Engineering:Lancair 360
From HandWiki
Short description: Two-seat monoplane aircraft
| Lancair 360 | |
|---|---|
| |
| Role | Kit Plane |
| Manufacturer | Lancair |
| Designer | Lance A. Neibauer |
| Status | Operational |
| Primary user | Civilian |
| Developed from | Lancair 320 |
The Lancair 360 is a two-seat aircraft marketed in kit form. It is a low-wing monoplane of conventional configuration with retractable tricycle undercarriage. The Lancair Legacy was chosen to replace the Lancair 360 in 1999.[1]
Variants
- Lancair 360TC - Carbon Fiber Turbocharged [2]
Specifications (Lancair 360)
Data from Lancair[3]
General characteristics
- Crew: 1
- Capacity: 2
- Length: 21 ft (6.4 m)
- Wingspan: 23 ft 6 in (7.162 m)
- Wing area: 76 sq ft (7.1 m2)
- Aspect ratio: 7.266
- Airfoil: NASA NLF(1)-0215F
- Empty weight: 1,090 lb (495 kg) Varies, based on Engine and Options
- Gross weight: 1,685 lb (765 kg)
- Fuel capacity: 40-44 gal
- Powerplant: 1 × IO-320/IO360 Lycoming, 160–180 hp (120–130 kW)
- Propellers: 2 or 3-bladed
Performance
- Maximum speed: 222–226 kn (255–260 mph, 410–418 km/h)
- Cruise speed: 205 kn (235 mph, 378 km/h)
- Stall speed: 59 kn (68 mph, 109 km/h) Landing Configuration
- Range: 510–640 nmi (580–730 mi, 940–1,180 km) (75%, std/opt fuel)
- g limits: +9.0 -4.5
- Wing loading: 22.17 lb/sq ft (108.2 kg/m2)
- Power/mass: 0.107
References
- ↑ Flying Magazine. November 1999. p. 36.
- ↑ Flying Magazine: 39. July 1998.
- ↑ "Lancair". http://www.lancair.com/media/builderupdates/235-320-360/320-360SPEC/320-360specs.pdf.
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