Cessna Skymaster

Airplanes

Length

8.8392 m

Flat Wing Span

11.5824 m

Height

2.7432 m

Flat Wing Area

18.6735 m²

Flat Wing Aspect Ratio

7.18

Max Seating

Cruise Speed

231.7455 km/h

Max Speed

320.2595 km/h

Max Ceiling

5943.6 m

Number of Engines

First Flight

1961-02-28

Entry Into service

1962-01-01

Number Built

2993

Maximum Take-Off Weight

1.9958 t (paragliders: kg)

Total Fuel Capacity

348.2579

Maximum Range

1553.017 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Cessna Skymaster	1.9958	348.2579	1553.017

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
OMA SUD Skycar		8.92	12	3	Compare
SGP M-222 Flamingo		8.8	11.9		Compare
Let L-200 Morava	Avia M 337	8.61	12.31	4	Compare
Beechcraft Duchess	Lycoming O-360	8.8392	11.5824	3	Compare
Piper PA-34 Seneca		8.72	11.86		Compare
SIAI-Marchetti S.210	Lycoming O-360	8.83	11.63	5	Compare

All data (28 fields)

Name: Cessna Skymaster
Manufacturer: Cessna Aircraft Company
Description: The Cessna Skymaster is an American twin-engine civil utility aircraft built in a push-pull configuration.
ICAO Code: C336
First Flight: 1961-02-28
Entry Into service: 1962-01-01
Production End: 1982-01-01
Designer: Cessna Aircraft Company
Type: Personal use and air taxi aircraft
Length (m): 8.8392
Height (m): 2.7432
Cockpit Crew: 1
Max Seating: 5
Max Speed (km/h): 320.2595
Cruise Speed (km/h): 231.7455
Min Speed (km/h): 111.0447
Max Ceiling (m): 5943.6
Rate of Climb (m/s): 6.096
Capacity Description: 5 passengers
National Origin: United States of America
Number Built: 2993
Powerplant Description: 2 × Continental IO-360-C air-cooled flat-six piston engine, 157 kW (210 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Cessna_Skymaster
Flat Wing Span (m): 11.5824
Flat Wing Area (m²): 18.6735
Flat Wing Aspect Ratio: 7.18
Wake Category: L
Number of Engines: 2