T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
NOTE: The flight control system controls and indicators
Sg 8, fr 2
consist of the following: aileron/stabilator trim switch,
Flight Controls
AILERON trim indicator, STBY STAB TRIM switch,
STABILATOR position indicator, rudder pedals, RUDDER
Fig 13: Flight
Controls
trim indicator, RUDDER TRIM control, C AUG caution light,
RUDDER PEDAL ADJUST knob, CONTR AUG switch,
FLAPS/SLATS switch, EMER FLAPS switch, FLAP position
Sg 8, fr 3
advisory light, SLATS caution light, SP BRK and FULL
Flaps/Slats
advisory lights, extend/retract switch.
The flaps/slats should not be lowered above 200 KIAS.
A.
Major components
1.
Flight controls
a.
Aileron system
b.
Stabilator system
c.
Rudder system
NOTE: Two stabilator vanes (strakes) are fixed
surfaces located on each side of the rear
fuselage, forward of the stabilator. With the
flaps extended and a high angle of attack, they
help direct airflow over the stabilator, providing
enhanced aircraft pitch control.
2.
Flaps/slats, speed brakes
Sg 8, fr 5
Normal Operation
B.
Flight controls
Rudder Trim
1.
Rudder system
Fig 14: Flight
a.
Control surface components
Controls -- Rudder
System Components
(1) Rudder
(2) Rudder trim tab
(3) Trim/Yaw damper actuator
(9-98) Original
Page 27-77
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