Piper Lance II User Manual

LANCE II
SERVICE MANUAL
e.
To check operation
of gear
back-up
extender actuator,
refer
to Paragraph
6-14 for
Check
and Adjustment
Procedures.
6-30.
SERVICING
HYDRAULIC
PUMP/RESERVOIR.
The fluid
level of the
reservoir of
the combination
pump
and reservoir
should be
checked every
50 hours by
viewing the
fluid
through the
filler plug
hole in the
hydraulic pump.
Access to
the pump is
through the
panel
at the left side of forward
baggage compartment.
To check fluid level, remove the
filler plug located on the forward side
of the pump and
ascertain that
fluid is within 1/2 inch of the bottom
of the filler plug hole. Should fluid
be
below this level, add fluid,
MIL-H-5606A, through the filler hole.
Reinstall the filler plug
and tighten.
NOTE
A
small vent hole
is located
under the vent
screw head.
Retain
1/64 inch clearance between
the screw head and
the small
vent hole.
THIS SPACE INTENTIONALLY LEFT BLANK
Issued:
1/3/78
HYDRAULIC SYSTEM
1113

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