T-45A UJPT, E2-C2, ADV, & IUT Eng-26
Engineering Review
(d) During all other ground
operations, illumination of the
light normally indicates a
failure of the indication circuit
only. It would require multiple
failures to have this caution
light, and actually, have no
brake pressure
(e) In flight with gear up, it is
possible to have the caution
light illuminate due to a single
component failure. If this
occurs, it may be associated
with a landing gear caution
light. If the gear is put down
and the brake pressure light
extinguishes, normal braking
is available. If the brake
pressure light remains on with
the gear down, assume loss
of brakes and make a short
field arrestment
CAUTION: Failure of weight-off-
wheels circuits will prevent anti-
skid activation on touchdown,
with no indication to the pilot,
and subsequent loss of brakes.
Placing the ANTI-SKID switch to
OFF will engage the normal (No
Anti-Skid) brake system and
restore braking authority.
NOTE: Anti-skid may be reset by
Sg 4, fr 7
cycling ANTI-SKID switch in either
cockpit.
2.
Nose wheel steering (NWS); dual-gain, full-
time (low-gain)
a.
Major components
NOSE WHEEL STEERING (NWS)
SYSTEM MAJOR COMPONENTS
Page 26-40
(8-03) Original
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