409:
29:
420:
441:
433:
357:
593:
334:
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
238:
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."
347:
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
343:
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.
1253:
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.
1181:
183:
Though the C90 was superseded by the O-200, and many of the designs utilizing the O-200 had gone out of production by 1980, with the 2004 publication of the United States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
1430:
1837:
2324:
387:, 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
2693:
1590:
319:(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
1991:
1178:
376:. 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
2592:
1958:
2004:
2156:
2075:
1434:
2374:
2171:
2118:
1912:
1709:
1651:
1629:
200:, 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
2602:
2582:
2434:
2166:
2052:
2607:
2597:
2334:
2128:
2113:
2151:
2098:
1404:(Jun. 15, 2006) Luftfahrt-Bundesamt (Federal Office of Civil Aviation). Federal Minister of Transport, Building and Urban Affairs. Germany.
395:
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).
2714:
2444:
2339:
2329:
1984:
1476:
2469:
1505:
1563:
2514:
1977:
2745:
336:
1597:
388:
348:
installation of a controllable-pitch propeller, and the -D model is a lower-weight version designed for light-sport aircraft.
2750:
2719:
2534:
1644:
462:
Lacks provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
2549:
2439:
492:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
486:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
480:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
474:
Has provisions for generator and starter drives, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
2509:
2499:
2000:
2504:
1660:
1659:
771:
696:
2484:
1969:
1637:
1361:(Jun. 27, 2003.) Department of Transportation. Federal Aviation Administration. Aircraft Certification Service.
1174:
1624:
2454:
681:
1534:
1287:
1402:
List 4: Propeller-driven aeroplanes not exceeding 8618 kg MTOM (including self-launching powered sailplanes.
328:
2539:
726:
621:
516:
Has vacuum pump drive provisions, 90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
161:
67:
561:
Similar to the "D" model except for engine dataplate identification, 100 hp (75 kW) continuous
231:
This engine family is considered to be dependable, according to both industry publications and the FAA.
2529:
2047:
2042:
856:
836:
2709:
2524:
2037:
2027:
691:
408:
2544:
2384:
2108:
1774:
1587:
1115:
380:—ran throughout the entire nine-day flight save for a four-minute shutdown due to a fuel problem.
2479:
2464:
2449:
751:
277:
and are all similar in size, displacement and weight. These engines are typically fitted with an
28:
686:
164:
these engines are used in many light aircraft designs of the United States, including the early
2740:
2429:
2414:
2409:
2364:
1922:
1876:
1229:
Revision 33. (Jul. 14, 2005.) Department of
Transportation. Federal Aviation Administration.
826:
256:
173:
1330:
Revision 23. (Jul. 8, 1993.) Department of
Transportation. Federal Aviation Administration.
1318:
Revision 32. (Oct. 1, 1997.) Department of
Transportation. Federal Aviation Administration.
1241:
Revision 44. (Mar. 31, 2003) Department of
Transportation. Federal Aviation Administration.
1217:
Revision 67. (Jun. 3, 2005.) Department of
Transportation. Federal Aviation Administration.
1202:
Revision 37. (Sep. 4, 1996.) Department of
Transportation. Federal Aviation Administration.
391:, four Pulitzer Trophies, and setting 16 speed records in its class. In one of those records,
157:
of 201 in (3.29 L) displacement, producing between 90 and 100 horsepower (67 and 75 kW).
2617:
2519:
2494:
2489:
1671:
1484:
1385:
Revision 3. (Jun. 19, 1979) Department of
Transportation. Federal Aviation Administration.
1373:
Revision 3. (Jan. 16, 1968) Department of Transportation. Federal Aviation Administration.
1056:
871:
866:
791:
731:
676:
549:
Model with provisions for a controllable pitch propeller, 100 hp (75 kW) continuous
530:
316:
95:
1513:
419:
796:
540:
340:
274:
185:
120:
8:
2070:
1940:
1784:
1428:
930:
846:
706:
555:
Similar to the "A" model, but with weight reductions, 100 hp (75 kW) continuous
260:
235:
2627:
2291:
2241:
1894:
1889:
1884:
1862:
1842:
1832:
1827:
881:
766:
721:
278:
2389:
2276:
2266:
2201:
2186:
1917:
1857:
1852:
1847:
1822:
1817:
1812:
1797:
1792:
1769:
1764:
1759:
1754:
1749:
1744:
1739:
1729:
1724:
1719:
1714:
1704:
1699:
1081:
1047:
711:
626:
377:
298:
271:
213:
133:
1999:
2554:
2296:
2080:
2032:
1076:
982:
Hydraulic lifters, two pushrod-actuated valves—one intake, one exhaust—per cylinder
861:
851:
841:
736:
716:
606:
290:
114:
651:
248:
2572:
2306:
2090:
1694:
1663:
1185:
921:
661:
656:
324:
286:
197:
154:
47:
1661:
Continental Motors, Teledyne Continental, and Continental Aerospace Technologies
2632:
2622:
2612:
2474:
2459:
2394:
2301:
2286:
2281:
2271:
2261:
2256:
2251:
2246:
2236:
2231:
2226:
2221:
2211:
2196:
2191:
2181:
2176:
2103:
2022:
1098:
1093:
993:
811:
372:, powered the 1986 nonstop, non-refueled global circumnavigation flight of the
369:
365:
309:
282:
264:
761:
2734:
2379:
2359:
2349:
2316:
1904:
1038:
912:
876:
831:
821:
816:
636:
581:
384:
373:
244:
205:
169:
2673:
2655:
2650:
2587:
2577:
2424:
2419:
2404:
2161:
2123:
806:
801:
701:
641:
611:
305:
263:
and the Reims F150 (a version of the Cessna 150 license-built in France by
252:
103:
99:
2143:
2133:
786:
776:
741:
631:
510:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
504:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
498:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
468:
90 hp (67 kW) continuous, 95 hp (71 kW) for take-off.
165:
2399:
2369:
2354:
2344:
989:
977:
963:
957:
781:
756:
671:
666:
646:
616:
597:
294:
240:
209:
177:
91:
87:
440:
1950:
1103:
746:
432:
320:
201:
356:
2683:
2665:
2642:
2564:
2062:
2012:
1932:
1542:
1456:
1295:
1263:
1013:
592:
364:
An engine designated the IOL-200, an O-200 variant modified with
1429:
Department of Transportation. Federal Aviation Administration.
302:
150:
44:
600:
built, this type is the most common application for the O-200.
323:
as the minimum fuel grade. Both are eligible for operation on
1676:
1003:
1413:
908:
Four-cylinder air-cooled horizontally opposed piston engine
281:, though the C90-8FJ, -12FJ, and -14FJ are equipped with
1359:
Special airworthiness information bulletin no. NE-03-45.
188:
regulations came a resurgence in demand for the O-200.
196:
The C90 was introduced in 1947 as a follow-on to the
1586:
1340:Berry, Mike (September 2004). "Continental O-200".
335:are models which provide for the installation of a
1292:Teledyne Continental Motors: Company Information
2732:
539:Model with special crankshaft and crankcase for
574:UL91 and UL94 95 hp alternate fuel engine.
1448:
1985:
1645:
1169:
1167:
1165:
1163:
1161:
1159:
1157:
1155:
1153:
1151:
580:The aft engine of the round the world flight
212:A. The engine was developed from the earlier
1498:
1469:
1397:
1395:
1393:
1391:
1149:
1147:
1145:
1143:
1141:
1139:
1137:
1135:
1133:
1131:
1510:Smithsonian: National Air and Space Museum
1481:Smithsonian: National Air and Space Museum
1280:
888:
1992:
1978:
1652:
1638:
1414:Teledyne Continental Motors (2003-03-28).
1376:
1268:Aerofiles: A Century of American Aviation
1210:
1208:
899:
1591:"Engine specifications: O-200-A & B"
1580:
1454:
1388:
1364:
1220:
1128:
896:Engine specifications: O-200-A & B.
565:
289:requiring no external power, driving two
191:
1422:
1407:
1321:
1256:
1232:
591:
439:
431:
425:Two views of an O-200-A in a Cessna 150H
355:
1527:
1309:
1205:
2733:
1383:Type certificate data sheet no. A22EU.
1227:Type certificate date sheet no. A-787.
351:
339:and one, the C90-12FP, designed for a
270:All versions of the C90 and O-200 are
1973:
1633:
1371:Type certificate data sheet no. E3IN.
1339:
1239:Type certificate data sheet no. 3A19.
1193:
1179:Type certificate data sheet no. E-252
543:, 100 hp (75 kW) continuous
533:, 100 hp (75 kW) continuous
448:
1352:
2715:US military gas turbine aeroengines
1416:Service Information Letter SIL98-9A
1333:
285:systems. They utilize a redundant
239:The Rolls-Royce O-200-A powers the
151:horizontally opposed, four-cylinder
13:
1244:
36:O-200-A installed in a Cessna 150
14:
2762:
1618:
1328:Aircraft specification no. A-694.
1316:Aircraft specification no. A-691.
1215:Aircraft specification no. A-759.
772:Miller-Bohannon JM-2 Pushy Galore
697:CubCrafters CC11-100 Sport Cub S2
1539:American Legend Aircraft Company
418:
407:
27:
1556:
1200:Aircraft specification no. 1A2.
1175:Federal Aviation Administration
792:Piper PA-18-95 Super Cub, L-18C
587:
1025:
787:Piper PA-11 Cub Special, L-18B
682:Civil Aviation Department MG-1
329:Supplemental Type Certificates
1:
2746:1940s aircraft piston engines
1121:
970:
612:Aeronca L-16B (Champion 7CCM)
2751:Continental aircraft engines
2720:Piston engine configurations
727:Flaeming Air FA 04 Peregrine
622:American Homebuilts John Doe
337:controllable-pitch propeller
149:are a family of air-cooled,
7:
1625:Teledyne Continental Motors
1190:Revision 34. (27 June 2013)
1065:
398:
68:Teledyne Continental Motors
10:
2767:
857:VTOL Aircraft Phillicopter
837:Taylorcraft F-19 Sportsman
315:Continental's recommended
312:valve, pushrod-activated.
293:, each of which fires one
234:In a cooperative venture,
16:Family of aircraft engines
2702:
2682:
2664:
2641:
2563:
2315:
2142:
2089:
2061:
2011:
1949:
1931:
1903:
1875:
1783:
1685:
1670:
692:CubCrafters Carbon Cub EX
607:Aeronca Champion 7EC, 7FC
301:. Each cylinder has one
216:by increasing the stroke
35:
26:
21:
1535:"The Rebirth of the Cub"
1116:List of aircraft engines
889:Specifications (O-200-A)
520:
2686:W-configuration inline)
2015:H-configuration inline)
2003:piston aircraft engine
1877:Aircraft Diesel engines
1588:Continental Motors Inc.
1506:"Sharp DR 90 "Nemesis""
1455:Aerofiles (July 2009).
1342:Light Plane Maintenance
1061:0.56 hp/lb (0.92 kW/kg)
900:General characteristics
752:Jodel DR1050 Excellence
204:and PA-11 Cub Special,
2666:VG (inverted-V inline)
2091:L (single-bank inline)
2063:IV (inverted-V inline)
2001:United States military
1688:horsepower designation
1672:Opposed piston engines
827:Ryson ST-100 Cloudster
742:IndUS Aviation Sport E
601:
566:Non-certified versions
453:
445:
437:
361:
257:Morane-Saulnier MS-880
249:Bölkow Bo 208 C Junior
192:Design and development
2643:V (inverted-V inline)
1431:"STC number SE2031CE"
1057:Power-to-weight ratio
966:, without accessories
962:170.18 lb (77.19 kg)
872:World Aircraft Spirit
867:Williams W-17 Stinger
732:Fleet Model 80 Canuck
687:Coupé-Aviation JC-200
677:Cessna 162 Skycatcher
595:
531:tractor configuration
443:
435:
359:
317:time between overhaul
275:reciprocating engines
166:Piper PA-18 Super Cub
96:Cessna 162 Skycatcher
2565:V (upright-V inline)
1288:"Company Background"
1012:6 US quart (5.7 L),
797:Pottier P.60 Minacro
541:pusher configuration
389:Louis Blèriot medals
341:pusher configuration
186:light-sport aircraft
1071:Related development
1043:0.5 hp/in (23 kW/L)
953:23.18 in (588.8 mm)
947:31.56 in (801.6 mm)
941:28.53 in (724.7 mm)
847:Victa Airtourer 100
707:Falconar F11 Sporty
577:IOL-200/Voyager 200
360:Continental IOL-200
352:Operational history
325:automobile gasoline
261:Victa Airtourer 100
253:Avions Robin DR 220
2005:designation system
1933:Inverted-V engines
1184:2021-06-02 at the
1088:Comparable engines
917:4.06 in (103.1 mm)
882:Zenith STOL CH 750
767:Mignet Pou-du-Ciel
757:Luscombe 8F, LSA-8
722:Fisher Dakota Hawk
602:
449:Certified versions
446:
438:
436:Continental O-200D
383:Formula One racer
362:
279:updraft carburetor
162:Continental Motors
119:2004-present (for
83:Major applications
2728:
2727:
1967:
1966:
1871:
1870:
1251:Federal Register.
1082:Continental O-300
1048:Compression ratio
926:3.88 in (98.6 mm)
712:Falconar Minihawk
627:Anglin J6 Karatoo
378:Continental O-240
227:
139:
138:
134:Continental O-190
2758:
1994:
1987:
1980:
1971:
1970:
1683:
1682:
1664:aircraft engines
1654:
1647:
1640:
1631:
1630:
1612:
1611:
1609:
1608:
1602:
1596:. Archived from
1595:
1584:
1578:
1577:
1575:
1573:
1568:
1560:
1554:
1553:
1551:
1550:
1541:. Archived from
1531:
1525:
1524:
1522:
1521:
1512:. Archived from
1502:
1496:
1495:
1493:
1492:
1483:. Archived from
1473:
1467:
1466:
1464:
1463:
1452:
1446:
1445:
1443:
1442:
1433:. Archived from
1426:
1420:
1419:
1411:
1405:
1399:
1386:
1380:
1374:
1368:
1362:
1356:
1350:
1349:
1337:
1331:
1325:
1319:
1313:
1307:
1306:
1304:
1303:
1294:. Archived from
1284:
1278:
1277:
1275:
1274:
1260:
1254:
1248:
1242:
1236:
1230:
1224:
1218:
1212:
1203:
1197:
1191:
1171:
1077:Continental A-65
862:Warner Sportster
852:VSR SR-1 Snoshoo
842:Vashon Ranger R7
737:Interstate Cadet
717:Fisher Celebrity
422:
411:
327:on the basis of
226:
225:
221:
217:
155:aircraft engines
130:
113:1947-1980s (for
84:
56:
31:
19:
18:
2766:
2765:
2761:
2760:
2759:
2757:
2756:
2755:
2731:
2730:
2729:
2724:
2698:
2685:
2678:
2660:
2637:
2559:
2311:
2138:
2085:
2057:
2014:
2007:
1998:
1968:
1963:
1945:
1927:
1899:
1890:CD-200 (TD-300)
1867:
1785:By displacement
1779:
1687:
1674:
1666:
1658:
1621:
1616:
1615:
1606:
1604:
1600:
1593:
1585:
1581:
1571:
1569:
1566:
1562:
1561:
1557:
1548:
1546:
1533:
1532:
1528:
1519:
1517:
1504:
1503:
1499:
1490:
1488:
1477:"Rutan Voyager"
1475:
1474:
1470:
1461:
1459:
1453:
1449:
1440:
1438:
1427:
1423:
1412:
1408:
1400:
1389:
1381:
1377:
1369:
1365:
1357:
1353:
1338:
1334:
1326:
1322:
1314:
1310:
1301:
1299:
1286:
1285:
1281:
1272:
1270:
1262:
1261:
1257:
1249:
1245:
1237:
1233:
1225:
1221:
1213:
1206:
1198:
1194:
1186:Wayback Machine
1172:
1129:
1124:
1068:
1028:
1019:Cooling system:
973:
935:201 in (3.29 L)
902:
891:
886:
662:Cassutt Special
657:Bushcaddy R-120
590:
568:
523:
456:
451:
430:
429:
428:
427:
426:
423:
414:
413:
412:
401:
354:
287:ignition system
245:Rollason Condor
223:
219:
218:
194:
153:, direct-drive
143:Continental C90
128:
118:
102:
98:
94:
90:
82:
55:National origin
54:
48:aircraft engine
17:
12:
11:
5:
2764:
2754:
2753:
2748:
2743:
2726:
2725:
2723:
2722:
2717:
2712:
2703:
2700:
2699:
2697:
2696:
2690:
2688:
2684:W (three-bank
2680:
2679:
2677:
2676:
2670:
2668:
2662:
2661:
2659:
2658:
2653:
2647:
2645:
2639:
2638:
2636:
2635:
2630:
2625:
2620:
2615:
2610:
2605:
2600:
2595:
2590:
2585:
2580:
2575:
2569:
2567:
2561:
2560:
2558:
2557:
2552:
2547:
2542:
2537:
2532:
2527:
2522:
2517:
2512:
2507:
2502:
2497:
2492:
2487:
2482:
2477:
2472:
2467:
2462:
2457:
2452:
2447:
2442:
2437:
2432:
2427:
2422:
2417:
2412:
2407:
2402:
2397:
2392:
2387:
2382:
2377:
2372:
2367:
2362:
2357:
2352:
2347:
2342:
2337:
2332:
2327:
2321:
2319:
2313:
2312:
2310:
2309:
2304:
2299:
2294:
2289:
2284:
2279:
2274:
2269:
2264:
2259:
2254:
2249:
2244:
2239:
2234:
2229:
2224:
2219:
2214:
2209:
2204:
2199:
2194:
2189:
2184:
2179:
2174:
2169:
2164:
2159:
2154:
2148:
2146:
2140:
2139:
2137:
2136:
2131:
2126:
2121:
2116:
2111:
2106:
2101:
2095:
2093:
2087:
2086:
2084:
2083:
2078:
2073:
2067:
2065:
2059:
2058:
2056:
2055:
2050:
2045:
2040:
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265:Reims Aviation
243:Series 1, the
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1603:on 2018-12-22
1599:
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1565:
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1545:on 2006-10-05
1544:
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1530:
1516:on 2006-09-01
1515:
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1487:on 2006-10-23
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1110:Related lists
1105:
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877:Zodiac 601 HD
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637:Barbaro RB-50
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582:Rutan Voyager
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385:Sharp Nemesis
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374:Rutan Voyager
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202:Piper J-3 Cub
199:
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174:Alon Aircoupe
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64:Manufacturer
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39:
34:
30:
25:
20:
2706:
2216:
2206:
1807:
1802:
1775:Tiara series
1734:
1605:. Retrieved
1598:the original
1582:
1570:. Retrieved
1558:
1547:. Retrieved
1543:the original
1538:
1529:
1518:. Retrieved
1514:the original
1509:
1500:
1489:. Retrieved
1485:the original
1480:
1471:
1460:. Retrieved
1450:
1439:. Retrieved
1435:the original
1424:
1415:
1409:
1401:
1382:
1378:
1370:
1366:
1358:
1354:
1345:
1341:
1335:
1327:
1323:
1315:
1311:
1300:. Retrieved
1296:the original
1291:
1282:
1271:. Retrieved
1267:
1258:
1250:
1246:
1238:
1234:
1226:
1222:
1214:
1199:
1195:
1173:
1109:
1108:
1087:
1086:
1070:
1069:
1055:
1046:
1037:
1031:
1018:
1009:
999:
992:with manual
986:Fuel system:
985:
976:
956:
950:
944:
938:
931:Displacement
929:
920:
911:
905:
893:
892:
807:Rokospol Via
802:RLU-1 Breezy
702:ERCO Ercoupe
642:Bearhawk LSA
596:With 23,949
588:Applications
392:
382:
363:
346:
333:
314:
269:
233:
230:
195:
182:
170:Champion 7EC
159:
146:
142:
140:
104:RLU-1 Breezy
100:ERCO Ercoupe
2144:O (opposed)
1348:(9): 18–21.
1026:Performance
1010:Oil system:
777:Miller JM-2
762:Malmö MFI-9
632:ARV Griffin
598:Cessna 150s
321:Avgas 80/87
272:four-stroke
259:, plus the
236:Rolls-Royce
206:Aeronca 7AC
2735:Categories
2656:V-1650 (L)
2618:V-1650 (P)
2340:R-370 (LB)
2317:R (radial)
1951:Turboprops
1686:By company
1607:2015-11-05
1549:2006-10-09
1520:2006-10-09
1491:2006-10-09
1462:2009-10-05
1441:2006-10-07
1302:2006-10-07
1273:2006-10-07
1122:References
1021:Air-cooled
1000:Fuel type:
990:carburetor
978:Valvetrain
971:Components
958:Dry weight
812:Rutan Q200
782:Nexaer LS1
672:Cessna 150
667:Cessna 140
647:Bede BD-12
617:AMD Zodiac
529:Model for
295:spark plug
241:Beagle Pup
210:Luscombe 8
178:Cessna 150
176:, and the
92:Cessna 150
88:Cessna 140
74:First run
22:C90/O-200
2707:See also:
2370:R-540 (K)
2365:R-540 (W)
2345:R-370 (K)
2287:O-540 (L)
2282:O-540 (F)
2247:O-360 (L)
2242:O-360 (C)
2212:O-200 (F)
2207:O-200 (C)
1572:14 August
1564:"O-200AF"
1457:"Aeronca"
1104:Rotax 912
894:Data from
160:Built by
110:Produced
1677:Gasoline
1264:"Motors"
1182:Archived
1066:See also
1014:wet sump
988:Updraft
571:O-200-AF
507:C90-14FJ
501:C90-14FH
489:C90-12FP
483:C90-12FJ
477:C90-12FH
399:Variants
308:and one
299:cylinder
291:magnetos
123:sector)
2674:VG-1410
2555:XR-7755
2081:IV-2220
2076:IV-2040
2071:IV-1430
2048:XH-3730
2043:XH-3130
2038:XH-2600
2033:XH-2470
2028:XH-2240
1941:XI-1430
1006:minimum
996:control
994:mixture
951:Height:
939:Length:
558:O-200-X
552:O-200-D
546:O-200-C
536:O-200-B
526:O-200-A
513:C90-16F
495:C90-14F
471:C90-12F
465:C90-8FJ
444:O-200AF
393:Nemesis
310:exhaust
222:⁄
2710:X-1800
2694:W-2779
2633:V-3420
2628:V-1950
2623:V-1710
2613:V-1570
2608:V-1560
2603:V-1510
2598:V-1460
2593:V-1440
2588:V-1400
2583:V-1237
2578:V-1150
2550:R-4360
2545:R-4090
2540:R-3350
2535:R-2800
2530:R-2600
2525:R-2180
2520:R-2160
2515:R-2060
2510:R-2000
2505:R-1860
2500:R-1830
2495:R-1820
2490:R-1750
2485:R-1690
2480:R-1670
2475:R-1640
2470:R-1535
2465:R-1510
2460:R-1454
2455:R-1340
2450:R-1300
2445:R-1044
2435:DR-980
2307:O-1230
2053:H-4070
2023:H-1640
1959:TP-500
1895:CD-300
1885:CD-155
1863:IO-550
1843:IO-370
1838:IO-368
1833:IO-360
1828:IO-346
1002:80/87
945:Width:
922:Stroke
459:C90-8F
303:intake
255:, the
251:, the
247:, the
228:inch.
208:, and
172:, the
168:, the
45:Piston
2651:V-770
2573:V-720
2440:R-985
2430:R-975
2425:R-915
2420:R-830
2415:R-790
2410:R-760
2405:R-755
2400:R-720
2395:R-680
2390:R-670
2385:R-600
2380:R-550
2375:R-545
2360:R-500
2355:R-440
2350:R-420
2335:R-270
2330:R-265
2325:R-250
2302:O-805
2297:O-580
2292:O-550
2277:O-520
2272:O-480
2267:O-470
2262:O-435
2257:O-425
2252:O-405
2237:O-335
2232:O-300
2227:O-290
2222:O-235
2217:O-205
2202:O-190
2197:O-180
2192:O-175
2187:O-170
2182:O-150
2177:O-145
2172:O-100
2134:L-825
2129:L-510
2124:L-440
2119:L-410
2114:L-390
2109:L-375
2104:L-365
2099:L-330
1923:R-975
1918:R-670
1913:R-544
1858:O-526
1853:O-520
1848:O-470
1823:O-300
1818:O-280
1813:O-240
1808:O-205
1803:O-200
1798:O-190
1793:O-170
1601:(PDF)
1594:(PDF)
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1052:7.0:1
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521:O-200
306:valve
214:O-190
147:O-200
77:1947
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2167:O-90
2162:O-45
2157:O-40
2152:O-15
1770:E225
1765:E185
1760:E165
1755:C145
1750:C140
1745:C125
1740:C115
1574:2013
913:Bore
368:and
297:per
145:and
141:The
1735:C90
1730:C85
1725:C75
1720:A80
1715:A75
1710:A70
1705:A65
1700:A50
1695:A40
964:dry
454:C90
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198:A65
121:LSA
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1177:,
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