This track has been raced on 4 configurations (The Circuit, 2.57 mi; 19, 2.92 mi; 1.83 mi; 3.02 mi). Laps on different configurations are not comparable, so only events on the 2.57 mile layout are shown; switch above to see the others.
FE has no laps in the events chosen. It ran at Super Tour Apr 2019, Super Tour Apr 2018, Super Tour Apr 2017: add those events.
F6 has no laps in the events chosen. It ran at Cal Club 2024: add that event.
One row per driver and car (a driver who changed cars has a row for each). Each cell is that driver's best in that car across the selected events, with the session it was set in. Best 5-lap stint is the mean of the driver's quickest five consecutive race laps, and consistency is how far their median race lap sat behind their best in that race (small is a driver who does it every lap); both come from the race with the best stint. The fastest in each column is purple, and a car whose best lap is more than 115% of the fastest in its class is greyed (marked ">115%" beside the driver) and left out of the colour scale. Click a column to sort, a row to highlight it.
Theoretical lap is the sum of the best sectors, whichever laps they came from, and never slower than the best lap (where a car's fastest laps were recorded without sector times, its best lap is used). The 115% mark is about the car's best lap only: a car whose best lap is within 115% of the fastest in its class is never marked. Greyed sectors with no theoretical lap mean the sector times on file do not add up to a believable lap. Letters refer to the events above; Q is qualifying, R a race.
Sectors
S1 SF → IM1 0.65 mi
S2 IM1 → IM2 0.75 mi
S3 IM2 → SF 1.17 mi
Spd In → Out 0.03 mi
Sectors are numbered in lap order from start/finish, whatever each event's timing called them; the loop names are SCCA timing's.
Rule changes between these events
Cal Club 2022 → Cal Club 2023 2022-02-17 to 2023-02-24
In P2 Table 1, AMAC, Asteck, Cheetah, Decker, Fox, LeGrand, Converted F5 spec line, change the notes as follows: "Wings up to 16.5in cord chord of single or dual element;" In P2 Table 1, AMAC-AM5, Fox-2-Seater, Zephyrus, Decker 1/2 spec line, change the notes as follows: "Wings up to 16.5in cord chord of single or dual element;" In P2 Table 1, Bobsy spec line, change the notes as follows: "Wings up to 16.5in cord chord of single or dual element only;" In P2 Table 1, Jondal spec line, change the notes as follows: "Wings up to 16.5in cord chord of single or dual element only;"
In F500, GCR Section 9.1.1.D.15.D., change as follows: "Stand-alone after market aftermarket ECUs are not permitted." In P2, GCR Section 9.1.8.F.3.a., change as follows: "As manufactured and ground by Oldsmobile or by an after after market aftermarket cam manufacturer to Oldsmobile factory specifications for Vin.A (W41) or Mantapart #OP 1149." In P2, GCR Section 9.1.8.F.3.b., change as follows: "As manufactured and ground by Oldsmobile or by an after market aftermarket cam manufacturer to Oldsmobile factory profile Vin. D or Mantapart #OP 1148."
P2 E&O Clarification of Chassis Construction Requirements
In P2, GCR section 9.1.8.C.A.1, add the following: "Chassis fully composed of composite structural materials or chassis partially composed of composite materials that is not capable of rolling on its wheels without the composite materials being installed." In P2, GCR section 9.1.8.C.C.1, add the following: "Allow for any form of chassis construction except fully composite chassis. A chassis partially composed of composite materials must satisfy the requirements of section 9.4.5.A, B, C, E, F and be capable of rolling on its wheels without the composite materials being installed."
In FE, GCR section 9.1.1.I.2.K.c, change as follows: "Master cylinders must be the Girling type: Girling F front master cylinder is .700" piston diameter, Part # WM802005 Girling R rear master cylinder is .750" piston diameter, Part # WM802006"
In FE, GCR section 9.1.1.I.2.G.a.17, change as follows: "A heat shield and heat insulation material may be used between the engine block and the exhaust system and is recommended for the purpose of protecting hoses, shifter cable, and wiring from the heat of the engine and exhaust. Heat insulation material may also be used to protect the fuel cell, fuel filter, fuel rail, and fuel lines."
In FE, GCR section 9.1.1.I.2.F.g, change as follows: "The front wing main plane, front wing secondary elements, front wing support mounts, and front wing endplates assembly and its related mounting components must be used and mounted as delivered from Enterprises. Any m Modifications to these parts, except as specifically noted herein, is strictly forbidden are prohibited. The front main wing plane angle is zeroed on the rear upper aft transmission surface measured with a suitable angle gauge, i.e.: digital level on the top main plane 2 inches outward from the nose box mounts element may be adjusted +2.5 to -0.5 degrees. It must meet a minimum measurement of negative .5 degrees (angled down in the back) and a maximum measurement of positive 2.5 degrees (angled up in the back). It is acceptable to shim the main plane to obtain this measurement. Shimming 2 of the 4 verticals through the main element mounting points to
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achieve adjustment range is allowed. The main element angle is measured relative to the reference plane. The main element is checked on the upper surface, midway between the vertical mounting and outer secondary elements on both sides. Note: The reference plane is the machined surface where the shock clevises are attached to the transmission case. Secondary wing elements may be used in any of the provided adjustment holes. Gurney flaps (0.500" +/- 0.030") are permitted allowed as an option for installation on the trailing edge upper surface of the front wing on secondary elements only, not the wing main plane. They Gurney flaps must be securely attached in a secure fashion, without modification to the wing element except for mounting hardware. Only .500” +/- .030” flaps are allowed. Maximum number of mounting locations on front flaps is 2 on each flap and maximum hardware size is with two #8 (.156) hardware or tape. Gurney flaps, where attached, shall be are bent or formed 90 degrees to have a sharp inner radiusand parallel to the upper surface of the wing element and. no t Tapered or "saw- toothed" Gurneys flaps are not permitted. Gurney flaps are measured for total height as mounted from the upper surface of the element." In FE, GCR section 9.1.1.I.2.F.h, change as follows: "The rear wing assembly and its related mounting components are to must be used and mounted as delivered. Any m Modifications, except as specifically notedherei n, are strictly prohibited. The lower plane angle, zeroed on the rear upper aft transmission surface, measured with a suitable angle gauge. i.e.; digital level on the top surface of the lower rear wing must meet a minimum of –3.0 degrees (angled down in the back) and a maximum of +2.0 degrees (angled up in the back). It is acceptable to adjust the lower rear element to meet these requirements element may be adjusted +2.0 to -3.0 degrees. Chamfering the upper inner corners of the wing mounting brackets to achieve the adjustment range is allowed. The element angle is measured relative to the reference plane. The element is checked on the top surface, near the center, without a Gurney flap. Note: The reference plane is the machined surface where the shock clevises are attached to the transmission case. The upper rear wing element may only be adjusted within the parameter profile of the wing endplates and wing adjusters as provided from Enterprises using any of the provided adjustment holes. No additional holes may be added. Gurney flaps (0.250" +/- 0.030") are permitted allowed as an optionfor installation on the trailing edge upper surface of the on one or both wing elements. They Gurney flaps must be securely attached in a secure fashion, without modification to the wing element except for mounting hardware. Only .250” +/- .030” flaps are allowed on one or both elements with five #8 hardware or tape.The Gurney flaps only, may extend beyond the parameters of the end plate are bent or formed 90 degrees to have a sharp inner radius. Maximum number of mounting locations is 5 and maximum hardware size is #8 (.156). Gurney flaps, where degrees and parallel to the upper surface of the wing element and no t Tapered or "saw-toothed" Gurneys flaps are not permitted. Gurney flaps are measured for total height as mounted from the upper surface of the element."
In P2, GCR section 9.1.8.A.1, change as follows: "Chassis fully composed of composite structural materials or chassis partially composed of composite materials that is not capable of rolling on its wheels without the composite materials being installed." In P2, GCR section 9.1.8.C.C.1, change as follows: "Allow for any form of chassis construction except fully composite chassis incorporating composite structural materials. A chassis partially composed of composite materials must satisfy the requirements of section 9.4.5.A, B, C, E, F, and be capable of rolling on its wheels without the composite materials being installed. Both tube frame and aluminum or steel monocoque chassis construction are allowed.”
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In P2, GCR section 9.1.8.C.2, change as follows: "Anti-intrusion panels are allowed anywhere on the sides of the chassis. Materials and attachment are is unrestricted. Attachment points must be at least 15cm (5.906 inches) apart center to center using fasteners no larger than 6.5mm (0.256 inches) diameter.” In P2 Table 1, add the following: P2 Table 1 (Spec Line Cars)
A specification table follows in the original; it is not shown here.
In P2, GCR section 9.1.8.C.D.2, change as follows: "Height: No part of the vehicle having special or significant aerodynamic function shall exceed a height of 115cm (45.275 inches) above the ground with the car in normal racing trim, driver aboard." In P2, GCR section 9.1.8.C.D.3, change as follows: "However, no portion shall extend more than 10cm (3.937 inches) beyond a plane tangent to the outer face of the front and rear wheels with tires." P2 Engine Table Spec
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Line Engine Series
A specification table follows in the original; it is not shown here.
In P2, GCR section 9.1.8.C.D.6, change as follows: "As viewed from the side, T the outermost surface of side pods body between the front and rear wheel openings and above the floor must have a minimum height equal to the height of the front axle centerline."
P2 Clarify closed cockpit single seat car allowance
In P2, GCR section 9.1.8.C.C, add a section as follows: "4. Closed cockpit single seat cars are not permitted unless specifically allowed by a spec line in Table 1."
P2 Correct Table 1 for Engine Date Range Specifications
In FE, GCR section 9.1.1.I.2.N.f, change as follows: "Any rain light is allowed. Effective 1/1/2024, a rain light that meets FIA Standard 8874-2019, Technical List No. 76, is required as specified in GCR section 9.3.32.B.2."
P2 E&O - Clarify B.1 modified engine range in AMAC spec lines
In FE, GCR section 9.1.1.I.2.P.c, add the following: "Racer's tape may be used to repair crash damage, or as a precautionary means of securing the body panels or retaining latches fasteners only. Crash-damage is defined as having occurred during the current event, and the tape should be of an appropriate color if possible. Taping of body seams is not allowed. Taping across heat exchanger openings as a way to control temperature is allowed and may serve no other purpose."
P2 Replacement Engine Crankcase for 07/08 Suzuki GSX-R1000 Engines
In P2 Engine Table, Spec Line B.1, add to notes as follows: "No modifications allowed on engines manufactured after 2008 model year. 2007-2008 Suzuki GSX-R1000 crankcase part #11300-21860 may be replaced with 2016-2019 Suzuki GSX-S1000 crankcase part #11301-04840."
Cal Club 2024 → Cal Club 2026 2024-02-23 to 2026-02-21
In P2 Engine Table, Spec Line E, change the notes as follows: "No engine modifications except for dry sump oil system, ECU mapping, and exhaust system the following: oil system, ECU, and exhaust are unrestricted."
In P2 Table 1, FIA Group CN spec line, change the notes as follows: "FIA Group CN homologated chassis, brake calipers and discs, hub carriers, and suspension components are required. V de V European Proto Endurance Series Challenge permitted bodywork, rear diffuser, wing, wheels, and assisted shifting are allowed. Car M must comply with all other P2 requirements. Competitors must have copies of FIA Group CN Technical Regulations and V de V European Proto Endurance Series Challenge Sporting and Technical Regulations in their possession and present them upon request are available here: https://www.scca.com/pages/technical-forms-and-downloads."
In FE, GCR section 9.1.8.I.2.M, add the following: "b. Hoosier FE/FE2 Decal Placement: Five (5) "Hoosier" decals are required in the following locations: One (1) small "Hoosier" decal on the nose or the front shock cover of the car. One (1) 12" "Hoosier" decal on the outside vertical plane of each front wing plate. One (1) 12" "Hoosier" decal on the vertical plane of each of the lower floor panels just in front of the rear wheels. Hoosier decals are available, free of charge, from all Hoosier tire distributors and SCCA Enterprises."
In FE, GCR section 9.1.1.I.2.U.b.3, change as follows: "Protest Fee: Regional -$25.00, National -$50.00. See GCR section 8.3.1.D for fees and payment procedure." In SRF, GCR section 9.1.8.D.1.U.b.3, change as follows: "Protest Fee: Regional -$25.00, National -$50.00. See GCR section 8.3.1.D for fees and payment procedure. Item 1 will be done by the CSR or other shop that is equipped for this type of work and will be paid directly."
FE Update on Letter 36620 with new Hoosier Contingency Decal Info
In FE, GCR section 9.1.1.I.2.M.b, change as follows: "Five (5) "Hoosier" decals are required in the following locations: One (1) small "Hoosier" decal on the nose or the front shock cover of the car. One (1) 12" "Hoosier" decal on the outside vertical plane of each front wing plate. One (1) 12" "Hoosier" decal on the vertical plane of each of the lower floor panels just in front of the rear wheels. Hoosier decals are available, free of charge, from all Hoosier tire distributors and SCCA Enterprises Per Hoosier's contingency program, three (3) decals are required to qualify for contingency awards. One (1) decal must be located on each side of the car and one (1) decal must be visible on the front."
In FE, GCR section 9.1.1.G.2.K, add the following: "g. If used, SCCA Enterprises Part # WM803010 Brake Line to Control Arm covers must be used as delivered and must be securely fastened with zip ties/tie straps or tape. Part # WM803010 is the only approved part and may serve no other purpose."
Effective 9/1/25 in FE, GCR section 9.1.1.G.1.A, change as follows: "Definition FE’s with the Mazda 2.0L MZR engine will be classed as “FE2” and will use the class designation FE2. The Mazda 2.0L MZR motor can be used in all SCCA events. It shall run under all FE Preparation rules except as noted below: a. 2.0L MZR may be run with an Elite 5SPD or a Complete SADEV 6SPD transmission Kit Must use the following: b. 2.0L only Intake Manifold Part # WM30106 c. Throttle Body Part # WM591930-Jenvey
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d. PE ECU Kit Part # 1192012 e. Nippon-Denso Alternator Part # WM902127 f. Oil Filter Adaptor Part # WM301050 & Oil Filter Part # G301022 g. PCV Valve Part # WM391502 h. The car shall weigh 1270 lbs. minimum, including the driver. i. 16” MAZDA logo on each side of the engine cowling and the Mazda wing & name logo on the front center of the nose cone. These are mandatory decals. j. 2.0L MZR required Spark Plug Part# ND ITV 24 Formula Enterprises cars "FE" with Mazda 2.0L MZR engine are classed as "FE2." FE2 is the primary class in all SCCA events and must run under all FE Preparation rules except as noted below: Mandatory items 16” MAZDA logo, each side of the engine cowling, Mazda wing logo, front center of the nose cone. Table 2 (Spec Line Cars) Car Engine Wheel Width (in) ± .060 Aero Transmission Weight Notes
A specification table follows in the original; it is not shown here.
In FE, GCR section 9.1.1.G.2.G.a.1, add the following: "NO MODIFICATIONS ARE ALLOWED EXCEPT WHERE SPECIFICALLY AUTHORIZED WITHIN THESE RULES. This includes all fuel injection and engine management components, including exhaust, cooling, electrical and lubrication systems. All systems are subject to test procedures and must conform to OEM / SCCA Enterprises specifications as stated and supplied by Enterprises. All fluids, except fuel, are unrestricted." In FE, GCR section 9.1.1.G.2.T, add the following: "If a competitor refuses to give their engine and/or unlabeled parts for testing per a request of the Class Compliance Chief (CCC) or Chief Steward, the following penalties will automatically be imposed:"
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In FE, GCR section 9.1.1.G.2.T.d, add the following: "The car and drivetrain are suspended from competition until the unit(s) specified by the CCC or Chief Steward are replaced." In FE, GCR section 9.1.1.G.2.T, add a new section as follows: "g. Any drivetrain part found to be out of spec, during voluntary or involuntary inspection, will constitute a Drivetrain Violation. Penalties may be assessed post event."
What the rules allowed changed as listed; this does not say what any particular car ran.