AIRCRAFT PROGRAM
| Lift type | Fixed wing | ||
| Construction type | Factory-built, Kit-built | ||
| Control type | Piloted | ||
| Engine type | Piston | ||
| Application | Ultralight | ||
| Search for other aircraft programs with these properties on the Aircraft Programs directory page. | |||
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Low wing single piston composite ultralight. Available as kit or factory assembled.
| Variant | Launch/First flight | Production end | |
| Atec 122 Zephyr | 2000 / 1996 | Ultralight/light sport aircraft. | |
| Atec 321 Faeta | 2003 / 2000 | Carbon fibre version. |
| Atec v.o.s. |
Other aircraft programs: Atec 212 Solo
| Garmin International | Analysis | Flight Management Systems. Note: Optional flight and navigation system (122 Zephyr) |
| Dynon Avionics, Inc. | Analysis | Electronic Flight Instrument Systems. Note: Optional Flight DEK-D180 (122 Zephyr) |
| Garmin International | Analysis | Engine Indicator Instruments. Note: Optional engine monitoring system (122 Zephyr) |
| Dynon Avionics, Inc. | Analysis | GPS. Note: Optional navigation system (122 Zephyr) |
| Dynon Avionics, Inc. | Analysis | Engine Health Monitoring. Note: Optional engine monitoring system (122 Zephyr) |
| BRP-Rotax GmbH & Co KG | Analysis | Piston Engines. R912 Series - Atec 122 Zephyr (Rotax 912 UL/ULS); Atec 321 Faeta (Rotax 912 UL/ULS/iS); Rotax 582 - Atec 122 Zephyr (Optional Rotax 582 UL) |
| Fiti Design s.r.o. | Analysis | Composite Propellers. Note: Two or three blade ground-adjustable pitch propeller, or two or three blade in-flight-adjustable propeller (122 Zephyr); ECO competition ground adjustable two or three blade propeller (321 Faeta) |
