Flight Controls
T-45A UJPT, E2-C2, ADV, & IUT Eng-11
(1) Location: incorporated into slat
selector assembly
(2) Function
(a) Protects hydraulic lines
against thermal expansion of
hydraulic fluid
3.
Cockpit controls/switches/indicators
Sg 3, fr 6
a.
FLAPS/SLATS lever
(1) Location: inboard of the throttle
quadrant
(2) Function: three-position control
with detents for selecting flaps/
SLAT CONTROLS AND INDICATORS
slats UP, 1/2, or DN. Forward and
aft controls are mechanically
linked and operate the flap
hydraulic valve via a common
electrical switch
(a) UP: slats retracted
(b) 1/2 or DN: slats extended
b.
SLATS caution light
(1) Location: warning/caution panel
(2) Function: illuminated when
(a) Slats not in selected position
or split slats
(b) Slats extended and airspeed
increases above 217 KIAS
(c) Slats selected when airspeed
is above 217 KIAS (slats will
not extend); sensor/ pickoff in
aft cockpit airspeed indicator
Page 11-25
(8-03) Original
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