628:
204:
The O-470 family of engines covers a range from 213 hp (159 kW) to 260 hp (194 kW). The engines were developed in the late 1940s and certification was applied for on 23 October 1950 on the regulatory basis of Part 13 of the US Civil Air
Regulations effective 1 August 1949 as
200:
The first engine in this series was the E165, a 471 cubic inch (7.7 L) engine producing 165 hp (123 kW), and was the first of the
Continental's "E" series engines. Later versions were given the company designation of E185 (185 hp (138 kW) continuous) and E225 (225 hp
386:
240 hp (179 kW) at 2600 rpm, dry weight 410 lb (186 kg), similar to O-470-A except increased power, different damper configuration, incorporation of inclined valve cylinders, downdraft pressure carburetor and induction changes. Identical to E185-9. Certified 4 December
271:
205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor, identical to E185-3 except for revised starter drive to accommodate dog rather than gear type
264:
205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor, identical to E185-1 but with revised starter drive with dog rather than gear type
42:
369:
213 hp (159 kW) at 2600 rpm, dry weight 405 lb (184 kg), identical to the 0-470-11 except: four sixth order damper crankshaft, propeller control provisions, revised engine mounting brackets and long skirt pistons. Certified 19 January
611:
250 hp (186 kW) at 2600 rpm, dry weight 475 lb (215 kg), equipped with a TCM 6022 fuel injector. The same as an IO-470-T, except that the crankshaft turns in opposite direction for use on twin-engined aircraft. Certified 18 March
330:
225 hp (168 kW) at 2600 rpm, dry weight 415 lb (188 kg), previously designated 0-470-13B. It is identical to the Model 0-470-13A except for the Bendix-Stromberg Model PS-5CD carburetor in place of the PS-5C. Certified 19 January
362:
225 hp (168 kW) at 2600 rpm, dry weight 415 lb (188 kg), identical to the 0-470-13 but with an additional tachometer drive through the camshaft gear and one fifth and one sixth order crankshaft damper. Certified 19 January
418:
230 hp (172 kW) at 2600 rpm, dry weight 404 lb (183 kg), similar to O-470-J except max rpm, crankshaft damper configuration, incorporation of shell-molded cylinder heads and revised mounting brackets. Certified 4 December
284:
205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor, identical to E185-8 but with revised mounting
399:
240 hp (179 kW) at 2600 rpm, dry weight 432 lb (196 kg), similar to O-470-M except crankshaft damper configuration, revised oil sump integral cast intake air passage and mounting brackets. Certified 4 December
337:
Non-certified military engine, identical to E185-3, 205 hp (153 kW) at 2600 rpm, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor. When equipped with 18 mm. spark plugs, it is designated
431:
240 hp (179 kW) at 2600 rpm, dry weight 410 lb (186 kg), same as O-470-B except crankshaft damper configuration and incorporation of shell-molded cylinder heads. Certified 4 December
412:
225 hp (168 kW) at 2550 rpm, dry weight 378 lb (171 kg), same as O-470-A except reduced max rpm and induction system risers, manifold and balance tube. Certified 4 December 1952.
406:
240 hp (179 kW) at 2600 rpm, dry weight 495 lb (225 kg), same as O-470-B with an extension propeller shaft, approved for pusher installations. Certified 4 December 1952.
278:
205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.
252:
205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.
240:
205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.
468:
230 hp (172 kW) at 2400 rpm, dry weight 412 lb (187 kg), similar to the O-470-S except max rpm rating and crankshaft damper configuration. Certified 4 December 1952.
425:
230 hp (172 kW) at 2600 rpm, dry weight 404 lb (183 kg), same as O-470-K except relocated carburetor, revised intake manifold oil sump. Certified 4 December 1952.
456:
230 hp (172 kW) at 2600 rpm, dry weight 401 lb (182 kg), same as O-470-R except piston oil cooling and semi-keystone piston rings. Certified 4 December 1952.
350:
213 hp (159 kW) at 2600 rpm, dry weight 391 lb (177 kg), identical to the 0-470-11 but with 0-470-15 cylinders and pistons. Certified 19 January 1951.
1481:
356:
225 hp (168 kW) at 2600 rpm, dry weight 415 lb (188 kg), one fifth and one sixth order dampers or two sixth order dampers. Certified 19 January 1951.
1437:
1380:
1274:
1311:
1154:
444:
240 hp (179 kW) at 2600 rpm, dry weight 432 lb (196 kg), identical to O-470-G except crankshaft damper configuration. Certified 4 December 1952.
201:(168 kW)). When the US military gave them all the designation of O-470 the company adopted the designation and future models were known as Continental O-470s.
1227:
462:
230 hp (172 kW) at 2400 rpm, dry weight 410 lb (186 kg), similar to the O-470-S except crankcase design and max rpm. Certified 4 December 1952.
618:
260 hp (194 kW) at 3000 rpm, dry weight 533 lb (242 kg), Supercharged model, specifically approved for helicopters. Certified 2 February 1955.
595:
260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 26 September 1967.
541:
260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 26 September 1967.
450:
230 hp (172 kW) at 2600 rpm, dry weight 401 lb (182 kg), same as O-470-L except crankshaft damper configuration. Certified 4 December 1952.
438:
240 hp (179 kW) at 2600 rpm, dry weight 410 lb (186 kg), same as O-470-M except crankshaft damper configuration. Certified 4 December 1952.
499:
260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 26 November 1958.
505:
260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 3 December 1958.
493:
260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 14 October 1958.
393:
225 hp (168 kW) at 2600 rpm, dry weight 390 lb (177 kg), same as O-470-A except downdraft pressure carburetor. Certified 4 December 1952.
583:
260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 28 August 1963.
565:
250 hp (186 kW) at 2600 rpm, dry weight 431 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 7 October 1960.
547:
260 hp (194 kW) at 2625 rpm, dry weight 428 lb (194 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 10 March 1960.
511:
250 hp (186 kW) at 2600 rpm, dry weight 431 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 30 March 1959.
589:
260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 15 June 1965.
535:
260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 9 March 1960.
571:
260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 10 May 1961.
797:
487:
250 hp (186 kW) at 2600 rpm, dry weight 410 lb (186 kg), equipped with a TCM 5620 or 5827 fuel injector. Certified 4 December 1952.
1459:
1814:
517:
260 hp (194 kW) at 2625 rpm, dry weight 432 lb (196 kg), equipped with a TCM 5620-2 fuel injector. Certified 7 August 1959.
481:
240 hp (179 kW) at 2600 rpm, dry weight 432 lb (196 kg), equipped with a TCM 5580 fuel injector. Certified 4 December 1952.
523:
225 hp (168 kW) at 2600 rpm, dry weight 400 lb (181 kg), equipped with a TCM 5612-1 fuel injector. Certified 31 July 1959.
1819:
1474:
559:
250 hp (186 kW) at 2600 rpm, dry weight 472 lb (214 kg), equipped with a TCM 5648 fuel injector. Certified 31 March 1961.
577:
250 hp (186 kW) at 2600 rpm, dry weight 475 lb (215 kg), equipped with a TCM 5648 fuel injector. Certified 1 July 1963.
553:
260 hp (194 kW) at 2625 rpm, dry weight 432 lb (196 kg), equipped with a TCM 5830 fuel injector. Certified 9 June 1960.
529:
225 hp (168 kW) at 2600 rpm, dry weight 400 lb (181 kg), equipped with a TCM 5807 fuel injector. Certified 9 June 1960.
1490:
1467:
344:
213 hp (159 kW) at 2600 rpm, dry weight 391 lb (177 kg), two sixth order dampers. Certified 19 January 1951.
1433:
1376:
1307:
1270:
1223:
1150:
324:
250 hp (186 kW) at 2600 rpm, dry weight 484 lb (220 kg), supercharged model. Certified 2 February 1955.
1341:
831:
817:
1441:
1384:
1278:
1158:
258:
185 hp (138 kW) at 2300 rpm, dry weight 343 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.
234:
165 hp (123 kW) at 2050 rpm, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.
228:
165 hp (123 kW) at 2050 rpm, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.
1315:
1231:
170:
82:
1667:
732:
1604:
1091:
720:
246:
185 hp (138 kW) at 2300 rpm, dry weight 351 lb (159 kg), Marvel-Schebler MA-4-5 carburetor.
222:
165 hp (123 kW) at 2050 rpm, dry weight 351 lb (159 kg), Marvel-Schebler MA-4-5 carburetor.
837:
316:
1809:
1752:
1706:
693:
1788:
1501:
1059:
782:
376:
225 hp (168 kW) at 2600 rpm, dry weight 378 lb (171 kg). Certified 4 December 1952.
309:
225 hp (168 kW) at 2650 rpm, dry weight 363 lb (165 kg). Certified 30 October 1950.
1742:
1539:
939:
889:
777:
303:
225 hp (168 kW) at 2650 rpm, dry weight 347 lb (157 kg). Certified 12 July 1950.
291:
225 hp (168 kW) at 2650 rpm, dry weight 359 lb (163 kg). Certified 19 July 1951.
1770:
1614:
964:
297:
225 hp (168 kW) at 2650 rpm, dry weight 355 lb (161 kg). Certified 5 July 1952.
110:
1724:
1719:
1714:
1692:
1672:
1662:
1657:
864:
752:
737:
688:
661:
631:
102:
1747:
1687:
1682:
1652:
1647:
1642:
1637:
1632:
1627:
1622:
1584:
1579:
1574:
1569:
1564:
1559:
1554:
1549:
1544:
1534:
1529:
1050:
842:
671:
644:
859:
106:
1524:
1493:
955:
899:
822:
162:
60:
909:
1079:
742:
703:
698:
666:
166:
41:
1803:
1734:
1041:
946:
812:
159:
72:
894:
854:
807:
772:
17:
1491:
Continental Motors, Teledyne
Continental, and Continental Aerospace Technologies
904:
827:
792:
708:
676:
649:
627:
1345:
192:
engines, and several specialty variants. It has been in production since 1950.
1001:
989:
973:
884:
879:
874:
869:
802:
767:
762:
757:
747:
155:
134:
130:
126:
122:
118:
114:
1780:
787:
1762:
205:
amended by 13-1. The first O-470 model was certified on 19 January 1951.
165:, air-cooled aircraft engines that was developed especially for use in
57:
1506:
1010:
626:
1463:
1779:
1761:
1733:
1705:
1613:
1515:
1500:
1438:"TYPE CERTIFICATE DATA SHEET NO. E-246 Revision 20"
1381:"TYPE CERTIFICATE DATA SHEET NO. E-267 Revision 10"
1275:"TYPE CERTIFICATE DATA SHEET NO. E-269 Revision 15"
1155:"TYPE CERTIFICATE DATA SHEET NO. E-273 Revision 36"
1312:"TYPE CERTIFICATE DATA SHEET NO. E-281 Revision 8"
1228:"TYPE CERTIFICATE DATA SHEET NO. 3E1 Revision 26"
1335:
1333:
1475:
994:One intake and one exhaust valve per cylinder
634:equipped with a Continental O-470R powerplant
173:. Engines designated "IO" are fuel-injected.
8:
1512:
1482:
1468:
1460:
315:260 hp (194 kW), flown in the
1428:
1426:
1424:
1422:
1145:
1143:
1141:
1139:
1137:
1135:
1133:
1131:
1129:
1127:
1103:
798:Maestranza Central de Aviación HF XX-02
1420:
1418:
1416:
1414:
1412:
1410:
1408:
1406:
1404:
1402:
1371:
1369:
1367:
1365:
1363:
1302:
1300:
1298:
1296:
1265:
1263:
1261:
1259:
1257:
1255:
1253:
1251:
1249:
1218:
1216:
1214:
1212:
1210:
1208:
1206:
1204:
1202:
1200:
1198:
1196:
1125:
1123:
1121:
1119:
1117:
1115:
1113:
1111:
1109:
1107:
31:
1194:
1192:
1190:
1188:
1186:
1184:
1182:
1180:
1178:
1176:
27:6-cylinder air-cooled aircraft engine
7:
925:Type Certificate Data Sheet E-269.
912:– experimental hover train project
163:six-cylinder, horizontally opposed
25:
1340:Shanaberger, Kenneth W. (2008).
49:Preserved Continental O-470-13A
40:
1434:Federal Aviation Administration
1377:Federal Aviation Administration
1308:Federal Aviation Administration
1271:Federal Aviation Administration
1224:Federal Aviation Administration
1151:Federal Aviation Administration
1:
1815:1950s aircraft piston engines
1000:Bendix-Stromberg Model PS-5C
818:SIAI-Marchetti FN.333 Riviera
176:The family also includes the
1820:Continental aircraft engines
1037:213 hp (159 kW) at 2,575 rpm
83:Teledyne Continental Motors
1836:
733:Associated Air Liberty 181
917:Specifications (O-470-11)
48:
39:
34:
1092:List of aircraft engines
938:six-cylinder air-cooled
721:Robertson SRX-1 Skyshark
1707:Aircraft Diesel engines
1064:0.54 hp/lb (0.90 kW/kg)
1046:0.45 hp/in³ (20.4 kW/L)
930:General characteristics
838:Taylorcraft Ranch Wagon
317:Robertson Skylark SRX-1
1518:horsepower designation
1502:Opposed piston engines
942:aircraft piston engine
694:Beechcraft T-34 Mentor
635:
196:Design and development
154:engine is a family of
1060:Power-to-weight ratio
783:Fanaero-Chile Chincol
743:Bellanca Cruisemaster
630:
940:horizontally opposed
890:Navion G Rangemaster
778:Falconar SAL Mustang
473:Fuel-injected models
1342:"Continental O-470"
978:391 lb dry (177 kg)
969:471 in (7.7 L)
1763:Inverted-V engines
1226:(September 1995).
1153:(September 1995).
1074:Comparable engines
865:Beechcraft Bonanza
753:Cessna 182 Skylane
738:Beechcraft Bonanza
689:Beechcraft Bonanza
662:Beechcraft Bonanza
636:
171:Continental Motors
103:Beechcraft Bonanza
98:Major applications
1797:
1796:
1701:
1700:
1379:(February 1974).
1310:(November 1973).
1051:Compression ratio
960:4.0 in (101.6 mm)
951:5.0 in (127.0 mm)
843:Yeoman Cropmaster
672:Muniz Casmuniz 52
645:Boisavia Mercurey
214:Carbureted models
152:Continental O-470
148:
147:
18:Continental E-185
16:(Redirected from
1827:
1513:
1494:aircraft engines
1484:
1477:
1470:
1461:
1454:
1453:
1451:
1449:
1444:on 5 August 2021
1440:. Archived from
1430:
1397:
1396:
1394:
1392:
1387:on 5 August 2021
1383:. Archived from
1373:
1358:
1357:
1355:
1353:
1344:. Archived from
1337:
1328:
1327:
1325:
1323:
1318:on 5 August 2021
1314:. Archived from
1304:
1291:
1290:
1288:
1286:
1281:on 5 August 2021
1277:. Archived from
1267:
1244:
1243:
1241:
1239:
1234:on 5 August 2021
1230:. Archived from
1220:
1171:
1170:
1168:
1166:
1161:on 5 August 2021
1157:. Archived from
1147:
860:Beechcraft Baron
830:(modified under
383:
382:
107:Beechcraft Baron
99:
69:
44:
32:
21:
1835:
1834:
1830:
1829:
1828:
1826:
1825:
1824:
1800:
1799:
1798:
1793:
1775:
1757:
1729:
1720:CD-200 (TD-300)
1697:
1615:By displacement
1609:
1517:
1504:
1496:
1488:
1458:
1457:
1447:
1445:
1432:
1431:
1400:
1390:
1388:
1375:
1374:
1361:
1351:
1349:
1339:
1338:
1331:
1321:
1319:
1306:
1305:
1294:
1284:
1282:
1269:
1268:
1247:
1237:
1235:
1222:
1221:
1174:
1164:
1162:
1149:
1148:
1105:
1100:
1071:
1031:
1022:Cooling system:
985:
932:
919:
900:Procaer Picchio
823:St-Just Cyclone
625:
475:
380:
379:
216:
211:
198:
133:
129:
125:
121:
117:
113:
111:Cessna Bird Dog
109:
105:
97:
68:National origin
67:
28:
23:
22:
15:
12:
11:
5:
1833:
1831:
1823:
1822:
1817:
1812:
1802:
1801:
1795:
1794:
1792:
1791:
1785:
1783:
1777:
1776:
1774:
1773:
1767:
1765:
1759:
1758:
1756:
1755:
1750:
1745:
1739:
1737:
1735:Radial engines
1731:
1730:
1728:
1727:
1722:
1717:
1711:
1709:
1703:
1702:
1699:
1698:
1696:
1695:
1690:
1685:
1680:
1675:
1670:
1665:
1660:
1655:
1650:
1645:
1640:
1635:
1630:
1625:
1619:
1617:
1611:
1610:
1608:
1607:
1602:
1597:
1592:
1587:
1582:
1577:
1572:
1567:
1562:
1557:
1552:
1547:
1542:
1537:
1532:
1527:
1521:
1519:
1510:
1498:
1497:
1489:
1487:
1486:
1479:
1472:
1464:
1456:
1455:
1436:(March 1974).
1398:
1359:
1348:on 29 May 2008
1329:
1292:
1245:
1172:
1102:
1101:
1099:
1096:
1095:
1094:
1083:
1082:
1080:Lycoming O-480
1070:
1067:
1066:
1065:
1056:
1047:
1042:Specific power
1038:
1030:
1027:
1026:
1025:
1019:
1013:
1004:
995:
984:
981:
980:
979:
970:
961:
952:
943:
931:
928:
918:
915:
914:
913:
907:
902:
897:
892:
887:
882:
877:
872:
867:
862:
857:
851:
850:
846:
845:
840:
835:
825:
820:
815:
810:
805:
800:
795:
790:
785:
780:
775:
770:
765:
760:
755:
750:
745:
740:
735:
729:
728:
724:
723:
717:
716:
712:
711:
706:
704:Fletcher FL-23
701:
699:Fletcher FD-25
696:
691:
685:
684:
680:
679:
674:
669:
667:Macchi M.B.320
664:
658:
657:
653:
652:
647:
641:
640:
624:
621:
620:
619:
616:
613:
609:
606:
604:
601:
599:
596:
593:
590:
587:
584:
581:
578:
575:
572:
569:
566:
563:
560:
557:
554:
551:
548:
545:
542:
539:
536:
533:
530:
527:
524:
521:
518:
515:
512:
509:
506:
503:
500:
497:
494:
491:
488:
485:
482:
479:
474:
471:
470:
469:
466:
463:
460:
457:
454:
451:
448:
445:
442:
439:
436:
433:
429:
426:
423:
420:
416:
413:
410:
407:
404:
401:
397:
394:
391:
388:
384:
377:
374:
371:
367:
364:
360:
357:
354:
351:
348:
345:
342:
339:
335:
332:
328:
325:
322:
319:
313:
310:
307:
304:
301:
298:
295:
292:
289:
286:
282:
279:
276:
273:
269:
266:
262:
259:
256:
253:
250:
247:
244:
241:
238:
235:
232:
229:
226:
223:
220:
215:
212:
210:
207:
197:
194:
167:light aircraft
146:
145:
142:
138:
137:
100:
94:
93:
90:
86:
85:
80:
76:
75:
70:
64:
63:
55:
51:
50:
46:
45:
37:
36:
26:
24:
14:
13:
10:
9:
6:
4:
3:
2:
1832:
1821:
1818:
1816:
1813:
1811:
1810:Boxer engines
1808:
1807:
1805:
1790:
1787:
1786:
1784:
1782:
1778:
1772:
1769:
1768:
1766:
1764:
1760:
1754:
1751:
1749:
1746:
1744:
1741:
1740:
1738:
1736:
1732:
1726:
1723:
1721:
1718:
1716:
1713:
1712:
1710:
1708:
1704:
1694:
1691:
1689:
1686:
1684:
1681:
1679:
1676:
1674:
1671:
1669:
1666:
1664:
1661:
1659:
1656:
1654:
1651:
1649:
1646:
1644:
1641:
1639:
1636:
1634:
1631:
1629:
1626:
1624:
1621:
1620:
1618:
1616:
1612:
1606:
1603:
1601:
1598:
1596:
1593:
1591:
1588:
1586:
1583:
1581:
1578:
1576:
1573:
1571:
1568:
1566:
1563:
1561:
1558:
1556:
1553:
1551:
1548:
1546:
1543:
1541:
1538:
1536:
1533:
1531:
1528:
1526:
1523:
1522:
1520:
1514:
1511:
1508:
1503:
1499:
1495:
1492:
1485:
1480:
1478:
1473:
1471:
1466:
1465:
1462:
1443:
1439:
1435:
1429:
1427:
1425:
1423:
1421:
1419:
1417:
1415:
1413:
1411:
1409:
1407:
1405:
1403:
1399:
1386:
1382:
1378:
1372:
1370:
1368:
1366:
1364:
1360:
1347:
1343:
1336:
1334:
1330:
1317:
1313:
1309:
1303:
1301:
1299:
1297:
1293:
1280:
1276:
1273:(June 1973).
1272:
1266:
1264:
1262:
1260:
1258:
1256:
1254:
1252:
1250:
1246:
1233:
1229:
1225:
1219:
1217:
1215:
1213:
1211:
1209:
1207:
1205:
1203:
1201:
1199:
1197:
1195:
1193:
1191:
1189:
1187:
1185:
1183:
1181:
1179:
1177:
1173:
1160:
1156:
1152:
1146:
1144:
1142:
1140:
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1136:
1134:
1132:
1130:
1128:
1126:
1124:
1122:
1120:
1118:
1116:
1114:
1112:
1110:
1108:
1104:
1097:
1093:
1090:
1089:
1088:
1087:
1086:Related lists
1081:
1078:
1077:
1076:
1075:
1068:
1063:
1061:
1057:
1054:
1052:
1048:
1045:
1043:
1039:
1036:
1035:Power output:
1033:
1032:
1028:
1023:
1020:
1017:
1014:
1012:
1008:
1005:
1003:
999:
996:
993:
991:
987:
986:
982:
977:
975:
971:
968:
966:
962:
959:
957:
953:
950:
948:
944:
941:
937:
934:
933:
929:
927:
926:
923:
916:
911:
908:
906:
903:
901:
898:
896:
893:
891:
888:
886:
883:
881:
878:
876:
873:
871:
868:
866:
863:
861:
858:
856:
853:
852:
848:
847:
844:
841:
839:
836:
833:
829:
826:
824:
821:
819:
816:
814:
813:PZL-104 Wilga
811:
809:
806:
804:
801:
799:
796:
794:
791:
789:
786:
784:
781:
779:
776:
774:
771:
769:
766:
764:
761:
759:
756:
754:
751:
749:
746:
744:
741:
739:
736:
734:
731:
730:
726:
725:
722:
719:
718:
714:
713:
710:
707:
705:
702:
700:
697:
695:
692:
690:
687:
686:
682:
681:
678:
675:
673:
670:
668:
665:
663:
660:
659:
655:
654:
651:
648:
646:
643:
642:
638:
637:
633:
629:
622:
617:
614:
610:
607:
605:
602:
600:
597:
594:
591:
588:
585:
582:
579:
576:
573:
570:
567:
564:
561:
558:
555:
552:
549:
546:
543:
540:
537:
534:
531:
528:
525:
522:
519:
516:
513:
510:
507:
504:
501:
498:
495:
492:
489:
486:
483:
480:
477:
476:
472:
467:
464:
461:
458:
455:
452:
449:
446:
443:
440:
437:
434:
430:
427:
424:
421:
417:
414:
411:
408:
405:
402:
398:
395:
392:
389:
385:
378:
375:
372:
368:
365:
361:
358:
355:
352:
349:
346:
343:
340:
336:
333:
329:
326:
323:
320:
318:
314:
311:
308:
305:
302:
299:
296:
293:
290:
287:
283:
280:
277:
274:
270:
267:
263:
260:
257:
254:
251:
248:
245:
242:
239:
236:
233:
230:
227:
224:
221:
218:
217:
213:
208:
206:
202:
195:
193:
191:
187:
183:
179:
174:
172:
168:
164:
161:
160:fuel-injected
157:
153:
143:
140:
139:
136:
132:
128:
124:
120:
116:
112:
108:
104:
101:
96:
95:
91:
88:
87:
84:
81:
79:Manufacturer
78:
77:
74:
73:United States
71:
66:
65:
62:
59:
56:
53:
52:
47:
43:
38:
33:
30:
19:
1677:
1605:Tiara series
1599:
1594:
1589:
1446:. Retrieved
1442:the original
1389:. Retrieved
1385:the original
1350:. Retrieved
1346:the original
1320:. Retrieved
1316:the original
1283:. Retrieved
1279:the original
1236:. Retrieved
1232:the original
1163:. Retrieved
1159:the original
1085:
1084:
1073:
1072:
1058:
1049:
1040:
1034:
1021:
1015:
1006:
998:Fuel system:
997:
988:
972:
965:Displacement
963:
954:
945:
935:
924:
921:
920:
910:Aérotrain 01
895:PAC Fletcher
855:Auster AOP.9
808:O-1 Bird dog
773:DINFIA IA 53
623:Applications
203:
199:
189:
185:
181:
177:
175:
151:
149:
29:
1448:28 December
1391:28 December
1352:28 December
1322:27 December
1285:27 December
1238:27 December
1165:27 December
1029:Performance
1016:Oil system:
905:Ryan Navion
875:Cessna 210A
828:Stinson 108
793:HAL Krishak
709:Ryan Navion
677:Ryan Navion
650:Luscombe 11
632:Cessna 182K
61:aero-engine
1804:Categories
1781:Turboprops
1516:By company
1098:References
1024:Air-cooled
1007:Fuel type:
1002:carburetor
990:Valvetrain
983:Components
974:Dry weight
885:Meyers 200
880:Cessna 310
870:Cessna 185
803:Meyers 200
768:Cessna 310
763:Cessna 188
758:Cessna 187
748:Cessna 180
603:TSIO-470-B
156:carbureted
144:1953–1986
135:Cessna 310
131:Cessna 210
127:Cessna 188
123:Cessna 185
119:Cessna 182
115:Cessna 180
89:First run
922:Data from
788:Fuji KM-2
615:FSO-470-A
608:LIO-470-A
598:GIO-470-A
592:IO-470-VO
538:IO-470-LO
359:O-470-13A
347:O-470-11B
338:0-470-7A.
285:brackets.
141:Produced
1507:Gasoline
1069:See also
1018:dry sump
586:IO-470-V
580:IO-470-U
574:IO-470-T
568:IO-470-S
562:IO-470-R
556:IO-470-P
550:IO-470-N
544:IO-470-M
532:IO-470-L
526:IO-470-K
520:IO-470-J
514:IO-470-H
508:IO-470-G
502:IO-470-F
496:IO-470-E
490:IO-470-D
484:IO-470-C
478:IO-470-A
366:O-470-15
353:O-470-13
341:O-470-11
312:GE260-2X
272:starter.
265:starter.
209:Variants
188:and the
1771:XI-1430
465:O-470-U
459:O-470-T
453:O-470-S
447:O-470-R
441:O-470-P
435:O-470-N
428:O-470-M
422:O-470-L
415:O-470-K
409:O-470-J
403:O-470-H
396:O-470-G
390:O-470-E
381:O-470-B
373:O-470-A
334:O-470-7
327:O-470-4
321:O-470-2
281:E185-11
275:E185-10
1789:TP-500
1725:CD-300
1715:CD-155
1693:IO-550
1673:IO-370
1668:IO-368
1663:IO-360
1658:IO-346
1009:80/87
956:Stroke
849:IO-470
306:E225-9
300:E225-8
294:E225-4
288:E225-2
268:E185-9
261:E185-8
255:E185-5
249:E185-3
243:E185-2
237:E185-1
231:E165-4
225:E165-3
219:E165-2
58:Piston
35:O-470
1753:R-975
1748:R-670
1743:R-544
1688:O-526
1683:O-520
1678:O-470
1653:O-300
1648:O-280
1643:O-240
1638:O-205
1633:O-200
1628:O-190
1623:O-170
1055:7.0:1
1011:avgas
936:Type:
727:O-470
612:1964.
432:1952.
419:1952.
400:1952.
387:1952.
370:1951.
363:1951.
331:1951.
92:1950
54:Type
1600:E225
1595:E185
1590:E165
1585:C145
1580:C140
1575:C125
1570:C115
1450:2008
1393:2008
1354:2008
1324:2008
1287:2008
1240:2008
1167:2008
947:Bore
715:E260
683:E225
656:E185
639:E165
190:E260
186:E225
182:E185
178:E165
158:and
150:The
1565:C90
1560:C85
1555:C75
1550:A80
1545:A75
1540:A70
1535:A65
1530:A50
1525:A40
832:STC
169:by
1806::
1401:^
1362:^
1332:^
1295:^
1248:^
1175:^
1106:^
184:,
180:,
1509:)
1505:(
1483:e
1476:t
1469:v
1452:.
1395:.
1356:.
1326:.
1289:.
1242:.
1169:.
1062::
1053::
1044::
992::
976::
967::
958::
949::
834:)
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
