Piper Lance II User Manual

LANCE
II
SERVICE
MANUAL
A341
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2
3 4
5
7 8
9
10 11
12
13
14
15
00
1.
HOUSING
.
PISTON
11.
SNAP
RING
2. SNAP
RING
7. YNA
SEAL
12. ROD,
PISTO
-—'
3.
BUSHING,
RETAINER
.
"O"
RING
13.
SPING,
RETAINING
4. SPRING
.
GLAND PACKING
14.
ROLL PIN
5.
"O" RING
10.
"O" RIN*
1S.
WASHER
Figure
7-19.
Brake
Master
Cylinder.
(Hand/Parking
Brake.)
7-62.
DISASSEMBLY
OF
BRAKE
MASTER
CYLINDER.
(Refer
to
Figure
7-19.)
a. Remove
the
cylinder
from
its mounting
bracket
as per
paragraph
7-61.
b.
To disassemble
the
cylinder,
first remove
the piston
rod assembly
by removing
the
snap
ring
(11) from
the
annular
slot at
the rod
end of
the cylinder.
Draw the
piston
rod
assembly
from
the
cylinder.
c.
The
piston
rod assembly
may
be
disassembled
by
first
removing
the small
snap
ring
(2)
securing
the retainer
bushing
(3), spring
(4),
piston
(6), seal
(7),
gland
(9), and,
if
desired,
the
large
return
spring
(13).
d.
Remove
the "O"
rings
from
the piston
and
gland.
7-63.
CLEANING,
INSPECTION
AND
REPAIR
OF BRAKE
MASTER
CYLINDER.
a. Clean
the cylinder
parts with
a suitable
solvent
and dry
thoroughly.
b. Inspect
the interior
walls of
the cylinder
for scratches,
burrs,
corrosion, etc.
c.
Inspect the
general
condition
of the fitting
threads
of the
cylinder.
d. Check
the piston
for scratches,
burrs, corrosion,
etc.
e.
Repairs to
the cylinder
are limited
to polishing
out small
scratches, burrs,
etc., and
"O" rings.
Issued:
1/3/78
LANDING
GEAR
AND
BRAKE
SYSTEM
1L8

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