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Falconar Minihawk
The Falconar Minihawk is a Canadian amateur-built aircraft, produced by Falconar Avia. The aircraft is supplied as a kit (US$11,600 kit only, less engine, 1998) or plans for amateur construction.
The aircraft features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a sliding canopy, fixed tricycle landing gear or, optionally, conventional landing gear, and a single engine in tractor configuration.
The Minihawk is made from wood, with its flying surfaces covered in doped aircraft fabric. The aircraft's recommended engine power range is 65 to 100 hp (48 to 75 kW) and standard engines used include the 100 hp (75 kW) Continental O-200 four-stroke powerplant. Construction time from the supplied kit is estimated as 1500 hours.
Even though a prototype was constructed, by November 2012 no examples were registered in its home country with Transport Canada.
On June 30, 2019, Falconar Avia Inc closed for business and assets dissolved. The Master Sets (Original Drawings, Plans, Info Kits, Documentation) sold included the F-9, F-10, F-11A, E, and E2, F-12A, and Minihawk Series to Manna Aviation
Engine: 1 × Continental O-200, 100 hp (75 kW)
Propellers: 2-bladed metal
Length: 18 ft 0 in (5.49 m)
Wingspan: 25 ft 6 in (7.77 m)
Wing area: 106 sq ft (9.8 m2)
Empty weight: 645 lb (293 kg)
Gross weight: 1,070 lb (485 kg)
Fuel capacity: 15 U.S. gallons (57 L; 12 imp gal)
Maximum speed: 128 mph (206 km/h; 111 kn)
Cruise speed: 115 mph (100 kn; 185 km/h)
Stall speed: 50 mph (43 kn; 80 km/h) flaps down
Range: 570 mi (495 nmi; 917 km)
Rate of climb: 1,350 ft/min (6.9 m/s)
Wing loading: 10.0 lb/sq ft (49 kg/m2)
Crew: one
Capacity: one passenger
Cockpit Width: 40 in (102 cm)

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