Flight Controls Flashcards
- The ailerons are operated by:
B. B. Mechanical inputs from the control wheels
- The aileron trim tab is operated by:
C. A mechanical trim knob on the rear pedestal.
- Regarding the rudder:
A. The pilot and copilot pedals are interconnected.
- The elevator:
A. Trim tabs are controlled only electrically.
- If hydraulic power is lost:
A. The flaps are inoperative.
- The wing flaps:
D. Can be selected to GROUND FLAP position on the ground or in flight; the ground flap selection is prohibited in flight.
- Regarding the gust lock:
B. The airplane should not be towed with it engaged.
- Moving the flap selector lever to any position:
C. Both A and B.
A. Energizes the hydraulic system loading valve closed.
B. Energizes the flap control valve to the selected position.
- If hydraulic failure occurs with the flaps extended and the FLAPS handle is moved, the flaps:
A. May move upward depending on air load
- Extended speedbrakes are maintained in that position by:
B. Trapped fluid in the lines from the control and safety valves
- The white HYD PRESS ON annunciator on the annunciator panel illuminates during speedbrake operation:
B. While the speedbrakes are extending and retracting
- A true statement concerning the speed-brakes is:
A. The white SPD BRK EXTEND annun-ciator illuminates when both sets of speedbrakes are fully extended.
- Speedbrakes must not be extended within:
A. 50 feet prior to landing
- The speedbrakes fully retract if:
C. Either throttle is advanced above 85%
N2 position with the electrical and hydraulic systems operating normally.
- If the RUDDER BIAS annunciator illuminates:
A. Rudder BIAS (bleed air) is not available from either engine to the actuator.
