Performance Aircraft Formula GT
| Formula GT | |
|---|---|
| Role | Homebuilt aircraft |
| National origin | United States |
| Manufacturer | Performance Aircraft |
| Introduction | 1990s |
| Status | Production completed |
| Number built | At least one |
| Unit cost |
US$25,500 (kit, project price, 1998) |
The Performance Aircraft Formula GT is an American homebuilt aircraft that was designed and produced by Performance Aircraft of Olathe, Kansas, introduced in the 1990s. When it was available the aircraft was supplied as a kit for amateur construction.[1]
Design and development
The Formula GT features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.[1]
The aircraft is made from composite materials. Its 28.5 ft (8.7 m) span wing, mounts slotted electric flaps and has a wing area of 100 sq ft (9.3 m2). The cabin width is 47 in (120 cm). The design includes dual side sticks and a large baggage compartment with its own external door. The acceptable power range is 250 to 350 hp (186 to 261 kW) and the standard engine specified is a 300 hp (224 kW) liquid-cooled V-8 automotive conversion powerplant.[1]
The aircraft has a typical empty weight of 1,400 lb (640 kg) and a gross weight of 2,300 lb (1,000 kg), giving a useful load of 900 lb (410 kg). With full fuel of 110 U.S. gallons (420 L; 92 imp gal) the payload for the pilot, passenger and baggage is 240 lb (110 kg).[1]
The standard day, sea level, no wind, take off with a 300 hp (224 kW) engine is 800 ft (244 m) and the landing roll is 600 ft (183 m).[1]
The manufacturer estimated the construction time from the supplied kit as 1500 hours.[1]
Operational history
In April 2015 one example was registered in the United States with the Federal Aviation Administration. It is powered by a Lycoming AEIO-540 engine.[2]
Specifications (Formula GT)
Data from AeroCrafter[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 28 ft 6 in (8.69 m)
- Wing area: 100 sq ft (9.3 m2)
- Aspect ratio: 8.1:1
- Empty weight: 1,400 lb (635 kg)
- Gross weight: 2,300 lb (1,043 kg)
- Powerplant: 1 × Liquid-cooled V-8 automotive conversion , 300 hp (220 kW)
Performance
- Maximum speed: 250 mph (402 km/h; 217 kn)
- Cruise speed: 230 mph (200 kn; 370 km/h)
- Stall speed: 61 mph (53 kn; 98 km/h) flaps down
- Range: 1,500 mi (1,303 nmi; 2,414 km)
- Service ceiling: 23,000 ft (7,010 m)
- Rate of climb: 2,000 ft/min (10 m/s)
- Wing loading: 23.0 lb/sq ft (112 kg/m2)
References
- 1 2 3 4 5 6 7 Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 355. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1
- ↑ Federal Aviation Administration (23 April 2015). "N-Number Inquiry Results - N260GT". Retrieved 23 April 2015.
