Landing Gear Hydraulic System Schematic - Piper SENECA III Pilot's Information Manual

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