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Lycoming IO-390

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Certified four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 215 hp (160 kW) at 2,700 rpm, dry weight 296 lb (134 kg). This model is the same as the C3A6, except that the propeller governor is located on left front of the crankcase.
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Certified version: four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 215 hp (160 kW) at 2700 rpm. This model is similar to the IO-390-A1A6, except with a lightweight oil sump, cold air induction housing, tuned intake pipes and
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Certified version: four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 215 hp (160 kW) at 2700 rpm. This model is the same as the C1A6, except that the propeller governor is located on left front of the crankcase. Certified 25
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Certified version: four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. This model includes provisions for a single-action controllable-pitch propeller. This model is similar to the A1A6 but has its
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Certified version: aerobatic, four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. This model is the same as IO-390-A3B6, except that it is equipped with an inverted oil system kit for aerobatic
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Certified version: aerobatic, four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. This model is the same as IO-390-A3A6, except that it is equipped with an inverted oil system kit for aerobatic
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Certified version: aerobatic, four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. This model is the same as IO-390-A1B6, except that it is equipped with an inverted oil system kit for aerobatic
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Certified version: aerobatic, four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. This model is the same as IO-390-A1A6, except that it is equipped with an inverted oil system kit for aerobatic
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Certified version: four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 215 hp (160 kW) at 2700 rpm. This model is the same as the C1A6, except that the propeller flange bushings are reindexed. Certified 25 January
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Certified version: four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. Same as the A3A6 except that the propeller governor is located on left front of the crankcase. Certified 5 April
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Certified version: four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. Same as the A1A6, except that the propeller governor is located on left front of crankcase. Certified 21 January
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The initial certified version: four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm. This model includes provisions for a single-action controllable-pitch propeller. Certified 30 March
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Four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm, dry weight 308 lb (140 kg), non-certified engine for experimental aircraft assembled by Lycoming's Thunderbolt
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Four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 210 hp (157 kW) at 2700 rpm, dry weight 308 lb (140 kg), The "X" designation is a generic indicator for all engines in the
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to increase the O-360's cylinder bore. (Although the IO-390 cylinder assembly is not the same part number as the IO-580, the cylinder barrels of both have a 5.318 bore and 4.375 stroke dimension.)
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The IO-390 family of engines, which Lycoming refers to as the IO-390-X, produce 200 hp (149 kW) to 215 hp (160 kW). The IO-390 was developed from the similar
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system which meters fuel in proportion to the induction airflow with fuel vaporization taking place at the intake ports. The engine has a
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and was at that time only available for installation on non-certified aircraft. The IO-390 was certified on 30 March 2009 to FAR 33.
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The IO-390 was initially marketed through Lycoming's custom engine subsidiary, Thunderbolt Engines, prior to the engine's
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version of the engine, which would have been designated O-390 and therefore the base model is the IO-390.
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The engine was originally conceived in the 1970s as the IO-400-X, but the project was never pursued.
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It features a tuned induction system, roller tappets and Slick Start ignition. The engine has a
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11.1 gallons per hour (42 liters per hour; 9.2 imperial gallons per hour) at 65 percent power
194: 522: 212: 8: 573: 525: 179: 489:- factory installed IO-390-C3B6 215 hp (160 kW) version on the SR20 G6 version 1594: 498: 414: 384: 739: 653: 399: 984: 1523: 1518: 1495: 1477: 1472: 1430: 1425: 1339: 976: 830: 772: 716: 205: 139: 64: 1550: 1445: 1440: 1435: 1368: 1342: 564: 504: 167: 135: 112: 108: 42: 1467: 1420: 1415: 1410: 1393: 1388: 1383: 1378: 1373: 1363: 1358: 1098: 683: 223: 175: 161: 1628: 1560: 1455: 555: 409: 183: 132: 54: 1308: 1073: 1555: 510: 477: 389: 230:
with a new or remanufactured IO-390-A3A6 engine. Also on November 12, 2009
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of 390 cubic inches (6.39 litres). The cylinders have air-cooled
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In November 2009 Lycoming announced that it had obtained an FAA
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Lycoming Specialty Datasheet & Type Certificate Data Sheet
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propeller flange bushings reindexed. Certified 27 August 2009.
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4-cylinder fuel-injected horizontally opposed aircraft engine
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In January 2009 the base price of the IO-390-EXP version was
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Part number 16A26081, Cylinder and Head Assembly, Nitrided
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an RSA-10 fuel injector. Certified 25 January 2016.
1231:"AVwebFlash Complete Issue: Volume 14, Number 31e" 860:"IO-390-A Series Engine Illustrated Parts Catalog" 1274: 1626: 1147: 1145: 1055:"How to Buy: For Experimental Pilots - Lycoming" 975: 829: 771: 715: 531: 1003: 1001: 453:can have an IO-390-A3A6 installed under an STC 1338: 1324: 1142: 1121: 1010:"Lycoming Gets IO-390 STC For Legacy Mooneys" 1222: 998: 935: 933: 931: 929: 835:"Lycoming's Certified IO-390 Series Engine" 767: 765: 763: 761: 759: 757: 755: 1614:AlliedSignal Aerospace/Honeywell Aerospace 1331: 1317: 1090: 969: 927: 925: 923: 921: 919: 917: 915: 913: 911: 909: 542: 495:- available in November 2009 under an STC 152: 1166: 1151: 752: 456: 444: 366: 1268: 1152:Burnside, Joseph E. (Jeb) (July 2009). 906: 901:Part Number 16A22887, Cylinder Assembly 825: 823: 711: 709: 707: 705: 703: 646:210 hp (160 kW) at 2700  374:have been fitted with the IO-390 engine 1627: 821: 819: 817: 815: 813: 811: 809: 807: 805: 803: 238:using the MTV-12-B/188-59b propeller. 1312: 1229:AVweb Editorial Staff (August 2008). 1197: 1127: 1022: 1007: 1071: 700: 1275:Aero-News Network (February 2009). 1210:from the original on 7 October 2020 1096: 800: 193:2002. It has a factory recommended 189:The IO-390 was first introduced at 13: 480:- available in July 2009 under an 327: 14: 1656: 1293: 1109:from the original on 26 July 2022 981:"Thunderbolt Engine Configurator" 673:0.68 hp/lb (1.12 kW/kg) 578:389 cu in (6.37 L) 222:to replace the originally fitted 605:308 lb (139.71 kg) dry 246: 27: 1243: 1191: 1065: 1057:. 22 March 2012. Archived from 1047: 1030:Federal Aviation Administration 941:Federal Aviation Administration 362: 358:flight. Certified 5 April 2012. 351:flight. Certified 5 April 2012. 344:flight. Certified 5 April 2012. 337:flight. Certified 5 April 2012. 1200:"Cirrus Updates SR22 And SR20" 1198:Grady, Mary (4 January 2017). 1176:. January 2017. Archived from 879: 852: 637: 1: 1635:2000s aircraft piston engines 1251:"P2010 P Twenty-Ten - Tecnam" 1008:Grady, Mary (November 2009). 694: 609: 569:4.375 in (111.1 mm) 560:5.319 in (135.1 mm) 220:Supplemental Type Certificate 197:of 2000 hours and requires a 16:Four-cylinder aircraft engine 532:Specifications (IO-390-A1A6) 166:by using cylinders from the 7: 677: 596:19.35 in (491 mm) 590:34.25 in (870 mm) 584:30.70 in (780 mm) 241: 10: 1661: 1097:Dye, Paul (25 July 2022). 887:"IO-580-B1A Parts Catalog" 440:Whisper X350 Generation II 228:Mooney M20E, M20F and M20J 1640:Lycoming aircraft engines 1606: 1588: 1569: 1532: 1504: 1486: 1454: 1349: 1128:Grady, Mary (July 2009). 26: 21: 1174:"Cirrus G6 announcement" 1074:"Cirrus Aircraft | SR20" 689:List of aircraft engines 234:received an STC for its 1570:Aero-derivative marine 1488:Aircraft diesel engines 892:. Lycoming. p. 3-3 543:General characteristics 493:Mooney M20 E, F & J 395:Ibis GS-750 Grand Magic 1351:Opposed piston engines 865:. Lycoming. p. 25 462: 454: 379:Amateur-built aircraft 375: 199:dynafocal engine mount 153:Design and development 777:"Specialty datasheet" 669:Power-to-weight ratio 460: 448: 370: 1032:(12 November 2009). 744:: CS1 maint: year ( 523:Lancair Synergy T-90 501:- proposed under STC 472:Aura Aero Integral R 461:Aura Aero Integral R 435:Van's Aircraft RV-15 430:Van's Aircraft RV-14 372:Van's Aircraft RV-8s 129:horizontally opposed 1595:Pratt & Whitney 943:(25 January 2017). 841:on 13 February 2012 721:"Lycoming IO-390-X" 526:Colombian Air Force 425:Van's Aircraft RV-8 420:Van's Aircraft RV-7 1645:2002 introductions 1078:cirrusaircraft.com 1072:Aircraft, Cirrus. 957:on 2 February 2017 499:Piper PA-28R Arrow 466:Certified aircraft 463: 455: 415:Pipistrel Panthera 385:Bearhawk Companion 376: 232:Commander Aircraft 138:, manufactured by 80:Major applications 1622: 1621: 1589:Joint development 1402: 662:Fuel consumption: 654:Compression ratio 517:Military Aircraft 400:Lancair Barracuda 390:Glasair Sportsman 118: 117: 1652: 1593:Avco (Lycoming)/ 1396: 1343:aircraft engines 1333: 1326: 1319: 1310: 1309: 1305: 1304: 1302:Official website 1288: 1287: 1285: 1283: 1272: 1266: 1265: 1263: 1261: 1247: 1241: 1240: 1238: 1237: 1226: 1220: 1219: 1217: 1215: 1195: 1189: 1188: 1186: 1185: 1180:on 27 March 2017 1170: 1164: 1163: 1161: 1160: 1149: 1140: 1139: 1137: 1136: 1125: 1119: 1118: 1116: 1114: 1094: 1088: 1087: 1085: 1084: 1069: 1063: 1062: 1051: 1045: 1044: 1042: 1040: 1026: 1020: 1019: 1017: 1016: 1005: 996: 995: 993: 992: 983:. Archived from 979:(January 2009). 977:Lycoming Engines 973: 967: 966: 964: 962: 956: 950:. Archived from 949: 937: 904: 903: 898: 897: 891: 883: 877: 876: 871: 870: 864: 856: 850: 849: 847: 846: 837:. Archived from 831:Lycoming Engines 827: 798: 797: 795: 794: 788: 782:. Archived from 781: 773:Lycoming Engines 769: 750: 749: 743: 735: 733: 732: 727:on 21 March 2012 723:. Archived from 717:Lycoming Engines 713: 170: 140:Lycoming Engines 105: 81: 65:Lycoming Engines 51: 31: 19: 18: 1660: 1659: 1655: 1654: 1653: 1651: 1650: 1649: 1625: 1624: 1623: 1618: 1602: 1584: 1565: 1528: 1500: 1482: 1450: 1345: 1337: 1300: 1299: 1296: 1291: 1281: 1279: 1273: 1269: 1259: 1257: 1249: 1248: 1244: 1235: 1233: 1227: 1223: 1213: 1211: 1196: 1192: 1183: 1181: 1172: 1171: 1167: 1158: 1156: 1150: 1143: 1134: 1132: 1126: 1122: 1112: 1110: 1095: 1091: 1082: 1080: 1070: 1066: 1053: 1052: 1048: 1038: 1036: 1027: 1023: 1014: 1012: 1006: 999: 990: 988: 987:on 14 July 2011 974: 970: 960: 958: 954: 947: 938: 907: 895: 893: 889: 885: 884: 880: 868: 866: 862: 858: 857: 853: 844: 842: 828: 801: 792: 790: 786: 779: 770: 753: 737: 736: 730: 728: 714: 701: 697: 680: 640: 631:Cooling system: 612: 545: 534: 505:Symphony SA-160 365: 330: 328:AEIO-390 models 249: 244: 226:engines in the 165: 155: 136:aircraft engine 122:Lycoming IO-390 113:Lycoming IO-580 111: 109:Lycoming IO-360 103: 87: 79: 50:National origin 49: 17: 12: 11: 5: 1658: 1648: 1647: 1642: 1637: 1620: 1619: 1617: 1616: 1610: 1608: 1604: 1603: 1592: 1590: 1586: 1585: 1583: 1582: 1576: 1574: 1567: 1566: 1564: 1563: 1558: 1553: 1548: 1542: 1540: 1530: 1529: 1527: 1526: 1521: 1516: 1510: 1508: 1502: 1501: 1499: 1498: 1492: 1490: 1484: 1483: 1481: 1480: 1475: 1470: 1464: 1462: 1456:Radial engines 1452: 1451: 1449: 1448: 1443: 1438: 1433: 1428: 1423: 1418: 1413: 1408: 1403: 1399:O-360 variants 1391: 1386: 1381: 1376: 1371: 1366: 1361: 1355: 1353: 1347: 1346: 1336: 1335: 1328: 1321: 1313: 1307: 1306: 1295: 1294:External links 1292: 1290: 1289: 1267: 1242: 1221: 1190: 1165: 1141: 1120: 1099:"Van's on Top" 1089: 1064: 1061:on 2012-03-22. 1046: 1021: 997: 968: 905: 878: 851: 799: 789:on 26 May 2012 751: 698: 696: 693: 692: 691: 686: 684:Lycoming O-360 679: 676: 675: 674: 665: 659: 650: 639: 636: 635: 634: 628: 619: 618:fuel-injection 611: 608: 607: 606: 597: 591: 585: 579: 570: 561: 552: 544: 541: 533: 530: 529: 528: 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1601:(Turboshaft) 1572:gas turbines 1405: 1280:. 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Retrieved 725:the original 667: 661: 652: 643: 630: 621: 616:Fuel system: 615: 599: 593: 587: 581: 574:Displacement 572: 563: 554: 548: 536: 535: 511:Tecnam P2010 478:Cessna 177RG 363:Applications 217: 210: 203: 188: 180:displacement 173: 159: 156: 145:There is no 144: 121: 119: 89:Tecnam P2010 1538:Turboshafts 638:Performance 487:Cirrus SR20 451:Mooney M20J 321:Cirrus SR20 315:IO-390-C3B6 308:IO-390-C3A6 301:IO-390-C1B6 294:IO-390-C1A6 287:IO-390-A3B6 280:IO-390-A3A6 273:IO-390-A1B6 266:IO-390-A1A6 147:carburetted 85:Cirrus SR20 43:aero-engine 1629:Categories 1534:Turboprops 1255:tecnam.com 1236:2008-08-01 1184:2017-01-04 1159:2009-07-28 1135:2009-07-28 1083:2017-01-30 1015:2009-11-15 991:2009-01-06 961:29 January 896:2022-07-21 869:2022-07-21 845:2009-01-07 793:2008-12-20 731:2009-01-07 695:References 633:air-cooled 622:Fuel type: 610:Components 601:Dry weight 405:Lancair ES 259:IO-390-EXP 236:model 112B 191:AirVenture 71:First run 1506:Turbofans 1460:H engines 1214:6 January 1103:KitPlanes 537:Data from 263:division. 95:Produced 1607:See also 1599:T800-APW 1340:Lycoming 1208:Archived 1107:Archived 1039:30 March 833:(2008). 775:(2004). 740:cite web 719:(n.d.). 678:See also 319:Used on 252:IO-390-X 242:Variants 164:engine, 1546:AGT1500 1496:DEL-120 1478:XH-2470 1473:XR-7755 1431:GSO-580 1426:TIO-541 1282:31 July 1260:7 April 1113:29 July 594:Height: 582:Length: 256:family. 22:IO-390 1524:LF 507 1446:O-1230 1441:IO-720 1436:IO-580 1406:IO-390 1369:IO-233 624:100LL 588:Width: 565:Stroke 168:IO-580 162:IO-360 125:engine 40:Piston 1580:TF-40 1468:R-680 1421:O-540 1416:O-480 1411:O-435 1394:O-360 1389:O-340 1384:O-320 1379:O-290 1374:O-235 1364:O-233 1359:O-145 1204:AVweb 955:(PDF) 948:(PDF) 890:(PDF) 863:(PDF) 787:(PDF) 780:(PDF) 658:8.9:1 626:avgas 549:Type: 312:2016. 291:2012. 277:2010. 270:2009. 184:heads 127:is a 74:2002 36:Type 1514:PLF1 1458:and 1284:2010 1262:2019 1216:2017 1115:2022 1041:2014 963:2017 746:link 556:Bore 449:The 120:The 1561:T55 1556:T53 648:rpm 482:STC 323:G6. 213:USD 195:TBO 1631:: 1597:: 1253:. 1206:. 1202:. 1144:^ 1105:. 1101:. 1076:. 1000:^ 908:^ 899:. 872:. 802:^ 754:^ 742:}} 738:{{ 702:^ 201:. 186:. 142:. 131:, 1536:/ 1401:) 1397:( 1332:e 1325:t 1318:v 1286:. 1264:. 1239:. 1218:. 1187:. 1162:. 1138:. 1117:. 1086:. 1043:. 1018:. 994:. 965:. 848:. 796:. 748:) 734:. 671:: 656:: 603:: 576:: 567:: 558::

Index


Piston
aero-engine
United States
Lycoming Engines
Cirrus SR20
Tecnam P2010
Lycoming IO-360
Lycoming IO-580
engine
horizontally opposed
four-cylinder
aircraft engine
Lycoming Engines
carburetted
IO-360
IO-580
fuel injection
displacement
heads
AirVenture
TBO
dynafocal engine mount
certification
USD
Supplemental Type Certificate
Lycoming O-360
Mooney M20E, M20F and M20J
Commander Aircraft
model 112B

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