BRAND and MODEL
TRI-R INDUSTRIES KIS TR-1
TYPE
Two-seat sport monoplane
ORIGIN
United States of America
ENGINE
One 93 kw (125 hp) Continental IO-240 four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 7.01 m (23 ft)
Length: 6.7 m (22 ft)
Height: 1.82 m (6 ft)
Wing area: 8.17 m² (88 sq ft)
Max speed: 314 km/h (195 mph)
Cruising speed: 273 km/h 170 mph
Rate of climb: 335 m/min (1,100 ft/min)
Service ceiling: 5,181 m (17,000 ft)
Stalling speed: 88 km/h (55 mph)
Range: 1,207 km (750 miles)
Take-off roll: 229 m (750 ft)
Landing roll: 335 m (1,100 ft)
Fuel capacity: 129 litres (28 imp gals)
Empty weight: 385 kg (850 lb)
Loaded weight: 658 kg (1,450 lb)
PHOTO
Airliners.net:Source of phothograph
