The ailerons are operated by: A) Hydraulic pressure. B) Mechanical inputs from the control wheels. C) A fly-by-wire system. D) An active control system that totally eliminates adverse yaw.
The aileron trim tab is operated by: A) An electrically operated trim tab motor. B) A hydraulically operated trim tab motor. C) A mechanical trim knob on the rear face of the center pedestal. D) Changing the angle of the aileron “fence”.
Regarding the rudder: A) The pilot's and copilot's pedals are interconnected. B) The trim tab actuator is powered only electrically. C) The servo is connected to the air data computer to restrict rudder pedal deflection at high airspeeds. D) It is independent of the nosewheel steering on the ground.
The elevator: A) Trim tab is controlled only electrically. B) Runaway trim condition can be alleviated by depressing the A/P TRIM DISC switch on either control wheel. C) Electric pitch trim has both high-and low-speed positions. D) Trim tab is located on the left elevator only.
Regarding the gust lock: A) The engines may be started with it engages. B) The airplane should not be towed with it engaged. C) It may be engaged for towing. D) If the airplane is towed past the 60º limit, nosewheel steering may be lost. It is still permissible to fly the airplane if the gear is left extended.
Extended speedbrakes are maintained in that position by: A) Hydraulic pressure (HYD PRESS) light remains illuminated. B) Trapped fluid in the lines from the solenoid valves. C) Internal locks in the actuators. D) External locks on the actuators.
The amber (HYD PRESS) light on the annunciator panel will illuminate during speedbrake operation: A) When the speedbrakes are fully extended. B) While the speedbrakes are extending and retracting. C) Both A and B. D) Neither A nor B.
A true statement concerning the speed brakes is: A) The white SPD BRK EXTEND light will illuminate whenever both sets of speedbrakes are extended. B) If DC electrical failure occurs while the speedbrakes are extended, they will remain extended since the hydraulic pressure is trapped on the extend side of the actuators. C) If hydraulic pressure loss should occur while the speedbrakes are fully extended (system bypass valve fails open). The speedbrakes will automatically blow to trail. D) The speedbrakes can be retracted only by placing the speedbrake switch to RETRACT.
Moving the flap handle to any position: A) Actuates both control switches in the pedestal, connecting AC power to two motors to operate the flaps. B) Actuates one control stich in the pedestal, connect AC power to one motor to operate the flaps. C) Actuates one of two switches in the pedestal, connecting DC power to two motors to operate the flaps. D) None of the above.
The flaps are actuated by: A) The pneumatic system. B) The hydraulic system. C) One electric motor normally; the other is a reserve motor. D) Two electric DC motors.
If main DC power is lost: A) The flaps will be inoperative. B) The flaps will operate with the backup motor but will extend at a reduced rate. C) There is no effect on wing flap operation. D) A split flap condition could result since power is applied to only one motor.
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