T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
(3) Stabilator position indicator: located on left
console, left of aileron trim indicator
NOTE: Simultaneous operation of trim
switches in opposite directions inhibits
operation of the stabilator trim main and
standby motors.
c.
Flaps/slats, speed brakes
Fig 17: Flaps/Slats
Speed Brakes
(1) Flap system
(a) System overview: augments lift to
wing, allowing flight operations at lower
airspeed
(b) Control surface components
(i)
Flap panels
(ii) Flap actuator
(iii) Pressure/thermal relief valves
(c) Cockpit controls/switches/indicators (all
located on left instrument panel, both
cockpits)
(i)
FLAPS/SLATS lever: three-
position switch (UP, 1/2, DOWN)
adjacent to throttle in both
cockpits
(ii) EMERG FLAPS switch: directs
pressure from wheel brake/
emergency flap accumulator in
event of HYD 1 failure to fully
extend flaps
(iii) FLAP position indicator
(9-98) Original
Page 27-80