Names and dates
| Market original model designation | CH-2 | | Market model designation (english translation or spelling) | CH-2 | | First flight date and time | 1964 | | Country of manufacture | Argentina |
Config info
| Rotorcraft type | Helicopter | | Config | Single rotor | | Way of counteracting main rotor torque | Tail rotor |
Weights
| Maximum Takeoff Weight (MTOW) | | | Manufacturers empty weight (MEW) | |
External dimensions
| Total length (rotors turning) | | | Overal height | |
Main rotor
| Main rotor diameter | | | Number of blades | 3 |
Tail rotor
| Tail rotor diameter | | | Number of blades | 2 |
Powerplant
| Engine model | Lycoming HO-360-1A1 | | Engine type | Piston | | Number of engines | 1 | | Total maximum continuous power | |
Performance
| Never exceed speed (Vne) | | | Cruise speed (Vc) | | | Best rate of climb | | | Maximum service ceiling | | | Maximum range | | | Maximum flight endurance | |
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