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| ROBIN HR 200/120B - ROBIN 200 |
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| SEATING |
2 Seats |
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| DIMENSIONS |
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| Length: |
21.8 ft - 6.64 m |
| Height |
6.35 ft - 1.94 m |
| Span |
27.3 ft - 8.33 m |
| Wing area |
135.6 sq ft - 12.5 m2 |
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| POWERPLANT |
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| Manufacturer: |
Lycoming |
| Type |
O-235-L2A, 4 cylinders |
| Power rating |
118 hp |
| T.B.0 |
2400 hours |
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| FUEL CAPACITY |
31,7 US Gal - 120 L |
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| LOADING |
|
| Empty weight |
1158 lb - 525 kg |
| Gross weight |
1720 lb - 780 kg |
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| PERFORMANCE |
|
| Cruising speed (75% power, best altitude) |
120 kt - 223 km/h |
| Range (without reserve, 75%, best altitude) |
565 nm - 1050 km |
| Max. rate of climb (max weight) |
770 ft/min - 3.9 m/s |
| Service ceiling |
12,800 ft |
| Take-off (max weight) |
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|
754 ft - 230 m |
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1673 ft - 510 m |
| Landing (max weight) |
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|
1460 ft - 445 m |
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754 ft - 230 m |
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Reference: Robin 200 Brochure, Avions Robin, France, 1993 |
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Given data is only for information. Please refer to the manufacturer for current
data. |
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