TM 55-1730-229-12
AG 320A0-OMM-000
TO 35C2-3-473-1
TM 1730-12/1
ELECTRICAL CONNECTOR, P16
HYDRAULIC MODULE
1.
9.
PUMP FITTING
2.
FRONT PANEL ASSEMBLY
10.
BOLT
11.
HOSES
3.
HYDRAULIC PUMP
12.
NUT
4.
WASHER
SPACER
13.
5.
GEARCASE PAD
DRAIN TUBE
14.
6.
GROMMET
STORAGE BRACKET
15.
7.
8.
ENGINE COMPARTMENT
Hydraulic Module, Pump, Lines and Hoses
cates that the hydraulic fluid is at
(1) As seen on figure FO-10,
the minimum temperature for operation.
hydraulic fluid from the AGPU reser-
Sensors TS2 and TS3 illuminate 1600F
voir is routed through a reservoir
If hy-
and 2400F indicator lights.
selector valve and passes four tem-
fluid reaches 275OF, TS4
perature sensors to the hydraulic
draulic
activates to illuminate HI TEMP light.
The temperature sensors (TS1
pump.
Activation of TS4 also interrupts the
through TS4 on figure FO-9) are set
circuit to the load valve pilot sole-
to close at various temperatures.
The
noid, and shuts down hydraulic power to
70F sensor (TS1) causes SYSTEM READY
aircraft.
This indi-
light DS5 to illuminate.
