AIRCRAFT PROGRAM
| Lift type | Fixed wing | ||
| Construction type | Factory-built | ||
| Control type | Piloted | ||
| Engine type | Piston | ||
| Application | Ultralight | ||
| Final assembly | Ramonchamp | ||
| Search for other aircraft programs with these properties on the Aircraft Programs directory page. | |||
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Two-seater, high wing, single piston ultralight. Includes the variants Tetras B, CS, CSL, CSR or CTS.
| Variant | Launch/First flight | Production end | |
| Humbert Tetras | 1992 / 1992 | Two-seat ultralight aircraft with high, trapezoidal wing. |
| Humbert Aviation |
Other aircraft programs: Humbert Moto du Ciel
| Beringer Aero (was Beringer SA) | Analysis | Aircraft Wheels: Optional wheels; Brake System Components: Optional brakes |
| Junkers Profly | Analysis | Whole Aircraft Parachutes: Optional Junkers 501 pyrotechnic emergency parachute |
| Becker Avionics GmbH | Analysis | Radar Transponders: Optional A/C and S mode transponder (Tetras CSR) |
| BRP-Rotax GmbH & Co KG | Analysis | Piston Engines: (R912 Series - Humbert Tetras - Rotax 912 UL (Tetras B), Rotax 912 ULS (Tetras CS/CSL/CSR/CTS) ) |
| DUC Hélices Propellers | Analysis | Composite Propellers: Two-blade forged carbon Windspoon tractor propeller; three-blade Swirl standard or Iconel tractor propeller; FC composite propeller |
