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| ROBIN 2160 |
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| CONFIGURATION |
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FAA certified aircraft
FAR 23, Acrobatic category (+6G/-3G)
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| SEATING |
2 Seats |
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| DIMENSIONS |
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| Length: |
7.10 m (23 ft 3 in) |
| Height |
2.13 m (7 ft) |
| Wingspan |
8.33 m (27 ft 4 in) |
| Wing area |
13 m2 (140 sq ft) |
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| POWERPLANT |
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| Manufacturer: |
Textron-Lycoming |
| Type |
O-320-D2A |
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4 cylinders |
| Power rating |
160 hp @ 2700 rpm |
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| PROPELLER |
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| Manufacturer |
Sensenich |
| Blades |
2 |
| Type |
fixed-pitch |
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| FUEL CAPACITY |
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| Standard |
120 L |
| Optional |
160 L |
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| LOADING |
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| Empty weight |
550 kg (1,235 lb) |
| Maximum weight |
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- When operated in "A" category |
800 kg (1,764 lb) |
- When operated in "U" category |
900 kg (1,984 lb) |
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| PERFORMANCE ("A" cat., at 800 kg max. weight) |
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| Max. cruising speed, @ 75% power, 8500 ft |
242 km/h (131 kt) |
| Max. range (std tank, no reserve) |
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- at 65% power / 127 kt / 11000 ft |
952 km (514 nm) |
- at 75% power / 131 kt / 8500 ft |
850 km (459 nm) |
| Max. rate of climb |
5.2 m/s (1,023 ft/min) |
| Service ceiling |
15,000 ft |
| Stalling speed (flaps down) |
85 km/h (46 kt) |
| Take-off roll |
230 m (754 ft) |
| Take-off run to 50 ft |
410 m (1,345 ft) |
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Reference: Robin 2160 Brochure, Avions Robin, France, 1994 |
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Given data is only for information. Please refer to the manufacturer for current
data. |
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