T-45C TS, ADV & IUT ENG-13
Flight Control System
(1) Location: outboard of flaps on trailing edge
of wings
(2) Function
(a) Provide primary lateral control
(b) Provide lateral trim
b.
Aileron actuators (power control units [PCUs])
Overlay 2
Aileron Actuators
(1) Location: mounted underneath wing trailing
edge in fairings (one PCU per aileron)
(2) Function
(a) Supplied with power from both
hydraulic systems for redundancy
(two actuators per PCU)
(b) Provide mechanical power to move
ailerons
Overlay 3
c.
Aileron trim actuator
Aileron Trim Actuator
(1) Location: aft of aft cockpit floor, right of
aircraft centerline
(2) Function: provides power to trim aileron
control surfaces
Overlay 4
d.
Aileron spring feel unit
Aileron Spring Feel
Unit
(1) Location: just forward of trim actuators
(2) Function: provides pilot with artificial "feel"
of aerodynamic forces acting on control
surfaces
2.
Cockpit controls/switches/indicators
(9-98) Original
Page 13-7
Previous Page
