Piper PA-32RT-300T User Manual

LANCE
II SERVICE
MANUAL
m.
Disconnect
the engine
oil temperature
lead
at the aft
end of the
engine.
n. Disconnect
the tachometer
drive
cable at
the engine.
o.
Untie the
ignition
harness
hoses and
lines at the
aft of the
engine.
p. Disconnect
the vacuum
pump
lines
at pump
and remove
fittings
from
pump.
q.
Disconnect
the oil
pressure line
at the
engine.
r. Disconnect
the static and
fuel flow
line at
the right rear
engine
baffle.
s. Disconnect
the manifold
pressure
line at
the right
rear side
of the
engine.
t.
Disconnect
the injector
line at
the flow
divider.
u. Disconnect
the alternator
leads
and the
cable attachment
clamps.
v.
Attach a
one-half
ton (minimum)
hoist
to the
hoisting
straps and
relieve
the tension
from
the
engine
mounts.
NOTE
Place
a tail
stand under
the
tail of
the airplane
before
removing
the
engine.
w. Check
the
engine
for any
attachments
remaining
to obstruct
its
removal.
x. Drain
the engine
oil, if desired,
and then
close drain.
y. Remove
the four engine
mount
assemblies
and swing the
engine free,
being careful
not to
damage
any attaching
parts.
8-14.
INSTALLATION
OF
ENGINE.
(Refer
to Figure
8-4.)
a.
Attach a one-half
ton (minimum)
hoist
to the engine
hoisting
straps and
swing the
engine
into alignment
with
its attaching
points.
b. Insert an
engine mount
bolt, with
washer against
head, in
the engine
mount and slide
half of
the mount
assembly
on the
bolt. (Refer
to
Figure 8-4
for proper
shock
mount
assembly.)
Repeat this
procedure
for the
other three
attachment
points.
NOTE
Shock
mount
Part
No. J-3049-38
sandwich
(17) must
be
positioned
on the compression
side
of the engine
lugs, with
the
upper mounts
on the forward
side,
and the lower
mounts
on the
aft side.
The part
number
is stamped
on
the metal
face
of the mount.
(Refer to
Figure 8-4.)
c.
Position
the mounting
lugs
of the
engine so
that they
align with
the
engine mount
attaching
points,
then move
the
engine rearward
onto
the mounts.
d. Slide
onto
each mounting
bolt
a spacer
and the
forward
half of
the mount.
Install
washer
and nut,
and torque
the nuts
of the bolts
to 450
to 500 inch-pounds.
e.
Connect
the alternator
leads
and
secure cable
with
clamps.
f. Connect
the injector
line to
the flow
divider.
g.
Connect
the manifold
pressure
line at
the right
rear side
of the
engine.
h. Connect
the static
and
fuel flow
line at the
right rear
engine baffle.
i.
Connect
the
oil pressure
line.
j. Install
the
line fitting
in the
vacuum
pump
and install
lines.
Issued:
1/3/78
POWER
PLANT
2A17

Piper PA-32RT-300T Specifications

General

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