Datos tecnicos
The Cessna 414 is a twin engined light corporate aircraft with pressurized cabin for a maximum of 7 passengers produced by US-American manufacturer Cessna Aircraft Company.
Crew 1-2
Passengers 5-7
Propulsion 2 Piston Engines
Engine Model Continental TSIO-520-N
Engine Power (each) 231 kW 310 hp
max. Cruise Speed 376 km/h 203 kts
234 mph
max. Speed (vne) 439 km/h 237 kts
273 mph
Service Ceiling 9.144 m 30.000 ft
Rate of climb 463 m/min 1520 ft/min
Range 2.459 km 1.328 NM
1.528 mi.
Empty Weight 1.973 kg 4.350 lbs
max. Takeoff Weight 3.062 kg 6.750 lbs
max. Landing Weight 3.062 kg 6.750 lbs
Wing Span 13,45 m 44,1 ft
Wing Area 21,0 m² 226 ft²
Length 11,09 m 36,4 ft
Height 3,49 m 11,5 ft
First Flight 1968
Production Status out of production
Production Range 1968-1985
Total Production 1070
Developed from Cessna 421
ICAO Code C414, C14T
FAA TCDS A7CE
Data for (Version) Cessna 414A Chancellor
Variants 414, 414A Chancellor, Turbo Star Pressurized 414
Remarks
The Cessna 414 is a less powerfull and lighter development of the Cessna 421.
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