Piper Lance II User Manual

1
2
4
5
6
7
1. SAFETY
WIRE
2.
END
GLAND
3.
"O"
RING
4. "O"
RING
5. PISTON
6.
BODY,
CYLINDER
7.
"O"
RING
Figure
6-7.
Nose
Gear
Actuating
Cylinder
CAUTION
Whenever
aircraft
is
placed
on
jacks
for
the
purpose
of
manually
retracting
the
nose
gear
assembly,
insure
the
nose
gear
downlock
is
fully
disengaged
before
releasing
the
nose
gear
drag
links.
Damage
could
occur
to
the
downlock
if not
disengaged
fully.
d.
Disconnect
the
aft
end
of
cylinder
from
its
attachment
fitting
and
remove
the
cylinder
from
the
wheel
well.
6-17.
DISASSEMBLY
OF
NOSE
GEAR
ACTUATING
CYLINDER
(Refer
to
Figure
6-7.)
a.
With
the
cylinder
removed
from
the
airplane,
mark
the
position
of
the
end
gland
(2)
to
facilitate
reinstallation.
b.
Remove
safety
wire
(1)
and
unscrew
end
gland
(2).
c.
Additional
disassembly
of
piston
(5)
and
"O"
rings
(3),
(4)
and
(7)
may
now
be
accomplished.
Issued:
1/3/78
HYDRAULIC
SYSTEM
LANCE
II SERVICE
MANUAL

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