Rockwell 685

Airplanes

Length

12.8016 m

Flat Wing Span

14.0208 m

Height

4.2672 m

Flat Wing Area

24.7122 m²

Max Seating

Cruise Speed

411.1436 km/h

Max Speed

449.007 km/h

Max Ceiling

8382 m

Number of Engines

Aircraft Engine

First Flight

1971-01-01

Maximum Take-Off Weight

4.0823 t (paragliders: kg)

Total Fuel Capacity

969.0654

Maximum Range

3089.94 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Rockwell 685	4.0823	969.0654	3089.94

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
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All data (22 fields)

Name: Rockwell 685
Manufacturer: Rockwell International
Description: The Rockwell Commander 685 or Aero Commander 685 is a light-twin piston-engined aircraft with a pressurized cabin originally built by the Aero Commander company, a division of Rockwell International from 1965.
First Flight: 1971-01-01
Designer: Rockwell International
Length (m): 12.8016
Height (m): 4.2672
Cockpit Crew: 1
Max Seating: 8
Max Speed (km/h): 449.007
Cruise Speed (km/h): 411.1436
Min Speed (km/h): 138.8999
Max Ceiling (m): 8382
Rate of Climb (m/s): 7.5692
Capacity Description: 7–8 passengers
National Origin: United States of America
Powerplant Description: 2 × Continental GTSIO-520-F air-cooled flat-six, 324 kW (435 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Rockwell_685
Flat Wing Span (m): 14.0208
Flat Wing Area (m²): 24.7122
Aircraft Engine: Continental IO-520
Number of Engines: 2