Aircraft Engine Types and Controls
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Aircraft Engine Types and Controls

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@IndulgentProsperity

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Questions and Answers

What is the horsepower rating of each Lycoming engine at sea level?

  • 160 horsepower
  • 220 horsepower
  • 200 horsepower
  • 180 horsepower (correct)
  • What type of fasteners is used to attach the upper cowl half of the aircraft?

  • Locking bolts
  • Screw-type fasteners
  • Quarter-turn fasteners (correct)
  • Panic buttons
  • What construction material is used for the engine mounts in this aircraft?

  • Aluminum
  • Plastic
  • Steel tubing (correct)
  • Fiberglass
  • Which controls are included in the engine controls for each engine?

    <p>Throttle, propeller control, and mixture control</p> Signup and view all the answers

    Where are the engine controls located in the aircraft?

    <p>On the control quadrant at the center of the instrument panel</p> Signup and view all the answers

    Study Notes

    Engine Type & Power

    • Two Lycoming four-cylinder engines power the aircraft.
    • Each engine produces 180 horsepower at 2700 RPM at sea level.

    Accessibility & Maintenance

    • Engines are accessible through removable cowls.
    • The upper cowl half is secured with quarter-turn fasteners, allowing for easy removal.

    Engine Mount

    • Engine mounts are made of steel tubing.
    • Dynafocal engine mounts reduce vibration, enhancing comfort and stability.

    Engine Controls

    • Controls consist of a throttle, propeller control, and mixture control lever for each engine.
    • Controls are centralized on the control quadrant, situated on the lower center of the instrument panel.
    • This arrangement makes controls easily accessible to both the pilot and copilot.

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    Description

    This quiz covers the fundamentals of aircraft engine types and their controls, focusing on Lycoming four-cylinder engines. Explore important aspects such as power generation, accessibility, maintenance, and control mechanisms. Perfect for aviation enthusiasts and students alike.

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