Flight CONTROLS Flashcards
The ailerons are operated by
A. hydraulic pressure
B. mechanical inputs from the control wheels
C. fly by wire system
D. active control system that totally eliminates adversial
B
Is the aileron trim tab is operated by
A. electrically Operated trim tab motor
B. hydraulically operated trim tab motor
C. mechanical Trim knob on the center pedestal
D. changing the angle of the aileron fence
C
Regarding the rudder
A. pilot and Copilot rudder pedals are interconnected
B. trim tab actuator is powered only electrically
C. Servo is connected to the air data computer to restrict rudder pedal deflection at high air speeds
D. independent of the nosewheel steering on the ground
A
Moving the flat selector lever to any position
A. energizes the hydraulic system control valve closed
B. energizes the flat syllaboid valve to the selected position
C. both a and B
D. has no effect on the stabilizer trim
C
The elevator
A. trim tab is controlled only electrically
B. runaway trim condition can be alleviated by momentarily depressing the red auto pilot trim disconnect switch
C. Electric pitchtrim has both high speed and low speed positions
D. trim tab is located on the right elevator only
B
The hydraulic power is lost
A. the flaps will be inoperative
B. The flaps will operate with the backup electrical system but will extend and retract at a reduced rate
C. there is no effect on the wingflap operation
D. a split flip condition could result if the flaps are lowered
A
The wing flaps
A. if the wing flaps are positioned up prior to takeoff no visual or oral warning is present
B. depend on both actuators to function to prevent a split flat condition
C. can be lowered manually if electrical power is lost but only if all hydraulic fluid has not been lost
D indirectly controls the position of the horizontal stabilizer position
D
Regarding the gust lock
A. the engines may be started with it engaged
B. the aircraft should not be toad with it engage
C. it must be engaged for towing
D. if the aircraft is towed nosewheel steering may be damaged it’s still permissible to fly if the gear is left down
B
If hydraulic failure occurs with the flaps extended the flaps
A. may blow upward immediately depending on airload if the flap handle is moved
B. cannot be fully retracted
C. can be retracted up electrically
D. flaps will remain in present position regardless if the flap handle is moved
A
Extended speed breaks are maintained in position by
A. continuous system hydraulic pressure
B. trapped fluid in the lines from the solenoid control valve
C. internal locks in the actuators
D. external locks in the actuators
B
The Amber HYD PRESS assassinator will illuminate during speedbreak operation
A. when the speedbreaks are fully extended
B. while the speed breaks are extending and retracting
C. both a and B
D. neither a nor B
B
The true statement concerning the speed brakes is is.
A. The white SPD BRK EXTEND annunciator will eliminate whenever both sets of speedbreaks are fully extended
B. If DC electrical failure occurs while the speedbreaks are extended they will remain extended since the hydraulic pressure is trapped on the extend side of the actuator
C. If the hydraulic pressure loss should occur while the speed breaks are extended hydraulic system control valve fails open the speedbrakes will automatically blow to trail
D. The speed breaks can only be retracted by placing the speed break switch to retract
A
If the STAB MIS COMP annunciator illuminates in flight with the flaps up
A. Reduce speed to 200 KIAS maximum and initiate a no flat landing
B. reduce speed to 200 KIAS maximum and prepare for a normal landing
C. reduce speed to 200 KIAS maximum and prepare for a 15ﾟ flap landing
D. slow to 150 KIAS maximum and land as soon as practical
B
The rubber bias system
A. will be inoperative with the thrust reverser deployed
B. will be inoperative with the either emergency STOW switch in EMER
C. utilize main system hydraulics
D. both a and B above
D
If the STBY P/S HTR announciator illuminates in icing conditions
A. the stick shaker will not operate correctly
B. the standby HSI will not be usable
C. normal airspeed indications may be unreliable
D. speed sensor protection for the horizontal stabilizer may not be available
D
