Cessna 402

Airplanes

Length

10.9728 m

Flat Wing Span

13.4112 m

Height

3.3528 m

Flat Wing Area

20.9775 m²

Cruise Speed

262.9838 km/h

Max Speed

427.8116 km/h

Max Ceiling

8199.12 m

Number of Engines

Aircraft Engine

First Flight

1965-08-26

Entry Into service

1967-01-01

Number Built

2000

Maximum Take-Off Weight

3.1071 t (paragliders: kg)

Total Fuel Capacity

779.7948

Maximum Range

2357.596 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Cessna 402	3.1071	779.7948	2357.596

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Cessna 414		10.9728	13.4112		Compare
AGO Ao 192		10.98	13.54	6	Compare
Aero Commander 500 family		11.22	14.95		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
Piaggio P.136		10.8	13.53		Compare

All data (28 fields)

Name: Cessna 402
Manufacturer: American Jet Industries
Description: The Cessna 401 and 402 are a series of 6 to 10 seat, light twin-piston engine aircraft.
ICAO Code: C402
First Flight: 1965-08-26
Entry Into service: 1967-01-01
Production End: 1985-01-01
Designer: American Jet Industries
Type: Corporate transport and airliner
Length (m): 10.9728
Height (m): 3.3528
Max Speed (km/h): 427.8116
Cruise Speed (km/h): 262.9838
Min Speed (km/h): 125.9359
Max Ceiling (m): 8199.12
Rate of Climb (m/s): 7.366
Capacity Description: Six passengers
National Origin: United States of America
Number Built: 2000
Powerplant Description: 2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 242 kW (325 hp) each
Primary Users: Cape Air
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Cessna_402
Flat Wing Span (m): 13.4112
Flat Wing Area (m²): 20.9775
Wake Category: L
Aircraft Engine: Continental IO-520
Number of Engines: 2