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137:, though a carbon fibre wing is under development. All flying surfaces are straight tapered and square tipped, the wing
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The Votec 252T has a cabin over the wing, with baggage space behind the seat, under a single piece
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The first prototype flew on 26 June 2009. A second prototype with a 260 kW (350 hp)
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and the tailplane located on the upper fuselage; the rudder extends down to the keel. The
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on all wheels. The nosewheel casters; there is a small tailskid for rudder protection.
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Jane's All the World's
Aircraft : development & production : 2012–13
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MTV-14 constant speed, 1.95 m (6 ft 5 in) diameter (diameter from )
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and was first flown in 2009. By
October 2011 only this first prototype has flown.
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The Votec 252T is a side-by side seat development of MSW's earlier
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179:, is under development but had not flown by October 2011.
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17.8 m/s (3,500 ft/min) maximum from sea level
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seat Votec 322. The prototype, powered by a modified
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320:1,398 km (869 mi, 755 nmi)
314:433 km/h (269 mph, 234 kn)
299:306 km/h (190 mph, 165 kn)
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305:106 km/h (66 mph, 57 kn)
190:Jane's All the World's Aircraft 2012–13
103:seating for two, designed and built in
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234:11.28 m (121.4 sq ft)
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222:7.70 m (25 ft 3 in)
216:6.75 m (22 ft 2 in)
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228:2.20 m (7 ft 3 in)
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507:Single-engined tractor aircraft
126:, marries the wooden wings and
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522:Aircraft first flown in 2009
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391:"MT Propellers – hydraulic"
369:. IHS Global. p. 615.
274:, 190 kW (250 hp)
255:950 kg (2,094 lb)
249:630 kg (1,389 lb)
145:are balanced with external
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497:2000s Swiss sport aircraft
336:Landing and take-off runs:
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365:Jackson, Paul A. (2012).
175:engine, redesignated the
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130:of the latter to a new,
195:General characteristics
59:MSW Aviation, built by
160:with fuselage mounted
158:tricycle undercarriage
111:Design and development
183:Specifications (252T)
121:Lycoming IO-540-J3A5
97:light-sport aircraft
35:light-sport aircraft
269:Lycoming AEIO-540-X
253:Max takeoff weight:
92:is a single engine
502:Homebuilt aircraft
310:Never exceed speed
512:Low-wing aircraft
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376:978-0-7106-3000-1
173:Lycoming AEIO-580
156:. It has a fixed
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61:Wassmer Aviation
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38:Type of aircraft
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272:flat-six engine
261:166 kg (365 lb)
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124:flat-six engine
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45:National origin
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166:speed fairings
164:legs and with
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90:MSW Votec 252T
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76:Developed from
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81:MSW Votec 322
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70:26 June 2009
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67:First flight
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56:Manufacturer
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517:MSW aircraft
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394:. Retrieved
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303:Stall speed:
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282:MT-Propeller
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239:Aspect ratio
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132:carbon fibre
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101:side-by-side
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28:Side-by-side
290:Performance
278:Propellers:
265:Powerplant:
139:low mounted
105:Switzerland
50:Switzerland
491:Categories
476:Votec 452T
471:Votec 352T
456:Votec 252T
345:References
232:Wing area:
177:Votec 352T
162:cantilever
466:Votec 351
461:Votec 322
451:Votec 221
396:19 August
324:g limits:
280:4-bladed
220:Wingspan:
208:Capacity:
188:Data from
128:empennage
32:homebuilt
30:two seat
441:aircraft
143:ailerons
135:fuselage
94:kitbuilt
226:Height:
214:Length:
373:
318:Range:
154:canopy
147:spades
117:tandem
338:300 m
202:Crew:
99:with
24:Role
19:252T
398:2012
371:ISBN
326:8/-8
267:1 ×
88:The
439:MSW
243:5.3
204:one
493::
353:^
149:.
431:e
424:t
417:v
400:.
379:.
312::
241::
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