T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
(b) SBI -- provides rudder trim and speed
brake-stabilator interconnect
capabilities
(c) RESET (momentary, spring loaded to
SBI) -- resets the system
g.
Paddle switch
(1) Location: lower front side of control stick
(2) Function: (momentary switch) deactivates
control augmentation system (airborne) or
NWS system (ground)
h.
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
5.
Flaps/controls/switches/indicators
a.
FLAPS/SLATS lever
(1) Location: inboard of the throttle quadrant
(2) Function: three position control with
detents for selecting flaps UP, 1/2, or DN.
Forward and aft controls are mechanically
linked and operate the flap hydraulic valve
via a common switch
b.
EMER FLAPS switch
(1) Location: landing gear panel, below
emergency gear handle
(2) Function: directs pressure from wheel
brake/emergency flap accumulator in event
of HYD 1 failure to fully extend flaps
(9-98) Original
Page 27-86
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