Lancair Propjet

Propjet
Role Kit aircraft
Manufacturer Lancair
Status Production completed 2012
Variants Lancair IV
Lancair Propjet at Sun 'n Fun 2004

The Lancair Propjet is a four-seat, pressurized, composite aircraft powered by a 750-hp Walter M601E turboprop engine. The aircraft is based on Lancair's successful kit-plane, the Lancair IV. Like its piston-powered predecessor, the Propjet is noted for its performance, with a typical cruise speed of 325 knots at 24,000 feet and a climb performance of 4,000 feet per minute.

Production of the aircraft kit was ended in 2012.[1]

Specifications

General characteristics

  • Crew: one
  • Capacity: 3 passengers
  • Length: 26 ft (7.92 m)
  • Wingspan: 30 ft 3 in (10.49 m)
  • Height: ()
  • Wing area: 98 ft² (9.10 m²)
  • Empty weight: 2,300 lb (1045 kg)
  • Useful load: 1,500 lb (682 kg)
  • Max. takeoff weight: 3,800 lb (1,727 kg)
  • Aspect Ratio: 9:1
  • Propeller: 3 blade, constant speed
  • Fuel Capacity: 125 gallons (standard); 145 gallons (extended)
  • Baggage Capacity: 150 lb (68 kg)
  • Cabin Width: 46 in (front); 43 in (rear)
  • Height: 48 in
  • Powerplant: 1 × Walter M601E-11 turbine, 750 hp at sea level (559 kW)

Performance

  • Cruise speed: 325 kn (370 mph, 600 km/h) at 24,000 ft (7,317 m)
  • Stall speed: 64 kn (74 mph, 120 km/h)
  • Range: 1,216 nmi (1,400 mi, 2,270 km) with reserves
  • Rate of climb: 7,000 ft/min (solo); 4,000 ft/min (gross) ()
  • Wing loading: 39 lb/ft² (190.7 kg/m²)
  • Power/mass: .2 hp/lb ()
  • Takeoff Roll: 1,200 ft (gross at sea level)
  • Landing Roll: 1,400 ft
  • Cross Wind Landing: 21 mph component
  • Fuel Consumption: 33 gal/h (330 hp 0.67 Sfc)
  • G Loading: +3.8, -1.9 g (normal)

References

  1. ↑ Lancair (2012). "Our Aircraft". Retrieved 15 November 2012.

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