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The aircraft's [[fuselage]] is made from composites with wooden bulkheads. The semi-tapered {{convert|9.6|m|ft|1|abbr=on}} span wing is made from [[plywood]] with composite [[Spar (aviation)|spars]] and [[leading edge]]s and employs a UA-2 [[airfoil]]. The wing is covered with [[Aircraft dope|doped]] [[aircraft fabric]]. The standard engine factory-supplied was the {{convert|100|hp|kW|0|abbr=on}} [[Rotax 912ULS]] [[four-stroke]] powerplant.<ref name="WDLA04" /><ref name="WDLA11" /><ref name="Aerocrafter" />
The Zephyr is noted for its low payload. With a useful load of {{convert|197.5|kg|lb|0|abbr=on}} and full fuel of {{convert|43|kg|lb|0|abbr=on}}, the specification leaves only {{convert|154.3|kg|lb|0|abbr=on}} for occupants and baggage.<ref name="WDLA04" /><ref name="WDLA11" />
The Zephyr was later developed into the [[ATEC 321 Faeta]].<ref name="WDLA04" />
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