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and the second, finished the following year, a 134 kW (180 hp) engine. MSW's numerical designation has two digits indicating power in hp/10, followed by the number of seats, suggesting an optimum 220 hp power unit.
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that April. First flight dates were not released by late 2011 but the first prototype was certainly flying by late May 2012. A full scale non-flying mock up has also been exhibited.
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The first prototype is Swiss-registered and the second German, the latter appearing at Aero 2011, held at
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Jane's All the World's
Aircraft : development & production : 2012-13
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MTV-12-B-C.C183-17e, 2.03 m (6 ft 8 in) diameter (diameter from)
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is also straight tapered, with a forward set tailplane mounted on top of the
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159:, placed over the wing, is covered with a single piece, starboard hinged
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Version for the US one design class with a 220 hp (164 kW)
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Externally, the Votec 221 resembles a scaled down (span, 80%)
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to require only a small cut-out for movement of the deep
387:, page 111. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
119:
straight tapered wings with blunt, almost square tips.
175:. It has a steerable tailwheel on a long cantilever.
309:84.54 kg/m (17.32 lb/sq ft) maximum
167:. The mainwheels are mounted on curved, sprung
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8:
400:, page 118. Flying Pages Europe SARL, 2015.
385:World Directory of Leisure Aviation 2011-12
473:
459:
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398:World Directory of Light Aviation 2015-16
383:Bayerl, Robby; Martin Berkemeier; et al:
297:1,398 km (869 mi, 755 nmi)
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215:Jane's All the World's Aircraft 2012-13
15:
7:
163:. Like the Votec 351, the 321 has a
396:Tacke, Willi; Marino Boric; et al:
247:7.10 m (76.4 sq ft)
241:5.85 m (19 ft 2 in)
235:5.66 m (18 ft 7 in)
14:
96:The Votec 221 is a single seat,
77:is a single engine, single seat
24:
550:Single-engined tractor aircraft
342:. IHS Global. pp. 614–5.
1:
135:, far enough forward on the
418:"MT Propellers - hydraulic"
272:, 160 kW (210 hp)
259:600 kg (1,323 lb)
576:
540:2000s Swiss sport aircraft
171:legs and enclosed by long
165:conventional undercarriage
489:
338:Jackson, Paul A. (2012).
253:420 kg (926 lb)
123:are assisted by external
23:
18:
84:, designed and built in
220:General characteristics
364:"Votec 221 on YouTube"
92:Design and development
82:light-sport aircraft
41:light-sport aircraft
257:Max takeoff weight:
179:Operational history
545:Homebuilt aircraft
151:and the rudder is
98:low wing monoplane
555:Low-wing aircraft
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349:978-0-7106-3000-1
267:Lycoming AEIO-390
102:Lycoming AEIO-390
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117:aspect ratio
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66:MSW Aviation
36:Single seat
288:Performance
276:Propellers:
263:Powerplant:
86:Switzerland
56:Switzerland
534:Categories
519:Votec 452T
514:Votec 352T
499:Votec 252T
316:References
245:Wing area:
169:cantilever
19:Votec 221
509:Votec 351
504:Votec 322
494:Votec 221
423:19 August
406:1368-485X
369:20 August
301:g limits:
278:3-bladed
239:Wingspan:
227:Capacity:
213:Data from
149:trim tabs
145:elevators
129:empennage
38:homebuilt
484:aircraft
191:Variants
173:fairings
133:fuselage
121:Ailerons
79:kitbuilt
233:Length:
203:engine.
196:MSW One
157:cockpit
143:. Both
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303:10/-10
295:Range:
161:canopy
155:. The
141:rudder
127:. The
125:spades
147:have
33:Role
425:2012
402:ISSN
371:2012
344:ISBN
265:1 ×
73:The
482:MSW
229:One
137:fin
536::
324:^
88:.
474:e
467:t
460:v
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373:.
352:.
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