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ROBIN AIGLON II |
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| SEATING |
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| Front: 2 |
Rear: 2 |
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| DIMENSIONS |
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| Length: |
7.26 m |
| Height |
2.38 m |
| Wingspan |
9.08 m |
| Wing area |
15.10 m2 |
| Cabin width, at elbow level |
1.13m (44.5 in) |
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| POWERPLANT |
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| Manufacturer: |
Lycoming |
| Type |
O-360-A3A |
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4 cylinders |
| Power rating |
180 BHP |
| Recommended TBO |
2,000 hours |
| Propeller |
2 blades, fixed pitch |
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| FUEL |
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| Usable fuel |
50 Imp Gal (228 L) |
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| LOADING |
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| Empty weight |
650 kg |
| Gross weight (take-off) |
1,150 kg |
| Useful load |
500 kg |
| Baggage load |
60 kg |
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| PERFORMANCE |
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| Max Authorized Speed (Vne) |
170 kts |
| Max level speed (at S/L) |
144 kts |
| Max cruising (75% power, at optimum height) |
134 kts |
| Econ. cruising speed (65% power) |
128 kts |
| Max rate of climb (at S/L) 1100 kg |
943 ft/mn |
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1,100 ft/mn |
| Demonstrated crosswind component |
22 kts |
| Service ceiling, 1000 kg |
16,400 ft |
| Stalling speed (flaps down) |
52 kts |
| Takeoff distance [ISA - 1,000 kg] |
285 m (934 ft) |
| Clear 50' obstacle [ISA - 1,000 kg] |
420 m (1,380 ft) |
| Landing distance [ISA - 1,000 kg] |
305 m (1,000 ft) |
| Fuel consumption 75% power |
8.4 gph |
| Fuel consumption 65% power |
7.9 gph |
| Range (no reserve) |
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720 nm |
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785 nm |
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Reference: Aiglon II 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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