Flight Controls
T-45A UJPT, E2-C2, ADV, & IUT Eng-11
(3) The YAW Damper controller
receives data from SAHRS,
SADS, Aileron Position Sensor,
FLAP position from FLAP/SLATS
Lever, rate of YAW from an
internal gyro and rudder trim inputs
from the pilot to compute/
determine what commands to
send to the Yaw Damper
Controller
e.
Rudder centering unit
Overlay 5
(1) Location: on aft face of aft seat
frame
(2) Function: produces light force
(resistance) during low-speed flight
and on deck for rudder centering
RUDDER CENTERING UNIT
f.
Rudder pedal shaker
(1) Location: attached to left rudder
pedal in forward cockpit
(2) Function: activated by AOA
system. Provides stall warning,
along with a stall warning tone
when AOA is 21.5 units or greater
2.
Cockpit controls/switches/indicators
a.
Rudder pedals
(1) Adjustable via rudder pedal adjust
knob, just forward of stick in both
cockpits
(2) Toe pedals independently operate
hydraulic wheel brakes
Page 11-13
(8-03) Original
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