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Mooney M20 Specifications
Mooney M20
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| Data for Aircraft | Mooney M20 |
| Year Introduced | 1955 |
| Number Built | |
| Rotor Diameter | |
| Wingspan | 36 ft 5 in (11.1 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 8 ft 4 in (2.5 m) |
| Wing Area | 175.7 sq ft (16.3 m²) |
| Wing Loading | 19.2 lb/ft² (96 kg/m²) |
| Length | 26 ft 9 in (8.15 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Continental TSIO-550-G Turbo-normalized with twin |
| Country of Origin | USA |
| Empty Weight | 2370 lb (1074 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 3374 lb (1528 kg) |
| Useful Load | 1004 lb (454 kg) |
| Seats | 3 passengers |
| Crew | one pilot |
| Power Loading | 12.0 lb/hp (0.11 kW/kg) |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | |
| Oil Capacity |
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