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The Fournier RF-47 is a 1990s French two-seat light aircraft designed and built by Avions Fournier.[1] First flown 9 April 1993, it is a low-wing tricycle landing gear monoplane.[1] The prototype was powered by a 90 hp (67 kW) Sauer modified Volkswagen air-cooled engine but it was intended that production aircraft would be fitted with a 90 hp (67 kW) Limbach L2400 engine with the Sauer engine as an option.[1] The RF-47 has an enclosed cockpit with side-by-side configuration seating for two under a single piece canopy, the canopy hinges at the rear.[1]

RF-47
Role	Two-seat light aircraft Type of aircraft
National origin	France
Manufacturer	Avions Fournier
First flight	9 April 1993

Specifications (utility)

Data from Lambert 1994, p. 93

General characteristics

• Crew: 2
• Length: 6.25 m (20 ft 6 in)
• Wingspan: 10.00 m (32 ft 9.25 in)
• Height: 2.10 m (6 ft 10.25 in)
• Wing area: 10.60 m² (114.1 sq ft)
• Empty weight: 380 kg (838 lb)
• Gross weight: 600 kg (1,323 lb)
• Powerplant: 1 × Limbach L2400 , 67 kW (90 hp)

Performance

• Maximum speed: 270 km/h (167 mph, 145 kn)
• Cruise speed: 190 km/h (118 mph, 103 kn)
• Stall speed: 72 km/h (45 mph, 39 kn)
• Service ceiling: 4,000 m (13,125 ft)
• g limits: +4.4 / -2.2
• Rate of climb: 4.00 m/s (787 ft/min)

References

Bibliography

На других языках

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[de] Fournier RF-47

Die Fournier RF-47 war der Entwurf eines zweisitzigen Schulungsflugzeugs, das der französische Luftfahrtkonstrukteur René Fournier Anfang der 90er Jahre für Arc Atlantique in Tours entwickelt hatte. Einige wenige Exemplare wurden Ende der 90er Jahre bei der französischen Euravial S.A. in Serie gebaut. Die Fournier RF-47 war der vorläufig letzte Flugzeugentwurf von René Fournier.

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- [en] Fournier RF-47

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[fr] Fournier RF-47

Le Fournier RF-47 est un avion biplace à aile basse conçu pour la formation au pilotage.

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