T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
(4) Rudder centering unit
(5) Yaw damper controller
(6) Rudder pedal shaker and audio tone
activated when AOA exceeds 21.5 units
b.
Operating characteristics
(1) Control augmentation system
WARNING: Initiating the CONTR AUG BIT
cycles the rudder and rudder tab. Ensure
the CONTR AUG BIT is completed prior to
taxi or takeoff.
(2) Yaw damping system and aileron rudder
interconnect operate automatically with
weight off wheels and airspeed less than
217 KIAS
(3) Rudder pedal operation may override yaw
damp system
(4) Operates in three modes
(5) Rudder deflection maximum:
20 + 0.5 degrees from neutral, including 6 +
1 degree maximum trim (limited by
electronic damping system)
(6) Rudder lock protects from wind up to
70 mph
(7) Simultaneously operating both trim
Sg 8, fr 10
switches in opposite directions disables the
Normal Operation
trim motor
Aileron Trim
2.
Aileron system
Fig 15: Flight
Controls -- Aileron
System Components
a.
Control surface components
NOTE: There are no aileron trim tabs on the
T-45C.
(9-98) Original
Page 27-78
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