420:
40:
431:
452:
444:
368:
604:
345:
While the C90 is approved for takeoff power of 95 horsepower (71 kW) for five minutes, the designation is derived from its continuous power rating of 90 hp (67 kW). As noted above, certain models of the C90 replace the usual carburetor with a fuel injection system. In addition, there
249:
produced these same designs in
England, under separate certification, with model designations beginning RR, e.g. the Rolls-Royce RR C90-12FH is the equivalent of the Continental C90-12FH; the Rolls-Royce versions are "directly interchangeable with the equivalent models manufactured by Continental."
358:
The O-200 is an updated and upgraded version of the engine, achieving increased power of 100 hp (75 kW) as a result of higher maximum rpm. The standard and most common model of the engine is the O-200-A; the -B model is designed for a pusher installation, the -C model provides for the
354:
installation. While having slightly less horsepower than the O-200, many floatplane operators prefer the performance of the C90 over the O-200, due to its higher torque at lower rpm. This is primarily due to the C90's camshaft design. The C90 is also known by its military designation of O-205.
1264:
Vol. 69, No. 143 (Jul. 27, 2004), pp. 44772-44882. Federal
Aviation Administration, 14 CFR Parts 1, 21, et al., "Certification of aircraft and airmen for the operation of light-sport aircraft;" Final rule.
1192:
194:
Though the C90 was superseded by the O-200, and many of the designs utilizing the O-200 had gone out of production by 1980, with the 2004 publication of the United States
Federal Aviation Administration
1441:
1848:
2335:
398:, designed and flown by Jon Sharp, was powered by a 'stock' O-200. Between 1991 and 1999, the aircraft won 45 of the 48 events in which it was entered, as well as winning three
2704:
1601:
330:(TBO) for these engines is 1,800 hours of operation or 12 years in service, whichever is reached first. The standard certification for the C90 and O-200 specifies
2002:
1189:
387:. The 110-horsepower (82 kW) IOL-200, also referred to as the Voyager 200, was the rear engine and—unlike the forward engine, another modified engine, a
2603:
1969:
2015:
2167:
2086:
1445:
2385:
2182:
2129:
1923:
1720:
1662:
1640:
211:, which had been in production since 1939. Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the
2613:
2593:
2445:
2177:
2063:
2618:
2608:
2345:
2139:
2124:
2162:
2109:
1415:(Jun. 15, 2006) Luftfahrt-Bundesamt (Federal Office of Civil Aviation). Federal Minister of Transport, Building and Urban Affairs. Germany.
406:
was clocked at more than 290 mph (467 km/h). By contrast, the O-200 powered Legend Cub cruises at 95 mph (152.9 km/h).
2725:
2455:
2350:
2340:
1995:
1487:
2480:
1516:
1574:
2525:
1988:
2756:
347:
1608:
399:
359:
installation of a controllable-pitch propeller, and the -D model is a lower-weight version designed for light-sport aircraft.
2761:
2730:
2545:
1655:
473:
Lacks provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
2560:
2450:
503:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
497:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
491:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
485:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
2520:
2510:
2011:
2515:
1671:
1670:
782:
707:
2495:
1980:
1648:
1372:(Jun. 27, 2003.) Department of Transportation. Federal Aviation Administration. Aircraft Certification Service.
1185:
17:
1635:
2465:
692:
1545:
1298:
1413:
List 4: Propeller-driven aeroplanes not exceeding 8618 kg MTOM (including self-launching powered sailplanes.
339:
2550:
737:
632:
527:
Has vacuum pump drive provisions, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
172:
78:
572:
Similar to the "D" model except for engine dataplate identification, 100 hp (75 kW) continuous
242:
This engine family is considered to be dependable, according to both industry publications and the FAA.
2540:
2058:
2053:
867:
847:
2720:
2535:
2048:
2038:
702:
419:
2555:
2395:
2119:
1785:
1598:
1126:
391:—ran throughout the entire nine-day flight save for a four-minute shutdown due to a fuel problem.
2490:
2475:
2460:
762:
288:
and are all similar in size, displacement and weight. These engines are typically fitted with an
39:
697:
175:
these engines are used in many light aircraft designs of the United States, including the early
2751:
2440:
2425:
2420:
2375:
1933:
1887:
1240:
Revision 33. (Jul. 14, 2005.) Department of
Transportation. Federal Aviation Administration.
837:
267:
184:
1341:
Revision 23. (Jul. 8, 1993.) Department of
Transportation. Federal Aviation Administration.
1329:
Revision 32. (Oct. 1, 1997.) Department of
Transportation. Federal Aviation Administration.
1252:
Revision 44. (Mar. 31, 2003) Department of
Transportation. Federal Aviation Administration.
1228:
Revision 67. (Jun. 3, 2005.) Department of
Transportation. Federal Aviation Administration.
1213:
Revision 37. (Sep. 4, 1996.) Department of
Transportation. Federal Aviation Administration.
402:, four Pulitzer Trophies, and setting 16 speed records in its class. In one of those records,
168:
of 201 in (3.29 L) displacement, producing between 90 and 100 horsepower (67 and 75 kW).
2628:
2530:
2505:
2500:
1682:
1495:
1396:
Revision 3. (Jun. 19, 1979) Department of
Transportation. Federal Aviation Administration.
1384:
Revision 3. (Jan. 16, 1968) Department of Transportation. Federal Aviation Administration.
1067:
882:
877:
802:
742:
687:
560:
Model with provisions for a controllable pitch propeller, 100 hp (75 kW) continuous
541:
327:
106:
1524:
430:
807:
551:
351:
285:
196:
131:
8:
2081:
1951:
1795:
1439:
941:
857:
717:
566:
Similar to the "A" model, but with weight reductions, 100 hp (75 kW) continuous
271:
246:
2638:
2302:
2252:
1905:
1900:
1895:
1873:
1853:
1843:
1838:
892:
777:
732:
289:
2400:
2287:
2277:
2212:
2197:
1928:
1868:
1863:
1858:
1833:
1828:
1823:
1808:
1803:
1780:
1775:
1770:
1765:
1760:
1755:
1750:
1740:
1735:
1730:
1725:
1715:
1710:
1092:
1058:
722:
637:
388:
309:
282:
224:
144:
2010:
2565:
2307:
2091:
2043:
1087:
993:
Hydraulic lifters, two pushrod-actuated valves—one intake, one exhaust—per cylinder
872:
862:
852:
747:
727:
617:
301:
125:
662:
259:
2583:
2317:
2101:
1705:
1674:
1196:
932:
672:
667:
335:
297:
208:
165:
58:
1672:
Continental Motors, Teledyne Continental, and Continental Aerospace Technologies
2643:
2633:
2623:
2485:
2470:
2405:
2312:
2297:
2292:
2282:
2272:
2267:
2262:
2257:
2247:
2242:
2237:
2232:
2222:
2207:
2202:
2192:
2187:
2114:
2033:
1109:
1104:
1004:
822:
383:, powered the 1986 nonstop, non-refueled global circumnavigation flight of the
380:
376:
320:
293:
275:
772:
2745:
2390:
2370:
2360:
2327:
1915:
1049:
923:
887:
842:
832:
827:
647:
592:
395:
384:
255:
216:
180:
2684:
2666:
2661:
2598:
2588:
2435:
2430:
2415:
2172:
2134:
817:
812:
712:
652:
622:
316:
274:
and the Reims F150 (a version of the Cessna 150 license-built in France by
263:
114:
110:
2154:
2144:
797:
787:
752:
642:
521:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
515:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
509:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
479:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
176:
2410:
2380:
2365:
2355:
1000:
988:
974:
968:
792:
767:
682:
677:
657:
627:
608:
305:
251:
220:
188:
102:
98:
451:
1961:
1114:
757:
443:
331:
212:
367:
2694:
2676:
2653:
2575:
2073:
2023:
1943:
1553:
1467:
1306:
1274:
1024:
603:
375:
An engine designated the IOL-200, an O-200 variant modified with
1440:
Department of Transportation. Federal Aviation Administration.
313:
161:
55:
611:
built, this type is the most common application for the O-200.
334:
as the minimum fuel grade. Both are eligible for operation on
1687:
1014:
1424:
919:
Four-cylinder air-cooled horizontally opposed piston engine
292:, though the C90-8FJ, -12FJ, and -14FJ are equipped with
1370:
Special airworthiness information bulletin no. NE-03-45.
199:
regulations came a resurgence in demand for the O-200.
207:
The C90 was introduced in 1947 as a follow-on to the
1597:
1351:Berry, Mike (September 2004). "Continental O-200".
346:are models which provide for the installation of a
1303:Teledyne Continental Motors: Company Information
2743:
550:Model with special crankshaft and crankcase for
585:UL91 and UL94 95 hp alternate fuel engine.
1459:
1996:
1656:
1180:
1178:
1176:
1174:
1172:
1170:
1168:
1166:
1164:
1162:
591:The aft engine of the round the world flight
223:A. The engine was developed from the earlier
1509:
1480:
1408:
1406:
1404:
1402:
1160:
1158:
1156:
1154:
1152:
1150:
1148:
1146:
1144:
1142:
1521:Smithsonian: National Air and Space Museum
1492:Smithsonian: National Air and Space Museum
1291:
899:
2003:
1989:
1663:
1649:
1425:Teledyne Continental Motors (2003-03-28).
1387:
1279:Aerofiles: A Century of American Aviation
1221:
1219:
910:
1602:"Engine specifications: O-200-A & B"
1591:
1465:
1399:
1375:
1231:
1139:
907:Engine specifications: O-200-A & B.
576:
300:requiring no external power, driving two
202:
1433:
1418:
1332:
1267:
1243:
602:
450:
442:
436:Two views of an O-200-A in a Cessna 150H
366:
1538:
1320:
1216:
14:
2744:
1394:Type certificate data sheet no. A22EU.
1238:Type certificate date sheet no. A-787.
362:
350:and one, the C90-12FP, designed for a
281:All versions of the C90 and O-200 are
1984:
1644:
1382:Type certificate data sheet no. E3IN.
1350:
1250:Type certificate data sheet no. 3A19.
1204:
1190:Type certificate data sheet no. E-252
554:, 100 hp (75 kW) continuous
544:, 100 hp (75 kW) continuous
459:
1363:
2726:US military gas turbine aeroengines
1427:Service Information Letter SIL98-9A
1344:
296:systems. They utilize a redundant
250:The Rolls-Royce O-200-A powers the
162:horizontally opposed, four-cylinder
24:
1255:
47:O-200-A installed in a Cessna 150
25:
2773:
1629:
1339:Aircraft specification no. A-694.
1327:Aircraft specification no. A-691.
1226:Aircraft specification no. A-759.
783:Miller-Bohannon JM-2 Pushy Galore
708:CubCrafters CC11-100 Sport Cub S2
1550:American Legend Aircraft Company
429:
418:
38:
1567:
1211:Aircraft specification no. 1A2.
1186:Federal Aviation Administration
803:Piper PA-18-95 Super Cub, L-18C
598:
1036:
798:Piper PA-11 Cub Special, L-18B
693:Civil Aviation Department MG-1
340:Supplemental Type Certificates
13:
1:
2757:1940s aircraft piston engines
1132:
981:
623:Aeronca L-16B (Champion 7CCM)
2762:Continental aircraft engines
2731:Piston engine configurations
738:Flaeming Air FA 04 Peregrine
633:American Homebuilts John Doe
348:controllable-pitch propeller
160:are a family of air-cooled,
7:
1636:Teledyne Continental Motors
1201:Revision 34. (27 June 2013)
1076:
409:
79:Teledyne Continental Motors
10:
2778:
868:VTOL Aircraft Phillicopter
848:Taylorcraft F-19 Sportsman
326:Continental's recommended
323:valve, pushrod-activated.
304:, each of which fires one
245:In a cooperative venture,
27:Family of aircraft engines
2713:
2693:
2675:
2652:
2574:
2326:
2153:
2100:
2072:
2022:
1960:
1942:
1914:
1886:
1794:
1696:
1681:
703:CubCrafters Carbon Cub EX
618:Aeronca Champion 7EC, 7FC
312:. Each cylinder has one
227:by increasing the stroke
46:
37:
32:
1546:"The Rebirth of the Cub"
1127:List of aircraft engines
900:Specifications (O-200-A)
531:
2697:W-configuration inline)
2026:H-configuration inline)
2014:piston aircraft engine
1888:Aircraft Diesel engines
1599:Continental Motors Inc.
1517:"Sharp DR 90 "Nemesis""
1466:Aerofiles (July 2009).
1353:Light Plane Maintenance
1072:0.56 hp/lb (0.92 kW/kg)
911:General characteristics
763:Jodel DR1050 Excellence
215:and PA-11 Cub Special,
2677:VG (inverted-V inline)
2102:L (single-bank inline)
2074:IV (inverted-V inline)
2012:United States military
1699:horsepower designation
1683:Opposed piston engines
838:Ryson ST-100 Cloudster
753:IndUS Aviation Sport E
612:
577:Non-certified versions
464:
456:
448:
372:
268:Morane-Saulnier MS-880
260:Bölkow Bo 208 C Junior
203:Design and development
2654:V (inverted-V inline)
1442:"STC number SE2031CE"
1068:Power-to-weight ratio
977:, without accessories
973:170.18 lb (77.19 kg)
883:World Aircraft Spirit
878:Williams W-17 Stinger
743:Fleet Model 80 Canuck
698:Coupé-Aviation JC-200
688:Cessna 162 Skycatcher
606:
542:tractor configuration
454:
446:
370:
328:time between overhaul
286:reciprocating engines
177:Piper PA-18 Super Cub
107:Cessna 162 Skycatcher
2576:V (upright-V inline)
1299:"Company Background"
1023:6 US quart (5.7 L),
808:Pottier P.60 Minacro
552:pusher configuration
400:Louis Blèriot medals
352:pusher configuration
197:light-sport aircraft
1082:Related development
1054:0.5 hp/in (23 kW/L)
964:23.18 in (588.8 mm)
958:31.56 in (801.6 mm)
952:28.53 in (724.7 mm)
858:Victa Airtourer 100
718:Falconar F11 Sporty
588:IOL-200/Voyager 200
371:Continental IOL-200
363:Operational history
336:automobile gasoline
272:Victa Airtourer 100
264:Avions Robin DR 220
2016:designation system
1944:Inverted-V engines
1195:2021-06-02 at the
1099:Comparable engines
928:4.06 in (103.1 mm)
893:Zenith STOL CH 750
778:Mignet Pou-du-Ciel
768:Luscombe 8F, LSA-8
733:Fisher Dakota Hawk
613:
460:Certified versions
457:
449:
447:Continental O-200D
394:Formula One racer
373:
290:updraft carburetor
173:Continental Motors
130:2004-present (for
94:Major applications
2739:
2738:
1978:
1977:
1882:
1881:
1262:Federal Register.
1093:Continental O-300
1059:Compression ratio
937:3.88 in (98.6 mm)
723:Falconar Minihawk
638:Anglin J6 Karatoo
389:Continental O-240
238:
150:
149:
145:Continental O-190
16:(Redirected from
2769:
2005:
1998:
1991:
1982:
1981:
1694:
1693:
1675:aircraft engines
1665:
1658:
1651:
1642:
1641:
1623:
1622:
1620:
1619:
1613:
1607:. Archived from
1606:
1595:
1589:
1588:
1586:
1584:
1579:
1571:
1565:
1564:
1562:
1561:
1552:. Archived from
1542:
1536:
1535:
1533:
1532:
1523:. Archived from
1513:
1507:
1506:
1504:
1503:
1494:. Archived from
1484:
1478:
1477:
1475:
1474:
1463:
1457:
1456:
1454:
1453:
1444:. Archived from
1437:
1431:
1430:
1422:
1416:
1410:
1397:
1391:
1385:
1379:
1373:
1367:
1361:
1360:
1348:
1342:
1336:
1330:
1324:
1318:
1317:
1315:
1314:
1305:. Archived from
1295:
1289:
1288:
1286:
1285:
1271:
1265:
1259:
1253:
1247:
1241:
1235:
1229:
1223:
1214:
1208:
1202:
1182:
1088:Continental A-65
873:Warner Sportster
863:VSR SR-1 Snoshoo
853:Vashon Ranger R7
748:Interstate Cadet
728:Fisher Celebrity
433:
422:
338:on the basis of
237:
236:
232:
228:
166:aircraft engines
141:
124:1947-1980s (for
95:
67:
42:
30:
29:
21:
2777:
2776:
2772:
2771:
2770:
2768:
2767:
2766:
2742:
2741:
2740:
2735:
2709:
2696:
2689:
2671:
2648:
2570:
2322:
2149:
2096:
2068:
2025:
2018:
2009:
1979:
1974:
1956:
1938:
1910:
1901:CD-200 (TD-300)
1878:
1796:By displacement
1790:
1698:
1685:
1677:
1669:
1632:
1627:
1626:
1617:
1615:
1611:
1604:
1596:
1592:
1582:
1580:
1577:
1573:
1572:
1568:
1559:
1557:
1544:
1543:
1539:
1530:
1528:
1515:
1514:
1510:
1501:
1499:
1488:"Rutan Voyager"
1486:
1485:
1481:
1472:
1470:
1464:
1460:
1451:
1449:
1438:
1434:
1423:
1419:
1411:
1400:
1392:
1388:
1380:
1376:
1368:
1364:
1349:
1345:
1337:
1333:
1325:
1321:
1312:
1310:
1297:
1296:
1292:
1283:
1281:
1273:
1272:
1268:
1260:
1256:
1248:
1244:
1236:
1232:
1224:
1217:
1209:
1205:
1197:Wayback Machine
1183:
1140:
1135:
1079:
1039:
1030:Cooling system:
984:
946:201 in (3.29 L)
913:
902:
897:
673:Cassutt Special
668:Bushcaddy R-120
601:
579:
534:
467:
462:
441:
440:
439:
438:
437:
434:
425:
424:
423:
412:
365:
298:ignition system
256:Rollason Condor
234:
230:
229:
205:
164:, direct-drive
154:Continental C90
139:
129:
113:
109:
105:
101:
93:
66:National origin
65:
59:aircraft engine
28:
23:
22:
18:Continental C90
15:
12:
11:
5:
2775:
2765:
2764:
2759:
2754:
2737:
2736:
2734:
2733:
2728:
2723:
2714:
2711:
2710:
2708:
2707:
2701:
2699:
2695:W (three-bank
2691:
2690:
2688:
2687:
2681:
2679:
2673:
2672:
2670:
2669:
2664:
2658:
2656:
2650:
2649:
2647:
2646:
2641:
2636:
2631:
2626:
2621:
2616:
2611:
2606:
2601:
2596:
2591:
2586:
2580:
2578:
2572:
2571:
2569:
2568:
2563:
2558:
2553:
2548:
2543:
2538:
2533:
2528:
2523:
2518:
2513:
2508:
2503:
2498:
2493:
2488:
2483:
2478:
2473:
2468:
2463:
2458:
2453:
2448:
2443:
2438:
2433:
2428:
2423:
2418:
2413:
2408:
2403:
2398:
2393:
2388:
2383:
2378:
2373:
2368:
2363:
2358:
2353:
2348:
2343:
2338:
2332:
2330:
2324:
2323:
2321:
2320:
2315:
2310:
2305:
2300:
2295:
2290:
2285:
2280:
2275:
2270:
2265:
2260:
2255:
2250:
2245:
2240:
2235:
2230:
2225:
2220:
2215:
2210:
2205:
2200:
2195:
2190:
2185:
2180:
2175:
2170:
2165:
2159:
2157:
2151:
2150:
2148:
2147:
2142:
2137:
2132:
2127:
2122:
2117:
2112:
2106:
2104:
2098:
2097:
2095:
2094:
2089:
2084:
2078:
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1045:100 hp (75 kW)
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381:liquid cooling
377:fuel injection
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294:fuel injection
276:Reims Aviation
254:Series 1, the
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1634:
1633:
1614:on 2018-12-22
1610:
1603:
1600:
1594:
1576:
1570:
1556:on 2006-10-05
1555:
1551:
1547:
1541:
1527:on 2006-09-01
1526:
1522:
1518:
1512:
1498:on 2006-10-23
1497:
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1469:
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1448:on 2018-05-01
1447:
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1428:
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1309:on 2006-11-24
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1121:Related lists
1116:
1113:
1111:
1108:
1106:
1103:
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1100:
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1091:
1089:
1086:
1085:
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1043:Power output:
1041:
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888:Zodiac 601 HD
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843:Socata Rallye
841:
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833:Rutan VariEze
831:
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828:Rutan Voyager
826:
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663:Bölkow Bo 208
661:
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648:Barbaro RB-50
646:
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634:
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593:Rutan Voyager
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396:Sharp Nemesis
392:
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385:Rutan Voyager
382:
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226:
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214:
213:Piper J-3 Cub
210:
200:
198:
192:
190:
186:
185:Alon Aircoupe
182:
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169:
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155:
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75:Manufacturer
74:
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57:
54:
51:
50:
45:
41:
36:
31:
19:
2717:
2227:
2217:
1818:
1813:
1786:Tiara series
1745:
1616:. Retrieved
1609:the original
1593:
1581:. Retrieved
1569:
1558:. Retrieved
1554:the original
1549:
1540:
1529:. Retrieved
1525:the original
1520:
1511:
1500:. Retrieved
1496:the original
1491:
1482:
1471:. Retrieved
1461:
1450:. Retrieved
1446:the original
1435:
1426:
1420:
1412:
1393:
1389:
1381:
1377:
1369:
1365:
1356:
1352:
1346:
1338:
1334:
1326:
1322:
1311:. Retrieved
1307:the original
1302:
1293:
1282:. Retrieved
1278:
1269:
1261:
1257:
1249:
1245:
1237:
1233:
1225:
1210:
1206:
1184:
1120:
1119:
1098:
1097:
1081:
1080:
1066:
1057:
1048:
1042:
1029:
1020:
1010:
1003:with manual
997:Fuel system:
996:
987:
967:
961:
955:
949:
942:Displacement
940:
931:
922:
916:
904:
903:
818:Rokospol Via
813:RLU-1 Breezy
713:ERCO Ercoupe
653:Bearhawk LSA
607:With 23,949
599:Applications
403:
393:
374:
357:
344:
325:
280:
244:
241:
206:
193:
181:Champion 7EC
170:
157:
153:
151:
115:RLU-1 Breezy
111:ERCO Ercoupe
2155:O (opposed)
1359:(9): 18–21.
1037:Performance
1021:Oil system:
788:Miller JM-2
773:Malmö MFI-9
643:ARV Griffin
609:Cessna 150s
332:Avgas 80/87
283:four-stroke
270:, plus the
247:Rolls-Royce
217:Aeronca 7AC
2746:Categories
2667:V-1650 (L)
2629:V-1650 (P)
2351:R-370 (LB)
2328:R (radial)
1962:Turboprops
1697:By company
1618:2015-11-05
1560:2006-10-09
1531:2006-10-09
1502:2006-10-09
1473:2009-10-05
1452:2006-10-07
1313:2006-10-07
1284:2006-10-07
1133:References
1032:Air-cooled
1011:Fuel type:
1001:carburetor
989:Valvetrain
982:Components
969:Dry weight
823:Rutan Q200
793:Nexaer LS1
683:Cessna 150
678:Cessna 140
658:Bede BD-12
628:AMD Zodiac
540:Model for
306:spark plug
252:Beagle Pup
221:Luscombe 8
189:Cessna 150
187:, and the
103:Cessna 150
99:Cessna 140
85:First run
33:C90/O-200
2718:See also:
2381:R-540 (K)
2376:R-540 (W)
2356:R-370 (K)
2298:O-540 (L)
2293:O-540 (F)
2258:O-360 (L)
2253:O-360 (C)
2223:O-200 (F)
2218:O-200 (C)
1583:14 August
1575:"O-200AF"
1468:"Aeronca"
1115:Rotax 912
905:Data from
171:Built by
121:Produced
1688:Gasoline
1275:"Motors"
1193:Archived
1077:See also
1025:wet sump
999:Updraft
582:O-200-AF
518:C90-14FJ
512:C90-14FH
500:C90-12FP
494:C90-12FJ
488:C90-12FH
410:Variants
319:and one
310:cylinder
302:magnetos
134:sector)
2685:VG-1410
2566:XR-7755
2092:IV-2220
2087:IV-2040
2082:IV-1430
2059:XH-3730
2054:XH-3130
2049:XH-2600
2044:XH-2470
2039:XH-2240
1952:XI-1430
1017:minimum
1007:control
1005:mixture
962:Height:
950:Length:
569:O-200-X
563:O-200-D
557:O-200-C
547:O-200-B
537:O-200-A
524:C90-16F
506:C90-14F
482:C90-12F
476:C90-8FJ
455:O-200AF
404:Nemesis
321:exhaust
233:⁄
2721:X-1800
2705:W-2779
2644:V-3420
2639:V-1950
2634:V-1710
2624:V-1570
2619:V-1560
2614:V-1510
2609:V-1460
2604:V-1440
2599:V-1400
2594:V-1237
2589:V-1150
2561:R-4360
2556:R-4090
2551:R-3350
2546:R-2800
2541:R-2600
2536:R-2180
2531:R-2160
2526:R-2060
2521:R-2000
2516:R-1860
2511:R-1830
2506:R-1820
2501:R-1750
2496:R-1690
2491:R-1670
2486:R-1640
2481:R-1535
2476:R-1510
2471:R-1454
2466:R-1340
2461:R-1300
2456:R-1044
2446:DR-980
2318:O-1230
2064:H-4070
2034:H-1640
1970:TP-500
1906:CD-300
1896:CD-155
1874:IO-550
1854:IO-370
1849:IO-368
1844:IO-360
1839:IO-346
1013:80/87
956:Width:
933:Stroke
470:C90-8F
314:intake
266:, the
262:, the
258:, the
239:inch.
219:, and
183:, the
179:, the
56:Piston
2662:V-770
2584:V-720
2451:R-985
2441:R-975
2436:R-915
2431:R-830
2426:R-790
2421:R-760
2416:R-755
2411:R-720
2406:R-680
2401:R-670
2396:R-600
2391:R-550
2386:R-545
2371:R-500
2366:R-440
2361:R-420
2346:R-270
2341:R-265
2336:R-250
2313:O-805
2308:O-580
2303:O-550
2288:O-520
2283:O-480
2278:O-470
2273:O-435
2268:O-425
2263:O-405
2248:O-335
2243:O-300
2238:O-290
2233:O-235
2228:O-205
2213:O-190
2208:O-180
2203:O-175
2198:O-170
2193:O-150
2188:O-145
2183:O-100
2145:L-825
2140:L-510
2135:L-440
2130:L-410
2125:L-390
2120:L-375
2115:L-365
2110:L-330
1934:R-975
1929:R-670
1924:R-544
1869:O-526
1864:O-520
1859:O-470
1834:O-300
1829:O-280
1824:O-240
1819:O-205
1814:O-200
1809:O-190
1804:O-170
1612:(PDF)
1605:(PDF)
1578:(PDF)
1063:7.0:1
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917:Type:
532:O-200
317:valve
225:O-190
158:O-200
88:1947
52:Type
2178:O-90
2173:O-45
2168:O-40
2163:O-15
1781:E225
1776:E185
1771:E165
1766:C145
1761:C140
1756:C125
1751:C115
1585:2013
924:Bore
379:and
308:per
156:and
152:The
1746:C90
1741:C85
1736:C75
1731:A80
1726:A75
1721:A70
1716:A65
1711:A50
1706:A40
975:dry
465:C90
278:).
209:A65
132:LSA
2748::
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1188:,
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