Piper PA-32RT-300T User Manual

LANCE
II SERVICE
MANUAL
TABLE
VIIA-I.
PROPELLER
SPECIFICATIONS
Hub, Model
Blade,
Model
Diameter
Blade
Angle
Propeller
RPM
Setting
HC-E2YR-1B
F
F8477(
)4
80 in.
Low
Pitch
(High
RPM)
High
Pitch
(Low
RPM)
Engine
Static
High
RPM
Description
15.6
± 0.2
°
(
1)
34.0
°
1.0
()
2700
RPM
max.
Required
Torque
(Dry)
60-70
foot-pounds
20-25
inch-pounds
20-22
foot-pound
Propeller
Torque
Limits
I
Propeller
Mounting
Nuts
Spinner
Attachment
Screws
Propeller
Bulkhead
Attachment
Bolts
(1)
MEASUREMENT
TAKEN
AT
30
INCH
RADIUS
d.
Observe
the
starter
ring
gear
to
make
sure
it is
mounted
properly
on
the
engine
crankshaft
flange.
One
of
the
bushings
on
the
crankshaft
is stamped
with
an
"O"
mark
and
it must
be
inserted
in the
starter
ring
gear
hole,
likewise
identified
with
an
"0"
mark.
e.
Wipe
crankshaft
and
propeller
pilot
to
assure
that
no
chips
or
foreign
matter
enter
the
propeller
mechanism.
f.
Check
interior
of
propeller
hub
for
proper
seating
of
"0"
ring.
Wipe
inside
of
hub
to
remove
any
traces
of
dirt.
Check
to
see
that
"O"
ring
is covered
with
grease.
g.
Install
rear
spinner
bulkhead.
h.
Apply
a
generous
brush
coating
of
EC776
adhesive
to
the
entire
circumference
of
propeller
hub
for
distance
as
shown
in
Figure
8A-1,
Sketch
A.
NOTE
EC776
adhesive
coating
can
be
purchased
through
the
Minnesota
Mining
and
Manufacturing
Company,
St.
Paul,
Minnesota.
NOTE
Propeller
hub
must
be
clean,
dry
and
free
from
oil
or
grease.
Revised:
9/2/78
POWER
PLANT
-
TURBO
2C13

Piper PA-32RT-300T Specifications

General

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