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]
Lancair 360 MKII
A Lancair 360 at Peachtree-Dekalb Regional Airport.
Variants
- Lancair 360TC - Carbon Fiber Turbocharged [2]
Specifications (Lancair 360)
Data from [3]
General characteristics
- Crew: 1
- Capacity: 2
- Length: 21 ft (6.4 m)
- Wingspan: 23.5 ft (7.2 m)
- Wing area: 76 sq ft (7.1 m2)
- Empty weight: 1,090 lb (494 kg)
- Gross weight: 1,685 lb (764 kg)
- Powerplant: 1 × IO-320/IO360 Lycoming
- Propellers: 2-bladed
Performance
- Maximum speed: 226 kn; 418 km/h (260 mph)
- Cruise speed: 204 kn; 378 km/h (235 mph)
Cruise speed (depending on engine choice) is 200–220 mph, rate of climb up to 1500 ft./min, Typical fuel consumption is 8–10 gal. per hr. Landing gear is retractable by hydraulic cylinders. Typical fuel capacity is 40–44 gallons.
See also
References
External links
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