T-45C TS, ADV & IUT ENG-13
Flight Control System
(b) SBI--provides rudder trim and speed
brake-stabilator interconnect
capabilities
(c) RESET (momentary, spring loaded to
SBI)--resets the system
g.
Paddle switch
Overlay 5
Paddle Switch
(1) Location: lower front side of control stick
(2) Function: (momentary switch) deactivates
the control augmentation system and the
NWS system with landing gear down
LESSON NOTES
Emphasize that the rudder is the only flight control not hydrau-
lically activated and that the rudder gust lock must be engaged
when the aircraft is parked.
h.
Rudder lock lever
Overlay 6
Rudder Lock Lever
(1) Location: right control unit support strut,
fwd cockpit only
(2) Function: locks rudder in neutral position
for protection while aircraft is parked
(9-98) Change 4
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