| General Data | |||
| First Flown: | 1956 | Length: | 9.4 m |
| Lift Capability: | Height: | 2.67 m | |
| Range: | 370 km | Rotor Span: | 8.18 m |
| Top Speed: | 95 kts | Empty Weight: | 480 kg |
| Service Ceiling: | 12,000 ft | Max Gross Weight: | 930 kg |
| Engines: | 1 Lycoming HIO-360 D1A four cylinder engine rated at 190 hp | ||
| Armament: | n/a | ||
| Accommodations: | 1 Pilot, 3 passengers | Cargo: | unknown |
| Operators: | Algeria, Brazil. Columbia, Ghana, Haiti, India, Kenya, Nicaragua, Sierra Leone, Spain, Sweden | ||
| | |||
| Similar Aircraft: | Model 300 | ||
| Other Features: | none | ||
| | |||
| | |||
| Notes | |||
| Built for the aeronautical industry based on a survey in 1955 which justified a helicopter of this type. | |||
| The original version of the 269 was a two seater. Later versions with three seats were designated the 300 (most common version). | |||
| These were used mostly for agriculture. | |||



