Piper Lance II User Manual

LANCE II SERVICE MANUAL
4.68
1.50
TORQUE-
15-23 Ft. Lbs.
4PLCS
THIS
END
FOR
HORIZONTAL 1.50R
MOUNT
NOTE; 12 NOTCHES 1/8 INCH
APART
STARTING AT EACH END. 1.5O
THIS END FOR
VERTICAL
OIL CHECK
PLUG
MOUNT
(TYPICAL TWO SIDES)
Figure
14-9.
Compressor
And Fabricated
Oil Dipstick
14-22. REPLACEMENT
OF COMPRESSOR AND/OR
ALTERNATOR DRIVE BELTS.
(Refer to Figure 14-10.)
a. Remove the old belts by removing the spinner, propeller, nose cowl, engine baffles
as required, starter reing gear assembly and drive belts.
b. Place the new
belt or belts in their appropriate positions
on the starter ring gear
sheaves.
c. Reinstall the starter ring gear assembly, propeller and spinner.
d. Route
the belts to the proper pulley
sheaves as shown in Figure 14-10.
CAUTION
Do not force the belts into the pulley sheaves. Remove the
idler
assemblies, if necessary,
and the alternator
lower
mounting bolts in order to install the belts.
e. Check the belt and pulley alignment
of the compressor and/or
alternator by the
following
method:
1. A datum
line must be established for checking
belt and pulley alignment.
A
nominal
dimension must be established between
the forward edge of the compressor
belt
and
the forward machined surface of the
ring gear. This dimension should be taken
at the
ring gear assembly where the belt
is in its sheave. The amount of misalignment
can then be
determined
at the other pulley sheaves by using
a stiff straightedge of sufficient length
to
extend from
the front of the ring gear
to the component sheaves.
NOTE
Insure adequate ring gear surface contact to provide a solid
base for the straightedge.
Issued: 1/3/78 ACCESSORIES AND UTILITIES
2K13

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