Cessna 414

Corporate Aircraft

Cessna 414A Chancellor, PH-SWN, 414A-0420 © Karsten Palt
Photo ©: Karsten Palt
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.
The Cessna 414 is a less powerfull and lighter development of the Cessna 421.
Propulsion2 Piston Engines
Engine ModelContinental TSIO-520-N
Engine Power (each)231 kW310 hp
max. Cruise Speed376 km/h203 kts
  234 mph
max. Speed (vne)439 km/h237 kts
  273 mph
Service Ceiling9.144 m30.000 ft
Rate of climb463 m/min1520 ft/min
Range2.459 km1.328 NM
1.528 mi.
Empty Weight1.973 kg4.350 lbs
max. Takeoff Weight3.062 kg6.750 lbs
max. Landing Weight3.062 kg6.750 lbs
Wing Span13,45 m44 ft 2 in
Wing Area21,0 m226 ft
Length11,09 m36 ft 5 in
Height3,49 m11 ft 5 in
First Flight1968
Production Statusout of production
Production Range1968-1985
Total Production1070
Developed fromCessna 421
ICAO CodeC14T C414
Data for (Version)Cessna 414A Chancellor
Variants414, 414A Chancellor, Turbo Star Pressurized 414

[Photo-ID: 1838] Karsten Palt 2009-04-03
Cessna 414A Chancellor, , PH-SWN, c/n 414A-0420, Karsten Palt, 2009Cessna
414A Chancellor
Reg.: PH-SWN
c/n: 414A-0420
[Friedrichshafen (EDNY / FDH)]