Lancair Propjet

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.

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

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

Specifications

General characteristics

  • Crew: one
  • Capacity: 3 passengers and 1,500 lb (682 kg) useful load
  • Length: 26 ft 0 in (7.92 m)
  • Wingspan: 30 ft 3 in (10.49 m)
  • Wing area: 98 sq ft (9.10 m2)
  • Empty weight: 2,300 lb (1,045 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 (559 kW) at sea level

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 (36 m/s) (solo); 4,000 ft/min (20 m/s) (gross)
  • Wing loading: 39 lb/sq ft (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)
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References
  1. Lancair (2012). "Our Aircraft". Archived from the original on 30 November 2012. Retrieved 15 November 2012.

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