Cessna 414

Airplanes

Length

10.9728 m

Flat Wing Span

13.4112 m

Height

3.3528 m

Flat Wing Area

20.9775 m²

Cruise Speed

338.9157 km/h

Max Speed

435.2196 km/h

Max Ceiling

9387.84 m

Number of Engines

First Flight

1968-11-01

Number Built

1070

Maximum Take-Off Weight

3.0617 t (paragliders: kg)

Total Fuel Capacity

806.2927

Maximum Range

2457.604 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Cessna 414	3.0617	806.2927	2457.604

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Cessna 402	Continental IO-520	10.9728	13.4112		Compare
AGO Ao 192		10.98	13.54	6	Compare
Aero Commander 500 family		11.22	14.95		Compare
Britten-Norman BN-2 Islander		10.668	14.9352	9	Compare
Cessna 421 Golden Eagle	Continental IO-520	10.9728	12.4968		Compare
Fleet 50 Freighter	Jacobs R-915	10.97	13.72	10	Compare

All data (24 fields)

Name: Cessna 414
Manufacturer: Cessna Aircraft Company
Description: The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna.
ICAO Code: C414
First Flight: 1968-11-01
Production End: 1985-01-01
Designer: Cessna Aircraft Company
Type: Six/eight-seat light transport
Length (m): 10.9728
Height (m): 3.3528
Max Speed (km/h): 435.2196
Cruise Speed (km/h): 338.9157
Min Speed (km/h): 133.3439
Max Ceiling (m): 9387.84
Rate of Climb (m/s): 7.7216
Capacity Description: four to six
National Origin: United States of America
Number Built: 1070
Powerplant Description: 2 × Continental TSIO-520-NB flat-six turbocharged piston, 231 kW (310 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Cessna_414
Flat Wing Span (m): 13.4112
Flat Wing Area (m²): 20.9775
Wake Category: L
Number of Engines: 2