BRAND and MODEL
CESSNA 401 And 402
TYPE
Business and executive aircraft
ORIGIN
United States of America
ENGINE
Two 224 kw (300 hp) Continental TSIO-520-E six-cylinder horizontally-opposed air-cooled engines
SPECIFICATIONS
Wingspan: 12.15 m (39 ft 11 in)
Length: 11 m (36 ft 1 in)
Height: 3.56 m (11 ft 8 in)
Wing area: 18.18 m² (195.7 sq ft)
Max speed at 4,877 m (16,000 ft): 424 km/h (263 mph)
Max cruising speed at 75% power at 3,048 m (10,000 ft): 356 km/h (221 mph)
Rate of climb at sea level: 491 m/min (1,610 ft/min)
Service ceiling: 7,980 m (26,180 ft)
Stalling speed flaps down: 130 km/h (81 mph)
Range at 276 km/h (171 mph) at 3,048 m (10,000 ft): 903 km (561 miles)
Range at 387 km/h (140 mph) at 6,096 m (20,000 ft) with 552 kg (1,218 lb) and max fuel: 2,001 km (1,243 miles)
Empty weight: 1,758 kg (3,875 lb)
Loaded weight: 2,858 kg (6,300 lb)
PHOTO
flugzeuginfo.net:Source of phothograph
