Engineering:Lancair Propjet
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Revision as of 05:44, 3 June 2021 by imported>Scavis2 (linkage)
| Propjet | |
|---|---|
| |
| Role | Kit aircraft |
| Manufacturer | Lancair |
| Status | Production completed 2012 |
| Variants | Lancair IV |
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
- ↑ Lancair (2012). "Our Aircraft". Archived from the original on 30 November 2012. https://web.archive.org/web/20121130001406/http://lancair.com/index.php?option=com_content&view=article&id=145&Itemid=140. Retrieved 15 November 2012.
External links
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