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| ROBIN 3000 |
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| SEATING |
4 Seats |
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| DIMENSIONS |
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| Length: |
24 ft 7 3/4 in (7.71 m) |
| Height |
8 ft 8 3/4 in (2.66 m) |
| Wingspan |
32 ft 2 1/4 in, (9.81 m) |
| Wing area |
155.75 sq ft (14.41 m2) |
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| POWERPLANT |
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| Manufacturer: |
Lycoming |
| Type |
O-360-A2A, 4 cylinders |
| Power rating |
180 hp |
| Recommended TBO |
2,000 h |
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| PROPELLER |
|
| Blades |
2 |
| Type |
Fixed-pitch |
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| FUEL CAPACITY |
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| Standard |
59 US Gal (225 L) |
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| LOADING |
|
| Empty weight |
1,433 lb (650 kg) |
| Gross weight (take-off) |
2,535 lb (1,150 kg) |
| Useful load |
1,102 lb (500 kg) |
| Baggage load |
88 lb (40 kg) |
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| PERFORMANCE |
|
| Max. level speed (at S/L) |
146 kt (270 km/h) |
| Max. cruising (75% power, at optimum height) |
138 kt (255 km/h) |
| Econ. cruising speed (65% power) |
128 kt (238 km/h) |
| Range (no reserve) |
|
|
805 NM (1,490 km) |
|
869 NM (1,610 km) |
| Max. rate of climb (at S/L) |
875 ft/min (4.45 m/s) |
| Service ceiling |
15,000 ft |
| Stalling speed (flaps down) |
49 kt (91 km/h) |
| Take-off run |
1,016 ft (310 m) |
| Take-off run to 50 ft (15 m) |
1,853 ft (565 m) |
| Landing from 50 ft (15 m) |
1,770 ft (540 in) |
| Landing run |
689 ft (210 in) |
| Demonstrated crosswind component |
22 kt (40 km/h) |
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All performance figures are based on standard day, standard atmosphere, at sea
level and gross weight, unless otherwise noted. |
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Reference: Robin 3000 Brochure, Avions Robin, France |
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Given data is only for information. Please refer to the manufacturer for current
data. |
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