Harman Patil (Editor)

Fournier RF 4

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Introduced
  
1966

Manufacturers
  
Sportavia-Pützer, Alpavia

Fournier RF-4 Fournier RF4 Photos AirplanePicturesnet

The Fournier RF-4 is a single-seater motor glider designed by René Fournier in 1966. It is an aerobatic version of the Fournier RF-3.

Contents

Fournier RF-4 Fournier RF4 Photos AirplanePicturesnet

Design and development

Fournier RF-4 httpsuploadwikimediaorgwikipediacommonsthu

Conceived as a motor glider and sport touring aircraft, the RF-4 was introduced in 1966. It is of all-wood construction and is fully aerobatic. The landing gear consists of a monowheel gear which retracts forward into a fibreglass cowling. The main wheel has a brake which is manually operated. There is a small steerable tailwheel and wing-mounted outrigger wheels.

Operational history

Fournier RF-4 Fournier Sportavia Serial Number List

An RF-4D was flown by Mira Slovak across the Atlantic Ocean while participating in the May 1969 Daily Mail Air Race. The flight won a £1,000 prize offered by the London Evening News for the best performance in the race by an aircraft under 5,000 lb (2,268 kg) gross take-off weight. The main landing gear fork is an ongoing maintenance issue, with regular replacements needed.

Variants

Fournier RF-4 Fournier Alpavia Sportavia RF3 RF4 RF5 sports aircraft
RF-4
Prototype aerobatic variant of the RF-3, three-built by Alpavia
RF-4D
Production variant, 155 built in Germany by Sportavia-Putzer, D was for Deutschland. 16 shipped to America

Specifications (RF-4D)

Data from In the Air:Number 230:Fournier RF-4D and Plane and Pilot

General characteristics

Fournier RF-4 Fournier Aircraft Photos AirplanePicturesnet

  • Crew: 1
  • Length: 6.05 m (19 ft 10 in)
  • Wingspan: 11.28 m (37 ft 0 in)
  • Height: 1.57 m (5 ft 2 in)
  • Wing area: 11.3 m2 (122 sq ft)
  • Aspect ratio: 11.2
  • Empty weight: 270 kg (595 lb)
  • Gross weight: 390 kg (860 lb)
  • Fuel capacity: 38 litres (8.4 imp gal; 10 US gal)
  • Powerplant: 1 × Rectimo 4 AR 1200 (VW) air-cooled flat-four piston engine, 29 kW (39 hp)
  • Propellers: 2-bladed Hoffmann, 1.50 m (4 ft 11 in) diameter
  • Performance

  • Maximum speed: 196 km/h; 106 kn (122 mph)
  • Cruise speed: 177 km/h; 96 kn (110 mph)
  • Stall speed: 74 km/h; 40 kn (46 mph)
  • Never exceed speed: 249 km/h; 135 kn (155 mph)
  • Range: 644 km; 348 nmi (400 mi)
  • Endurance: 4
  • Service ceiling: 5,800 m (19,000 ft)
  • g limits: 11
  • Maximum glide ratio: 20:1
  • Rate of climb: 3.5 m/s (690 ft/min)
  • References

    Fournier RF-4 Wikipedia