Piper SENECA III - Landing Gear Hydraulic System Schematic

PIPER
AIRCRAFT
CORPORATION
SECTION
7
PA-34-220T,
SENECA III
DESCRIPTION
&
OPERATION
RIGHT
MAIN
GEAR
LEFT
MAIN
G€AR
HYDRAULIC
CYLINDER
HyOAAU IC
cytlNDER
O
O
WN
DOWN
NOSE
GEAR
PRESSURE
SWITCH
RESTRICTOR
FREE
ALL
CONTROL
600
2000
PSI
RE$ERVO
UNTRE-
THERMAL
REMEF
4000
PSI
CONTROL
660±hõO
PSI GEAR
UP
CNfcMVALVE
DELivERED
PRE5$
400-800 PSI
LANDING
GEAR
HYDRAULIC
SYSTEM
SCHEMATIC
Figure
7-7
ISSUED:
JANUARY
8, 1981
REPORT: VB-1110
7-9