Stepper Motors & Rotor Control Quiz

302 Questions | Total Attempts: 57

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Machine Quizzes & Trivia

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Questions and Answers
  • 1. 
    The type of rotor control that is phased out during conversion from heli mode to acft mode is the?
    • A. 

      Flaperons

    • B. 

      Elevators

    • C. 

      Rudders

    • D. 

      Cyclic

  • 2. 
    How many pounds per square foot is the cabin floor limit load?
    • A. 

      300

    • B. 

      400

    • C. 

      500

    • D. 

      600

  • 3. 
    What windows are configured with explosive (fast burn) escape separators to provide emergency egress for the pilots?
    • A. 

      Left/right windshields

    • B. 

      Left/right side windows

    • C. 

      Left/right cockpit windwos

    • D. 

      Left/right look-down windows

  • 4. 
    The pilot and copilot seats adjust through a range of?
    • A. 

      Five inches vertically and five inches longitudinally

    • B. 

      Five inches vertically and three inches longitudinally

    • C. 

      Seven inches vertically and five inches longitudinally

    • D. 

      Seven inches vertically and three inches longitudinally

  • 5. 
    What configuration is flight ready with the nacelles rotated to the vertical position, and the wing rotated perpendicular to the fuselage?
    • A. 

      FULL STOW

    • B. 

      AIRPLANE

    • C. 

      HELICOPTER

    • D. 

      EMERGENCY WING STOW

  • 6. 
    Which digit of the four-digit numbering system identifies zones and areas with access provisions on the Osprey is a numerical identification of the panel/door within a zone?
    • A. 

      First

    • B. 

      Second

    • C. 

      Third

    • D. 

      Fourth

  • 7. 
    While both cabin doors have normal opening/closing mechanisms, what is the only door that is given emergency opening provisions?
    • A. 

      Side

    • B. 

      Upper

    • C. 

      Lower

    • D. 

      Escape

  • 8. 
    How many feet above the ground or deck are the rudders that are located on the rear of the edge of the vertical stabilizers?
    • A. 

      7 to 10

    • B. 

      10 to 15

    • C. 

      11 to 17

    • D. 

      11 to 20

  • 9. 
    All aircraft fuel servicing/defueling operations will be performed in accordance with local activities supplemental instructions and?
    • A. 

      Naval Air Systems Command (NAVAIR) 00-80T-109

    • B. 

      Technical Order (TO) 1V-22(C)B-1

    • C. 

      NAVAIR A1-V22AC-MRC-000

    • D. 

      TO 1V-22(C)B-6

  • 10. 
    What mode of operation does the ground refuel/defuel panel (GRDP) operate in?
    • A. 

      NORMAL

    • B. 

      REFUEL

    • C. 

      OFF

    • D. 

      ON

  • 11. 
    What system on the nose landing gear (NLG) provides the means to raise the nose of the nose of the aircraft during ground maintenance and towing of the aircraft?
    • A. 

      Hike

    • B. 

      Chamber

    • C. 

      Elevation

    • D. 

      Extension

  • 12. 
    What provides control and indication of the primary landing gear extension/retraction system and control of the emergency extension system in the event the primary system fails?
    • A. 

      Drag strut/actuator

    • B. 

      Gas control manifold (GCM)

    • C. 

      Landing gear control unit (LGCU)

    • D. 

      Emergency gear extension unit (EGEU)

  • 13. 
    How many degrees of steering authority left or right of center is provided by the nose wheel steering system while on the ground?
    • A. 

      45

    • B. 

      60

    • C. 

      75

    • D. 

      90

  • 14. 
    What parking brake component applies hydraulic pressure seperately to the main landing gear left and right wheels and brakes and retains hydraulic pressure for parking brake engagement?
    • A. 

      Transfer module

    • B. 

      1st stage relief valve

    • C. 

      Master brake cylinders

    • D. 

      Pressure reducer valve module

  • 15. 
    What independent hydraulic system(s) provide hydro power to the Osprey?
    • A. 

      Auxiliary hydraulic power system

    • B. 

      Hydraulic system 1 and 2 only

    • C. 

      Main hydraulic power system

    • D. 

      Hydraulic system 1, 2, and 3

  • 16. 
    What monitors the fluid level in the reservoirs for hydraulic systems 1, 2, and 3?
    • A. 

      Hydraulic reservoir quantity multi-function display control layer

    • B. 

      Hydraulic fluid level monitor (HFLM)

    • C. 

      Fluid compensation valves

    • D. 

      Remote switching valves

  • 17. 
    Hydraulic pump 1 delivers how many gallons per minute (GPM) of hydraulic fluid?
    • A. 

      30 Helicopter and 30 airplane

    • B. 

      34 Helicopter and 30 airplane

    • C. 

      38 Helicopter and 32 airplane

    • D. 

      44 Helicopter and 36 airplane

  • 18. 
    What components provide artificial feel forces and magnetic brake functions for the mehcanical flight controls?
    • A. 

      Cockpit control thrust dirve actuators and cockpit control feel drive actuators

    • B. 

      CCTDAs and cockpit control position transducers (CCPT)

    • C. 

      CCPTs and thrust control levers (TCL)

    • D. 

      CCFDAs and CCPTS

  • 19. 
    Which panel has the capability to activate and/or reset the automated flight control system (AFCS), adjust individual engine torque values, and engage backup hydraulic power drive units (HPDU) on the conversion actuators?
    • A. 

      Flight control

    • B. 

      Engine control

    • C. 

      Backup flight control

    • D. 

      Primary flight control

  • 20. 
    What component prevents inadvertent engine shutdown when the condition lever is moved from FLY to START position?
    • A. 

      Nacelle waste gate

    • B. 

      CRANK/START gate

    • C. 

      CRANK/START lever

    • D. 

      Rotor brake control lever

  • 21. 
    In what mode do the rotor hub flapping sensors correct excessive flapping?
    • A. 

      AIRPLANE MODE

    • B. 

      TRANSITION MODE

    • C. 

      HELICOPTER MODE

    • D. 

      Vertical short take-off and landing (VSTOL) MODE

  • 22. 
    What percentage of the max hinge movement required of the surface are the left, right, and center elevator servo actuators capable of supplying?
    • A. 

      40

    • B. 

      50

    • C. 

      60

    • D. 

      70

  • 23. 
    What hydraulic system powers each section of the swashplate actuators?
    • A. 

      Sections A and B are powered by hydraulic system 1, while section C is powered by system 2

    • B. 

      Sections A and B are powered by hydraulic system 2, while section C is powered by system 2

    • C. 

      Sections A and B are powered by hydraulic system 1, while section C is powered by system 3

    • D. 

      Sections A and B are powered by hydraulic system 2, while section C is powered by system 3

  • 24. 
    With the doors open, the cargo hook external doors must be latched open prior to flight when the speed will be above how many knots?
    • A. 

      65

    • B. 

      70

    • C. 

      75

    • D. 

      80

  • 25. 
    In knots, what is the max speed for flight with a latched open cargo door?
    • A. 

      250

    • B. 

      200

    • C. 

      180

    • D. 

      150