Flight Controls
T-45A UJPT, E2-C2, ADV, & IUT Eng-11
d.
Full extension of flaps is approximately
50 degrees, half approximately 25
degrees
e.
EMERG FLAPS switch fully extends
flaps if adequate accumulator pressure
is available. No flap extension if
accumulator pressure is below 2,200
psi
NOTE: Operations with EMER FLAPS
selected, when normal HYD1 power is
available, is restricted to 30 seconds
with engine rpm less than or equal to
90%. Except in an actual emergency,
use of EMER FLAPS is restricted to
FCF profiles.
f.
Speed restriction for deployment: 200
KIAS
g.
Maneuvering envelope with flaps
extended symmetrical: 0 to +2.0 g
max. Maneuvering envelope with an
unsymmetrical load condition: +1.0 to
+1.5 g max
NOTE: Due to the design of the T-45A, a split flap
condition is highly unlikely. Be advised that this is
not an impossibility and would be a very dangerous
situation should it occur.
B.
Slat system 1.5.4.1.2.1, 1.5.4.1.2.1.2,
Sg 3, fr 5
1.5.4.1.2.1.1
HYD 1
MECHANICAL
ELECTRICAL
FWD/AFT
Flaps/Slats
1.
System overview: augments lift to wing
Slat Selector
when extended, decreasing stall speed and
Valve
Slat Actuator
Slat Actuator
increasing aircraft control and stability
during slow speed flight
2.
Control surface components
SLAT SYSTEM COMPONENTS--
SIMPLIFIED
a.
Slats
Page 11-23
(8-03) Original
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