Aircraft Control System Design Quiz

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Questions and Answers

What factor of safety must the support structure have for the control surface maximum moment load?

  • 1.75
  • 1.50
  • 1.25 (correct)
  • 1.10

What should the control system be designed to prevent?

  • Incorrect assembly
  • Excessive deflection
  • Excessive friction
  • Jamming by foreign objects (correct)

Under what conditions must the system be capable of continued operation?

  • A jam occurs in the system (correct)
  • No failure of any element occurs
  • Triple electrical or hydraulic systems fail
  • System operates beyond 80% specific limit load

What is the minimum diameter for cables used on aileron, elevator, and rudder control systems?

<p>0.125” (3.17mm) (A)</p> Signup and view all the answers

What is the maximum allowable change in direction for a cable after passing through a fairlead?

<p>3° (D)</p> Signup and view all the answers

What must pulleys be fitted with to prevent cable displacement or fouling?

<p>Guards (C)</p> Signup and view all the answers

What must be provided to prevent inadvertent flight-deck operation of lift and drag devices on the ground?

<p>A means for preventing inadvertent operation (C)</p> Signup and view all the answers

What type of system must wing flaps have to prevent asymmetric operation?

<p>A synchronising system strong enough to prevent asymmetric operation (B)</p> Signup and view all the answers

When must flight-deck indication be provided with warnings of asymmetrical operation?

<p>When lift and drag devices are designed for ground use (D)</p> Signup and view all the answers

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