The Starfire Firebolt, sometimes called the Starfire Firebolt Convertible, due to its removable canopy, is an American homebuiltaerobaticbiplane that was designed by G. H. "Mac" McKenzie and produced by Starfire Aviation of Tempe, Arizona. When it was available the aircraft was supplied in the form of plans for amateur construction, with some pre-fabricated parts available.[1][2][3]
The aircraft is made of mixed construction, with a welded steel tubing, aluminum and wooden structure, all covered in dopedaircraft fabric. Its 24.00 ft (7.3 m) span wing employs a NACA 63A015/0012airfoil and has a wing area of 150.0 sq ft (13.94 m2). The cockpit width is 29 in (74 cm). The acceptable power range is 180 to 300 hp (134 to 224 kW) and the standard engine used is the 300 hp (224 kW) Lycoming IO-540 powerplant. With that engine the aircraft has a cruise speed of 202 mph (325 km/h) and an initial climb rate of 4,000 ft/min (20 m/s).[1][4]
The Firebolt has a typical empty weight of 1,325 lb (601 kg) and a gross weight of 2,000 lb (910 kg), giving a useful load of 675 lb (306 kg). With full fuel of 39 U.S. gallons (150 L; 32 imp gal) the payload for the pilot, passenger and baggage is 441 lb (200 kg).[1]
The standard day, sea level, no wind, take off with a 300 hp (224 kW) engine is 400 ft (122 m) and the landing roll is 800 ft (244 m).[1]
The manufacturer estimated the construction time from the supplied plans as 3000 hours.[1]
Operational history
By 1998 the company reported that six aircraft were completed and flying.[1]