T-45A UJPT, E2-C2, ADV, & IUT Eng-26
Engineering Review
iii)
Provides system pressure
relief caused by system
heat
(b) Physical: multi-valve package
consisting of:
i)
Priority valve
ii)
A pressure relief valve
iii)
Two check valves
C.
HYD 2 description:
The HYD 2 reservoir supplies fluid to the HYD 2
EDP, which produces hydraulic pressure to
power the ailerons and stabilator
D.
HYD 2 components
1.
EDP
a.
Location: forward left side of engine
accessory gearbox
b.
Description: identical to HYD 1 pump,
except supplies power to HYD 2
system
2.
Reservoir
a.
Location: RAT bay, top side of aircraft,
forward of tail section
b.
Description: similar to HYD 1 reservoir,
has less capacity
3.
FC accumulator
a.
Location: left intake above wing
b.
Description: identical to HYD 1
accumulator
Page 26-24
(8-03) Original
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