Flight Controls Flashcards
What is the impact of using alternate trim during autopilot operation?
Alternate trim does not cause autopilot disengagement.
UNSCHED STAB TRIM light illuminates.
What is the impact of using electric trim on the control wheel during autopilot operation?
Single autopilot use- autopilot will disengage
Multi autopilot use- autopilot will not disengage. Electric trim switches are inhibited during multiple autopilot use.
Explain how the flap load relief system operates on all 757’s (and some 767’s).
If flaps 30 selected and overspeed occurs the flaps will retract to 25. The flaps will return to the flap lever selected position once the speed decreases below flap placard limit speed.
Explain how the flap load relief system operates on the 767ER.
If flaps 25 OR 30 selected and overspeed occurs, the flaps will retract to 20. The flaps will return to the flap lever selected position once the speed decreases below flap placard limit speed.
What assists ailerons in roll control?
Spoilers
When using the alternate flap/slat extension system, what is the maximum flap setting directed by the QRH?
Flaps 20
Describe the function of the alternate LE or TE switches on the 757.
On the 757, hydraulics are removed from BOTH systems, and the selected alternate drive unit is enabled
Describe the function of the alternate LE or TE switches on the 767.
Hydraulics are removed from the selected system and the selected alternate drive unit is enabled. The flap lever must continue to be moved on the 767 to hydraulically operate the system which still has hydraulics.
Example: During a 767 TE flap disagreement, the QRH will direct the pilot to select the TE alternate flap switch. The trailing edges will be controlled electrically with the ALTERNATE FLAPS SELECTOR switch, but the leading edges (slats) must still be controlled hydraulically using the flap lever.
When is leading edge slat asymmetry protection provided on the 757?
At all times.
What protections are provided during normal flap operation?
Asymmetry protection
Disagreement protection
Flap Load Relief Protection
What occurs upon detection of a flap asymmetry or disagreement?
Hydraulic power is automatically shut off
A LEADING EDGE or TRAILING EDGE discrete light illuminates
When do the outboard ailerons operate on the 767?
At low speeds.
How does the 767 control column nudger work?
Warning of an impending stall is provided by left and right stick shakers, which independently vibrate the left and right control columns. If the flaps are in the retracted position and the angle of attack continues to increase, a control column nudger moves the control column forward. Both systems are energized in flight and deactivated on the ground through air/ground logic.
What is the rudder ratio system?
Uses left hydraulic system pressure to reduce rudder deflection (based on airspeed).
How does the rudder ratio system work?
As airspeed increases, the ratio changer desensitizes the rudder and trim inputs from the pilot to reduce the rudder deflection. The ratio changer receives air data computer airspeed inputs and provides control commands to an actuator powered by the left hydraulic system. The actuator then dampens the pilots’ inputs to the rudder.