T-45A UJPT, E2-C2, ADV, & IUT Eng-26
Engineering Review
(4) No provisions to extend or retract
slats with HYD 1 failure
(5) Full extension of slats is 15 de-
grees
(6) Speed restriction for deployment
or flying with slats extended:
200 KIAS
NOTE: There is no blow back
feature in the slat hydraulic sys-
tem.
(7) Maneuvering envelope with slats
extended: 0 to +2.0 g max; ma-
neuvering envelope for slats down
with an asymmetrical load on wing
pylons: +1.0 to +1.5 g max
NOTE: A split slat condition is
highly unlikely in the T-45A; how-
ever, it is not impossible and
would be very dangerous should it
occur.
3.
Speed brake system
Sg 5, fr 9
a.
Components
(1) Left/right speed brakes
(2) Hydraulic actuator
b.
Cockpit controls/switches/indicators
SPEED BRAKES
(1) SPD BRK advisory light: illumi-
nates green to indicate brakes not
fully retracted
(2) SPD BRK FULL advisory light:
illuminates green to indicate speed
brakes fully extended
Page 26-55
(8-03) Original
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