Flight Controls
T-45A UJPT, E2-C2, ADV, & IUT Eng-11
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
h.
In the event of a total hydraulic failure,
one way check valves prevent an
uncommanded pitch up or down
C.
Rudder system 1.4.14.3.1.4, 1.4.14.2.1.3,
Sg 2, fr 10
1.4.14.3
(5 Overlays)
1.
Control surface components
a.
Rudder
(1) Location: trailing edge of vertical
FLIGHT CONTROLS-RUDDER
stabilizer
SYSTEM COMPONENTS
(2) Function: provides primary yaw
Overlay 1
control
Rudder
(3) Max deflection: 20 +/- 0.5 degrees
Overlay 2
Rudder Trim Tab
b.
Rudder trim tab
Page 11-11
(8-03) Original
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