RULES FOR NORTHWEST
SUPER SPORT RACE
New language in red,
deleted language in strikethrough
1. Purpose: It is
the intent that this event will serve as an
intermediate racing class between Northwest Sport
Race and the AMA racing events.
2. All pertinent rules from the AMA
control-line racing unified rules section shall
apply in regard to safety and the conduct of
races, except as follows.
3. Engine:
3.1 The
"engine" is defined as the complete unit, ready to
run, needing only prop, fuel and starting voltage,
except that the glow plug, venturi and/or
restrictor and spraybar and needle valve, gaskets,
bolts, drive washer, front washer, prop nut,
shims, piston ring(s) (if used), and ball bearings
(if used) need not be considered part of the
production unit. The glow
plug must have a thread dimension of 1/4x32. These parts
are not subject to the rules regarding quantity or
source.
3.2. No
tuned pipes or exhaust extensions are allowed
except bona fide mufflers which do not increase
engine performance. Engines shall operate on
suction feed. No variable or in-flight adjusting
carburetors are allowed; however, any other
modification of the intake is permissible except
as noted below.
3.3. Two
types Three
categories of engines will be allowed:
3.3.1. Engines
of .36 c.i.d. maximum with single bypass intake
port. These engines shall not be restricted in
regard to venturi dimension. There is also no
restriction regarding engine rework, except that
all major components shall be produced by the
original manufacturer. No material or part may be
added.
3.3.2. Any
engine currently legal in Northwest Sport Race
is allowed.
3.3.23 (a). Engines
of maximum total nominal displacement of 0.4020
cubic inches (6.6 cc). Engines must be production
units assembled from factory available production
parts. Engines and parts, with the exception of
the venturi-spraybar assembly, must have been
produced in quantities greater than 500,
and all must be available through normal retail
outlets in the U.S.A. Parts substitution shall
be limited to catalog listed parts produced in
quantities greater than 500 units for the engine
being altered and available commercially to
anyone from the manufacturer of the engine.
Engines may only be modified by removing parts or
material from parts. No material or part may be
added.
3.3.23 (b). The
engine must be of the front-intake, single-bypass
configuration. All air for the combustion process
must come through the crankshaft. Altering nominal
subport induction, timed holes in the case and the
sleeve, or other techniques to circumvent the
requirement that all air come through the
specified venturi opening, are prohibited.
3.3.23 (c). No
ABC or AAC piston/sleeve configurations are
allowed.
3.3.23 (d). Each
engine shall be equipped with a venturi and
spraybar meeting the following restrictions: The
venturi shall have an inside circular bore of not
more than 0.315 inch. The venturi will maintain
this diameter for at least 0.25 inch above and
below the spraybar centerline. The spraybar
assembly will be located precisely through the
centerline of the venturi bore and shall have a
circular cross section of diameter not less than
0.155 inch for the portion in the throat of the
venturi. Exception: R/C carburetors as originally supplied with the
engine may
be used with the opening fixed in one position.
3.3.23 (e). The
complete engine/venturi/spraybar system shall
weigh less than 10.5 ounces (excluding muffler).
4. Aircraft: The
model shall conform to the AMA slow rat
specifications:
"Models must be of profile fuselage type,
and must conform to the general profile
definition. The model must have a minimum fuselage
length of 24" when measured from the propeller
thrust washer face to the leading edge of the
movable elevator surface.
"The minimum wing area shall be 300 square
inches. The wing must have a minimum thickness of
one inch when measured at any point along the
span, with the exception of the last two inches
before each wing tip.
"All models must have a canopy, horizontal
stabilizer, elevator and vertical fin Models must
have a fixed landing gear with a minimum of one
wheel."
5. Fuel tank: The
fuel tank shall be fully external and forward of
the wing leading edge, and located on the outboard
side of the fuselage. The tank may not be designed
so as to cowl the engine. The tank may not be
pressurized, but the vents may be directed forward
into the airstream.
6. Pull test: The
plane and entire control system shall undergo pull
test of 35 pounds.
7. Lines: The
minimum diameter of lines shall be .018". Lines
shall be of the stranded type, with a length of 60
feet measured from the handle grip to the
fuselage, plus or minus 6" tolerance.
8. Races: Preliminary
heats shall be of 70 laps duration, with one pit
stop minimum required. The final or feature
race(s) shall be of 140 laps duration, with three
pit stops minimum required. All races shall be
flown with at least two entrants, and not more
than three entrants. At contests where entrants
fly preliminary heats to determine finalists, at
least three entries shall proceed to the final
race(s). The decision on the number of finalist
entrants shall be made by the event director and
be made before the start of any preliminary heats.
10/89/DC/jmt//Ed:jmt/4/15/93//rev/prop/mh/7/29/24
Existing
rules
RULES
FOR NORTHWEST SUPER SPORT RACE
1. Purpose: It is
the intent that this event will serve as an
intermediate racing class between Northwest Sport
Race and the AMA racing events.
2. All pertinent rules from the AMA
control-line racing unified rules section shall
apply in regard to safety and the conduct of
races, except as follows.
3. Engine:
3.1 The
"engine" is defined as the complete unit, ready to
run, needing only prop, fuel and starting voltage,
except that the glow plug, venturi and/or
restrictor and spraybar and needle valve, gaskets,
bolts, drive washer, front washer, prop nut,
shims, piston ring(s) (if used), and ball bearings
(if used) need not be considered part of the
production unit. These parts are not subject to
the rules regarding quantity or source.
3.2. No
tuned pipes or exhaust extensions are allowed
except bona fide mufflers which do not increase
engine performance. Engines shall operate on
suction feed. No variable or in-flight adjusting
carburetors are allowed; however, any other
modification of the intake is permissible except
as noted below.
3.3. Two
types of engines will be allowed:
3.3.1. Engines
of .36 c.i.d. maximum with single bypass intake
port. These engines shall not be restricted in
regard to venturi dimension. There is also no
restriction regarding engine rework, except that
all major components shall be produced by the
original manufacturer. No material or part may be
added.
3.3.2 (a). Engines
of maximum total nominal displacement of 0.4020
cubic inches (6.6 cc). Engines must be production
units assembled from factory available production
parts. Engines and parts, with the exception of
the venturi-spraybar assembly, must have been
produced in quantities greater than 500, and all
must be available through normal retail outlets in
the U.S.A. Parts substitution shall be limited to
catalog listed parts produced in quantities
greater than 500 units for the engine being
altered and available commercially to anyone from
the manufacturer of the engine. Engines may only
be modified by removing parts or material from
parts. No material or part may be added.
3.3.2 (b). The
engine must be of the front-intake, single-bypass
configuration. All air for the combustion process
must come through the crankshaft. Altering nominal
subport induction, timed holes in the case and the
sleeve, or other techniques to circumvent the
requirement that all air come through the
specified venturi opening, are prohibited.
3.3.2 (c). No
ABC or AAC piston/sleeve configurations are
allowed.
3.3.2 (d). Each
engine shall be equipped with a venturi and
spraybar meeting the following restrictions: The
venturi shall have an inside circular bore of not
more than 0.315 inch. The venturi will maintain
this diameter for at least 0.25 inch above and
below the spraybar centerline. The spraybar
assembly will be located precisely through the
centerline of the venturi bore and shall have a
circular cross section of diameter not less than
0.155 inch for the portion in the throat of the
venturi. Exception: R/C carburetors may be used
with the opening fixed in one position.
3.3.2 (e). The
complete engine/venturi/spraybar system shall
weigh less than 10.5 ounces (excluding muffler).
4. Aircraft: The
model shall conform to the AMA slow rat
specifications:
"Models must be of profile fuselage type,
and must conform to the general profile
definition. The model must have a minimum fuselage
length of 24" when measured from the propeller
thrust washer face to the leading edge of the
movable elevator surface.
"The minimum wing area shall be 300 square
inches. The wing must have a minimum thickness of
one inch when measured at any point along the
span, with the exception of the last two inches
before each wing tip.
"All models must have a canopy, horizontal
stabilizer, elevator and vertical fin Models must
have a fixed landing gear with a minimum of one
wheel."
5. Fuel tank: The
fuel tank shall be fully external and forward of
the wing leading edge, and located on the outboard
side of the fuselage. The tank may not be designed
so as to cowl the engine. The tank may not be
pressurized, but the vents may be directed forward
into the airstream.
6. Pull test: The
plane and entire control system shall undergo pull
test of 35 pounds.
7. Lines: The
minimum diameter of lines shall be .018". Lines
shall be of the stranded type, with a length of 60
feet measured from the handle grip to the
fuselage, plus or minus 6" tolerance.
8. Races: Preliminary
heats shall be of 70 laps duration, with one pit
stop minimum required. The final or feature
race(s) shall be of 140 laps duration, with three
pit stops minimum required. All races shall be
flown with at least two entrants, and not more
than three entrants. At contests where entrants
fly preliminary heats to determine finalists, at
least three entries shall proceed to the final
race(s). The decision on the number of finalist
entrants shall be made by the event director and
be made before the start of any preliminary heats.
10/89/DC/jmt//Ed:jmt/4/15/93
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