TAYLOR MINI IMP

 

BRAND and MODEL
TAYLOR MINI IMP
TYPE
Single-seat high-performance sport aircraft
ORIGIN
United States of America
ENGINE
One 75 kw (100 hp) Continental O-200 four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS

Wingspan: 7.77 m (25 ft 6 in)

Length: 4.87 m (16 ft)

Wing area: 6.96 m² (75 sq ft)

Max speed: 322 km/h (200 mph)

Max cruising speed: 290 km/h (180 mph)

Economical cruising speed: 209 km/h (130 mph)

Stalling speed clean: 80 km/h (50 mph)

Stalling speed landing configuration: 72 km/h (45 mph)

Rate of climb: 305 m/min (1,000 ft/min)

Service ceiling: 6,096 m (20,000 ft)

Range: 805 km (500 miles)

Fuel capacity: 49 litres (10.8 imp gals)

Take-off and landing run: 183 m (600 ft)

Empty weight: 236 kg (520 lb)

Baggage capacity weight: 23 kg (50 lb)

Loaded weight: 363 kg (800 lb)

PHOTO
buildandfly.shop:Source of phothograph