RS-180 Sportsman
Role Sport aircraft
National origin Germany
Manufacturer Sportavia-Pützer
Designer René Fournier
First flight 1978[1]
Number built 18[2]
Developed from Fournier RF-6

The Sportavia-Pützer RS-180 Sportsman is a four-seat sport aircraft that was produced in Germany in the late 1970s.[3]

The aircraft is a conventional, low-wing cantilever monoplane with fixed tricycle undercarriage.[1] The pilot and passengers are seated in 2+2 configuration under a large bubble canopy.[4] The structure is of wood, covered in plywood and given an outer skin of fibreglass.[1]

Design and development

Rhein-Flugzeugbau (RFB) was founded in 1956. In 1976 it acquired the assets of Sportavia-Pützer, which had been formed in 1966 to take over from Alpavia SA the production of several light aircraft types designed by René Fournier. Sportavia-Pützer produced Fournier aircraft beginning in 1966, and in 1970 Fournier initiated the design of a new four-seat cabin monoplane, the Sportsman. The first prototype Sportsman first flew on 1 March 1973, but the second prototype, which made its maiden flight on 28 April 1976, was a completely redesigned version which was created by Sportavia. This redesigned model was designated the RF-6C Sportsman when it entered production in late 1976, and was renamed RS-180 Sportsman when a new empennage design was added in early 1978, following the fatal crash of the prototype in May 1977.[5] The extensive redesign included reshaping the horizontal tail and relocating it part-way up the fin,[5] changing the wing profile,[5] and removing the turned-down wingtips of the RF-6C.[5] In this form, the RS-180 gained German type certification in 1978.[6]

Basic structure of the Sportsman is wood, with a low-wing cantilever monoplane configuration. The surface is covered with fibreglass. A fixed nosewheel undercarriage with wheel fairings is used. The cabin employs a large bubble canopy.

At the end of 1980, Sportavia-Pützer was integrated into the RFB organisation, the RS-180 being re-designated FRB RS-180 Sportsman. Production was halted in early 1981, after fewer than two dozen units had been completed.[2][7]

Specifications (RS 180)

Data from Wurster 2001, p. 89; Mondey, p. 218

General characteristics

  • Crew: one pilot
  • Capacity: three passengers
  • Length: 7.15 m (23 ft 5.5 in)
  • Wingspan: 10.5 m (34 ft 5.5 in)
  • Height: 2.56 m (8 ft 5 in)
  • Wing area: 14.5 m2 (156.08 sq ft)
  • Aspect ratio: 7.60
  • Empty weight: 640 kg (1,411 lb)
  • Gross weight: 1,100 kg (2,425 lb)
  • Powerplant: 1 × Lycoming O-360-A3A , 134 kW (180 hp)

Performance

  • Maximum speed: 320 km/h (200 mph, 170 kn)
  • Cruise speed: 225 km/h (140 mph, 120 kn)
  • Range: 1,210 km (746 mi, 648 nmi)
  • Service ceiling: 5,400 m (17,715 ft)

Notes

  1. 1 2 3 "Team Test 43: Sportavia RS 180", p. 88
  2. 1 2 Simpson 1995, p. 378
  3. Taylor 1989, p.839
  4. "Team Test 43: Sportavia RS 180", p.89
  5. 1 2 3 4 Barnett, Field, Hurst et al. 1978, p. 1438
  6. "Certification du RS 180 Sportsman", p. 42
  7. Mondey

References

  • Barnett, Cliff; Hugh Field; Mike Hurst; Mark Lambert; Nigel Moll; Doug Richardson (13 May 1978). "Hanover Review". Flight International: 1436–48. Retrieved 13 March 2011.
  • "Certification du RS 180 Sportsman". Aviation Magazine International: 42. 1978.
  • Simpson, R.W. (1995). Airlife's General Aviation. Shrewsbury: Airlife.
  • Mondey, David (1981). Encyclopedia of The World's Commercial and Private Aircraft. New York: Crescent Books. p. 218.
  • Taylor, John W.R. (1977). Jane's All the World's Aircraft 1977–78. London: Jane's Yearbooks.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • "Team Test 43: Sportavia RS 180". Flight International: 88–95. 12 January 1980. Retrieved 13 March 2011.
  • Wurster, Rolf (2001). 50 Jahre Deutsche Motorflugzeuge. Norderstedt: Books on Demand.
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