T-45A UJPT, E2-C2, ADV, & IUT Eng-26
Engineering Review
(6) ANTI-SKID caution light
(7) ANTI-SKID advisory light
NOTE: ANTI-SKID switch must be
on in both cockpits to illuminate
the advisory light and for system
operation.
c.
Limitations
(1) During takeoff or landing when
anti-skid is selected, wheels must
spin up to 30 kts ground speed
before system is activated
(2) Anti-skid is not operational below
10-13 kts ground speed to allow
for directional braking during
aircraft taxi (used if NWS
inoperative)
(3) If anti-skid dumps all pressure for
more than 2 seconds (as in touch-
down protection mode with con-
stant pressure on brake pedals,
continuous braking on ice or if no
wheel spin up is detected for more
than 3 seconds), anti-skid system
shuts down and ANTI-SKID cau-
tion light comes on--after 1-sec-
ond delay, system reverts to
manual braking
(4) Brake pressure release during
catapult launch (163599 thru
165079 after T-45A AFC-256)
(a) The brake pressure release
system activates with left
MLG down and locked, launch
bar down, LAUNCH BAR
switch UP, throttle position
greater than 95 percent, the
Page 26-38
(8-03) Original
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