T-45C TS, ADV & IUT ENG-13
Flight Control System
3.
Operating characteristics/limitations
Yaw Damper
Controller
Trim/Yaw Damper
Actuator
Fwd/Aft Rudder
Rudder/Yaw
Trim Switches
Damper Actuator
Linkage
Fwd/Aft
CONTR AUG
Switches
Fwd/Aft
Rudder
Rudder Pedals
Centering Unit
LEGEND
MECHANICAL LINKS
ELECTRICAL
Figure 10: RUDDER SYSTEM COMPONENTS--SIMPLIFIED
a.
Control augmentation system (CAS)
Sg 2, fr 33
Fig 10: Rudder
NOTE: GINA mode manipulation results in yaw
System Components--
Simplified
damper degradation and a C AUG caution light.
A CONTR AUG system reset is required to
reestablish control augmentation operation.
(1) SBI and rudder trim available with weight
on or off wheels. Aileron-rudder
interconnect (ARI) and yaw damping
available only with weight off wheels
(2) Yaw damping commands are zero with
airspeed above 217 KIAS, except when
trimming rudder
(3) SBI system provides stabilator trim inputs
to reduce pitch transients during speed
brake extension or retraction
(9-98) Original
Page 13-22
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