Knowledge

MSW Votec 322

Source 📝

37: 182:, a single seater. This flew for the first time on 23 September 2006. It has the same external dimensions as the Votec 322 but is 50 kg (110 lb) lighter when empty and has the more powerful 261 kW (350 hp) 174:
flat-six piston engine driving a three-bladed tractor propeller. Later a four-bladed propeller was installed to reduce noise. The cockpit has room for two in tandem with a one-piece side-hinged canopy.
166:
first flew on 6 April 2001. The Votec 322 is a low-wing cantilever monoplane with a steel-tube fuselage, wooden wings with a carbon fibre fuselage skin, and
152: 193:, another Votec 322 variant, first flew on 4 June 2010. It is similar to its predecessor in span and weight but has a 336 kW (451 hp) 557: 140: 625: 548: 640: 516: 497: 615: 222:
In mid 2010 six Votec 322 aircraft appeared on the European civil registers, together with the lone 351 and the 452T.
478: 17: 620: 630: 541: 167: 431: 156: 132: 103: 635: 534: 194: 160: 178:
In 2006 the eighth Votec 322 was converted into the first and, as of October 2011, the only
8: 136: 53: 512: 493: 474: 427: 317: 183: 171: 186:
flat six engine. One consequence is an improvement in the climb rate of about 0.3%.
490:
Jane's All the World's Aircraft  : development & production : 2012-13
170:
with a steerable tailwheel. The aircraft is powered by a 330 hp (246 kW)
594: 589: 574: 115: 609: 584: 569: 214: in) longer. The prototype remains the only example in October 2011. 128: 197: 36: 526: 473:. Coulsdon, Surrey, United Kingdom: Jane's Information Group. 413:, page 112. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X 44:
Votec 322C landing in Ambri at the Oris Fly-In 2013.
234:Original tandem seat DR 107 One Design derivative. 607: 159:which MSW Aviation bought. The first prototype, 542: 250: 426:, page 118. Flying Pages Europe SARL, 2015. 411:World Directory of Leisure Aviation 2011-12 549: 535: 506: 471:Jane's All the World's Aircraft 2004-2005 424:World Directory of Light Aviation 2015-16 409:Bayerl, Robby; Martin Berkemeier; et al: 341:322 km/h (200 mph, 170 kn) 335:418 km/h (260 mph, 230 kn) 146: 131:two-seat low-wing monoplane based on the 441: 439: 487: 468: 396: 394: 392: 347:105 km/h (65 mph, 56 kn) 259:Jane's All the World's Aircraft 1989-90 246:Turboprop-powered, tandem-seat version. 14: 608: 217: 530: 436: 416: 403: 292:7.30 m (23 ft 11.5 in) 448: 389: 320:flat-six , 246 kW (330 hp) 422:Tacke, Willi; Marino Boric; et al: 298:2.50 m (8 ft 2.5 in) 24: 286:6.50 m (21 ft 4 in) 240:Single-seat, higher-power version. 25: 652: 371:17.8 m/s (3,500 ft/min) 556: 511:. Air Britain (Historians) Ltd. 509:European registers handbook 2010 35: 626:Single-engined tractor aircraft 461: 488:Jackson, Paul A., ed. (2012). 469:Jackson, Paul A., ed. (2004). 13: 1: 377: 641:Aircraft first flown in 2001 151:The MSW 322 was designed by 7: 310:950 kg (2,094 lb) 304:630 kg (1,389 lb) 225: 200:engine and is 700 mm ( 10: 657: 616:2000s Swiss sport aircraft 251:Specifications (Votec 322) 565: 507:Partington, Dave (2010). 168:conventional landing gear 43: 34: 29: 382: 265:General characteristics 445:Jackson 2012, pp.614-6 157:Rihn DR-107 One Design 147:Design and development 133:Rihn DR-107 One Design 104:Rihn DR-107 One Design 195:Rolls-Royce M250-B17D 155:and derived from the 400:Jackson 2004, p. 486 137:amateur construction 218:Operational history 621:Homebuilt aircraft 631:Low-wing aircraft 603: 602: 518:978-0-85130-425-0 499:978-0-7106-3000-1 353:3 hours 0 minutes 318:Lycoming AEIO-540 260: 184:Lycoming AEIO-580 172:Lycoming AEIO-540 135:and designed for 121: 120: 16:(Redirected from 648: 551: 544: 537: 528: 527: 522: 503: 484: 455: 454:Partington, 2010 452: 446: 443: 434: 420: 414: 407: 401: 398: 328: 267: 258: 213: 212: 208: 205: 112: 100: 66: 58:Type of aircraft 39: 27: 26: 21: 656: 655: 651: 650: 649: 647: 646: 645: 606: 605: 604: 599: 561: 555: 525: 519: 500: 481: 464: 459: 458: 453: 449: 444: 437: 421: 417: 408: 404: 399: 390: 385: 380: 324: 263: 253: 228: 220: 210: 206: 203: 201: 149: 110: 98: 65:National origin 64: 59: 23: 22: 15: 12: 11: 5: 654: 644: 643: 638: 633: 628: 623: 618: 601: 600: 598: 597: 592: 587: 582: 577: 572: 566: 563: 562: 554: 553: 546: 539: 531: 524: 523: 517: 504: 498: 492:. IHS Global. 485: 479: 465: 463: 460: 457: 456: 447: 435: 415: 402: 387: 386: 384: 381: 379: 376: 373: 372: 369:Rate of climb: 366: 360: 354: 348: 342: 336: 333:Maximum speed: 322: 321: 311: 305: 299: 293: 287: 281: 275: 252: 249: 248: 247: 244: 241: 238: 235: 232: 227: 224: 219: 216: 148: 145: 119: 118: 113: 111:Developed into 107: 106: 101: 99:Developed from 95: 94: 91: 87: 86: 85:Max Vogelsang 83: 79: 78: 75: 71: 70: 67: 61: 60: 57: 50: 46: 45: 41: 40: 32: 31: 18:MSW Votec 452T 9: 6: 4: 3: 2: 653: 642: 639: 637: 634: 632: 629: 627: 624: 622: 619: 617: 614: 613: 611: 596: 593: 591: 588: 586: 583: 581: 578: 576: 573: 571: 568: 567: 564: 559: 552: 547: 545: 540: 538: 533: 532: 529: 520: 514: 510: 505: 501: 495: 491: 486: 482: 480:0-7106-2614-2 476: 472: 467: 466: 451: 442: 440: 433: 429: 425: 419: 412: 406: 397: 395: 393: 388: 375: 370: 367: 364: 361: 358: 355: 352: 349: 346: 343: 340: 339:Cruise speed: 337: 334: 331: 330: 329: 327: 319: 315: 312: 309: 308:Gross weight: 306: 303: 302:Empty weight: 300: 297: 294: 291: 288: 285: 282: 279: 276: 273: 270: 269: 268: 266: 261: 257: 245: 242: 239: 236: 233: 230: 229: 223: 215: 199: 196: 192: 187: 185: 181: 176: 173: 169: 165: 162: 158: 154: 153:Max Vogelsang 144: 142: 138: 134: 130: 126: 125:MSW Votec 322 117: 114: 109: 108: 105: 102: 97: 96: 93:6 April 2001 92: 90:First flight 89: 88: 84: 81: 80: 77:MSW Aviation 76: 74:Manufacturer 73: 72: 68: 63: 62: 55: 51: 48: 47: 42: 38: 33: 28: 19: 636:MSW aircraft 579: 508: 489: 470: 462:Bibliography 450: 423: 418: 410: 405: 374: 368: 362: 356: 350: 345:Stall speed: 344: 338: 332: 325: 323: 313: 307: 301: 295: 289: 283: 277: 271: 264: 262: 255: 254: 221: 190: 188: 179: 177: 163: 150: 141:MSW Aviation 124: 122: 69:Switzerland 326:Performance 314:Powerplant: 280:1 passenger 143:of Wohlen. 610:Categories 595:Votec 452T 590:Votec 352T 575:Votec 252T 378:References 363:Roll rate: 351:Endurance: 243:Votec 452T 191:Votec 452T 161:registered 116:Votec 252T 56:sportplane 30:Votec 322 585:Votec 351 580:Votec 322 570:Votec 221 432:1368-485X 357:g limits: 290:Wingspan: 278:Capacity: 256:Data from 237:Votec 351 231:Votec 322 198:turboprop 180:Votec 351 82:Designer 54:homebuilt 52:Two-seat 560:aircraft 226:Variants 296:Height: 284:Length: 209:⁄ 515:  496:  477:  430:  365:420°/s 164:HB-YJY 383:Notes 272:Crew: 129:Swiss 127:is a 49:Role 513:ISBN 494:ISBN 475:ISBN 428:ISSN 316:1 × 189:The 123:The 558:MSW 359:±10 139:by 612:: 438:^ 391:^ 202:27 550:e 543:t 536:v 521:. 502:. 483:. 274:1 211:2 207:1 204:+ 20:)

Index

MSW Votec 452T

homebuilt
Rihn DR-107 One Design
Votec 252T
Swiss
Rihn DR-107 One Design
amateur construction
MSW Aviation
Max Vogelsang
Rihn DR-107 One Design
registered
conventional landing gear
Lycoming AEIO-540
Lycoming AEIO-580
Rolls-Royce M250-B17D
turboprop
Lycoming AEIO-540



ISSN
1368-485X


ISBN
0-7106-2614-2
ISBN
978-0-7106-3000-1
ISBN

Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.