BRAND and MODEL
CESSNA 414 CHANCELLOR
TYPE
Pressurised light utility transport
ORIGIN
United States of America
ENGINE
Two 231 kw (310 hp) Continental TSIO-520-J six-cylinder horizontally-opposed air-cooled turbo-supercharged engines
SPECIFICATIONS
Wingspan over wing-tip tanks: 12.15 m (39 ft 10¼ in)
Length: 10.29 m (33 ft 9 in)
Height: 3.61 m (11 ft 10 in)
Wing area: 18.18 m² (195.72 sq ft)
Max speed at sea level: 365 km/h (227 mph)
Cruising speed at 75% power at 7,260 m (25,000 ft): 405 km/h (252 mph)
Cruising speed at 75% power at 3,048 m (10,000 ft): 354 km/h (220 mph)
Rate of climb at sea level: 482 m/min (1,580 ft/min)
Rate of climb: at sea level on one engine: 73 m/min (240 ft/min)
Service ceiling: 9,175 m (30,100 ft)
Single-engine service ceiling: 3,460 m (11,350 ft)
Take-off run: 517 m (1,695 ft)
Take-off distance over 15 m (50 ft) obstacle: 568 m (1,865 ft)
Landing run: 245 m (805 ft)
Range with max fuel, no reserve, at 75% power at 7,620 m (25,000 ft): 2,129 km (1,323 miles)
Max range at 7,620 m (25,000 ft): 2,304 km (1,432 miles)
Empty weight: 1,832 kg (4,039 lb)
Loaded weight: 2,880 kg (6,350 lb)
PHOTO
planesalesusa.com:Source of phothograph
