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Type of aircraft From Wikipedia, the free encyclopedia
The ATEC 122 Zephyr 2000 is a Czech ultralight aircraft, designed by Oldrich Olansky and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.[2][3][4][5]
| 122 Zephyr 2000 | |
|---|---|
| |
| Role | Ultralight aircraft and Light-sport aircraft |
| National origin | Czech Republic |
| Manufacturer | ATEC v.o.s. |
| Designer | Oldrich Olansky |
| Introduction | 1996[1] |
| Status | In production |
| Number built | more than 200 |
| Variants | ATEC 321 Faeta |
The Zephyr was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear, a T-tail and a single engine in tractor configuration.[2][3][4]
The aircraft's fuselage is made from composites with wooden bulkheads. The semi-tapered 9.6 m (31.5 ft) span wing is made from plywood with composite spars and leading edges and employs a UA-2 airfoil. The wing is covered with doped aircraft fabric. The standard engine factory-supplied was the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant.[2][3][4][5]
The Zephyr is noted for its low payload. With a useful load of 197.5 kg (435 lb) and full fuel of 43 kg (95 lb), this leaves only 154.3 kg (340 lb) for occupants and baggage.[2][3][4]
The Zephyr was later developed into the ATEC 321 Faeta.[2]
Data from Bertrand and Purdy[2][5]
General characteristics
Performance
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