Lancair 360

Lancair 360
Lancair 360
General information
Type	Kit Plane
Manufacturer	Lancair
Designer	Lance A. Neibauer
Status	Operational
Primary user	Civilian
History
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: 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.

[1] "Flying Magazine". November 1999: 36. {{cite journal}}: Cite journal requires |journal= (help)

[2] Flying Magazine: 39. July 1998. {{cite journal}}: Missing or empty |title= (help)

[3] "Lancair" (PDF). Lancair.com. Archived from the original (PDF) on 2014-12-23.

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