The Cessna 120, 140, and 140A, are single-engine, two-seat, conventional landing gear (tailwheel), light general aviation aircraft that were first produced in 1946, immediately following the end of World War II. Production ended in 1951, and was succeeded in 1959 by the Cessna 150, a similar two-seat trainer which introduced tricycle gear. Combined production of the 120, 140, and 140A was 7,664 units in five years.
Specifications
General Characteristics
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- Wingspan 40.7ft (12.4m)
- Length 30.8ft (9.4m)
- Height 11.6ft (3.5m)
- Empty Weight 3,529lbs (1,600kg)
- Loaded Weight 11,406lbs (5,173kg)
Performance
- Horse Power/Weight Ratio 0.087
- Wing Loading 43.3lbs/ft2 (211.2kg/m2)
- Wing Area 263.7ft2 (24.5m2)
- Drag Points 3516
Parts
- Number of Parts 31
- Control Surfaces 5
- Performance Cost 222
