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ROCKWELL COMMANDER 112A
SPECIFICATIONS
Seats

4
ENGINE

    Manufacturer

 Avco Lycoming
    Model
 IO-360-C1D6

    Rating (hp)

 200

    Number of Cylinders

 4
WEIGHTS

    Max. Take-off Weight (lbs/kg)

 2,650/1202

    Empty Weight (lbs/kg)

 1,688/766
WING AREA

    Wing Area (sq.ft./m2)

 152/14.12
DIMENSIONS

    Wing Span

 32 ft 9 in (9.98 m)

    Length

 24 ft 11 in (7,59 m)

    Height

 8 ft 5 in (2,51 m)

PERFORMANCE

    Maximum Speed at Sea Level (mph/kmh)

  

171/275
    Cruise at 75% Power at Optimum Altitude (mph/kmh)
  

161/259
    Range at 75% Power (mls/km)
  

880/1416
      (45 min reserves at 45% Power)
    
    Optimum Range (mls/km)
   975/1569
    Initial Climb (fpm/m/sec)
  

1,000/5.08
    Service Ceiling (ft/m)

13,900/4337
Reference: Green, W., Punnett, D., The Observer's Book of Aircraft, 1975 Ed., p. 168-169, Frederick Warne & Co Ltd, London, 1975.
Given data is only for information. Please refer to the manufacturer for current data.
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