Beech 1900-prop

16 Questions | Total Attempts: 303

Settings
Please wait...
Aircraft Quizzes & Trivia

Questions and Answers
  • 1. 
    The flight Idle prop blade angle is____degrees
    • A. 

      -3

    • B. 

      13

    • C. 

      7

    • D. 

      0

  • 2. 
    • A. 

      The hydraulic overspeed would limit the prop to 1768rpm

    • B. 

      The prop will feather

    • C. 

      The fuel-topping governor will limit the prop to 106% of selected rpm

    • D. 

      The prop will stay on speed and in sync

  • 3. 
    During the takeoff roll the left primary governor fails:
    • A. 

      The left prop will govern at 1768 rpm

    • B. 

      The left prop will govern at 96% of selected rpm

    • C. 

      The left prop will feather

    • D. 

      The prop will move to idle position

  • 4. 
    The normal operating range of the BE1900 propeller is:
    • A. 

      1400-1700rpm

    • B. 

      1550-1700rpm

    • C. 

      1200-1700rpm

    • D. 

      900-1700rpm

  • 5. 
    Which of the following is a true statement?
    • A. 

      The position of the pitch stop is controlled in the cockpit by the prop lever

    • B. 

      To enter the Beta range, the prop lever must be in the full forward position

    • C. 

      Both ground and flight low pitch stops are set by the beta valve

    • D. 

      Is is advisable to place the power levers in the reverse position while the props are feathered

  • 6. 
    The fuel topping governor is set to what % of the primary governor when the power levers are in reverse
    • A. 

      104

    • B. 

      106

    • C. 

      96

    • D. 

      94

  • 7. 
    The prop sync system uses the left engine as the master
    • A. 

      True

    • B. 

      False

  • 8. 
    For which type of landing should the propellers be in the forward position
    • A. 

      Full stop landings

    • B. 

      Maximum reverse thrust landings

    • C. 

      Short field landings

    • D. 

      All of the above are correct

  • 9. 
    The propellers should not be in reverse below:
    • A. 

      40 knots

    • B. 

      50 knots

    • C. 

      60 knots

    • D. 

      70 knots

  • 10. 
    For testing, the hydraulic overspeed governor should read between:
    • A. 

      1643-1802 rpm

    • B. 

      1700-1768 rpm

    • C. 

      1520-1610 rpm

    • D. 

      1400-1550 rpm

  • 11. 
    A propeller rpm of 1565 on takeoff would indicate:
    • A. 

      The primary governor has failed

    • B. 

      The overspeed governor is stuck in the test position

    • C. 

      The low pitch solenoid has not reset

    • D. 

      Is is acceptable since the propeller is still indicating in the green arc

  • 12. 
    The fuel topping governor:
    • A. 

      Provides protection against power turbine overspeed

    • B. 

      Limits power turbine speed (N2) to 36000 rpm

    • C. 

      Is set to a higher value for reversing

    • D. 

      None of the above are correct

  • 13. 
    If the low pitch solenoid is inoperative:
    • A. 

      The propellers will not attain 1700 RPM

    • B. 

      The propellers will not go into reverse

    • C. 

      The propeller can not be feathered

    • D. 

      None of the above are correct

  • 14. 
    The maximum allowable propeller rpm is:
    • A. 

      1700

    • B. 

      1768

    • C. 

      1802

    • D. 

      1870

  • 15. 
    If the propeller doesnt manually feather during an inflight engine failure:
    • A. 

      The propeller cant be feathered any other way

    • B. 

      The propeller may be feathered using the autofeather system

    • C. 

      The propeller will go to an overspeed condition

    • D. 

      None of the above are correct

  • 16. 
    As oil leaves the propeller dome:
    • A. 

      Propeller blade angle increases

    • B. 

      Propeller blade angle decreases

    • C. 

      Propeller pitch decreases

    • D. 

      Propeller rpm increases