Introduction to T-45C Configuration
T-45C TS, ADV & IUT ENG-01
3.
Control location: throttle quadrant and associated
starting and fuel control switches--left consoles, both
cockpits
PROGRESS CHECK
Question 3 — 1.4.6.3.1.1
ANSWER: 7 stages
C.
Fuel system 1.4.7.3.1.1
Sg 3, fr 5
Fig 4: T-45C Fuel
System Diagram
FUSELAGE
FUEL
TANK
SHUTOFF VALVE
BOOST
H P FUEL
L P FUEL
INTEGRAL WING TANK
PUMP
PUMPS
PUMP
GTS
443 GAL. (3012 lbs.) TOTAL
427 GAL. (2904 lbs.) USABLE
MANUAL
FUEL CONTROL
THROTTLE
FUEL SYSTEM
UNIT
ENGINE
Figure 4: T-45C FUEL SYSTEM DIAGRAM
1.
Description: 443-gal internal fuel supply carried in
fuselage tank and integral wing tank
2.
Function
a.
Pressure-fed with boost pumps assist to ensure
fuel supply is uninterrupted under negative-g
conditions
Page 1-10
(9-98) Original
Previous Page
