Flight Controls
T-45A UJPT, E2-C2, ADV, & IUT Eng-11
(1) Aileron trim
(2) Rudder trim
(3) Standby stabilator trim
(4) Trim indicator (aileron, rudder, and
stabilator)
b.
28 VDC essential services bus powers
primary stabilator trim only
E.
Summary:
The aileron, stabilator, and rudder systems
make up the flight controls. The aileron and
stabilator systems are hydraulically operated
with redundant actuators. The rudder system is
mechanical and should be locked when the
aircraft is parked. Toe pedals on the rudder
pedals activate the independent hydraulic wheel
brakes. All flight controls have trim capability.
The control augmentation system enhances the
flight characteristics of the aircraft.
III. Flaps/slats, speed brakes
Sg 3, fr 1
Lesson Organization
A.
Flap system 1.5.4.1.2.1, 1.5.4.1.2.1.2,
1.5.4.1.2.1.1
Sg 3, fr 2
1.
System overview: augments lift to wing,
HYD 1
allowing flight operations at lower airspeeds
MECHANICAL
ELECTRICAL
Fwd/AftFlaps/SlatsLevers
2.
Control surface components
a.
Flap panels - Double-slotted fowler
LeftFlap
Right Flap
FlapPCU/Actuator
Pressure and Thermo Relief Valves
flaps
FLAP SYSTEM COMPONENTS--
(1) Location: trailing edge of each
SIMPLIFIED
wing panel (extending from wing
root), inboard of trailing edge of
each wing
Page 11-20
(8-03) Original
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