Lancair_360 Knowpia

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

^ "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.

[1]

[2]

[3]

Summary

Variants edit

Specifications (Lancair 360) edit

References edit