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Grob G103a Twin II Specifications
Grob G103a Twin II
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| Data for Aircraft | Grob G103a Twin II |
| Year Introduced | |
| Number Built | |
| Rotor Diameter | |
| Wingspan | 57 ft 5 in (17.50 m) |
| Aspect Ratio | 17.1; 17.1 |
| Disc Loading | |
| Height | 5 ft 1 in (1.55 m) |
| Wing Area | 191.0 square feet (17.74 m2) |
| Wing Loading | |
| Length | 26 ft 10 in (8.18 m) |
| Lift-to-Drag Ratio | |
| Engine Type | , 0 kW (0 HP), 0.0 kN (0 lbf) thrust |
| Country of Origin | |
| Empty Weight | 869 lb (394 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 1280 lb (581 kg) |
| Useful Load | |
| Seats | |
| Crew | Two |
| Power Loading | |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | |
| Oil Capacity |
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