Lancair 360
| 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[edit]
- Lancair 360TC - Carbon Fiber Turbocharged [2]
Specifications (Lancair 360)[edit]
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[edit]
Wikimedia Commons has media related to Lancair 360.
- ^ "Flying Magazine". November 1999: 36.
{{cite journal}}: Cite journal requires|journal=(help) - ^ Flying Magazine: 39. July 1998.
{{cite journal}}: Missing or empty|title=(help) - ^ "Lancair" (PDF). Lancair.com. Archived from the original (PDF) on 2014-12-23.