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SIPA S.90

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In later years, the S.90 series readily found buyers in the secondhand market and examples have flown with private owners in Belgium, Germany, Switzerland and the United Kingdom. Nine further aircraft were built later with plywood covering in lieu of fabric, receiving new designations. In 2001, 15
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100 aircraft were ordered by the French government, on behalf of the aeroclubs, and these were powered by the 75 hp (56 kW) Minie 4DC engine as the SIPA S.901. The first made its initial flight on 25 June 1948. Deliveries were completed in the early 1950s. Various engines were later
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The initial production S.90 was a low-wing aircraft with fixed tailwheel undercarriage and side-by-side seating for two. It was powered by a 75 hp (56 kW)
143:(SIPA). The prototype first flew on 15 May 1947, winning a French government competition for a new light two-seat aircraft for operation by the French aero clubs. 531: 140: 67: 264: 238: 254: 646: 136: 198: 147: 563: 558: 636: 728: 522: 743: 738: 491: 472: 178:
A SIPA S.903 in 1989; this Swiss-registered variant was powered by the 90 hp (67 kW) Continental C90 engine
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4-cylinder air-cooled horizontally-opposed piston engine, 64 kW (86 hp)
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2 new aircraft as S.902 but with plywood-covered fuselage and wings
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examples remained airworthy in France, Switzerland and the UK.
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installed in the S.901, giving rise to new model numbers.
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1 passenger or a payload of 234 kg (516 lb)
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5 new aircraft as S.91 with 90 hp (67 kW)
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1 new aircraft as S.91 with 75 hp (56 kW)
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1 new aircraft as S.91 with 85 hp (63 kW)
166:Total production of all models was 113 aircraft. 715: 532:Société Industrielle Pour l’Aéronautique (SIPA) 281: 123:was a French-built two-seat light touring and 630: 516: 637: 623: 523: 509: 207:100 aircraft with 75 hp (56 kW) 376:194 km/h (121 mph, 105 kn) 370:217 km/h (135 mph, 117 kn) 153: 211:engine. Most were re-engined as follows. 197:4 aircraft with 75 hp (56 kW) 181: 173: 141:Société Industrielle Pour l’Aéronautique 33:SIPA S.901 at Berck-sur-Mer in May 1957 481: 462: 458:. Macdonald & Co. (Publishers) Ltd. 382:510 km (320 mi, 280 nmi) 716: 190:The following variants were produced: 618: 504: 453: 315:5.74 m (18 ft 10 in) 237:S.901 with 75 hp (56 kW) 227:S.901 with 90 hp (67 kW) 217:S.901 with 85 hp (63 kW) 13: 391:0.11 kW/kg (0.067 hp/lb) 321:8.74 m (28 ft 8 in) 150:engine. Four examples were built. 14: 755: 327:1.75 m (5 ft 9 in) 186:SIPA 903 at Old Warden, June 2014 24: 729:Single-engined tractor aircraft 434: 425: 416: 407: 355:2-bladed fixed-pitch propeller 135:The SIPA S.90 was designed by 1: 484:The General Aviation Handbook 395: 744:Aircraft first flown in 1947 7: 739:1940s French sport aircraft 339:600 kg (1,323 lb) 282:Specifications (SIPA S.902) 169: 10: 760: 467:. Airlife Publishing Ltd. 653: 539: 456:The Aircraft of the World 431:Simpson, 2005, p. 280-281 333:366 kg (807 lb) 130: 32: 23: 18: 465:Airlife's World Aircraft 289:Airlife's World Aircraft 127:of the 1940s and 1950s. 454:Green, William (1955). 294:General characteristics 486:. Midland Publishing. 187: 179: 154:Production and service 645:Aircraft designed by 482:Simpson, Rod (2005). 463:Simpson, Rod (2001). 440:Simpson, 2001, p. 508 413:Simpson, 2005, p. 280 185: 177: 422:Green, 1955, p. 171 347:Continental C85-12F 229:Continental C90-14F 219:Continental C85-12F 103:1948 - early 1950s 90:Primary users 275:Continental C90-8F 188: 180: 95:French aero clubs 734:Low-wing aircraft 711: 710: 612: 611: 125:training aircraft 117: 116: 751: 639: 632: 625: 616: 615: 525: 518: 511: 502: 501: 497: 478: 459: 441: 438: 432: 429: 423: 420: 414: 411: 363: 296: 110: 54: 46:Type of aircraft 43:trainer aircraft 28: 16: 15: 759: 758: 754: 753: 752: 750: 749: 748: 714: 713: 712: 707: 649: 643: 613: 608: 535: 529: 494: 475: 445: 444: 439: 435: 430: 426: 421: 417: 412: 408: 398: 359: 292: 284: 172: 156: 133: 108: 94: 53:National origin 52: 47: 12: 11: 5: 757: 747: 746: 741: 736: 731: 726: 709: 708: 706: 705: 700: 695: 690: 685: 680: 675: 670: 665: 660: 654: 651: 650: 642: 641: 634: 627: 619: 610: 609: 607: 606: 601: 596: 591: 586: 584:S.251 Antilope 581: 576: 571: 566: 561: 556: 551: 546: 540: 537: 536: 528: 527: 520: 513: 505: 499: 498: 492: 479: 473: 460: 450: 449: 443: 442: 433: 424: 415: 405: 404: 403: 402: 397: 394: 393: 392: 383: 377: 371: 368:Maximum speed: 357: 356: 350: 340: 334: 328: 322: 316: 310: 304: 283: 280: 279: 278: 271: 268: 265:Salmson 5AQ-01 261: 258: 251: 248: 245: 242: 239:Salmson 5AQ-01 235: 232: 225: 222: 215: 212: 205: 202: 195: 171: 168: 155: 152: 132: 129: 115: 114: 111: 105: 104: 101: 97: 96: 93:private owners 91: 87: 86: 83: 79: 78: 75: 71: 70: 65: 61: 60: 55: 49: 48: 45: 39: 35: 34: 30: 29: 21: 20: 9: 6: 4: 3: 2: 756: 745: 742: 740: 737: 735: 732: 730: 727: 725: 724:SIPA aircraft 722: 721: 719: 704: 701: 699: 696: 694: 691: 689: 686: 684: 681: 679: 676: 674: 671: 669: 666: 664: 661: 659: 656: 655: 652: 648: 640: 635: 633: 628: 626: 621: 620: 617: 605: 602: 600: 597: 595: 592: 590: 587: 585: 582: 580: 579:S.200 Minijet 577: 575: 572: 570: 567: 565: 562: 560: 557: 555: 552: 550: 547: 545: 542: 541: 538: 533: 526: 521: 519: 514: 512: 507: 506: 503: 495: 493:1-85780-222-5 489: 485: 480: 476: 474:1-84037-115-3 470: 466: 461: 457: 452: 451: 447: 446: 437: 428: 419: 410: 406: 400: 399: 390: 388: 384: 381: 378: 375: 374:Cruise speed: 372: 369: 366: 365: 364: 362: 354: 351: 348: 344: 341: 338: 337:Gross weight: 335: 332: 331:Empty weight: 329: 326: 323: 320: 317: 314: 311: 308: 305: 302: 299: 298: 297: 295: 290: 288: 276: 272: 269: 266: 262: 259: 256: 255:Mathis 4GB-62 252: 249: 246: 243: 240: 236: 233: 230: 226: 223: 220: 216: 213: 210: 209:Minié 4.DC.32 206: 203: 200: 196: 193: 192: 191: 184: 176: 167: 164: 160: 151: 149: 144: 142: 138: 128: 126: 122: 112: 107: 106: 102: 99: 98: 92: 89: 88: 84: 82:Introduction 81: 80: 76: 74:First flight 73: 72: 69: 66: 64:Manufacturer 63: 62: 59: 56: 51: 50: 44: 41:Personal and 40: 37: 36: 31: 27: 22: 17: 657: 573: 483: 464: 455: 448:Bibliography 436: 427: 418: 409: 385: 379: 373: 367: 360: 358: 352: 342: 336: 330: 324: 318: 312: 306: 300: 293: 291: 286: 285: 189: 165: 161: 157: 145: 134: 120: 118: 109:Number built 77:15 May 1947 19:S.90 series 647:Yves Gardan 589:S.261 Anjou 361:Performance 353:Propellers: 343:Powerplant: 137:Yves Gardan 718:Categories 396:References 387:Power/mass 199:Mathis G4F 148:Mathis G4F 319:Wingspan: 307:Capacity: 287:Data from 121:SIPA S.90 100:Produced 534:aircraft 170:Variants 139:for the 325:Height: 313:Length: 703:GY-120 698:GY-110 693:GY-100 668:S.1100 663:S.1000 604:S.1100 599:S.1000 490:  471:  380:Range: 277:engine 267:engine 257:engine 241:engine 231:engine 221:engine 201:engine 131:Design 58:France 688:GY-90 683:GY-80 678:GY-30 673:GY-20 594:S.300 401:Notes 301:Crew: 234:S.904 224:S.903 214:S.902 204:S.901 85:1948 38:Role 658:S.90 574:S.90 569:S.70 564:S.50 559:S.20 554:S.12 549:S.11 544:S.10 488:ISBN 469:ISBN 345:1 × 270:S.94 260:S.93 250:S.92 244:S.91 194:S.90 119:The 113:113 68:SIPA 720:: 638:e 631:t 624:v 524:e 517:t 510:v 496:. 477:. 389:: 303:1

Index


trainer aircraft
France
SIPA
training aircraft
Yves Gardan
Société Industrielle Pour l’Aéronautique
Mathis G4F


Mathis G4F
Minié 4.DC.32
Continental C85-12F
Continental C90-14F
Salmson 5AQ-01
Mathis 4GB-62
Salmson 5AQ-01
Continental C90-8F
Continental C85-12F
Power/mass
ISBN
1-84037-115-3
ISBN
1-85780-222-5
v
t
e
Société Industrielle Pour l’Aéronautique (SIPA)
S.10
S.11

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