Hydraulic Subsystems
T-45A UJPT, E2-C2, ADV, & IUT Eng-13
f.
ANTI-SKID switch
Sg 2, fr 6
GTSFIRE
GTS
(1) Location: left console, both
ROTATION
EGT/RPM
CABINALT
OILPRESS
OY E
XGN
SPDBRK
cockpits
HYDFAIL
SPDBRKFULL
BRAKEPRESS
SEATUNARMED
CNP
AOY
ECA
TAILPIPEHOT
SAS
LT
MANUAL FUEL
HYD1PRESS
ACINVERTER
(2) Purpose
HYD2PRESS
EA
C
NOSEWHLSTR
ANTI-SKID
RATEXTEND
AVIONICSHOT
FUELLOW
PARKBRAKE
ANTI-SKID
LPPUMP
NOSEWHLSTR
O
N
(a) Enables operation of anti-skid
FUELPRESS
CONTRAUG
OFF
ACCEL
ANTI-SKID
system
ANTI-SKID SYSTEM CONTROLS
AND INDICATORS
(b) To function, switch must be
set to ON in both cockpits
(c) Resets anti-skid control if no
malfunction within system
g.
ANTI-SKID caution light
(1) Location: WCP, both cockpits
(2) Purpose: illuminates when
(a) Failure condition has been
detected by anti-skid control
box; accompanied by flashing
MSTR ALERT and caution
tone
h.
ANTI-SKID advisory light
(1) Location: advisory panel, both
cockpits
(2) Purpose: illuminates in both
cockpits when anti-skid is selected
and landing gear are down and
locked
i.
BRAKE PRESS Caution Light (163599
THRU 165079 AFTER T-45A AFC-
256)
Page 13-22
(8-03) Original
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