Rockwell Commander Turbo 680

Turboprop • twin engine • High Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

170
KTAS
Cruise Speed
6
Occupants
1137
nm
Max Range
842
lbs
Wet Payload

Estimated Ownership Costs

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About the Rockwell Commander Turbo 680

The Rockwell Commander Turbo 680 (680T) is a member of the Aero Commander 500 family, a series of light-twin piston-engined and turboprop aircraft that was originally built by Aero Design and Engineering Company in the late 1940s. The initial production version was the 7-seat Aero Commander 520, which was later improved to the 500S, also known as the Shrike Commander. The aircraft was designed by Ted Smith and was initially intended for small feeder airliner firms, but it found use in private business aircraft and military markets. The Aero Commander was popular with pilots due to its “pilot-friendly” design and was operated by various government agencies, military units, and civilian operators.

Technical Specifications

Dimensions

Wingspan
46.7 ft
Length
41.5 ft
Height
14.5 ft

Weights

Max Takeoff Weight
8,950 lbs
Max Landing Weight
8,500 lbs
Useful Load
3,100 lbs
Fuel Capacity
337 gal

Performance

Cruise Speed
170 KTAS
Range
1137 NM
Service Ceiling
20,000 ft
Rate of Climb
1000 fpm

Engines

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