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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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