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Chasle YC-10 Migrateur

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but after early flight trials streamlined wing tip bodies called salmons and also dihedral were added. It was powered by a 75 kW (100 hp)
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6.26 m (20 ft 6 in) (6.96 m (22 ft 10 in) after salmons and dihedral added)
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The Migrateur made its first flight on 29 May 1981. After only 29 hours of flight it crashed at
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The Chasle YC-10 was designed by Yves Chasle and built by Charles Pagès. It was a
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in the early 1980s. Only one was built and it flew for less than 30 hours.
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233 km/h (145 mph, 126 kn) at 1,500 m (4,921 ft)
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6.4 m (69 sq ft) before wing modifications
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and was not repaired. Only the prototype was built.
320:(2009 ed.). Brive: Ver Luisant. p. 211. 423: 318:Fox Papa - Registre des avions Français amateur 353: 116:, with the pilot under a prominent two piece 112:. Its single seat cockpit was over the wing 286: 284: 282: 78:was a single seat sports aircraft built in 360: 346: 279: 262:209 km/h (130 mph, 113 kn) 85: 367: 290: 424: 309: 341: 295:. Paris: Éditions EPA. p. 188. 155:had cantilever legs attached to the 315: 13: 293:Les Avions Francais de 1965 à 1990 197:6.20 m (20 ft 4 in) 14: 463: 169: 153:fixed conventional undercarriage 135:. This carried a deep, tapered 447:Single-engined tractor aircraft 229:Rolls-Royce Continental O-200-A 106:Rolls-Royce Continental O-200-A 1: 272: 123:. Behind, the round section 452:Aircraft first flown in 1981 7: 437:1980s French sport aircraft 221:520 kg (1,146 lb) 127:tapered rapidly to a broad 10: 468: 235:, 75 kW (100 hp) 27:Single seat sport aircraft 376: 291:Gaillard, Pierre (1991). 215:360 kg (794 lb) 18: 182:General characteristics 177:Gaillard (1981), p.188 86:Design and development 76:Chasle YC-10 Migrateur 151:mounted on top. Its 327:978-2-3555-1-066-3 316:Chillon, Jacques. 442:Low-wing aircraft 419: 418: 72: 71: 459: 362: 355: 348: 339: 338: 332: 331: 313: 307: 306: 288: 249: 184: 110:flat-four engine 65: 37: 29:Type of aircraft 19:YC-10 Migrateur 16: 15: 467: 466: 462: 461: 460: 458: 457: 456: 432:Chasle aircraft 422: 421: 420: 415: 372: 366: 336: 335: 328: 314: 310: 303: 289: 280: 275: 245: 180: 172: 88: 63: 36:National origin 35: 30: 12: 11: 5: 465: 455: 454: 449: 444: 439: 434: 417: 416: 414: 413: 408: 403: 398: 393: 388: 383: 377: 374: 373: 365: 364: 357: 350: 342: 334: 333: 326: 308: 301: 277: 276: 274: 271: 270: 269: 263: 257: 254:Maximum speed: 243: 242: 236: 222: 216: 210: 204: 198: 192: 171: 170:Specifications 168: 87: 84: 70: 69: 66: 60: 59: 56: 52: 51: 48: 44: 43: 38: 32: 31: 28: 25: 21: 20: 9: 6: 4: 3: 2: 464: 453: 450: 448: 445: 443: 440: 438: 435: 433: 430: 429: 427: 412: 409: 407: 404: 402: 399: 397: 394: 392: 391:Tourbillon II 389: 387: 384: 382: 379: 378: 375: 370: 363: 358: 356: 351: 349: 344: 343: 340: 329: 323: 319: 312: 304: 302:2 85120 392 4 298: 294: 287: 285: 283: 278: 267: 264: 261: 260:Cruise speed: 258: 255: 252: 251: 250: 248: 240: 237: 234: 230: 226: 223: 220: 219:Gross weight: 217: 214: 213:Empty weight: 211: 208: 205: 202: 199: 196: 193: 190: 187: 186: 185: 183: 178: 176: 167: 165: 160: 158: 154: 150: 146: 142: 139:and formed a 138: 134: 131:, triangular 130: 126: 122: 119: 115: 114:trailing edge 111: 107: 103: 99: 96: 93: 83: 81: 77: 67: 62: 61: 57: 55:First flight 54: 53: 49: 46: 45: 42: 39: 34: 33: 26: 23: 22: 17: 396:Raz de Mareé 380: 317: 311: 292: 265: 259: 253: 246: 244: 238: 224: 218: 212: 206: 200: 194: 188: 181: 179: 174: 173: 161: 89: 75: 73: 64:Number built 58:29 May 1981 50:Yves Chasle 369:Yves Chasle 247:Performance 239:Propellers: 231:air-cooled 225:Powerplant: 108:air-cooled 426:Categories 401:Hirondelle 386:Tourbillon 273:References 266:Endurance: 207:Wing area: 157:wing roots 95:cantilever 411:Sprintair 381:Migrateur 233:flat-four 201:Wingspan: 189:Capacity: 175:Data from 145:tailplane 143:with its 98:monoplane 47:Designer 371:aircraft 241:2-bladed 149:elevator 125:fuselage 102:dihedral 92:low wing 195:Length: 118:perspex 406:YC-320 324:  299:  164:Tarbes 141:T-tail 137:rudder 121:canopy 80:France 41:France 129:chord 24:Role 322:ISBN 297:ISBN 268:3 hr 227:1 × 147:and 74:The 191:One 133:fin 428:: 281:^ 159:. 68:1 361:e 354:t 347:v 330:. 305:.

Index

France
France
low wing
cantilever
monoplane
dihedral
Rolls-Royce Continental O-200-A
flat-four engine
trailing edge
perspex
canopy
fuselage
chord
fin
rudder
T-tail
tailplane
elevator
fixed conventional undercarriage
wing roots
Tarbes
Rolls-Royce Continental O-200-A
flat-four



ISBN
2 85120 392 4
ISBN
978-2-3555-1-066-3

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