1946 Cessna 120

The 1946 Cessna 120 is a classic light aircraft that holds a significant place in aviation history, especially for private pilots and vintage aircraft enthusiasts. Annual Inspection currrently being processed in November 2025 The Cessna 120 is a two-seat, taildragger aircraft produced from 1946 to 1948, serving as a budget version of the Cessna 140. Key differences include the lack of flaps, a rear window, and a standard electrical system on the 120, though many have been retrofitted with these features. The aircraft is powered by a Continental C-85 or C-90 engine, has a maximum speed of about 123 mph, and a range of approximately 420 miles. Specifications: Engine: Continental C-85 or C-90 (85 hp) Maximum Speed: 123 mph Cruise Speed: Approximately 90-100 mph Range: 420 miles Fuel Capacity: 25 gallons Crew: 1 pilot + 1 passenger Wingspan: 32 feet, 10 inches Length: 21 feet, 6 inches Height: 6 feet, 3 inches Gross Weight: 1,450 lbs Stall Speed: 43 KIAS Key differences from the Cessna 140 Flaps: The 120 lacks the flaps found on the Cessna 140. Windows: The original 120 did not have rear side windows, while they were standard on the 140. Electrical System: A standard electrical system (including a starter, battery, and lights) was not included on the base model 120, but was an option on the 140. Many 120s have since been upgraded. Performance and operating costs: The 120 is often described as an affordable and simple tailwheel trainer that is capable of operating from grass fields. Fuel costs can be as low as $20-25 per hour, depending on the engine and fuel prices. The absence of flaps and a fixed landing gear contributes to its simplicity and lower purchase price.