T-45A UJPT, E2-C2, ADV, & IUT Eng-26
Engineering Review
(3) Rudder pedal operation may
override yaw damper 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
switches in opposite directions
disables the trim motor
C.
Flaps/slats, speed brakes
Sg 5, fr 8
1.
Flap system
a.
System overview: augments lift to
wing, allowing flight operations at lower
airspeeds
b.
Control surface components
FLAPS/SLATS
(1) Flap panels
(2) Flap actuator
(3) Pressure/thermal relief valves
c.
Cockpit controls/switches/indicators
(1) FLAPS/SLATS lever: three-
position switch (UP, 1/2, DOWN)
adjacent to throttle in both cockpits
(2) EMERG FLAPS switch: directs
pressure from wheel brake/emer-
gency flap accumulator in event of
HYD 1 failure to fully extend flaps
Page 26-52
(8-03) Original
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