31:
548:
537:
1289:
172:
split case by four main bearings and one ball-thrust bearing, and lubricating oil is supplied from a 12 quart wet sump. The camshaft rides in journals that do not employ bearing inserts. The accessory housing supports two magnetos, a starter, a generator, and a dual tach drive. A spare mounting pad is included for a vacuum pump.
457:, vertically-mounted engine model for helicopters, with a dry sump oil system. It produces 260 hp (194 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 468 lb (212 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on May 12, 1961.
441:, vertically-mounted engine model for helicopters, with a dry sump oil system. It produces 260 hp (194 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 468 lb (212 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on May 12, 1961.
505:
Turbocharged, vertically-mounted engine model for helicopters, with a wet sump oil system, different accessory section and a higher power rating. It produces 280 hp (209 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 490 lb (222 kg) and fitted with
491:
Turbocharged, vertically-mounted engine model for helicopters, with a dry sump oil system. It has TCM (formerly Bendix) S-200 series magnetos. It produces 270 hp (201 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 464 lb (210 kg) and fitted with a
470:
Turbocharged, vertically-mounted engine model for helicopters, with a dry sump oil system and TCM (formerly Bendix) S6RN-1208 and S6LN-1209 magnetos. It produces 270 hp (201 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 479 lb (217 kg) and fitted
463:
Turbocharged, vertically-mounted engine model with internal piston cooling oil jets, for helicopters, with a dry sump oil system and cylinder assemblies machined for long-reach spark plugs. It produces 270 hp (201 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight
424:
Vertically-mounted engine model for helicopters, with a dry sump oil system. It has internal piston cooling oil jets and heavy duty cylinders and may be converted to a model TVO-435-A1A. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of
417:
Vertically-mounted engine model for helicopters, with a dry sump oil system and 6RN-200 or S6LN-204 magnetos. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 392 lb (178 kg) and fitted with a Marvel MA-4-5AA carburetor. Type
410:
Vertically-mounted engine model for helicopters, with a dry sump oil system, with crankcase and oil sump modifications for increased strength. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 390 lb (177 kg) and fitted with a
265:
Engine model with increased maximum continuous rating and the generator pad omitted, approved for helicopter installations. It produces 250 hp (186 kW) at 3000 rpm, with a compression ratio of 7.3:1, a dry weight of 405 lb (184 kg) and fitted with a Marvel MA-4-5 carburetor. Type
244:
Engine model, with revised type valves, valve guides, an accessory case with generator and starter drive, producing 175 hp (130 kW) at 2300 rpm, with a compression ratio of 6.25:1, a dry weight of 366 lb (166 kg) and fitted with a Marvel MA-4 carburetor. Type certified on
January
498:
Turbocharged, vertically-mounted engine model for helicopters, with a dry sump oil system and a Kelly
Aerospace (formerly AiResearch) TK-0659 turbocharger. It produces 260 hp (194 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 490 lb (222 kg) and
484:
Turbocharged, vertically-mounted engine model for helicopters, with a dry sump oil system. It has a TK-0659 turbocharger and TCM (formerly Bendix) S6RN-1208 (retarded breaker) and S6LN-1209 magnetos. It produces 270 hp (201 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a
403:
Vertically-mounted engine model for helicopters, with a dry sump oil system, which incorporates a crankcase and oil sump modification giving increased strength and an oil pump housing which is machined for a hydraulic pump drive. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a
382:
Base model, vertically-mounted engine for helicopters, with a dry sump oil system and side-mounted AN type accessory drives. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 396 lb (180 kg) and fitted with a Marvel MA-4-5 or
333:
Geared engine model which incorporates a dual generator and vacuum pump drive. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 430 lb (195 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on
February
326:
Geared engine model with provisions for a hydraulic propeller and governor. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 430 lb (195 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on
November 6,
292:
Baseline geared engine model. It incorporates six 3rd-order crankshaft torsional vibration dampers and reduction gearing. It produced 210 hp (157 kW) at 3000 rpm, with a compression ratio of 6.25:1, a dry weight of 407 lb (185 kg) and fitted with a Marvel MA-4-5 carburetor. Type
319:
Geared engine model, with a dry sump and without provisions for a hydraulic propeller control or governor, producing 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 432 lb (196 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor.
312:
Geared engine model, incorporates S6LN-20 or -21 magnetos, producing 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 438 lb (199 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on
January 2, 1951, cancelled on
171:
The powerplant is a horizontally opposed
Lycoming six-cylinder design. It is a direct-drive or geared, air-cooled, and normally aspirated engine. The cylinders have steel barrels with aluminum heads, and the valves are operated by hydraulic lifters. The crankshaft is supported in an aluminum-alloy
278:
Civil modified military engine model, by the
Associated Aircraft Modification Company, with Bendix PS-5C carburetor with 380123-1 setting. It produces 235 hp (175 kW) at 3200 rpm, with a compression ratio of 7.5:1, a dry weight of 405 lb (184 kg). Only military O-435-2 engines
526:
Turbocharged, vertically-mounted military engine model for helicopters, with a dry sump oil system. This military model is similar to the -A1A, except it has cylinder assemblies from the -B1A. It produces 260 hp (194 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry
431:
Vertically-mounted engine model for helicopters, with a redesigned accessory drive section, a wet oil sump and a higher compression ratio. It produces 265 hp (198 kW) at 3200 rpm for takeoff, with a compression ratio of 8.7:1, a dry weight of 419 lb (190 kg) and fitted with a
512:
Turbocharged, vertically-mounted engine model for helicopters, with a dry sump oil system and a different automatic waste gate control setting for a higher power rating. It produces 280 hp (209 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 465 lb
477:
Turbocharged, vertically-mounted engine model for helicopters, with a dry sump oil system and a T-1112 turbosupercharger. It produces 380 hp (283 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 478 lb (217 kg) and fitted with a Marvel-Schebler
305:
Geared engine model which incorporates an improved crankcase and cylinder assembly. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 422 lb (191 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on
210:
Engine model with provisions for automotive type accessories, producing 190 hp (142 kW) at 2550 rpm, with a compression ratio of 6.5:1, a dry weight of 348 lb (158 kg) with a -8 magneto and 342 lb (155 kg) with a -20 magneto and fitted with a Marvel MA-4-5 or PS-5C
519:
Turbocharged, vertically-mounted engine model for helicopters, with a dry sump oil system and different magnetos. It produces 280 hp (209 kW) at 3200 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 464 lb (210 kg) and fitted with a Marvel-Schebler MA-6AA
396:
Vertically-mounted engine model for helicopters, with a dry sump oil system and a modified accessory section. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 391 lb (177 kg) and fitted with a Marvel MA-4-5 or MA-4-5AA
389:
Vertically-mounted engine model for helicopters, with a dry sump oil system and side-mounted AN type accessory drives. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 396 lb (180 kg) and fitted with a Marvel MA-4-5 or
217:
Engine model with a redesigned improved crankcase, cylinders, valves and valve seats, exhaust valve guides and rocker shaft bushing. It also has provisions for automotive-type accessories. It produced 225 hp (168 kW) at 3000 rpm, with a compression ratio of 7.5:1, a dry weight of
230:
Engine model with provisions for AN type accessories, producing 235 hp (175 kW) at 3000 rpm, with a compression ratio of 7.5:1, a dry weight of 362 lb (164 kg) and fitted with a Marvel MA-4-5 carburetor. Type certified on
October 7, 1943 and cancelled on November 2,
361:
Geared engine model with S6LN-20, or -21 magnetos. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 420 lb (191 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on
September 27,
340:
Geared engine model with S6LN-20, or -21 magnetos. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 430 lb (195 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on
February 28,
258:
Engine model that incorporates a GO-435-C2 accessory case and crankcase. It produces 240 hp (179 kW) at 3000 rpm, with a compression ratio of 7.3:1, a dry weight of 405 lb (184 kg) and fitted with a Marvel MA-4-5 carburetor. Type certified on January 24,
347:
Geared engine model producing 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 422 lb (191 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on November 24, 1953 and cancelled on July 5,
354:
Geared engine model producing 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 420 lb (191 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on July 20, 1954 and cancelled on July 5,
251:
Engine model, with provisions for O-435-C accessories carburetor, producing 175 hp (130 kW) at 2300 rpm, with a compression ratio of 6.25:1, a dry weight of 368 lb (167 kg) and fitted with a Marvel MA-4SPA carburetor. Type certified on January 2,
368:
Geared engine model with a dry sump oil system and crosswise accessory drives. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1 and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on September 25,
237:
Engine model with provisions for AN type accessories, producing 175 hp (130 kW) at 2300 rpm, with a compression ratio of 6.25:1, a dry weight of 356 lb (161 kg) and fitted with a Marvel MA-4SPA carburetor. Type certified on January 11,
1143:
1082:
1027:
1184:
1227:
200:
Baseline engine model, producing 175 hp (130 kW) at 2300 rpm, with a compression ratio of 6.25:1, a dry weight of 347 lb (157 kg) and fitted with a Marvel MA-4 carburetor.
184:
to indicate the specific configuration of the engine. There are also numerous engine suffixes, denoting different accessories such as different manufacturers' carburetors, or different
1136:
1075:
1020:
1321:
404:
compression ratio of 7.3:1, a dry weight of 399 lb (181 kg) and fitted with a Marvel MA-4-5 or MA-4-5AA carburetor. Type certified on July 18, 1954.
1177:
1216:
1635:
218:
365 lb (166 kg) and fitted with a Marvel MA-4-5 carburetor. Type certified on October 19, 1949 and cancelled on February 25, 1944.
30:
1625:
1314:
606:
552:
1274:
1604:
1389:
1212:
1173:
1132:
1071:
1016:
485:
dry weight of 465 lb (211 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on March 10, 1966.
878:
1307:
601:
527:
weight of 493 lb (224 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on June 10, 1963.
1589:
464:
of 478 lb (217 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on November 21, 1962.
1293:
721:
944:
1630:
1478:
1536:
591:
425:
399 lb (181 kg) and fitted with a Marvel MA-4-5AA carburetor. Type certified on March 6, 1961.
513:(211 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on January 11, 1968.
736:
716:
108:
1504:
801:
148:
1570:
547:
636:
575:
565:
100:
88:
1585:
661:
1270:
900:
646:
596:
141:
1514:
1509:
1486:
1468:
1463:
1421:
1416:
1330:
616:
201:
185:
156:
68:
1541:
1436:
1431:
1426:
1396:
1359:
1333:
792:
611:
586:
536:
48:
383:
MA-4-5AA carburetor. Type certified on October 11, 1954. Was re-designated as VO-435-A1A.
1458:
1411:
1406:
1384:
1379:
1374:
1369:
1364:
1354:
1349:
932:
920:
843:
696:
641:
160:
128:
1619:
1551:
1446:
783:
706:
686:
681:
676:
666:
631:
96:
1546:
651:
454:
438:
390:
MA-4-5AA carburetor. Type certified on October 29, 1954. Re-designated from VO-435.
279:
with serial numbers L00849-11 through L-1117-11 are eligible for this modification.
499:
fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on March 7, 1967.
1562:
1341:
726:
711:
701:
691:
671:
656:
626:
621:
145:
1528:
838:
822:
749:
570:
400:
VO-435-A1C (military designations O-435-23, O-435-23A O-435-23B and O-435-23C)
152:
104:
1524:
1299:
411:
Marvel MA-4-5 or MA-4-5AA carburetor. Type certified on September 27, 1956.
1288:
471:
with a Marvel-Schebler MA-6AA carburetor. Type certified on June 20, 1966.
1496:
1450:
541:
506:
a Marvel-Schebler MA-6AA carburetor. Type certified on January 22, 1968.
847:
731:
581:
492:
Marvel-Schebler MA-6AA carburetor. Type certified on February 23, 1967.
92:
299:
Type certified on October 19, 1949 and cancelled on February 8, 1955.
41:
224:
Type certified on January 5, 1951 and cancelled on February 8, 1955.
546:
535:
432:
Marvel MA-4-5AA carburetor. Type certified on December 15, 1965.
44:
1303:
293:
certified on August 30, 1944 and cancelled on November 2, 1950.
1269:
Hammersmith, London: HarperCollinsPublishers (1994 reprint).
159:. The engine is a six-cylinder version of the four-cylinder
779:
Six-cylinder horizontally-opposed gasoline piston engine
850:
actuated), one inlet and one exhaust valve per cylinder
478:
MA-6AA carburetor. Type certified on November 21, 1962.
180:
All engines have an additional prefix preceding the
1597:
1579:
1560:
1523:
1495:
1477:
1445:
1340:
1076:"Type Certificate Data Sheet No. E-279 Revision 10"
1021:"Type Certificate Data Sheet No. E-228 Revision 17"
896:
212 hp (158 kW) at 3,000 rpm at sea level
1137:"Type Certificate Data Sheet No. 1E13 Revision 8"
520:carburetor. Type certified on November 25, 1968.
211:carburetor. Type certified on February 11, 1942.
313:February 8, 1955 and reinstated July 15, 1955.
1315:
8:
874:Air-cooled by fan (helicopter installations)
460:TVO-435-B1A (military designation O-435-25A)
397:carburetor. Type certified on June 10, 1955.
1605:AlliedSignal Aerospace/Honeywell Aerospace
1322:
1308:
1300:
407:VO-435-A1D (military designation O-435-6A)
386:VO-435-A1A (military designation O-435-21)
393:VO-435-A1B (military designation O-435-6)
302:GO-435-C2 (military designation O-435-17)
1267:Jane's All the World's Aircraft 1945-46.
1011:
1009:
1007:
1005:
1003:
1001:
999:
997:
995:
993:
991:
989:
987:
985:
248:O-435-C2 (military designation O-435-13)
241:O-435-C1 (military designation O-435-11)
1178:"Type Certificate Data Sheet No. 5E-12"
1168:
1166:
1164:
1127:
1125:
1123:
1066:
1064:
1062:
1060:
1058:
1056:
1054:
1052:
1050:
1048:
983:
981:
979:
977:
975:
973:
971:
969:
967:
965:
961:
262:O-435-K1 (military designation O-435-4)
1190:from the original on September 2, 2022
1121:
1119:
1117:
1115:
1113:
1111:
1109:
1107:
1105:
1103:
1088:from the original on December 20, 2016
1033:from the original on December 16, 2016
234:O-435-C (military designation O-435-1)
227:O-435-B (military designation O-435-5)
20:
1207:
1205:
7:
1233:from the original on April 19, 2021
1149:from the original on April 11, 2021
320:Type certified on October 24, 1957.
1217:"Helicopter Specification No. 1H1"
607:de Havilland Canada Super Chipmunk
540:A Lycoming TVO-435 installed in a
14:
551:Lycoming O-435 on display at the
1287:
29:
1213:Federal Aviation Administration
1174:Federal Aviation Administration
1133:Federal Aviation Administration
1072:Federal Aviation Administration
1017:Federal Aviation Administration
418:certified on October 15, 1959.
16:American 1940s aircraft engine
1:
1636:1940s aircraft piston engines
266:certified on March 30, 1951.
118:1942–1975 out of production
1652:
856:Marvel-Schebler carburetor
602:D'Apuzzo Senior Aero Sport
1626:Lycoming aircraft engines
722:St Croix Sopwith Triplane
28:
23:
945:List of aircraft engines
757:Specifications (O-435-D)
1561:Aero-derivative marine
1479:Aircraft diesel engines
771:General characteristics
1342:Opposed piston engines
1251:Bridgman 1994, p. 78d.
1215:(September 26, 1950).
555:
544:
272:Military engine model.
167:Design and development
592:Bellanca Cruisemaster
550:
539:
204:on February 11, 1942.
1296:at Wikimedia Commons
1135:(November 4, 2010).
1074:(November 4, 2010).
737:Vertical Hummingbird
717:Stinson L-5 Sentinel
146:horizontally opposed
109:Stinson L-5 Sentinel
1586:Pratt & Whitney
1265:Bridgman, Leonard.
915:Related development
862:100 octane gasoline
788:4.875 in (123.8 mm)
149:fixed-wing aircraft
140:is an American six-
927:Comparable engines
868:Pressure pump type
818:43.5 in (1,105 mm)
797:3.875 in (98.4 mm)
637:Hiller OH-23 Raven
576:Beechcraft Bonanza
566:Aero Commander 500
556:
553:Museum of Aviation
545:
101:Hiller OH-23 Raven
89:Beechcraft Bonanza
84:Major applications
1613:
1612:
1580:Joint development
1393:
1292:Media related to
1019:(June 23, 2010).
901:Compression ratio
827:433 lb (196.6 kg)
806:434 cu in (7.1 L)
647:Jeffair Barracuda
597:Boisavia Mercurey
306:October 19, 1949.
134:
133:
1643:
1584:Avco (Lycoming)/
1387:
1334:aircraft engines
1324:
1317:
1310:
1301:
1291:
1252:
1249:
1243:
1242:
1240:
1238:
1232:
1221:
1209:
1200:
1199:
1197:
1195:
1189:
1182:
1170:
1159:
1158:
1156:
1154:
1148:
1141:
1129:
1098:
1097:
1095:
1093:
1087:
1080:
1068:
1043:
1042:
1040:
1038:
1032:
1025:
1013:
812:33.5 in (851 mm)
617:Fleetwings PQ-12
157:Lycoming Engines
125:
85:
69:Lycoming Engines
57:
33:
21:
1651:
1650:
1646:
1645:
1644:
1642:
1641:
1640:
1616:
1615:
1614:
1609:
1593:
1575:
1556:
1519:
1491:
1473:
1441:
1336:
1328:
1284:
1279:
1261:
1256:
1255:
1250:
1246:
1236:
1234:
1230:
1219:
1211:
1210:
1203:
1193:
1191:
1187:
1180:
1172:
1171:
1162:
1152:
1150:
1146:
1139:
1131:
1130:
1101:
1091:
1089:
1085:
1078:
1070:
1069:
1046:
1036:
1034:
1030:
1023:
1015:
1014:
963:
958:
953:
912:
890:
872:Cooling system:
834:
773:
759:
741:
662:Karhumäki Karhu
612:Fleetwings BQ-2
587:Bell H-13 Sioux
534:
448:
376:
286:
194:
178:
169:
155:engine made by
123:
107:
103:
99:
95:
91:
83:
56:National origin
55:
49:aircraft engine
17:
12:
11:
5:
1649:
1647:
1639:
1638:
1633:
1628:
1618:
1617:
1611:
1610:
1608:
1607:
1601:
1599:
1595:
1594:
1583:
1581:
1577:
1576:
1574:
1573:
1567:
1565:
1558:
1557:
1555:
1554:
1549:
1544:
1539:
1533:
1531:
1521:
1520:
1518:
1517:
1512:
1507:
1501:
1499:
1493:
1492:
1490:
1489:
1483:
1481:
1475:
1474:
1472:
1471:
1466:
1461:
1455:
1453:
1447:Radial engines
1443:
1442:
1440:
1439:
1434:
1429:
1424:
1419:
1414:
1409:
1404:
1399:
1394:
1390:O-360 variants
1382:
1377:
1372:
1367:
1362:
1357:
1352:
1346:
1344:
1338:
1337:
1329:
1327:
1326:
1319:
1312:
1304:
1298:
1297:
1294:Lycoming O-435
1283:
1282:External links
1280:
1278:
1277:
1262:
1260:
1257:
1254:
1253:
1244:
1201:
1160:
1099:
1044:
960:
959:
957:
954:
952:
949:
948:
947:
936:
935:
933:Franklin O-335
924:
923:
921:Lycoming O-290
911:
908:
907:
906:
897:
889:
886:
885:
884:
879:Reduction gear
875:
869:
863:
857:
851:
844:Overhead valve
833:
830:
829:
828:
819:
813:
807:
798:
789:
780:
772:
769:
758:
755:
754:
753:
746:
745:
740:
739:
734:
729:
724:
719:
714:
709:
704:
699:
697:Ra-Son Warrior
694:
689:
684:
679:
674:
669:
664:
659:
654:
649:
644:
642:Interstate TDR
639:
634:
629:
624:
619:
614:
609:
604:
599:
594:
589:
584:
579:
573:
568:
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452:
447:
446:TVO-435 models
444:
443:
442:
436:
433:
429:
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412:
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398:
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212:
208:
205:
202:Type certified
198:
193:
190:
177:
174:
168:
165:
161:Lycoming O-290
138:Lycoming O-435
132:
131:
129:Lycoming O-290
126:
124:Developed from
120:
119:
116:
112:
111:
86:
80:
79:
76:
72:
71:
66:
62:
61:
60:United States
58:
52:
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39:
35:
34:
26:
25:
15:
13:
10:
9:
6:
4:
3:
2:
1648:
1637:
1634:
1632:
1631:Boxer engines
1629:
1627:
1624:
1623:
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1606:
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1600:
1596:
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1553:
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1548:
1545:
1543:
1542:LTS101/LTP101
1540:
1538:
1535:
1534:
1532:
1530:
1526:
1522:
1516:
1513:
1511:
1510:ALF 502/YF102
1508:
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1500:
1498:
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1229:
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1214:
1208:
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1145:
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1128:
1126:
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946:
943:
942:
941:
940:
939:Related lists
934:
931:
930:
929:
928:
922:
919:
918:
917:
916:
909:
904:
902:
898:
895:
894:Power output:
892:
891:
887:
882:
880:
876:
873:
870:
867:
864:
861:
858:
855:
852:
849:
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836:
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742:
738:
735:
733:
730:
728:
725:
723:
720:
718:
715:
713:
710:
708:
707:Saab 91 Safir
705:
703:
700:
698:
695:
693:
690:
688:
687:Piaggio P.149
685:
683:
682:Piaggio P.148
680:
678:
677:Miles Aerovan
675:
673:
670:
668:
667:Kawasaki KH-4
665:
663:
660:
658:
655:
653:
650:
648:
645:
643:
640:
638:
635:
633:
632:Helio Courier
630:
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423:
420:
416:
413:
409:
406:
402:
399:
395:
392:
388:
385:
381:
378:
377:
374:VO-435 models
373:
367:
364:
360:
357:
353:
350:
346:
343:
339:
336:
332:
329:
325:
322:
318:
315:
311:
308:
304:
301:
298:
295:
291:
288:
287:
284:GO-435 models
283:
277:
274:
271:
268:
264:
261:
257:
254:
250:
247:
243:
240:
236:
233:
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97:Helio Courier
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65:Manufacturer
64:
63:
59:
54:
53:
50:
46:
43:
40:
37:
36:
32:
27:
22:
19:
1592:(Turboshaft)
1563:gas turbines
1401:
1275:000 470831-8
1266:
1259:Bibliography
1247:
1237:September 2,
1235:. Retrieved
1223:
1194:September 2,
1192:. Retrieved
1153:September 2,
1151:. Retrieved
1092:September 2,
1090:. Retrieved
1037:September 2,
1035:. Retrieved
938:
937:
926:
925:
914:
913:
899:
893:
883:Direct-drive
877:
871:
865:
859:
854:Fuel system:
853:
837:
821:
815:
809:
802:Displacement
800:
791:
782:
776:
764:
761:
760:
652:Kaman K-190A
532:Applications
455:Turbocharged
439:Turbocharged
192:O-435 models
181:
179:
170:
137:
135:
18:
1529:Turboshafts
888:Performance
866:Oil system:
727:UTVA Aero 3
712:Stinson 108
702:Ryan Navion
692:Pilatus P-4
672:LIBIS KB-11
657:Kaman K-225
627:Fokker S-11
622:Fokker F.25
516:TVO-435-G1B
509:TVO-435-G1A
502:TVO-435-F1A
495:TVO-435-E1A
488:TVO-435-D1B
481:TVO-435-D1A
474:TVO-435-C1A
467:TVO-435-B1B
451:TVO-435-A1A
435:TVO-435-A1A
337:GO-435-C2B2
330:GO-435-C2B1
316:GO-435-C2A2
1620:Categories
1525:Turboprops
951:References
860:Fuel type:
839:Valvetrain
832:Components
823:Dry weight
750:M22 Locust
571:AISA I-115
523:TVO-435-25
428:VO-435-B1A
421:VO-435-A1F
414:VO-435-A1E
358:GO-435-C2E
351:GO-435-C2D
344:GO-435-C2C
323:GO-435-C2B
309:GO-435-C2A
275:O-435-2-M1
153:helicopter
105:M22 Locust
75:First run
1497:Turbofans
1451:H engines
762:Data from
365:GO-435-D1
296:GO-435-A2
115:Produced
1598:See also
1590:T800-APW
1331:Lycoming
1228:Archived
1185:Archived
1144:Archived
1083:Archived
1028:Archived
910:See also
559:Aircraft
542:Bell 47G
334:8, 1955.
245:2, 1948.
221:O-435-A3
214:O-435-A2
186:magnetos
176:Variants
142:cylinder
1537:AGT1500
1487:DEL-120
1469:XH-2470
1464:XR-7755
1422:GSO-580
1417:TIO-541
1224:faa.gov
848:pushrod
816:Height:
732:UTVA 56
582:Bell 47
269:O-435-2
255:O-435-K
207:O-435-A
93:Bell 47
1515:LF 507
1437:O-1230
1432:IO-720
1427:IO-580
1397:IO-390
1360:IO-233
1273:
846:(OHV,
810:Width:
793:Stroke
765:Jane's
752:- tank
379:VO-435
289:GO-435
42:Piston
24:O-435
1571:TF-40
1459:R-680
1412:O-540
1407:O-480
1402:O-435
1385:O-360
1380:O-340
1375:O-320
1370:O-290
1365:O-235
1355:O-233
1350:O-145
1231:(PDF)
1220:(PDF)
1188:(PDF)
1181:(PDF)
1147:(PDF)
1140:(PDF)
1086:(PDF)
1079:(PDF)
1031:(PDF)
1024:(PDF)
956:Notes
905:7.5:1
777:Type:
744:Other
369:1953.
362:1956.
355:1956.
348:1956.
341:1956.
327:1952.
259:1951.
252:1948.
238:1943.
231:1950.
197:O-435
78:1939
38:Type
1505:PLF1
1449:and
1271:ISBN
1239:2022
1196:2022
1155:2022
1094:2022
1039:2022
784:Bore
151:and
136:The
47:and
45:tank
1552:T55
1547:T53
182:435
1622::
1588::
1226:.
1222:.
1204:^
1183:.
1176:.
1163:^
1142:.
1102:^
1081:.
1047:^
1026:.
964:^
188:.
163:.
144:,
1527:/
1392:)
1388:(
1323:e
1316:t
1309:v
1241:.
1198:.
1157:.
1096:.
1041:.
903::
881::
841::
825::
804::
795::
786::
767:.
578:,
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
