QMARA COMPETITION CLASSES & RULES 2008
QUICKIE
500 / SID RULES
Engine
The engine must be a commercially available, front-intake, side-exhaust. The
engine shall be stock, except for modifications as listed below.
Displacement
Maximum displacement is 7.6cc (0.46 cubic inches).
Exhaust System
The engine shall be equipped with an expansion chamber muffler or zero-boost
muffler as provided by the engine manufacturer for that particular model.
The muffler shall be stock, except for modifications as follows:
(a) Replacement of bolts, or screws and welding or gluing to improve reliability
is permitted.
(b) The muffler may be tapped for a pressure fitting to supply pressure to the
fuel system.
Tuned mufflers and tuned pipes are prohibited.
Intake
The carburettor as supplied by the manufacturer shall be used and must be
capable of reducing the engine speed to idling. The carburettor and any
associated remote needle valve shall be stock, except for longevity-enhancing
modifications as follows:
(a) Adjustment screws and idle needle valves may be held in place with
commercially available thread locker, epoxy, or other adhesives and safe tied
with rubber bands, wire, or plastic ties.
(b) Barrel retaining screws or pins may be replaced with commercially available
screws or pins of harder material and may be held in place with commercially
available adhesives. Barrels may be de-burred for smoother movement and may be
safe tied with rubber bands, wire, or plastic ties.
(c) Throttle arms may be modified or replaced.
Fuel Feed
Other than muffler pressure, no fuel system pressurization is permitted.
Modifications
The following parts may be substituted for the original engine parts and may
come from any source:
Backplate mount (provided the crankcase volume is not varied)
Bearings
Gaskets
Glow plug
Head and crankcase bolts
Propeller nut (spinners may be used)
Propeller washer
The head clearance of the engine may be altered from the manufacturer's setting
by adding or removing head shims.
Approved Engine List
Sample engines are tested and a list of permissible engines is published
annually by the relevant pylon racing governing bodies. Criteria include
purchase price and power output in both the normal takeoff rpm range and the
presumed in-air ("unloaded") rpm range. See Annex 1 for current engine approval
list.
Wings
Area
Minimum 3225 cm2 (500 square inches).
Wing Span
Minimum 1270mm (50 inches), maximum 1321mm (52 inches) projected.
Chord
Constant for at least 1207mm (47-1/2 inches) of span.
Airfoil Thickness
Minimum 30mm (1-3/16 inches) for at least 1207mm (47-1/2 inches) of span.
Fuselage
Depth
Minimum 89mm (3-1/2 inches) at its deepest point, which must occur within the
wing chord.
Width
Minimum 73mm (2-7/8 inches) at its widest point, which must occur within the
wing chord. Width and depth points need not coincide.
Cross Section
The fuselage shall have a simple, rectangular "box" cross-section with a maximum
radius of 6.5mm at the corners. Diamond-shaped cross sections are prohibited.
Fillets or fairings between the fuselage and wing are prohibited. Canopies and
turtle decks are acceptable but shall not be included in width or depth
measurements. The front firewall shall be a rectangular, flat plate measuring at
least 57mm by 57mm inches. The perimeter of the front firewall may be rounded to
a maximum radius of 6.5mm.
Engine Installation
The engine and engine mount shall be fully exposed. No cowling or streamlining
of the engine is permitted. A back plate type radial engine mount that replaces
the stock engine back plate may be used so long as it displaces the same
crankcase volume as the stock back plate assembly. Corners and edges of the
engine mount may be rounded to a maximum radius of 6.5mm.
Weight
The weight of an assembled aircraft, ready for flight, but less fuel shall be a
minimum of 1580grams (3-1/2 pounds) and a maximum of 2040grams (4-1/2 pounds).
Amendments for Queensland Airframe Rules see Annex 2.
Landing Gear
The landing gear shall be fixed, with at least 2 main wheels of a diameter not
less than 57mm. The main wheels shall be at least 178mm apart, measured parallel
to the wing span. No wheel pants, wheel spats, or strut fairings shall be used
to streamline the main landing gear. Struts shall be either round wire, at least
3mm in diameter, or flat stock no more than 3mm thick. Flat stock may be filed
or otherwise shaped to an airfoil cross-section but must have a blunt leading
edge. Nose or tail wheels, if used, may be streamlined or enclosed.
Propeller
Material
APC composite or a similar commercially available composite.
(14/5/06 Suggest change this sentence to : Propellers shall be made from glass
fibre reinforced nylon by an injection moulding process.)
Propellers containing continuous filament carbon fibre are not permitted.
Dimensions
Minimum diameter 10 inches. Nominal pitch 6 inches, as indicated by the
manufacturer's stamp or packaging.
Modifications
Propellers shall be stock and commercially available. One blade may be modified
for balancing.
Fuel
The organisers shall supply fuel to a standard formula for glow plug motors
containing 80% methanol and 20% castor oil.
Special Provisions
Inspections
Routine inspections are encouraged: The CD or the CD's designee may elect to
check the top 3 finishers engines for legality at the end of the contest.
Rule Variations
The engine rules specified have been used to limit the cost and power output of
engines used in this event. Any variations from the rules specified above should
be noted in all pre-contest publicity. Note: Any variation that results in the
use of engines larger than 0.46 cu. in. displacement, tuned mufflers, or tuned
pipes will result in the aircraft not being sanctioned as Quickie 500.
Pylon Course Layout
Short Course - QM course
General Rules
The Australian Safety & General Pylon Racing Rules shall apply (Including all
Paragraphs contained therein) unless otherwise stated in the Q500 Rules above.
_________________________________________________________________________________
Annex 1. Approved Engines for Q500
The following engines are approved for use in Q500.
AMPRA Championships, National Championships
Thunder Tigre .46, OS 46AX, OS 46FX, Super Tigre G45
Victoria (All Q500 events)
Thunder Tigre .46, OS 46AX, OS 46FX, Super Tigre G45
Annex 2. QUEENSLAND AIRFRAME AMENDMENTS
SID racers can be included and can run at the same weight as Q500 models.
_________________________________________________________________________________
QE46
Engine
The engine must be a commercially available, front-intake, side-exhaust. The
engine can be modified by using Tuned or nelson type mufflers, carburetors can
be altered and internals using the original manufacturers internals or
replacement original manufacturers spares, however engines must be able to idle
and shut off at command. The use of race engine internals such as Nelson, Jett,
F3d piston and liners and Crankshafts is not permitted. The use of full length
pipes are not permitted.
Displacement
Maximum displacement is 7.6cc (0.46 cubic inches).
Exhaust System
The engine shall be equipped with an expansion chamber muffler.
Tanks:
Pressurized fuel tanks are permitted. (Viz. Crankcase or muffler pressure)
Approved Engines for QE46
The following engines are approved for use in QE46.
Thunder Tigre .46, OS 46AX, OS 46FX, Super Tigre G45, Irvine 46, Force 46. Lower
cost engines can be added upon recognition from Queensland rules commitee.
No race engines eg. Rossi, Nelson, Jett, MVVS, Picco etc. can be used.
Airframes
Full molded composite airframes are permitted including Q500, F400, F3d and the
US Q40 airframes.
Original designs are permitted as long as they apply to the following weight and
size requirements.
Wings
The total area of the wing shall be a minimum of 2000cm2.
Flying wings and Deltas will not be allowed in this event.
Airfoil Thickness
Minimum 22mm.
Weight
The weight of an assembled aircraft, ready for flight, but less fuel shall be a
minimum of 1580grams.
Fuselage Area
The Fuselage must be a minimum of 50cm2.
Landing Gear
The landing gear shall be fixed, with at least 2 main wheels of a diameter not
less than 57mm.
Pylon Course Layout
Short course event.
This class is directed for the beginner or F400 pilot that wants to design his
own airframe or to work on their engines. Low cost engines ensure that if you go
too far and make the engine useless a replacement engine and or parts are
affordable.
_________________________________________________________________________________
FORMULA
400 PYLON RULES (F400):
Definition of Radio Control Pylon Racing Model Aircraft:
A Radio controlled pylon racing Model Aircraft is an aircraft in which the
propulsion energy is provided by a piston type engine - the lift is obtained by
aerodynamic forces acting on the supporting surfaces which, except for control
areas, must remain fixed in flight. The Model Aircraft must be of a semi-scale
type and their general lines must be in accordance with those of full-size
aircraft. Competitors may be required to justify any unusual or unconventional
features of their Model Aircraft design, with documentary evidence of similar
full size aircraft.
Engine:
The engine must be of the reciprocating type, be commercially available and have
a maximum swept volume of 7.5 cc. The engine must of front induction – side
exhaust configuration.
Shut – Off:
The engine must be equipped with a positive radio-controlled shut off. The pilot
shall be able to shut off his engine by radio control on the ground or in the
air.
Tanks:
Pressurized fuel tanks are permitted. (Viz. Crankcase or muffler pressure)
Silencer:
The engine shall be fitted with a silencer; within the general length there
shall be an expansion chamber not less than 19mm diameter, with a minimum length
of 32mm. The silencer shall have a single orifice with a maximum outlet diameter
of 10mm. Alternatively, such other muffler as is produced by the manufacturer of
the engine used and specified by the manufacturer for that Engine may be used,
even though it does not meet the above specifications.
Full length tuned pipes are not permitted – Magic Muffler types are allowed.
Propeller:
Only fixed propellers shall be used. Two-bladed wooden or two or more blade
composite resin continuous fibre construction propellers may be used.
Black APC racing props may be used. (Qld only)
Spinner:
A rounded nose spinner is required.
Fuselage:
Cross Section –The fuselage shall have a minimum height of 125mm, and a minimum
width of 75mm.
Landing Gear:
At least two wheels shall be used. The two main wheels must be a minimum lateral
distance of 15cm, when the Model Aircraft is at rest on the ground. A retracting
undercarriage is permissible.
Lifting Surfaces:
Area The total area of the wing shall be a minimum of 2550cm2. On biplanes with
different wings, the smaller wing shall be at least two thirds of the larger
wing. Flying wings and deltas will not be allowed in this event.
Wing Thickness:
The depth of the wing must be a minimum of 22mm at the root of the root cord of
a monoplane, and 17 mm if a biplane. On a biplane with wings of a different
size, the smaller wing must be at least 15mm thick at the root.
If the wing is not uniform in thickness, then the thickness must decrease in a
straight line from root to tip as viewed from the leading or trailing edge.
Note: “Root” is defined as the innermost wing section, excluding fillets that
may be measured without removing the wing from the fuselage. On a completely
exposed wing, much as that of a parasol monoplane or the top wing of most
biplanes, the root is that section of the wing that is intersected by a
projection of the outline of the fuselage as seen in the top view, i.e. The root
section would be 50mm from the center line of an exposed wing on a Model
Aircraft with a 100mm wide fuselage.
Weight:
The minimum weight of an assembled aircraft, ready for flight, but less fuel
shall be 1.8kg.
Fuel:
The organizers shall supply fuel to a standard formula for glow plug motors. Its
composition shall be 80% methanol, 20% castor oil.
F400 Course Layout:
The F400 course will be the same as the FA1 pylon course, refer to rule 5.3.1.7
The Australian Safety & General Pylon Racing Rules shall apply (Including all
Paragraphs contained therein). Unless otherwise stated in the F400 Rules above.
_______________________________________________________________________________________________

Volume F3D
Radio Control Pylon Racing
2007 Edition
Effective 1st January 2007
F3D – RC PYLON RACING
VOLUME F3D
PART FIVE – TECHNICAL REGULATIONS FOR RADIO CONTROL CONTESTS
5.2. CLASS F3D: PYLON RACING MODEL AIRCRAFT
5.2.1. Definition of Radio Control Pylon Racing Model aircraft:
Model aircraft in which the propulsion energy is provided by a piston type motor and in which the lift
is obtained by aerodynamic forces acting on the supporting surfaces, which except for the control
areas must remain, fixed in flight.
The model aircraft must be of conventional design with forward wing and an aft empennage with the
general lines of a full size aircraft. Unusual or unconventional features must be justified with three
view drawings or photographs of similar features used on full size aircraft.
Para B.3.1. of Section 4b (Builder of the Model aircraft) is not applicable to class F3D.
A pylon team shall consist of a pilot and a mechanic/caller.
All pilots must be accompanied by a caller/mechanic for reasons of safety. The caller can be the
team manager, another competitor from the same team or a third party. In all cases the caller must
be the holder of an FAI licence not necessarily issued by the NAC of the pilot, and must have paid an
entry fee.
Each pilot and mechanic/caller shall be registered as a team from the beginning of the competition
through to its end.
5.2.2. Motor(s)
Motor(s) must be of the reciprocating piston type, with a maximum total swept volume of 6,6 cm
3.Propeller(s) must rotate at the speed of the crankshaft. Air intake into the engine is limited to a total
of 114mm
2.5.2.3. Shut-off
The pilot must be able to shut off his engine by radio control, on the ground, or in the air, within five
seconds of command, irrespective of aircraft altitude. The radio system used to control the aircraft
must be equipped with a fail safe. This fail safe shall be set to shut off the engine if radio signal is
lost.
5.2.3.1. Silencer
The motor(s) shall be fitted with a silencer. Within its length there shall be an expansion chamber of
not less than 30 mm diameter and 100 mm length; the exhaust outlet's total area shall not be more
than 80 mm
25.2.4. Propeller
Only fixed propellers may be used. Two-bladed wooden or two or more blade composite resin
continuous fibre construction propellers may be used.
5.2.5. Propeller Spinner
A rounded nose spinner of at least 25 mm diameter must be fitted.
5.2.6. Fuselage
5.2.6.1. Cross-section
The fuselage shall have a minimum height of 175 mm and a minimum width of 85 mm, the
measurements to be of the fuselage body and are to exclude any fins, attachments or spacers. Both
minimum dimensions must occur at the same cross-section location. The fuselage at this point will
have a minimum cross sectional area of 100 cm
2 excluding fillets and competitors will be required toprovide templates to prove this. Fillets are not considered part of the fuselage or lifting surfaces.
5.2.6.2. Cowls
The motor or motor(s) must be enclosed, with the exception of the silencer, cylinder head and
controls that must be manipulated during operation of the motor. The cylinder head for this purpose
is defined as the top (or outer) 1 centimetre of the motor, excluding ignition plug or compression
screw.
5.2.6.3. Landing Gear
The landing gear may have two or three wheel design with the main wheels having a minimum track
of 150 mm. The minimum diameter of the main wheels shall be 57 mm. The competitor must give
the organiser the possibility to check that measurement. A tail skid may be used in lieu of a tail
wheel. A positive means of steering on the ground shall be provided, rudder control acceptable.
Retracting gears are allowed.
5.2.6.4. Cockpit
A cockpit or canopy profile must be evident and capable of enclosing a pilot's head 50 mm from the
chin to the top of the head. The canopy need not be transparent and a pilot need not be fitted.
5.2.7. Lifting Surfaces
5.2.7.1. Area of Surfaces
Total projected area of the lifting surfaces (wing and horizontal tail combined) shall be a minimum of
34 dm
2. With a biplane, the smaller of the two wings shall have at least 2/3 of the area of the largerwing. No delta or flying wing type aircraft are allowed.
5.2.7.2. Wing Span
Minimum wing span shall be 1150 mm for a monoplane and 750 mm for the largest wing of a
biplane. The maximum wing span shall be 1800mm.
5.2.7.3. Wing Thickness
Wing thickness of the root shall be at least 22 mm for a monoplane, and 18 mm for a biplane. On a
biplane with different size wings, the smaller wing must be at least 13 mm thick at the root. Wing
thickness may decrease in a straight line taper from root to tip as viewed from the leading or trailing
edge.
Note: Root shall be defined as the innermost wing section, not counting fillets that may be measured
without removing wing from fuselage.
On a completely exposed wing, such as on a parasol monoplane or the top wing of most biplanes,
the root is that section of the wing that is intersected by a projection of the outline of the fuselage as
seen in the top view, i.e. the root section would be 50 mm from the centreline of an exposed wing on
a model aircraft with a 100 mm wide fuselage.
5.2.8. Weight
Weight less fuel, but including all equipment necessary for flight shall be at least 2200 g and not
more than 3000 g. If ballast is used it must be permanently and safely affixed.
5.2.9. Fuel
The organisers will supply fuel to a standard formula for glow plug and spark ignition motors. Its
composition shall be 80% methanol, 20% castor oil.
5.2.10. Racing Course Specification
The triangular course will be laid out as follows: The course is 10 laps with individual length of 400 m.
Total distance travelled is 4 km. The race starts at the start-finish line. All take-offs will be ROG, no
mechanical device will be used to assist the aircraft, but hand pushing is permitted. The race is
terminated at the start-finish line 10 full laps later. The racecourse specification may be modified in
the interest of safety or to suit existing field conditions if safety is not compromised. The pylons
should have a minimum height of 4 m and should not exceed 5 m height. Pylons shall be made of a
rigid material at least 70mm in diameter at any point. The pylon must be finished in a bright colour in
order to enhance visibility.

5.2.11. Organisation for Radio Controlled Pylon Racing Contests
For transmitter and frequency control see Section 4b, Para. B.10.4.
No alcohol may be consumed by any pilot, mechanic/caller or official during the official published
times of practice and the contest.
All officials on the racecourse and all competitors must wear a crash helmet with a chin strap.
Helmets must be worn during practice and during the official event.
Heats shall be arranged in accordance with the radio frequencies in use to permit simultaneous
flights. Each competitor has to introduce two different frequencies, distant of a minimum of 20 kHz,
which he must be able to use on all the model aircraft entered in the contest.
During practice, no more than three aircraft and seven people (pilots, callers, starter) may be on the
course before or during the event.
A safety inspection of all aircraft before or during registration shall be conducted by the contestant
under the supervision of a contest official. This list should include the following:
a. Push/pull rods or cables, control horns, and servo leads shall be installed in such a way that they
will not become disconnected in flight. Clevises shall be physically held closed by short pieces of
fuel tubing or similar material. Metal clevises shall be protected from deterioration of the threads
due to vibration by means of a jam nut, thread treatment such as Loctite
®, or Vibra-tite®, or asimilar method. Ball links shall be tight.
b. All screws holding the engine to the mount and the mount to the firewall shall be in place and
secure.
c. The radio receiver and battery pack shall be surrounded by soft foam rubber or other vibration
dampening material and adequately protected against contamination by engine exhaust, raw fuel,
or fuel residue.
d. Batteries shall be of adequate capacity for the size and number of servos used. Minimum battery
capacity shall be 500 milliamp-hours (mah).
e. Servos controlling the pitch and roll functions shall be of adequate strength for the weight and
speed of the aircraft. Whenever a single servo is used to control one of these functions, it shall
be designed and built to accommodate at least four mounting screws. When two or more servos
are used together to control the same function, as in the case of dual aileron servos or the
movable tail surfaces on a “v” tailed aircraft, each of such servos may be of the two-screw variety.
f. Control surfaces shall be firm on the hinge line without excessive play. Safety inspectors shall be
alert to the danger of excessive play whenever electronic servo throw reduction is used in
combination with a mechanically inefficient linkage.
g. All screws holding the servos to the servo rails or trays and holding any trays to the airframe shall
be in place and secure. Rubber grommets shall be used on all servos designed to accept them.
If the heads of the servo mounting screws are small enough to pull through the grommets,
washers shall be used to prevent this.
h. Pushrods shall have only one threaded end that is free to turn. The other end shall consist of a “z”
bend, an “I” bend with a keeper or collar, a metal clevis that is soldered on, or a threaded ball-link
that is glued or otherwise secured so that it cannot turn.
i. Wings, if removable, shall be securely attached to the fuselage with bolts or screws.
j. Wheels shall be securely attached and shall turn freely.
k. The aircraft shall be free of stress cracks and any other indication of structural damage.
5.2.12. Operation of the Race
5.2.12.1. Flight timers and lap counters: Each competitor shall be assigned one official during each heat. This
official will time the competitor's aircraft for the required ten laps. In doing so he will count the laps
flown and advise the pilot when he has completed the necessary 10 laps. He will keep the recorded
time on his timing device until he has entered the time on the score sheet under the supervision of
the starter. On the start/finish line an electronic activated signal will be provided for each competitor.
The number 1pylon judges will operate these signals. These judges shall signal the competitor when
the competitor’s aircraft has passed the number 1 pylon. The pylon judges will be located from the
course as described in the course specification drawing (5.2.10). Each signaller will have a
distinctive colour allocated, and the Contest Director will arrange for each model to be identified by
one signaller before the start of every heat.
5.2.12.2. The judges will have their signals off as the aircraft reach midcourse between No. 3 and No. 1
pylons, or earlier. At the instant the model draws level with the No. 1 pylon the signaller will switch
his signal on. There will be no pilot’s helpers at any of the pylons.
5.2.12.3. At the No. 2 and No. 3 pylons, the Official Judges will place themselves in a position in accordance
with the course layout (5.2.10) to the pylon they are judging.
5.2.12.4. A sideline judge will be posted in the front on the pit area on the spectator side of the racing course.
The sideline judge will record as an infringement, any over flight of the pit or spectator areas.
Two sideline judges will be posted near the No. 1 pylon judges on the spectator side of the racing
course. The sideline judges will record as an infringement any over flight of the sideline and any
flight below the height of the pylon as stated in rule 5.2.12.11.
The judges at No. 2 and No. 3 pylons will record a cut pylon infringement. At the end of each race
the sideline and pylon judges will inform the Race Starter of any infringement by any competitor.
5.2.12.5. A maximum of 3 model aircraft per heat will be allowed.
5.2.12.6. The Race Starter is in charge of each heat, the starter will ensure that all competitors and Race
Officials are ready to commence. Each signaller will have a signal of a distinctive colour, the starter
will arrange for each model aircraft to be identified by one signaller before the start of any heat. A
radio operation check from each competitor will be made prior to starting motor(s).
A maximum of 1 minute will be allowed for starting and adjusting the motor(s), at which point the race
will commence. A competitor whose engine is not running at the end of the 1-minute period will be
disqualified from the heat. No competitor shall be permitted to take off once the first model aircraft
has passed the start/finish line heading from No. 1 to No. 2 pylon on the first lap, and no time shall
be given him for that heat.
5.2.12.7. All laps are to be flown counter-clockwise with turns to the left.
5.2.12.8. At the completion of the 10 laps the Starter must immediately instruct the competitor to remove his
aircraft from the course.
5.2.12.9. A penalty will be incurred if the competitor releases the model aircraft before the drop of the starter's
flag or starting signal, cuts a pylon or flies outside the Sideline Judge. Two infringements constitute
disqualification for that flight.
5.2.12.10 Starting positions in all races will be determined by draw with the No.1 position being closest to No. 2
pylon. Model aircraft will be released from the starting line on the starting signal (flag drop or light
signal) at one-second intervals with timing commencing at the starting signal for that particular model
aircraft. The main wheels of each model aircraft landing gear must remain behind the starting line
until the starting signal.
5.2.12.11 The Contest Director has the right to request any competitor to make a flight to demonstrate the
airworthiness of his model aircraft and/or ability to fly the aircraft around the course. If during the
race, the Contest Director considers any model aircraft to be flying erratically, dangerously, or so low
as to endanger Course Officials, he may disqualify the competitor from that heat or from all heats
and require the model aircraft to be landed immediately. Persistent flying below the top of the pylons
shall be considered dangerous. After passing the first pylon on the first lap of the race, flying below
the top of the pylon will result as one infringement. Two or more infringements during the same heat
shall cancel the flight.
5.2.12.12 In each race, the caller must release the model aircraft at the start and give the pilot verbal
information regarding the flying course of his model aircraft and official signals. Electronic
communication with the pilot shall be prohibited.
The pilot or mechanic of one team may act as the mechanic/helper in one or more other teams.
However, any one model aircraft may not be used by more than one team, nor may roles be
interchanged in a team.
5.2.12.13 After the starting signal (flag drop or light signal) is given, any contact between model aircraft shall be
considered a collision and the model aircraft involved must land immediately. The Contest Director
is required to give such competitors a second opportunity to record a score in that round, provided
that in his opinion the aircraft is still airworthy or the competitor has an airworthy reserve model
aircraft.
In the event of a malfunction of the timing, lap counting, signalling or other such equipment which is
the responsibility of the organisers, the competitor(s) affected by such malfunction shall be given the
opportunity to record a score for that round.
5.2.12.14 The loss of any part of the model aircraft after the starting signal (flag drop or light signal) and before
the engine stops disqualifies the model aircraft for that flight except as a result of a collision where
Para. 5.2.12.13 applies.
5.2.12.15 At the completion of a heat, all aircraft must be landed in an area designated by the contest director.
All pilots and callers must not enter the designated landing area until all aircraft have completed
landing to a full stop.
5.2.13. Scoring
5.2.13.1. The flight of each model aircraft shall be timed with a timing device measuring to at least 1/100th of a
second) by a lap counter/timekeeper. Timing shall start when the starting signal is given to the
individual competitor.
The lap counter/timekeeper stops his timing device after ten laps have been completed by the
competitor and, supervised by the starter, records the elapsed time from the timing device on the
competitor's score sheet.
At the completion of each heat, the pylon and side-line judges notify the starter as to which model
aircraft have infringed. The starter then advises the lap counters/timekeepers of those who will
record the total number of infringements for each competitor on his score sheet.
The score sheets are then processed by a scorer who will: a) if one infringement was incurred, add
1/10th of the flyer's time for ten laps to give the corrected time; b) if two or more infringements were
incurred, cancel the flight.
5.2.13.2. Points shall be awarded after each race as follows: The competitor's score is his corrected time in
seconds and hundredths of a second. If the competitor fails to complete his flight or is disqualified
the score shall be 200.
5.2.13.3. The winner of the event is the competitor who has accumulated the lowest score after the conclusion
of all heats. If four or more rounds are flown, each competitor's worst score shall be discarded. If
nine or more rounds are flown, each competitor's worst (highest) two scores shall be discarded. If
twelve or more rounds are flown, each competitor’s worst (highest) three scores shall be discarded.
5.2.13.4. If the time permits and there is no frequency conflict, ties shall be broken by a fly off race.
Otherwise, the best single race score shall be considered in resolving a tie.
5.2.13.5. Team classification
To establish the national team scores for the team classification, add the individual scores of the
members of the team. Teams are ranked according to the lowest numerical score to the highest;
with complete three competitor teams ahead of two competitor teams which in turn are ranked ahead
of one competitor teams. In a case of a team tie, the team with the lower sum of place numbers,
given in order from the top, wins. If still equal, the best individual placing decides.
5.2.13.6 Awards
At the prize giving, a medal and a diploma will be awarded to the pilots and a diploma to the callers
classified first, second, and third, as well as a medal and a diploma to the pilots and team managers,
and a diploma to the callers of the teams classified first, second, and third.
The Organisers may award further prizes at their discretion.