Piper Lance II User Manual

LANCE
II
SERVICE
MANUAL
The
following
list of
material
were
use
d
In making
the balancer:
.1
I I. Base
12 x 11
0.10 2024
T3 clad
aluminum
alloy
-2
2
. Toe
2.
x xll
0.190
2024
T4
extruded
aluminum
alloy
-3
2 ea.
Sid
14
x 11
0.12
2024
T3
clad
aluminum
alloy
-4
1 . Axie
0.125
x 10.25
4130
steel,
normalized
4 2 .
Nuts AN
365424
4 2
ea. Spacer
0.50
x 2.25
50524
aluminum
tubing
2
ea. Spacer
050
x 1.25
50524
aluminum
tubing
-7
2
ea.
Bushing
1.480
x
1.625
x
1.00
Richillant,
phenoiic
or
aluminum
2 ea.
Bushing
2.240
x 1.37
x
1.00
Richlight.
pheonoiic
or
aluminum
-4
1
Pipe
1/0 x
9 3
black
steel
pipe
2
. Bearings
Save
two
of
each
size worn
wheel
bearings
from
previous
inspection.
Figure
2-9a.
Tire
Balancer
Added:
9/2/78
1C5
HANDLING
AND
SERVICING

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