T-45A UJPT, E2-C2, ADV, & IUT Eng-05
Fuel System
(2) Wing ribs with holes provide
transfer and baffling
(3) Fuel drain valves on underside of
wing
(4) Water drain valves on underside
of wing negative-g compartment
(5) Capacity: approximately 223
gallons (1,540 lb), including collec-
tor tank with negative-g compart-
ment
3.
Collector tank
Overlay 3
Collector Tank
a.
Location: center compartment of the
wing tank
b.
Physical description
(1) Separated from wing tank by
diaphragms
(2) Spring-loaded check valve on
each side permits fuel flow from
the wing tank
(3) Capacity: 60 gallons (approxi-
mately 400 lb), including negative-
g compartment
c.
Functional description: sump into
which fuel feeds from wing tank
4.
Negative-g compartment
Overlay 4
Negative-G Compartment
a.
Location: forward part of the collector
tank
b.
Physical description
(1) Bounded by front spar
(8-03) Original
Page 5-5
Previous Page
