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Cessna 140 Specifications
Cessna 140
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| Data for Aircraft | Cessna 140 |
| Year Introduced | 1946 |
| Number Built | 7664 (120 & 140) |
| Rotor Diameter | |
| Wingspan | 33 ft 4 in (10.25 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 6 ft 3 in (1.92 m) |
| Wing Area | 159.3 ft² (15.1 m²) |
| Wing Loading | 8.68 lb/ft² (42.4 kg/m²) |
| Length | 21 ft 6 in (6.6 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Continental C85-12, 85 hp (63 kW), ; (; ), with a |
| Country of Origin | USA |
| Empty Weight | 770 lbs (Cessna 120) 890 lbs (Cessna 140) (349 kg (Cessna 120) 403 kg (Cessna 140)) |
| Max Landing Weight | |
| Max Ramp Weight | 1,450 lb (658 kg) |
| Useful Load | 680 lbs (Cessna 120) 560 lbs (Cessna 140) (309 kg (Cessna 120) 255 kg (Cessna 140)) |
| Seats | one passenger |
| Crew | one pilot |
| 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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