Flight Controls Flashcards
What powers the Power Control Units (PCU) that move various flight controls?
Hydraulic pressure
The trailing rudder deflects at _____ the rate of the fore rudder rate.
2x
The trailing rudder is connected to the fore rudder by which component?
Geared push rods
What controls the distance the rudder can travel?
2 systems:
Flaps setting
FCECU based on airspeed
What is the distance the rudder can travel either side of center when the flaps are set to 0 degrees?
12 degrees left or right of center
With the flaps set to 5 degrees or greater, what is the maximum rudder travel either side of center?
18 degrees of travel either side of center
T/F: At low speeds, the FCECU does not limit hydraulic pressure to the rudder.
TRUE
T/F: At low speeds, the FCECU limits hydraulic pressure to the rudder.
FALSE, at low speeds it does not limit pressure providing greater travel
T/F: At high airspeeds, hydraulic pressure to the rudder is reduced.
TRUE
T/F: At high airspeeds, hydraulic pressure to the rudder is not limited.
FALSE, it is limited to reduce the rudder deflection
How do pilots know if the elevator trim position signal fails?
Elevator trim pointer indicates off-scale (can be off scale nose down or nose up)
T/F: If the trim position signal fails, the trim still operates normally.
TRUE
What provides roll control for the aircraft?
2 ailerons and 4 spoilers
T/F: The ailerons are directly operated by the First Officer’s control column.
TRUE
T/F: The ailerons are directly operated by the Captain’s control column.
FALSE, they are linked, but the spoilers are directly operated by the Captain’s control column
The ailerons are mechanically controlled and _____.
Cable operated
The spoilers are mechanically controlled and _____.
Hydraulically operated
T/F: The aircraft has a roll disconnect handle that allows the control wheels to be separated in the event of an aileron or spoiler jam.
TRUE
How far will the control yokes travel to either side?
70 degrees
Give 17 degrees of aileron travel either side of center
Which direction does the geared tab move on the aileron?
Opposite direction of the aileron to reduce control forces