Piper PA-32RT-300T User Manual

LANCE
II
SERVICE
MANUAL
0.0050.020
Figure
8-19.
Stop
Pin
Installation
Dimension
e. Do
not
tighten
puller
handle
further
after
coupling
cam releases
from
the shaft.
This
could
damage
the flyweight
if the
flyweight
is
caught
under
the woodruff
key.
Remove
the
puller
from the
shaft.
Then
while
holding
both flyweight
tips inward,
left
cam
from the
shaft,
and
remove
woodruff
key
from
rotor
shaft.
8-33.
INSPECTION
OF
IMPULSE
COUPLING.
a.
Check
clearance
between
each
flyweight
and
each
stop
pin by
the
following
method:
1.
Bend
the end
of a
stiff piece
of
wire into
a right
angle,
1/8
inch long
maximum.
2. Hold
the
magneto
as shown
in Figure
8-18.
Pull the
heel
of
the flyweight
outward
with the
fabricated
hooked
wire
and
make
certain
that
a feeler
gauge
of 0.015
of
an
inch
minimum
thickness
will
pass between
the
stop pin
and
the highest
point
of the
flyweight.
NOTE
A true
and accurate
check of
the clearance
between
the
flyweights
and
stop
pins can
only
be obtained
by pulling
the
flyweight
outward
as described.
Do not
attempt
the check
by
pushing
in on
the flyweight
at
point
"A" of
Figure
8-18.
b. Inspect
impulse
coupling
stop
pins
for damage.
If pins
are bent,
damaged
or
excessively
worn,
remove
pins
using
a suitable
drift
and
arbor
press.
Press
new
pins
into
flange
until dimension
shown
in Figure
8-19
is obtained.
c.
Visually
inspect
flyweight
securing
washers
and
flyweights,
particularly
in area
around
the axle
hole
for cracks.
Grip
washers
with pliers
and
exert
moderate
turning
force
to
check
looseness.
If washer
moves
or any
cracks
are found,
reject
cam
assembly.
Issued:
1/3/78
POWER
PLANT
2B12

Piper PA-32RT-300T Specifications

General

Brand	Piper
Model	PA-32RT-300T
Category	Aircrafts
Language	English