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Diamond DA40 Specifications
Diamond DA40
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| Data for Aircraft | Diamond DA40 |
| Year Introduced | |
| Number Built | |
| Rotor Diameter | |
| Wingspan | 39 ft 2 in (11.9 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 6 ft 6 in (1.98 m) |
| Wing Area | 145.3 ft² (13.5 m²) |
| Wing Loading | |
| Length | 26 ft 5 in (8.1 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Lycoming IO-360-M1A, 180 hp (134 kW) |
| Country of Origin | |
| Empty Weight | 1,755 lb (795 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 2,645 lb (1198 kg) |
| Useful Load | 890 lb (403 kg) |
| Seats | 3 passengers |
| Crew | 1 pilot |
| Power Loading | 14.7 lb/hp (110 W/kg}} ==See also== {{aircontent) |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | |
| Oil Capacity |
