Lancair Propjet
| Lancair Propjet | |
|---|---|
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| Type: | Kit plane |
| Design country: | |
| Manufacturer: | |
| Production time: |
to 2012 |
The Lancair Propjet is a four-seat kit aircraft made by Lancair . It is made of composite materials produced and used by a turboprop engine type Walter M601 E with an output of 750 hp (552 kW driven). It also has a pressurized cabin and a retractable nose wheel landing gear . The construction is based on the Lancair IV . The aircraft reaches a cruising speed of 325 kn (602 km / h ) at an altitude of 24,000 ft (7,315 m ) and a rate of climb of 4,000 feet per minute. The production of the Lancair Propjet ceased in 2012.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| Passengers | 3 |
| length | 7.92 m |
| span | 10.5 m |
| height | 2.8 m |
| Wing area | 9.1 m² |
| Wing extension | 9.0 |
| Load factor | 3.8 g / −1.9 g |
| payload | 455 kg |
| Empty mass | 1,045 kg |
| Max. Takeoff mass | 1,500 kg |
| Cruising speed | 320 kn (593 km / h) |
| Top speed | 370 kn (685 km / h) |
| consumption | 125 L / h |
| Service ceiling | 35,000 ft (10,668 m) |
| Range | 1,400 NM (2,593 km) |
| Engine | Walter M601E-11 with 750 PS (552 kW) |
Web links
Commons : Lancair Propjet - collection of images, videos and audio files
Individual evidence
- ↑ Lancair propjet. Lanceair, accessed May 2, 2018 .
- ↑ 2005 Lancair Propjet. CB Aviation, accessed on May 2, 2018 .
- ↑ LANCAIR “IV / IV-P / PROPJET”. Article in Plane & Pilot Magazine, May 1, 2009, accessed May 2, 2018 .
- ↑ Lancair propjet. Specifications. A photo. Avia.Pro, February 9, 2016, accessed on May 2, 2018 .