Two-seat monoplane aircraft
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 Lancair [3]
General characteristics
Crew: 1Capacity: 2Length: 21 ft (6.4 m)Wingspan: 23 ft 6 in (7.162 m)Wing area: 76 sq ft (7.1 m2 )Aspect ratio : 7.266Airfoil : NASA NLF(1)-0215FEmpty weight: 1,090 lb (495 kg) Varies, based on Engine and OptionsGross weight: 1,685 lb (765 kg)Fuel capacity: 40-44 galPowerplant: 1 × IO-320/IO360 Lycoming, 160–180 hp (120–130 kW)Propellers: 2 or 3-bladedPerformance
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 ConfigurationRange: 510–640 nmi (580–730 mi, 940–1,180 km) (75%, std/opt fuel)g limits: +9.0 -4.5Wing loading: 22.17 lb/sq ft (108.2 kg/m2 )Power/mass : 0.107
References Wikimedia Commons has media related to Lancair 360 .
^ "Flying Magazine". November 1999: 36. ^ Flying Magazine : 39. July 1998. ^ "Lancair" (PDF) . Lancair.com . Archived from the original (PDF) on 2014-12-23.