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  9. SCORPION Super Stinger 1975 User manual

SCORPION Super Stinger 1975 User manual

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~···-
io·
1975
Scorpion
Super
Stinger
Service
Manual
Engine
Section
1
SERVICE
MANUAL-
1975
SCORPION
SUPER
STINGER
ENGINE
SYSTEM
Functional
Description:
2-CYCLE ENGINE FUNDAMENTALS
The
Rockwell
2-cycle
air
-
coo
l
ed
gasoline
engine,
particularly
the
axial
fan-cooled
twin
cylinder
engine,
has
become
very
popular
today
for
snowmobiles.
It
is
uniquely
qualified
for
this
ap-
plication
because
of
its
high
power
output,
light
weight
and
ease
of
lubrication,
with
fewer
moving
parts
than
other
conventional
2-cycle
and
4
-c
ycle
engines.
However,
in
order
to
get
the
best
possib
le
use
and
ensure
that
it
retains
its
high
degree
of
dependability
and
endurance,
it
must
receive
proper
care
and
maintenance.
Therefore,
it
is
necessary
for
us
to
know
something
about
the
basic
fundamentals
of
.
this
engine
and
how
it
functions.
OPERATION
The
Rockwell
2-cycle
Twin
Cylinder
engine
is
of
the
loop-scavenged
third
port
type,
the
most
wide
ly
used
design
today.
It
uses
a
mixture
of
gasoline,
oi
l
and
air
for
combustion,
lubrication
and
cooling.
It
fires
on
every
stroke
of
each
piston.
There
ore
two
power
strokes
for
every
revolution
of
the
crankshaft.
As
the
piston
moves
upward
in
the
cylinder
it
draws
the
fuel/air
mixture
into
the
crankcase
through
the
intake
manifold
while
at
the
same
time
compressing
fuel
that
has
been
forced
into
the
combustion
chamber.
See Fig.
1-1
A.
As
the
piston
nears
top
dead
center
the
spark
plug
is
fired
and
the
compressed
fuel/air
mix-
ture
burns
and
expands
thereby
forcing
the
piston
downward
on
a
power
stroke.
As
the
downward
stroke
of
the
piston
turns
the
crankshaft,
it
also
starts
to
compress
the
fuel/air
mixture
in
the
crankcase
and,
simultaneously,
opens
the
exhaust
port
and
cl
oses
the
intake
port.
See
Figs. 1-1 B &
C.
1-2
I
NTAKE
0
EXH/UST
TRANSFER
FIG.
1-1
SERVICE
MANUAL· 1975
SCORPION
SUPER
STINGER
After
the
exhaust
port
is
fully
open
and
the
in-
take
port
is
fully
closed,
further
piston
travel
starts
to
open
the
transfer
ports.
The
com-
pressed
fuel/air
mixture
from
the
crankcase
then
travels
up
the
transfer
ports
and
into
the
combustion
area.
After
most
of
the
burned
exhaust
gases
have
left
the
cylinder,
an
incoming
charge
of
fuel/air
mixture
scavenges
the
combustion
area
giving
it
a
fresh
charge
and
the
cycle
is
then
repeated.
SeeFig.l-1
D.
Because
lubrication
is
dependent
on
the
m1xmg
of
oil
and
fuel,
it
is
extremely
important
that
good
quality
oil
and
gasoline
are
properly
mixed.
The
proper
ratio
of
oil
to
gasoline
will
prevent
possible
engine
overheating,
piston
or
cylinder
scoring,
or
eventual
engine
seizure.
Too
much
oil
and
not
enough
gasoline
can
lead
to
incomplete
combustion,
fouled
plugs,
carbon
build-up
and
muffler
clogging.
l-3
SERVICE
MANUAL·
1975
SCORPION
SUPER
STINGER
EXHAUST
SYSTEMS
SELECTION
Selection
of
an
exhaust
system
(including
exhaust
manifold,
intermediate
pipes,
elbows
and
muffler),
is a
result
of
thorough
test
procedures
involving
measurement
of
fuel
con-
sumption,
horsepower
and
noise
level.
Contrary
to
popular
belief,
the
exhaust
system
is
not
only
for
quieting
the
engine,
but
also
serves
to
in-
crease
horsepower
output
(by
as
much
as
25%).
Changes
made
to
the
original
equipment
exhaust
system
by
changing
any
component
in
the
system
can
result
in
loss
of
power
and/or
severe
engine
damage.
For
these
reasons,
intermediate
lengths
of
pipe
between
the
cylinder
and
the
muffler
are
particularly
critical.
TUNED MUFFLERS
Tuned
mufflers
allow
the
engine
to
exhaust
its
spent
charge
int
o
an
adequate
volume
and
properly
matched
muffling
system.
More
im-
portant,
the
mufflers
that
are
tuned,
incorporate
designs
that
suck
the
exhaust
gas
from
the
cylin-
der
allowing
fuel
and
air
to
rapidly
replace
it
and
also
"cram"
over-scavenged
fuel
and
air
mixture
from
the
exhaust
pipe
back
into
the
cylinder
using
sound
waves
and
sound
energy.
This
is
ac-
complished
at
the
speed
of
sound
which
allows
the
engine
to
produce
higher
torque
at
higher
RPMs.
1-4
Donaldson
FIG.
1·2
n
Tuning
Courtesy
of
Dona
l
dson
Muffler
Co
)
FIG.
1·3
SERVICE
MANUAL·
1975
.SCORPION
SUPER
STINGER
HOW
TUNING
WORKS
The
megaphone
effect
of
the
expanded
intake
tube
scavenges
exhaust
gas
from
the
cylinder
allowing
rapid
replacement
of
the
fuel/air
mix-
ture
from
the
crankcase.
Reflected
sound
waves
and
sound
energy
stop
over-scavenging
and
return
fuel/air
mixture
to
the
cylinder.
It
gives
a
supercharging
effect
even
though
it
operates
from
the
exhaust
rather
than
the
intake
side.
Over-scavenging
is
also
retarded
by
moderate
muffler
back
pressure.
Silencing
is
accomplished
after
power
is
maximized
by
acoustical
packing
in
the
resonator
outlet
tube
plus
chambering
and
baffling
which
gives
an
effective
2-pass
muffler
design.
1·5
SERVICE
MANUAL-
1975
SCORPION
SUPER
S
TING
ER
TABLE OF
SPECI
FICATIONS
ENGINE MODEL
DESCR
IPTION 2F
440-
3 2F
400
-8 2F
440-8
2.
658"
2.559"
2.
658"
BORE
(67.5mm)
(
65.0mm)
(67.5mm)
J
STROKE
2.362"
(60mm)
DISPLACEMENT IN cc
428
398
428
COMPRESSION RATI
ON
(actual)
12.5:1 12:1 12:1
I
GNITION
SYSTEM Bosch
Flywhe
el
Magneto
LIGHTING COIL
VOLTAGE
AND
OUTPUT
12V
75W
1
2V
150W
12V
150W
*TIMING
BEFORE
TDC
(CENTRIFUGAL .
102
-
.112
.102-.112
.1
02-
.
112
WEIGHT
ADVANCED)
TIMING
BEFORE
TDC (CENTRIFUGAL .0
18"
to
.
020"
.018
"
to
.020"
.0
18"
to
.020"
WEIGHT RETARDED)
BREAKER POINT
GAP
.014"to
.01
6"
SPARK
PL
UG THREAD
14mm.
x 1
.25
-
3/
4"
reach
.020"
.
020"
.020
"
SPARK PLUG
GAP
(0.
5mm
.)
(0.5mm.) (0.5mm.)
SPARK PLUG-BOSCH
(ORIGINAL
W260T2
W260T2
W260T2
EQUIPMENT)
TYPE
OF
ENGINE
COOLING
Axia
l Fl
ow
Fan
ROTA
TION
OFCRANKSHAFT
Counterclockwise
(PTO
side)
CARBURETOR
Wa
l
bro
FUEL/OIL RA
TI
O
As
Specified
on
Scorpion
Oil
Conta
i
ner
GASO
LI
NE
95
octane,
mini
mum
(lead
free
not
accep
t
ab
l
e)
TYPE
OF
O
IL
Special 2-Cycle
Snowmobi
le
Oil
*
Do
no
t
exceed
indicated
advance,
as
this
will
result
m
severe
engme
damage.
1-6
0
TORQUE SPECIFICATIONS
CYLINDER HEAD NUTS
CYLINDER B
ASE
NUTS
FlYWHEEL NUT
INTAKE
MANIFOLD
NUTS
FAN
HOUSING
SCREWS
FAN
WHEEL NUT
RING GEAR
SCREWS
(6mm.)
RING GEAR
SCREWS
(8mm.)
SERVICE
MANUAL-
1975
SCORPION
SUPER
STINGER
TABLE OF SPECIFICATIONS
-8 -9 2F-
440-3
2F-400-6 2F-440-5
19 28
to
32
ft./lbs.
16
to
18
ft./lbs.
44
to
50
ft./lbs.
56
to
72
ft./lbs.
56
to
72
ft./lbs
.
16
to
18
ft./lbs.
16
to
18
ft./lbs.
22
to
24
ft./lbs.
6
to
7
ft./lbs.
not
applicable
not
applicable
10
to
12
ft./lbs.
not
applicable
10
to
12
ft./lbs.
Tightening
Sequence
for
Cylinder
Base
Nuts
0 0 8 0
PTO
SIDE
0
G)
0 8
Tightening
Sequence
for:
Cylind
er
Head
Nuts,
Fan
Housing,
Ring
Gear
Flange,
Intak
e
Manifold
and
Recoil
Starter
Clamps
0
8 0 0
'74-
'75
'74
-
'75
®
290s
400s
340s
440s
AI
I
previous
G)
models
®
0 0
CD
1-7
SERVICE
MANUAL
-
1975
SCORPION
SUPER
STINGER
ROCKWELL
TWIN
CYLINDER ENGINES
MODELS 2F-400-.8
DISASSEMBLY
2F-440-8
A.
Recoil
Starter
Remove
four
(4)
screws
holding
the
recoil
assembly
to
the
fan
housing.
See Fig. 1-4.
See
pages
1-
28
A,
B,
C
for
recoil
starter
disassembly.
B.
Lower
Fan
Pulley
and
Carrier
Assembly
l-8
Remove
the
three
(3)
hex
head
bolts
on
the
carrier.
Remove
carrier,
lower
pulley
assembly
and
V-belt.
See Figs. 1-5, 1-6.
FIG. 1-4
A
(.:
FIG. 1-5
FIG. 1-6
c
SERVICE
MANUAL
· 1
975
SC
ORPION SU
PER
S
TI
NGER
C.
Upper
Fan
Belt
Pulley
Assembly.
Insert
a
3/
16"
dri
ll
or
a
suitable
punch
through
the
indexing
hole
into
the
im-
pe
ll
er
body.
With
a
17
mm
socket
wrench,
remove
the
fan
nut
,
lock
washer
,
pulley
halves
and
spacers.
See
Figs. 1-7
,1
-8,1-9.
FIG. 1-8
FIG. 1-7
FIG. 1-9
1·9
SERVICE
MANUAL
-
1975
SCORPION
SUPER
STINGER
D.
Flywheel
Magneto
Remove
the
crankshaft
nut
using
a
27
mm
socket
wrench
.
Pull
th
e
flywheel
by
attaching
flywheel
puller
444-31-8
43
-2
to
the
flywheel
flange
using
bolts
provided.
Screw
the
three
bolts
through
the
puller
into
the
flange
and
tighten
evenly.
With
a
socket
wrench,
tighten
the
puller
bolt
until
the
flywheel
loosens
on
the
crankshaft.
See
Figs.
1-10,
1-11, 1-12, 1-
13.
FIG. 1-12
NOTE:
It
is
important
that
care
is
taken
to
remove
the
positioning
key
in
crank-
shaft
before
attempting
to
remove
the
flywheel
assembly.
Failure
to
do
this
could
result
in
damage
to
advance
mechanism.
1-
10
()
FIG. 1-10
Q.
FIG. 1-11
FIG. 1-13