Aero Commander 500 family

· Aero Commander

Airplanes

Length

11.22 m

Flat Wing Span

14.95 m

Height

4.42 m

Flat Wing Area

23.69 m²

Flat Wing Aspect Ratio

9.45

Cruise Speed

326 km/h

Max Speed

346 km/h

Max Ceiling

5913 m

Number of Engines

First Flight

1948-04-23

Entry Into service

1952-10-01

Number Built

2902

Maximum Take-Off Weight

3.062 t (paragliders: kg)

Maximum Range

1735 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Aero Commander 500 family	3.062	1735

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
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All data (25 fields)

Name: Aero Commander 500 family
Manufacturer: Aero Commander
Description: The Aero Commander 500 family is a series of light twin piston-engined and turboprop aircraft originally built by the Aero Design and Engineering Company in the late 1940s, renamed the Aero Commander company in 1950, and later a division of Rockwell International in 1965.
First Flight: 1948-04-23
Entry Into service: 1952-10-01
Production End: 1986-01-01
Designer: Aero Commander
Type: Utility and business aircraft
Length (m): 11.22
Height (m): 4.42
Max Speed (km/h): 346
Cruise Speed (km/h): 326
Min Speed (km/h): 109
Max Ceiling (m): 5913
Rate of Climb (m/s): 6.8
Capacity Description: four passengers
National Origin: United States of America
Number Built: 2902
Powerplant Description: 2 × Lycoming IO-540-E1B5 air-cooled flat-six piston engines, 216 kW (290 hp) each
Status: Active
Wikipedia Article (URL): en.wikipedia.org/wiki/Aero_Commander_500_family
Flat Wing Span (m): 14.95
Flat Wing Area (m²): 23.69
Flat Wing Aspect Ratio: 9.45
Number of Engines: 2