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The single engine Commander was designed and origianlly built by the Rockwell
General Aviation Division. Rockwell stopped producing the single engine
Commander in 1979.
Rockwell Commander Aircraft Comparison Data
Piston/Single Engine Land
| Aircraft Description |
HP Rating |
Max Structural Speed (KTS) |
Max Cruise Speed (KTS) |
Stall / Landing Config (KTS) |
Total Capacity Fuel * |
Max Service Ceiling |
Rate Of Climb |
| 114A, GRAN TURISMO |
260 |
166 |
156 |
54 |
68 |
16,500 |
1,030 |
| 114 |
260 |
166 |
156 |
54 |
68 |
17,400 |
1,088 |
| 112TC, -A, Alpine |
210 |
170 |
162 |
54 |
68 |
20,000 |
914 |
| 112B |
200 |
150 |
142 |
51 |
68 |
15,050 |
950 |
| 112A |
200 |
149 |
140 |
54 |
68 |
13,900 |
1,020 |
| 112 |
200 |
152 |
143 |
53 |
60 |
17,000 |
1,000 |
* The 112 was also offered with a 48-gallon "standard" fuel capacity.
The fuel tanks were the same size, but the fuel-filler ports were moved farther
inboard to make the tanks overflow earlier, preventing filling the extra 20 gallons.
| Aircraft Description |
T/O Over 50ft OBST |
Land Over 50FT OBST |
Gross Weight LBS |
Empty Weight LBS |
Lenght FT/IN |
Height FT/IN |
Wing Span FT/IN |
| 114A, GRAN TURISMO |
2,150 |
1,200 |
3,260 |
2,070 |
25'1" |
8'5" |
32'9" |
| 114 |
1,990 |
1,200 |
3,140 |
1,905 |
25'1" |
8'5" |
32'9" |
| 112TC, -A, Alpine |
1,750 |
1,275 |
2,950 |
2,035 |
25'1" |
8'5" |
35'7" |
| 112B |
1,829 |
1,039 |
2,800 |
1,773 |
25'1" |
8'5" |
35'7" |
| 112A |
1,585 |
1,310 |
2,650 |
1,691 |
24'10" |
8'5" |
32'9" |
| 112 |
1,460 |
1,310 |
2,550 |
1,530 |
24'11" |
8'5" |
32'9" |
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