T-45A UJPT, E2-C2, ADV, & IUT Eng-02
Engine
1.
Fuel: aircraft fuel system
Sg 5, fr 2
2.
Mechanical: throttle controls
FUSELAGE
FUEL
TANK
SHUTOFF VALVE
3.
Electrical power: 28 VDC essential
BOOST
LP FUEL
HP FUEL
INTEGRAL WING TANK
PUMP
PUMP
PUMP
services bus from electrical system for
GTS
443GAL.(3012lbs.)TOTAL
427GAL.(2904lbs.)USABLE
MANUAL
FUELCONTROL
THROTTLE
FUEL SYSTEM
UNIT
engine igniters, ECA power, and fuel
BOOST
PUMPS
AIRCRAFT 163629 AND UP;
ENGINE
ALSO163600-163628AFTER
control switching
AFC-48
SIMPLIFIED FUEL SYSTEM BLOCK
DIAGRAM
B.
Outputs
1.
Air
a.
OBOGS
b.
ECS
c.
Fuel tank pressurization
d.
P1 probe anti-icing
2.
Mechanical drive items: in addition to
engine peculiar items (fuel and oil pumps)
a.
b.
HYD 1 and HYD 2 pumps
3.
Electrical (sensing)
a.
CWS signals
(1) Warning/caution
Sg 5, fr 3
(a) FIRE
GTSFIRE
FIRE
EGT/RPM
CABINALT
OILPRESS
OXYGEN
HYDFAIL
B A EP ES
RK RS
(b) GTS FIRE
SEATUNARMED
CANOPY
TAILPIPEHOT
SAS
LT
HD1PES
Y
RS
ACINVERTER
HD2PES
Y
RS
ECA
(c) EGT/RPM
RATEXTEND
AVIONICSHOT
FUELLOW
PARKBRAKE
LPPUMP
NOSEWHLSTR
FUELPRESS
C NRA G
OT U
ACCEL
ANTI-SKID
(d) OIL PRESS
WARNING/CAUTION LIGHT PANEL
(e) TAILPIPE HOT
(8-03) Original
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