C-17a Loadmaster Basic Mqf Test

10 Questions | Total Attempts: 190

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Military Quizzes & Trivia

Questions and Answers
  • 1. 
    Instructions or procedures prefaced by the word ________ are mandatory. 
    • A. 

      May

    • B. 

      Should

    • C. 

      Must

    • D. 

      Shall

  • 2. 
    The C-17A max design zero fuel weight is _________. 
    • A. 

      585,000

    • B. 

      586,000

    • C. 

      170,900

    • D. 

      447,400

  • 3. 
    To override the #2 and #3 hydraulic aux. pumps for an auto shutdown due to low quantity or overheat, _________.
    • A. 

      Press and hold appropriate Aux pump switch for 5 seconds.

    • B. 

      Press and hold XFER pump switch for 5 seconds

    • C. 

      Press and hold appropriate Aux pump switch for 3 seconds

    • D. 

      Press and hold XFER pump switch for 3 seconds

  • 4. 
    An automatic shut down override switchlight provides a means to override all APU ECU automatic shutdown signals except _________. 
    • A. 

      Over temperature

    • B. 

      Low fuel inlet pressure

    • C. 

      High oil temperature

    • D. 

      Indicated fire or overspeed

  • 5. 
    When the APU alert start feature is used, there will be no _______ until the battery bus is powered. 
    • A. 

      Fuel flow

    • B. 

      Available power

    • C. 

      Fire detection or protection

    • D. 

      Emergency exit lights

  • 6. 
    When the warning horn makes the tone of a squeal it indicates what warning situation? 
    • A. 

      APU Fire Warning

    • B. 

      Avionics/IRU Smoke, Avionics Overtemp

    • C. 

      Cabin Altitude Warning

    • D. 

      IRU- Battery On

  • 7. 
    The Battery Direct Bus, the Battery Bus, the AC and DC Emergency Buses, and the AC and DC Transfer Buses comprise the ______. 
    • A. 

      Electrical power system

    • B. 

      Battery power system

    • C. 

      External power system

    • D. 

      Emergency power system

  • 8. 
    Flight rules governing cargo-passenger aircraft require immediate descent to below ________ feet altitude upon complete loss of cabin pressurization. 
    • A. 

      10,000

    • B. 

      15,000

    • C. 

      20,000

    • D. 

      25,000

  • 9. 
    If the APU is started and the AVAIL light does not illuminate, the ____ must be cycled from ON to RESET to ON. 
    • A. 

      BATT switch

    • B. 

      APU PWR switch

    • C. 

      EMERG PWR switch

    • D. 

      APU ALERT START switch

  • 10. 
    If the Ground Operations Power source is the APU only, the battery switch must be in the ___ position. 
    • A. 

      APU

    • B. 

      OFF

    • C. 

      STND BY

    • D. 

      ON

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