King Air 350i

138 Preguntas | Total Attempts: 168

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King Air 350i

Procedimientos Normales, Anormales y Sistemas


Questions and Answers
  • 1. 
    Electrical power for the Emergency Exit Signs are provided through
    • A. 

      Battery bus

    • B. 

      Triple fed bus

    • C. 

      Dual fed bus

    • D. 

      Four C-cell alkaline batteries

  • 2. 
    To open the emergency exit from the inside, pull down on the "Exit-Pull" handle
    • A. 

      True

    • B. 

      False

  • 3. 
    What normally terminates an engine start sequence?
    • A. 

      Motive flow pressure switch

    • B. 

      Strart disengage button

    • C. 

      Start switch moved to OFF at 50% N1

  • 4. 
    • A. 

      No loss of aircraft flight instruments or data

    • B. 

      No adverse condition as the 350 has no inverters for AC avionics systems

    • C. 

      A red warning annunciator and loss of appropiate AC bus equipment

  • 5. 
    What does illumination of a single GEN TIE OPEN annunciator indicate?
    • A. 

      A generator is offline

    • B. 

      Respective generator bus has been isolated from center bus

    • C. 

      Battery has been completely isolated

  • 6. 
    The entry light circuit powers the cockpit emergency lights which is powered by the  _______ bus
    • A. 

      Battery

    • B. 

      Triple fed

    • C. 

      Dual fed

    • D. 

      Either battery or dual fed

  • 7. 
    Normal generator voltaje is __________ VDC
    • A. 

      24.0

    • B. 

      28.25 +- .25

    • C. 

      28.75

  • 8. 
    Generator load is limited to ____________ percent during ground operations below 70% N1
    • A. 

      75

    • B. 

      88

    • C. 

      100

  • 9. 
    With th ebattery switch OFF and the battery bus switch EMER OFF, what should the battery bus voltaje read?
    • A. 

      24 VDC

    • B. 

      Battery volts

    • C. 

      0 volts

  • 10. 
    What are the three sources from which the triple fed bus receives voltaje?
    • A. 

      Battery, left & right generator buses

    • B. 

      Center bus, left &right generator buses

    • C. 

      Triple fed relay, left & right generator bus ties

  • 11. 
    The battery bus voltaje with the battery switch in the OFF position can still be read on the voltmeter with the voltmeter selector switch in the battery position.
    • A. 

      True

    • B. 

      False

  • 12. 
    The EXT POWER annunciator flashes with a GPU voltaje low or the GPU is electrically disconnected fron the aircraft.
    • A. 

      True

    • B. 

      False

  • 13. 
    Placing the BAT BUS switch in EMER OFF will open the battery relay, BAT tie and the RCCB.
    • A. 

      True

    • B. 

      False

  • 14. 
    The White LDG/TAXI advisory light indicates which of the following?
    • A. 

      The landing and taxi lights should be switched on for landing

    • B. 

      At least one of the three landing and taxi lights switches are ON, and the nose gear uplock switch is engaged

    • C. 

      At least one of the three landing and taxi lights are burned out.

  • 15. 
    The cabin headliner lights will illuminate full-bright when oxygen pressure is supplied to the passenger masks.
    • A. 

      True

    • B. 

      False

  • 16. 
    The PT6 used in the King Air 350 is described as a ___________________ engine.
    • A. 

      Reverse-flow, free turbine.

    • B. 

      Turboshaft

    • C. 

      Free-flow, reverse-turbine, horizontally opposed

    • D. 

      Option 4

  • 17. 
    The conpressor bleed valve is closed above approximately _______________% N1
    • A. 

      97.8

    • B. 

      60.5

    • C. 

      90.0

  • 18. 
    When should engine oil be checked for an accurate quantity Reading?
    • A. 

      During preflight inspection

    • B. 

      Within 15-20 minutes after engine shutdown

    • C. 

      Within 30 minutes after engine shutdown

    • D. 

      Option 4

  • 19. 
    What is the máximum ITT allowed during engine start with no inspection required?
    • A. 

      1,090°F for 5 seconds

    • B. 

      820°C - 850°C for 20 seconds

    • C. 

      1,000°C for 5 seconds

  • 20. 
    If the start swich is left in the IGNITION and ENGINE START position, which of the following cannot be activated?
    • A. 

      Auxiliary fuel transfer

    • B. 

      Auto-ignition

    • C. 

      Generator

    • D. 

      Auxiliary fuel transfer and generator

  • 21. 
    Which of the following engine limitations are correct?
    • A. 

      156% transient torque for 20 seconds

    • B. 

      ITT above 850°C. for 20 seconds transient and 1,000°C. for 5 seconds during start

    • C. 

      60 PSI mínimum oil pressure at a máximum 62% torque

    • D. 

      785°C máximum cruise climb ITT

    • E. 

      104% máximum N1

    • F. 

      All of the above

  • 22. 
    Below 1,000 propeller RPM, torque is limited to 62%
    • A. 

      True

    • B. 

      False

  • 23. 
    Oil pressure between 60 and 90 PSI should be tolerated only for completion of the flight and torque limited to 62%
    • A. 

      True

    • B. 

      False

  • 24. 
    Placing the test switch in the DET position illuminates the
    • A. 

      EXTENGUISHER PUSH switch lights

    • B. 

      ENGINE FIRE switch lights

    • C. 

      Both of the above

  • 25. 
    A portable fire extinguisher is in the cockpit
    • A. 

      Under the copilot's seat

    • B. 

      Under the pilot's seat

    • C. 

      Behind the copilot's seat