Conceived in 1969, First Flight on 12 March 1974
The preliminary study of the RF6 also included a 2 place training version, designated the RF6B, that ended up being designed first. Mr. Fournier was convinced that a niche existed in the trainer market for a racy and responsive direct competitor to the sleepy and numb Cessna C-150.
In 1981, Fournier sold the development rights of the RF6B to Slingsby in the UK who renamed it the T67. Originally built of wood it was redesigned for composite construction, and renamed T67.
| F | GB | D | Metrisch | US |
|---|---|---|---|---|
| Type de Construction | Type of Construction | Bauweise | Bois / Wood / Holz | |
| Moteur | Engine | Triebwerk | Limbach SL1700 | |
| Puissance | Power | Leistung | 68 HP @ 3600 rpm | |
| Hélice | Propeller | Propeller | Hoffmann HO-V62R | |
| No. de places | No. Seats | Anz. Sitzplätze | 2 | |
| Train d’atterrissage | Landing Gear | Fahrwerk | Mono mit Stützrädern unter den Flügeln | |
| Facteurs de Charge | Load Factor | Lastvielfache | ? | |
| Envergure | Span | Spannweite | 17,2 m | 55.84′ |
| Longueur | Length | Länge | 7,71 m | 25.3′ |
| Hauteur | Height | Höhe | 1,96 m | 6.43′ |
| Surface alaire | Wing Area | Flügelfläche | 19 m2 | 204.5 ft2 |
| Allongement | Aspect Ratio | Flügelstreckung | 15,25 | |
| Profil de l’aile | Wing Airfoil | Tragflächenprofil | NACA23015 | NACA23012 |
| Masse a vide | Empty Weight | Leergewicht | 470 kg | 1,036 lbs |
| Masse max | max. Take-Off Weight | max. Abfluggewicht | 680 kg | 1,500 lbs |
| Charge utile | Payload | Zuladung gesamt | 210 kg | 463 lbs |
| Carburant | Fuel capacity | Kraftstoffvorrat | 32,5 L | 8.58 us gal |
| Vitesse max. (VNE) | max. Speed (VNE) | max. Geschwindigkeit (VNE) | 225 km/h | 121.5 kts |
| Vitesse de manœuvre (VA) | maneuvering Speed (VA) | Manövergeschwindigkeit (VA) | 165 km/h | 89 kts |
| Vitesse de croisière (VCR) | cruise speed (VCR) | Reisegeschwindigkeit (VCR) | 190 km/h | 102.5 kts |
| Vitesse de décrochage (VS) | Stall Speed (VS) | Überziehgeschwindigkeit (VS) | 68 km/h | 36.7 kts |
| Taux de Montée | Rate of Climb | Steiggeschwindigkeit | ? m/s | ? fpm |
| Taux de chute min. | Minimum Sink | Sinkgeschwindigkeit | 0,95 m/s | 187 fpm |
| Finesse max | L/D Max | Gleitzahl | 26:1 | |
| Dist. de decollage | Take-Off Distance roll | Startstrecke roll | ? m | ? ft |
| Take-Off Distance over 50 ft | Startstrecke über 15 m | ? m | ? ft | |
| Dist. d’atterrissage | Landing Distance over 50 ft | Landestrecke aus 15 m | ? m | ? ft |
| Plafond pratique | Service Ceiling | Dienstgipfelhöhe | ? m | ? ft |
| Autonomie | Endurance | Flugdauer | 3 - 4 hrs | |
| Dist. franchissable | Range | Reichweite | 420 km | 226 nm |
| Vent Travers max. | max. Crosswind | max. Seitenwind | ? | ? |