The wing spoilers on the CARAVAN I are designed to: A) Improve lateral control of the airplane at low speeds. B) Be used as speed reduction devices. C) Increase the effectiveness of the flaps. D) Balance control forces in the aileron system. . The rudder lock is operated by a T-handle which: A) Must be pulled out during engine start. B) Is automatically released when the fuel condition lever is moved out of CUTOFF. C) Must be pushed in to lock the rudder. D) Is located on the center pedestal. . The rudder trim system: A) Operates a trim tab on the rudder. B) Is operated electrically. C) Is controlled by a knob on the instrument panel. D) Operates against the nosewheel steering bungee. The standby flap system is operates: A) Until the flaps reach their stops. B) By using the crank on the overhead panel. C) Until the flap position indicator reaches the desired setting. D) Hydraulically. . The Control Lock is provided to lock: A) Aileron. B) Elevator C) Rudder D) Both A and B. . The vane-type stall warning unit is installed in the leading edge of the _______ wing and is
______________ connected to the ____________________: A) Left Mechanically Stall Warning Horn. B) Right Electrically Autopilot. C) Left Mechanically Autopilot. D) Left Electrically Stall Warning Horn. . The vane-type stall warning senses the change in airflow over the wing an operates the
warning horn at airspeeds of between ___________ above the stall in all configurations. A) 0 and 10 knots. B) 5 and 8 knots. C) 5 and 10 knots. D) 8 and 15 knots. The stall warning system should be checked during the preflight inspection (________) by
momentarily turning the ___________ on and actuating the ________ in the wing. A) Left side Battery Vane. B) Cabin External Power warning horn switch. C) Cabin Battery Vane. D) Left side External Power Vane. . The stall warning system is protected by a circuit breaker labeled “STALL WRN” which
can be pulled to shut off the warning horn in the event the vane sticks in the on position.
This circuit breaker must be maintained out for landing: A) Thru B) False . The vane and sensor unit in the wing leading edge is equipped with a heating element. The
heated part of the system is operated by the STALL HEAT switch on the DEICE/ANTI-ICE
switch panel and is protected by the STALL WRN circuit breaker on the circuit breaker
panel. A) Thru B) False. The standby system can be used to operate the flaps: A) With the Primary system operates. B) With the Primary system malfunction. C) As desired. D) None of the above. . To operate the flap with the standby system, what are you first to do? A) Place the STBY FLAP MOTOR switch in the STBY position. B) Place the STBY FLAP MOTOR switch in the NORMAL position. C) Place the STBY FLAP MOTOR circuit breakers pull out. D) Place the STBY FLAP MOTOR circuit breakers reset in. .
