Cessna 425

Airplanes

Length

10.668 m

Flat Wing Span

13.4112 m

Height

3.6576 m

Flat Wing Area

20.9013 m²

Cruise Speed

388.9197 km/h

Max Speed

488.9276 km/h

Max Ceiling

10576.56 m

Number of Engines

Aircraft Engine

First Flight

1978-09-12

Number Built

236

Maximum Take-Off Weight

3.7195 t (paragliders: kg)

Total Fuel Capacity

1385.461

Maximum Range

3048.392 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Cessna 425	3.7195	1385.461	3048.392

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Tecnam P2012 Traveller		11.8	14	9	Compare
Beagle B.206	Continental IO-520	10.0584	13.716	6	Compare
Piaggio P.136		10.8	13.53		Compare
Cessna 404 Titan		11.8872	14.0208	8	Compare
Cessna 421 Golden Eagle	Continental IO-520	10.9728	12.4968		Compare
Cessna 402	Continental IO-520	10.9728	13.4112		Compare

All data (23 fields)

Name: Cessna 425
Manufacturer: Cessna Aircraft Company
Description: The Cessna 425, known as the Corsair and later as the Conquest I, is an eight-seat American pressurized turboprop twin-engined light aircraft.
First Flight: 1978-09-12
Production End: 1986-01-01
Designer: Cessna Aircraft Company
Type: Utility monoplane
Length (m): 10.668
Height (m): 3.6576
Max Speed (km/h): 488.9276
Cruise Speed (km/h): 388.9197
Min Speed (km/h): 146.3079
Max Ceiling (m): 10576.56
Rate of Climb (m/s): 10.2972
Capacity Description: four–six passengers
National Origin: United States of America
Number Built: 236
Powerplant Description: 2 × Pratt & Whitney Canada PT6A-112 turboprops, 336 kW (450 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Cessna_425
Flat Wing Span (m): 13.4112
Flat Wing Area (m²): 20.9013
Aircraft Engine: Pratt & Whitney Canada PT6
Number of Engines: 2