T-45C TS, ADV & IUT ENG-07
Aircraft Fuel System
I.
Aircraft fuel system major component identification 1.4.7.3.1
Sg 1, fr 2
Lesson Organization
A.
Fuel tanks
FUEL SYSTEM
NOTE: The T-45C has a total fuel capacity of 443 U.S.
* Major component
gallons rated at 3012 lb JP-5 total (2904 lb JP-5,
identification
2776 lb JP-4, JP-8 2861 usable).
* Operational characteristics
* Controls, switches, and
1.
Fuselage tank
indicators
* Aircraft interfaces
a.
Location: between the two engine intakes, just
aft of the cockpit
Sg 1, fr 4
(10 Overlays)
Fig 2: Aircraft Fuel
b.
Physical description
System Block Diagram
(1) Baffled, rubberized bag tank, hung inside
fuselage (not a self-sealing tank)
Overlay 1
Fuselage Tank
(2) Fitted for plumbing connections
(a) Gravity filler cap
(b) Pressure control valve
(c) Vent/pressurization lines
(d) Fuel transfer lines
(e) Capacitance-type fuel quantity
indicating system
(3) Capacity: approximately 220 gallons
(1500 lb)
2.
Integral wing tank
Overlay 2
Integral Wing Tank
a.
Location: Between the front and rear spars on
each side of the center line
b.
Physical description
(1) Formed by wing surface above and below
(wet wings and is not a self-sealing tank)
Original (9-98)
Page 7-4
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