Landing Gear Hydraulic System Schematic - Piper SARATOGA II HP PA-32R-301 Pilot Operating Handbook

PA-32R-301, SARATOGA II HP
•
NOSE
GEAR
UP
t
0
LOW
PRESSURE
CONTROL
\
MAIN
GEAR
UP
RESTRICTOR
NIPPLE
t
RESERVOIR
0.020 DIA.
BLEED HOLE
t
SECTION7
DESCRIPTION
&
OPERATION
HIGH PRESSURE CONTROL
I
/ERMAL RELIEF
PRESSURE
SWITCH.
GEAR DOWN
EMERGENCY
FREE FALL
VALVE
LANDING GEAR HYDRAULIC SYSTEM SCHEMATIC
Aircraft equipped with Oildyne pump and cable emergency gear release
Figure 7-7
ISSUED: JUNE 30,1997 REPORT: VB-1669
7-23