Rockwell Commander 112
Piston • single engine • Low Wing • Retractable gear
Range Visualization
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Default: 190 lbs (FAA standard)
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Mission Profile
About the Rockwell Commander 112
The Rockwell Commander 112 is a four-seat single-engined general aviation aircraft designed and built by North American Rockwell starting in 1972. It was produced in various models, including the 112TC and 114, with improvements made over the years to address issues such as underpowering and poor door fit. The aircraft underwent several redesigns and upgrades, including the introduction of a turbocharged engine and a new avionics suite. After Rockwell shut down production in 1980, the design rights were sold to Gulfstream, then to Commander Aircraft in 1988, which continued to produce and upgrade the aircraft, including the Commander 114B and 114TC models, until production ended in 2002.
Technical Specifications
Dimensions
- Wingspan
- 32.8 ft
- Length
- 24.9 ft
- Height
- 8.4 ft
Weights
- Max Takeoff Weight
- 3,250 lbs
- Max Landing Weight
- 3,140 lbs
- Useful Load
- 983 lbs
- Fuel Capacity
- 70 gal
Performance
- Cruise Speed
- 150 KTAS
- Range
- 750 NM
- Service Ceiling
- 16,000 ft
- Rate of Climb
- 1070 fpm
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