Rockwell Commander 112

Rockwell Aircraft

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SPECIFICATIONS
Average used price:  $71,000
Engine make/model:  Lycoming TO-360-C1A6D 
Horsepower @rpm@altitude: 200@2575@SL
Horsepower For Takeoff: 210
TBO hours: 1800
Fuel Type: 100LL
Propeller type/diameter (in.): Hartzell two blade CS/77 
Landing gear type: Tri/Retr.
Max landing weight (lbs.): 2950
Gross weight (lbs): 2950
Std. empty weight (lbs.): 2035
Equipped weight (as tested) (lbs.): 1900
Useful load - std. (lbs.): 1050
Useful load - (equipped) (lbs.): 1050
Payload - full std. fuel (lbs.): 630
Fuel capacity (gals.): 68
Oil capacity (qts.): 8
Wingspan (ft.-in) 35 ft. 7 in.
Overall length (ft.): 25 ft. 1 in.
Height (ft.-in): 8 ft. 5 in.
Wing area (sq. ft.): 163.8
Wing loading (lbs./sq. ft.): 18
Power loading (lbs./hp.): 14
Wheel base (in.) 6 ft. 10 in.
Wheel track (in.) 10 ft. 11 in.
Tire size (mains) (in.): 7.00 x 6
Tire size (nose) (in.):  5.00 x 5
Seating capacity: 4
Cabin doors: 2
Cabin width (in.):  44
Cabin height (in.): 49
Baggage capacity (lbs./cu. ft): 200/22
PERFORMANCE
Max. level speed capacity (knots/mph): 170/196
Cruise speed @ 20,000 ft. (knots/mph):
75% power: 163/196
65% power: 154/177
55% power: 137/158
Max range (with reserve) (nm/sm):
75% power: 665/765
65% power: 835/960
55% power: 900/1035
Fuel consumption (gph.):
75% power: 13.2
65% power.: 10.0
55% power: 8.5
Estimated endurance (65%) (hrs.): 6.8
Stall speed (gear, flaps up) (kts./mph):  58/67
Stall speed (gear, flaps down) (kts./mph): 54/62
Best rate of climb (fpm):  914
Service ceiling (ft.):  20,000
Takeoff over 50-ft. obstacle (ft.):  1750