BRAND and MODEL
SMITH AEROSTAR
TYPE
Light business and executive aircraft
ORIGIN
United States of America
ENGINE
(601P)
Two 216 kw (290 hp) Lycoming TIO-540-S1A5 six-cylinder horizontally-opposed air-cooled engines
SPECIFICATIONS
Wingspan: 11.18 m (36 ft 8 in)
Length: 10.61 m (34 ft 9¾ in)
Height: 3.68 m (12 ft 1½ in)
Wing area: 16.54 m² (178 sq ft)
Max speed at 7,620 m (25,000 ft): 476 km/h (296 mph)
Cruising speed at 6,100 m (20,000 ft): 420 km/h (261 mph)
Stalling speed in landing configuration: 119 km/h (74 mph)
Initial rate of climb: 600 m/min (1,970 ft/min)
Single-engine rate of climb: 77 m/min (254 ft/min)
Take-off run: 579 m (1,900 ft)
Max operating altitude: 9,144 m (30,000 ft)
Range at 65% power with 45 mins reserves: 2,285 km (1,420 miles)
Empty weight: 1,814 kg (4,000 lb)
Loaded weight: 2,721 kg (6,000 lb)
