| SQ2000 | |
|---|---|
| Role | Homebuilt aircraft
Type of aircraft
|
| National origin | United States |
| Manufacturer | Glassic Composites LLC |
| Status | Production completed |
| Number built | 8 |
The Glassic SQ2000 (also written as SQ 2000 and SQ-2000) is an American homebuilt aircraft, designed and produced by Glassic Composites LLCofSale Creek, Tennessee. When it was available the aircraft was supplied as a kit for amateur construction.[1][2]
The SQ2000 features a cantilever mid-wing with tip rudders and a canard, a four-seat enclosed cabin accessed via doors, fixed or optionally retractable tricycle landing gear and a single engine in pusher configuration.[1]
The aircraft is made from composites. Its 26.58 ft (8.1 m) span wing has a wing area of 104.0 sq ft (9.66 m2). The cabin width is 48 in (120 cm). The acceptable power range is 160 to 260 hp (119 to 194 kW) and the standard engine used is the 200 hp (149 kW) Lycoming IO-360 powerplant.[1]
Like many canard designs, the SQ2000 has lengthy runway requirements. The standard day, sea level take-off run is 1,600 ft (488 m), while the landing roll is 1,500 ft (457 m).[1]
By 1998 the company reported that two kits had been sold and that one aircraft had been completed and was flying.[1]
In December 2013 five examples were registered in the United States with the Federal Aviation Administration, although a total of eight had been registered at one time.[2]
Data from AeroCrafter[1]
General characteristics
Performance
