Quik Aircraft

The Pegasus Quik is a British flying wing ultralight trike, designed and produced by Pegasus Aviation and later by P&M Aviation

The Quik’s design goal was to produce a faster trike and to this end a smaller wing in both span and area than normal is employed. The initial wing used has on a span of 8.0 m (26.2 ft) and an area of 10.6 m2 (114 sq ft). The smaller wing also gives improved turbulence resistance, but at the cost of a higher stall speed.



Mainair Pegasus Quik

Quik 912S Executive
Version circa 2003 powered with a Rotax 912ULS engine of 74.5 kW (100 hp) and using a conventional cable-braced wing with a kingpost. Maximum gross weight of 409 kg (902 lb) and a cruise speed of 132 km/h (82 mph).[1]
2012 production version with Rotax 912ULS engine of 74.5 kW (100 hp), strut-braced “topless” wing, maximum gross weight of 409 kg (902 lb) and a cruise speed of 129 km/h (80 mph).[3]
2012 production version, designed to be even faster with a 8.45 m (27.7 ft) span, strut-braced “topless” wing of 11.43 m2 (123.0 sq ft) wing area. Gross weight of 450 kg (992 lb), Rotax 912ULS engine of 74.5 kW (100 hp), topless wing and cruise speed of 161 km/h (100 mph). Stall speed is 64 km/h (40 mph).[2][4]

Specifications (Quik 912S Executive)

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wing area: 10.6 m2 (114 sq ft)
  • Empty weight: 193 kg (425 lb)
  • Gross weight: 409 kg (902 lb)
  • Fuel capacity: 49 litres (11 imp gal; 13 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder four stroke aircraft engine, 75 kW (100 hp)


  • Maximum speed: 168 km/h (104 mph; 91 kn)
  • Cruising speed: 132 km/h (82 mph; 71 kn)
  • Stall speed: 61 km/h (38 mph; 33 kn)
  • Rate of climb: 5 m/s (980 ft/min)
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