The Buethe Barracuda is an American two-seat cabin monoplane designed by William Buethe and sold as plans or kits for amateur construction.[1]

Barracuda
Role Homebuilt cabin monoplane
National origin United States
Manufacturer W.B. Buethe Enterprises
Designer William Buethe
First flight 29 June 1975

Design and development

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The prototype Barracuda first flew on 29 June 1975, it is an all-wood, low-wing monoplane with a retractable tricycle landing gear. The enclosed cabin has side-by-side configuration seating for two with dual controls. The prototype was powered by a 250 hp (186 kW) Lycoming IO-540-C4B5 engine but it was designed to take engines between 150 and 300 hp (112-234 kW).[1]

Specifications (Prototype)

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Data from Jane's All the World's Aircraft 1989-90[1]

General characteristics

  • Crew: 2
  • Length: 21 ft 5 in (6.55 m)
  • Wingspan: 21 ft 9 in (7.54 m)
  • Wing area: 120.0 sq ft (11.15 m2)
  • Empty weight: 1,570 lb (712 kg)
  • Gross weight: 2,300 lb (1,043 kg)
  • Powerplant: 1 × Lycoming IO-540-C4B5 , 250 hp (186 kW)

Performance

  • Maximum speed: 208 mph (335 km/h, 181 kn)
  • Cruise speed: 187 mph (300 km/h, 162 kn)
  • Stall speed: 64 mph (103 km/h, 56 kn)
  • Range: 920 mi (1,480 km, 800 nmi)
  • Rate of climb: 2,500 ft/min (13 m/s)

References

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Notes

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  1. ^ a b c Taylor 1989, p. 564

Bibliography

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  • Taylor, John W.R., ed. (1989). Jane's All the World's Aircraft 1989-90. London, United Kingdom: Jane's Yearbooks. ISBN 0-7106-0896-9.