T-45A UJPT, E2-C2, ADV, & IUT Eng-07
Electrical
(b) Generator voltage with
generator operating and on
line
(2) Battery switches (BATT 1 and 2):
control battery connection to 28
VDC essential services bus
NOTE: Battery switches are not
provided in the aft cockpit.
(3) AC RESET switch: spring-loaded
center-on, used to reset AC in-
verter No. 1 or AC inverter No. 2
(4) Generator (GEN) switch: OFF/
ON/RESET positions allow control
of generator
2.
WCP
Sg 2, fr 9
GTSFIRE
a.
Location: right side of instrument
EGT/RPM
CABINALT
OILPRESS
OY E
XGN
panel, both cockpits
HYDFAIL
GENERATOR
BRAKEPRESS
SEATUNARMED
CNP
AOY
TAILPIPEHOT
SLATS
b.
Function
HYD1PRESS
ACINVERTER
HYD2PRESS
EA
C
RATEXTEND
AVIONICSHOT
FUELLOW
PARKBRAKE
LPPM
UP
NOSEWHLSTR
(1) GENERATOR warning light illumi-
FUELPRESS
CONTRAUG
ACCEL
ANTI-SKID
nates when generator is off-line
WARNING/CAUTION PANEL
INDICATIONS
(2) AC INVERTER caution light will
illuminate if one or both inverters
fails or is tripped off-line
Sg 3, fr 1
III. Aircraft lighting system 1.4.4.3.2
Lesson Organization
Sg 3, fr 2
A.
Exterior lighting
Anti-Collision Light
Formation Lights
(Red)
Starboard Wingtip
Tail Navigation Light
Strobe
Upper & Lower Surface
(White)
(White)
(Amber)
1.
Navigation lights
Formation Lights
Starboard
Port Wingtip
Navigation Light
Upper & Lower Surface
(Green)
(Amber)
a.
Location
Anti-CollisionLight
(Red)
PortNavigationLight
(Red)
Approach Light
Assembly
Taxi/Landing
(1) Green on right wingtip
Light Assembly
EXTERIOR LIGHT LOCATIONS
Page 7-16
(8-03) Original
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