Lancair Propjet

Propjet
General information
Type	Kit aircraft
Manufacturer	Lancair
Status	Production completed 2012
History
Variant	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 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)

References

1. Lancair (2012). "Our Aircraft". Archived from the original on 30 November 2012. Retrieved 15 November 2012.

External links

• Media related to Lancair Propjet at Wikimedia Commons