Volume 2. 2A651 CDC ( Q 45-58)

14 Questions | Attempts: 126
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CDC Quizzes & Trivia

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Questions and Answers
  • 1. 

    The major sections of a turboprop engine are the power unit,torquemeter assembly, and

    • A.

      Turbine assembly.

    • B.

      Compressor assembly.

    • C.

      Combustion assembly

    • D.

      RGB assembly.

    Correct Answer
    D. RGB assembly.
  • 2. 

    On the T56 turboprop engine, how many stages of reduction are in the RGB's main reduction gear train?

    • A.

      1.

    • B.

      2.

    • C.

      3.

    • D.

      4.

    Correct Answer
    B. 2.
  • 3. 

    On the T56 turboprop engine, what is the overall reduction ratio of the RGB's main reduction gear train?

    • A.

      .3125 to 1.

    • B.

      4.333 to 1.

    • C.

      13.54 to 1.

    • D.

      13,820 to 1.

    Correct Answer
    C. 13.54 to 1.
  • 4. 

    On the T56 turboprop engine, there are mounting pads on the aft side of the accessory drive for the fuel control, fuel pump,and

    • A.

      Speed-sensitive valve.

    • B.

      Engine main oil pump.

    • C.

      Speed-sensitive control.

    • D.

      External scavenge oil pump.

    Correct Answer
    D. External scavenge oil pump.
  • 5. 

    On the T56 turboprop engine, which compressor section assembly disperses compressor discharge air and directs it to the combustion chambers?

    • A.

      Diffuser.

    • B.

      Compressor rotor.

    • C.

      Compressor housing.

    • D.

      Compressor air inlet housing.

    Correct Answer
    A. Diffuser.
  • 6. 

    In the T56 engine, which RGB component rotates at the same speed as the power unit rotors?

    • A.

      Sun gear.

    • B.

      Ring gear.

    • C.

      Main drive gear.

    • D.

      Pinion input gear.

    Correct Answer
    D. Pinion input gear.
  • 7. 

    What is the total gear reduction ratio of the RGB?

    • A.

      3.125:1.

    • B.

      4.333:1.

    • C.

      12.85:1.

    • D.

      13.54:1.

    Correct Answer
    D. 13.54:1.
  • 8. 

    What is not a propeller brake positions?

    • A.

      Locked.

    • B.

      Applied.

    • C.

      Engaged.

    • D.

      Released

    Correct Answer
    C. Engaged.
  • 9. 

    The propeller brake is in which position when the aircraft is on the ground and the engine is stopped?

    • A.

      Locked.

    • B.

      Applied

    • C.

      Engaged.

    • D.

      Released.

    Correct Answer
    B. Applied
  • 10. 

    Which valve in the propeller control assembly is actuated by the NTS actuator rod to increase propeller blade angle?

    • A.

      Pilot.

    • B.

      Feather.

    • C.

      Beta backup.

    • D.

      Alpha backup

    Correct Answer
    B. Feather.
  • 11. 

    Which  components comprise the torquemeter assembly?

    • A.

      Torque shaft, torquemeter housing,and front coupling assembly.

    • B.

      Two concentric shafts, torquemeter housing,and torquemeter pickup.

    • C.

      Two outer shafts, torquemeter pickup assembly, and torquemeter backup assembly.

    Correct Answer
    A. Torque shaft, torquemeter housing,and front coupling assembly.
  • 12. 

    The amount of twisting deflection is determined by the

    • A.

      Torque shaft.

    • B.

      Reference shaft.

    • C.

      Safety coupling

    • D.

      Pinion input gear.

    Correct Answer
    A. Torque shaft.
  • 13. 

    The torquemeter exciter wheels are in phase when

    • A.

      The shaft power output is transmitted from the power unit.

    • B.

      Negative or positive torque is transmitted to the torque indicator.

    • C.

      The rectangular teeth on the exciter wheels are aligned at zero torque.

    • D.

      There is a change in the torque transmitted to the torque shaft exciter wheel

    Correct Answer
    C. The rectangular teeth on the exciter wheels are aligned at zero torque.
  • 14. 

    The perpose of the T56 safety coupling is to

    • A.

      Prevent overspeed of the propeller.

    • B.

      Increase propeller pitch as negative torque occurs.

    • C.

      Maintain constant engine speed by decreasing propeller blade angle.

    • D.

      Disconnect the power section from the RGB assembly

    Correct Answer
    D. Disconnect the power section from the RGB assembly

Quiz Review Timeline +

Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.

  • Current Version
  • Jan 22, 2013
    Quiz Edited by
    ProProfs Editorial Team
  • Dec 21, 2010
    Quiz Created by
    Vison
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