Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
FILTER
RESERVOIR
LOW PRESSURE
CONTROL
650 150 psi
SHUTTLE
VALVE
DELIVERED
PRESSURE
400
to 800
psi
HIGH
PRESSURE
CONTROL
/
2000 to
2500
psI
THERMAL
RELIEF
2250
+
250
psi
GEAR
UP
CHECK VAL
VE
DIFFERENTIAL
PRESSURE
SWITCH
OFF
at
1400
+
100
ps
ON at
200 to
400 psi
I
1
a
Figure
6-1.
Schematic
Diagram
of
Hydraulic
System
Revised 6/15/79
HYDRAULIC
SYSTEM
1H16

Piper Lance II Specifications

General

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers