • 17. 
     Emergency in-flight hydraulic power is provided by a variable delivery auzitiary pump at a rate of
    • A. 

      27 gpm

    • B. 

      40 gpm

    • C. 

      55 gpm

    • D. 

      72 gpm

  • 18. 
     The F-22 main aircraft brake system receives hydraulic pressure from
    • A. 

      System 1 only

    • B. 

      System 2 only

    • C. 

      Both system 1 and 2

    • D. 

      A dedicated hydraulic circuit

  • 19. 
    Each of the F-22 global inertian navigation system (GNIS) units contains 
    • A. 

      2 RLG, 2 accelerometers and 1 GPS receiver

    • B. 

      2 RLG, 2 accelerometers and 2 GPS receivers

    • C. 

      3 RLG, 3 accelerometers and 1 GPS receiver

    • D. 

      3 RLG, 3 accelerometers and 2 GPS receivers

  • 20. 
     The F-22 flight control system is part of what larger aircraft system for data management and integration?
    • A. 

      Guidance and propulsion system

    • B. 

      Vehicle management system (VMS)

    • C. 

      Global inertial navigation system (GINS)

    • D. 

      Integrated vehicle system controller (IVSC)

  • 21. 
    The F-22 radar provides multimode air-to-air search and track fuctions in all of the following degrading environments except
    • A. 

      Weather

    • B. 

      Traffic

    • C. 

      Clutter

    • D. 

      Electronic counter-countermeasures

  • 22. 
    When should you verify the aircraft safe for maintenance task be performed on the F-22 aircraft?
    • A. 

      Shortly after the aircraft lands

    • B. 

      Prior to performing any maintenace

    • C. 

      Upon completion of the first flight only

    • D. 

      Only when you're directed to by the ranking technician on the job

  • 23. 
     What are you verifying when you ensure the F-22 aircraft exterior is safe for maintenance?
    • A. 

      That the crew chief did his/her job

    • B. 

      That it's okay to apply electrical power

    • C. 

      That avionic systems are safe for maintenance

    • D. 

      Basically, that all applicable safety/lockpins are installed

  • 24. 
    If you find the F-22 ejection seat sequencer is red, how long should you wait before performing maintenance  on the aircraft?
    • A. 

      1 hour

    • B. 

      2 hours

    • C. 

      4 hours

    • D. 

      8 hours

  • 25. 
     What area around the intake of an operating jet engine must be avoided?
    • A. 

      15 ft away from the intake

    • B. 

      25 ft away from the intake

    • C. 

      35 ft away from the intake

    • D. 

      45 ft away from the intake

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