Transport Atlas

How The World Moves
Sign In
Text size
100%
Theme
Vehicle

Rockwell Commander 685

General Aviation and Light Aircraft

The Rockwell Commander 685, also sold as the Aero Commander 685, is a pressurised light twin built by the Aero Commander company, a division of Rockwell International from 1965. It is the piston-engined sibling of the turboprop Commander 690: a high-wing cantilever monoplane with an enclosed nine-seat cabin, retractable nose-wheel landing gear and two wing-mounted 435 horsepower Continental GTSIO-520 engines driving three-bladed Hartzell feathering propellers. The Federal Aviation Administration type certified the Model 685 on 17 September 1971. It entered service that year and was retired from production in 1976, after only 66 aircraft, and the Jetprop series followed as the next generation of the line. Published performance figures give a maximum speed of 449 kilometres per hour at 20,000 feet and a range of about 3,090 kilometres.

Facts
Year
1971 1
Engine Class
Piston 1
Status
Out of production 1
Units Built
66 1
Top Speed (km/h)
449 1
Mass (kg)
2731 1
Maximum Mass (kg)
4082 1
Engine
Two Continental GTSIO-520 piston engines of 435 hp each 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Rockwell 685 (Wikipedia)

Of Make

Source Rockwell 685 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Rockwell 685 (Wikipedia)Lead, ownership
Quote, Lead, ownership
originally built by the Aero Commander company, a division of Rockwell International from 1965
Sources
1. Rockwell 685 (Wikipedia)
  • Lead, introduction
    The introduction was in 1971 and the retired in 1976; in this time are built 66 aircraft.
  • Lead, piston engines
    is a light-twin piston-engined aircraft with a pressurized cabin
  • Design and development
    two wing-mounted 435 hp Continental GTSIO-520K piston engines in tractor configuration
  • Lead, retirement
    The introduction was in 1971 and the retired in 1976
  • Lead, production
    in this time are built 66 aircraft
  • Specifications, empty weight
    Empty weight: 6,021 lb (2,731 kg)
  • Specifications, maximum take-off weight
    Max takeoff weight: 9,000 lb (4,082 kg)
  • Specifications, maximum speed
    Maximum speed: 279 mph (449 km/h, 242 kn) at 20,000 ft (6,100 m) (TAS)
  • Lead, ownership
    originally built by the Aero Commander company, a division of Rockwell International from 1965
  • In Group: Twin-Engine and Turboprop Utility Aircraft, Lead, twin-engined type
    is a light-twin piston-engined aircraft with a pressurized cabin
  • Exemplifies: Aviation, Lead, aircraft
    is a light-twin piston-engined aircraft with a pressurized cabin
View the Source
Comments (0)
No comments yet. Be the first to share a thought.
Reader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.