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
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineTwo Continental GTSIO-520 piston engines of 435 hp each 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
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, ownershipQuote, 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
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