T-45C TS, ADV & IUT ENG-13
Flight Control System
NOTE: Both motors are de-energized by
travel limit switches. Lifting the STBY STAB
TRIM switch guard disables the main trim
motor and allows use of the standby trim
switch.
c.
Maximum stabilator deflection: control stick
full aft--leading edge 15 degrees down; control
stick full forward--leading edge 6.6 degrees up
d.
Maximum stabilator trim deflection: provides a
range from 3 degrees leading edge up to
8 degrees leading edge down
e.
Simultaneous operation of the stabilator trim
switches in opposite directions by both cockpits
will disable the trim motor
f.
Standby trim selection can be made from either
cockpit and will disable main trim control
g.
Rate of trim change from either main or standby
control: approximately 2 degrees per second
Sg 2, fr 20
C.
Rudder system 1.4.14.3.1.4, 1.4.14.2.1.3, 1.4.14.3
(5 Overlays)
Fig 8: Flight
1.
Control surface components
Controls-Rudder
System Components
a.
Rudder
Overlay 1
Rudder
(1) Location: trailing edge of vertical stabilizer
(2) Function: provides primary yaw control
(3) Max deflection 20 +/- .5 degrees
Overlay 2
b.
Rudder trim tab
Rudder Trim Tab
(1) Location: lower trailing edge of rudder
(2) Function: provides pressure relief for rudder
pedals
(9-98) Original
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