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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.
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is made from composites with wooden bulkheads. The semi-tapered 9.6 m (31.5 ft) span wing is made from
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436:, page 124. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
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AeroCrafter - Homebuilt
Aircraft Sourcebook, Fifth Edition
400:"Atec, v.o.s. Czech manufacturer of Hi-Tech ultralights"
458:, page 27. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
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60 litres (13 imp gal; 16 US gal)
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505:, page 118. BAI Communications, 15 July 1998.
128:, designed by Oldrich Olansky and produced by
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480:, page 29. Flying Pages Europe SARL, 2015.
456:World Directory of Leisure Aviation 2011-12
434:World Directory of Leisure Aviation 2003-04
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152:microlight rules. It features a cantilever
148:The Zephyr was designed to comply with the
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478:World Directory of Light Aviation 2015-16
454:Bayerl, Robby; Martin Berkemeier; et al:
377:46.92 kg/m (9.61 lb/sq ft)
359:215 km/h (134 mph, 116 kn)
353:265 km/h (165 mph, 143 kn)
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220:The Zephyr was later developed into the
236:base model for FAI microlight category.
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365:65 km/h (40 mph, 35 kn)
334:four cylinder, liquid and air-cooled,
150:Fédération Aéronautique Internationale
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432:Bertrand, Noel; Rene Coulon; et al:
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297:10.07 m (108.4 sq ft)
476:Tacke, Willi; Marino Boric; et al:
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291:9.6 m (31 ft 6 in)
371:6.5 m/s (1,280 ft/min)
250:Specifications (122 Zephyr 2000)
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624:Single-engined tractor aircraft
614:2000s Czech ultralight aircraft
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318:472.5 kg (1,042 lb)
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199:. The wing is covered with
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338:, 75 kW (101 hp)
158:side-by-side configuration
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312:275 kg (606 lb)
160:enclosed cockpit under a
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270:General characteristics
172:and a single engine in
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144:Design and development
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174:tractor configuration
166:tricycle landing gear
619:Light-sport aircraft
398:ATEC v.o.s. (2015).
258:ATEC 122 Zephyr 2000
243:Light-sport aircraft
138:amateur construction
119:ATEC 122 Zephyr 2000
41:Light-sport aircraft
575:Ultralight aircraft
195:and employs a UA-2
134:Libice nad Cidlinou
126:ultralight aircraft
37:Ultralight aircraft
265:Bertrand and Purdy
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156:, a two-seats-in-
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44:Type of aircraft
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19:122 Zephyr 2000
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179:The aircraft's
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369:Rate of climb:
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222:ATEC 321 Faeta
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110:ATEC 321 Faeta
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101:more than 200
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91:In production
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629:ATEC aircraft
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357:Cruise speed:
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285:one passenger
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403:. Retrieved
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363:Stall speed:
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208:Rotax 912ULS
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97:Number built
344:Performance
336:four stroke
328:Powerplant:
239:Zephyr 2550
233:Zephyr 2000
211:four-stroke
130:ATEC v.o.s.
66:ATEC v.o.s.
608:Categories
405:16 January
385:References
295:Wing area:
593:321 Faeta
486:1368-485X
289:Wingspan:
283:Capacity:
263:Data from
106:Variants
72:Designer
588:212 Solo
568:aircraft
228:Variants
181:fuselage
164:, fixed
154:low-wing
302:Airfoil
197:airfoil
185:plywood
88:Status
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170:T-tail
277:Crew:
245:model
201:doped
189:spars
123:Czech
121:is a
83:1996
33:Role
566:ATEC
507:ISBN
482:ISSN
407:2015
330:1 ×
306:UA-2
191:and
168:, a
117:The
39:and
279:one
132:of
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558:e
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304::
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