1946 CESSNA 120

Caractéristiques

Cellule

Moteur & hélice

Poids & carburant

Description

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.

Avionique & équipement

ADSB Nav Light
4 Avionics new
Turn Coordinator
Air Speed
Altimeter
VSI

Cellule

Super clean
New Paint 2012
Scotts Castering Tail wheel Upgrade
New AvioniX
New Whelen Beacon