42:
559:
548:
1300:
183:
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.
468:, 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.
452:, 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.
516:
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
502:
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
481:
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
474:
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
435:
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
428:
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
421:
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
276:
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
255:
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
509:
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
495:
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
414:
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
393:
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
344:
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
337:
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,
303:
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
330:
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.
323:
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
182:
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
289:
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
537:
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
442:
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
523:
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
488:
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
316:
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
221:
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
530:
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
407:
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
400:
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
228:
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
241:
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,
372:
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,
351:
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,
269:
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,
358:
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,
365:
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,
262:
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,
379:
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,
248:
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,
1154:
1093:
1038:
1195:
1238:
211:
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.
195:
to indicate the specific configuration of the engine. There are also numerous engine suffixes, denoting different accessories such as different manufacturers' carburetors, or different
1147:
1086:
1031:
415:
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.
1188:
1227:
1515:
1581:
1332:
229:
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.
1646:
496:
dry weight of 465 lb (211 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on March 10, 1966.
17:
538:
weight of 493 lb (224 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on June 10, 1963.
1636:
1325:
617:
563:
475:
of 478 lb (217 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on November 21, 1962.
1285:
1615:
1400:
1304:
1223:
1184:
1143:
1082:
1027:
889:
1318:
612:
41:
1600:
436:
399 lb (181 kg) and fitted with a Marvel MA-4-5AA carburetor. Type certified on March 6, 1961.
524:(211 kg) and fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on January 11, 1968.
732:
955:
1641:
1489:
1547:
602:
747:
727:
119:
8:
812:
394:
MA-4-5AA carburetor. Type certified on October 11, 1954. Was re-designated as VO-435-A1A.
159:
1596:
647:
586:
576:
111:
99:
672:
1281:
911:
657:
607:
152:
1525:
1520:
1497:
1479:
1474:
1432:
1427:
1341:
627:
401:
MA-4-5AA carburetor. Type certified on October 29, 1954. Re-designated from VO-435.
290:
with serial numbers L00849-11 through L-1117-11 are eligible for this modification.
212:
196:
167:
79:
1552:
1447:
1442:
1437:
1407:
1370:
1344:
803:
622:
597:
558:
510:
fitted with a Marvel-Schebler MA-6AA carburetor. Type certified on March 7, 1967.
59:
1469:
1422:
1417:
1395:
1390:
1385:
1380:
1375:
1365:
1360:
943:
931:
854:
707:
652:
171:
139:
411:
VO-435-A1C (military designations O-435-23, O-435-23A O-435-23B and O-435-23C)
1630:
1562:
1457:
794:
717:
697:
692:
687:
677:
642:
107:
1310:
1557:
662:
547:
465:
449:
422:
Marvel MA-4-5 or MA-4-5AA carburetor. Type certified on September 27, 1956.
482:
with a Marvel-Schebler MA-6AA carburetor. Type certified on June 20, 1966.
1573:
1352:
737:
722:
712:
702:
682:
667:
637:
632:
156:
517:
a Marvel-Schebler MA-6AA carburetor. Type certified on January 22, 1968.
1539:
849:
833:
760:
581:
503:
Marvel-Schebler MA-6AA carburetor. Type certified on February 23, 1967.
163:
115:
1535:
310:
Type certified on October 19, 1949 and cancelled on February 8, 1955.
235:
Type certified on January 5, 1951 and cancelled on February 8, 1955.
1507:
1461:
552:
858:
742:
592:
103:
443:
Marvel MA-4-5AA carburetor. Type certified on December 15, 1965.
1299:
1222:
1142:
1081:
1026:
304:
certified on August 30, 1944 and cancelled on November 2, 1950.
52:
1280:
Hammersmith, London: HarperCollinsPublishers (1994 reprint).
170:. The engine is a six-cylinder version of the four-cylinder
1183:
55:
790:
Six-cylinder horizontally-opposed gasoline piston engine
861:
actuated), one inlet and one exhaust valve per cylinder
489:
MA-6AA carburetor. Type certified on November 21, 1962.
191:
All engines have an additional prefix preceding the
1087:"Type Certificate Data Sheet No. E-279 Revision 10"
1032:"Type Certificate Data Sheet No. E-228 Revision 17"
907:
212 hp (158 kW) at 3,000 rpm at sea level
1148:"Type Certificate Data Sheet No. 1E13 Revision 8"
1628:
531:carburetor. Type certified on November 25, 1968.
222:carburetor. Type certified on February 11, 1942.
324:February 8, 1955 and reinstated July 15, 1955.
1340:
1326:
885:Air-cooled by fan (helicopter installations)
471:TVO-435-B1A (military designation O-435-25A)
408:carburetor. Type certified on June 10, 1955.
767:
1616:AlliedSignal Aerospace/Honeywell Aerospace
1333:
1319:
781:
418:VO-435-A1D (military designation O-435-6A)
397:VO-435-A1A (military designation O-435-21)
404:VO-435-A1B (military designation O-435-6)
313:GO-435-C2 (military designation O-435-17)
177:
1278:Jane's All the World's Aircraft 1945-46.
1022:
1020:
1018:
1016:
1014:
1012:
1010:
1008:
1006:
1004:
1002:
1000:
998:
996:
557:
546:
259:O-435-C2 (military designation O-435-13)
252:O-435-C1 (military designation O-435-11)
1189:"Type Certificate Data Sheet No. 5E-12"
1179:
1177:
1175:
1138:
1136:
1134:
1077:
1075:
1073:
1071:
1069:
1067:
1065:
1063:
1061:
1059:
994:
992:
990:
988:
986:
984:
982:
980:
978:
976:
273:O-435-K1 (military designation O-435-4)
14:
1629:
1201:from the original on September 2, 2022
1132:
1130:
1128:
1126:
1124:
1122:
1120:
1118:
1116:
1114:
1099:from the original on December 20, 2016
1044:from the original on December 16, 2016
245:O-435-C (military designation O-435-1)
238:O-435-B (military designation O-435-5)
1314:
1218:
1216:
1172:
1056:
973:
1244:from the original on April 19, 2021
1160:from the original on April 11, 2021
1111:
331:Type certified on October 24, 1957.
24:
1228:"Helicopter Specification No. 1H1"
1213:
618:de Havilland Canada Super Chipmunk
551:A Lycoming TVO-435 installed in a
25:
1658:
1292:
562:Lycoming O-435 on display at the
456:
1298:
384:
294:
40:
1269:
1224:Federal Aviation Administration
1185:Federal Aviation Administration
1144:Federal Aviation Administration
1083:Federal Aviation Administration
1028:Federal Aviation Administration
542:
202:
1256:
898:
429:certified on October 15, 1959.
27:American 1940s aircraft engine
13:
1:
1647:1940s aircraft piston engines
961:
842:
277:certified on March 30, 1951.
129:1942–1975 out of production
7:
920:
186:
10:
1663:
867:Marvel-Schebler carburetor
613:D'Apuzzo Senior Aero Sport
1637:Lycoming aircraft engines
1608:
1590:
1571:
1534:
1506:
1488:
1456:
1351:
733:St Croix Sopwith Triplane
39:
34:
966:
956:List of aircraft engines
768:Specifications (O-435-D)
1572:Aero-derivative marine
1490:Aircraft diesel engines
782:General characteristics
1353:Opposed piston engines
1262:Bridgman 1994, p. 78d.
1226:(September 26, 1950).
566:
555:
283:Military engine model.
178:Design and development
603:Bellanca Cruisemaster
561:
550:
215:on February 11, 1942.
1307:at Wikimedia Commons
1146:(November 4, 2010).
1085:(November 4, 2010).
748:Vertical Hummingbird
728:Stinson L-5 Sentinel
157:horizontally opposed
120:Stinson L-5 Sentinel
18:Avco Lycoming O-435A
1597:Pratt & Whitney
1276:Bridgman, Leonard.
926:Related development
873:100 octane gasoline
799:4.875 in (123.8 mm)
160:fixed-wing aircraft
151:is an American six-
938:Comparable engines
879:Pressure pump type
829:43.5 in (1,105 mm)
808:3.875 in (98.4 mm)
648:Hiller OH-23 Raven
587:Beechcraft Bonanza
577:Aero Commander 500
567:
564:Museum of Aviation
556:
112:Hiller OH-23 Raven
100:Beechcraft Bonanza
95:Major applications
1624:
1623:
1591:Joint development
1404:
1303:Media related to
1030:(June 23, 2010).
912:Compression ratio
838:433 lb (196.6 kg)
817:434 cu in (7.1 L)
658:Jeffair Barracuda
608:Boisavia Mercurey
317:October 19, 1949.
145:
144:
16:(Redirected from
1654:
1595:Avco (Lycoming)/
1398:
1345:aircraft engines
1335:
1328:
1321:
1312:
1311:
1302:
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1098:
1091:
1079:
1054:
1053:
1051:
1049:
1043:
1036:
1024:
823:33.5 in (851 mm)
628:Fleetwings PQ-12
168:Lycoming Engines
136:
96:
80:Lycoming Engines
68:
44:
32:
31:
21:
1662:
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1204:
1202:
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1191:
1182:
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1112:
1102:
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1096:
1089:
1080:
1057:
1047:
1045:
1041:
1034:
1025:
974:
969:
964:
923:
901:
883:Cooling system:
845:
784:
770:
752:
673:Karhumäki Karhu
623:Fleetwings BQ-2
598:Bell H-13 Sioux
545:
459:
387:
297:
205:
189:
180:
166:engine made by
134:
118:
114:
110:
106:
102:
94:
67:National origin
66:
60:aircraft engine
28:
23:
22:
15:
12:
11:
5:
1660:
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1500:
1494:
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1458:Radial engines
1454:
1453:
1451:
1450:
1445:
1440:
1435:
1430:
1425:
1420:
1415:
1410:
1405:
1401:O-360 variants
1393:
1388:
1383:
1378:
1373:
1368:
1363:
1357:
1355:
1349:
1348:
1338:
1337:
1330:
1323:
1315:
1309:
1308:
1305:Lycoming O-435
1294:
1293:External links
1291:
1289:
1288:
1273:
1271:
1268:
1265:
1264:
1255:
1212:
1171:
1110:
1055:
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965:
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960:
959:
958:
947:
946:
944:Franklin O-335
935:
934:
932:Lycoming O-290
922:
919:
918:
917:
908:
900:
897:
896:
895:
890:Reduction gear
886:
880:
874:
868:
862:
855:Overhead valve
844:
841:
840:
839:
830:
824:
818:
809:
800:
791:
783:
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769:
766:
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757:
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750:
745:
740:
735:
730:
725:
720:
715:
710:
708:Ra-Son Warrior
705:
700:
695:
690:
685:
680:
675:
670:
665:
660:
655:
653:Interstate TDR
650:
645:
640:
635:
630:
625:
620:
615:
610:
605:
600:
595:
590:
584:
579:
573:
572:
571:
544:
541:
540:
539:
535:
532:
528:
525:
521:
518:
514:
511:
507:
504:
500:
497:
493:
490:
486:
483:
479:
476:
472:
469:
463:
458:
457:TVO-435 models
455:
454:
453:
447:
444:
440:
437:
433:
430:
426:
423:
419:
416:
412:
409:
405:
402:
398:
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296:
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260:
257:
253:
250:
246:
243:
239:
236:
233:
230:
226:
223:
219:
216:
213:Type certified
209:
204:
201:
188:
185:
179:
176:
172:Lycoming O-290
149:Lycoming O-435
143:
142:
140:Lycoming O-290
137:
135:Developed from
131:
130:
127:
123:
122:
97:
91:
90:
87:
83:
82:
77:
73:
72:
71:United States
69:
63:
62:
50:
46:
45:
37:
36:
26:
9:
6:
4:
3:
2:
1659:
1648:
1645:
1643:
1642:Boxer engines
1640:
1638:
1635:
1634:
1632:
1617:
1614:
1613:
1611:
1607:
1602:
1598:
1593:
1589:
1583:
1580:
1579:
1577:
1575:
1570:
1564:
1561:
1559:
1556:
1554:
1553:LTS101/LTP101
1551:
1549:
1546:
1545:
1543:
1541:
1537:
1533:
1527:
1524:
1522:
1521:ALF 502/YF102
1519:
1517:
1514:
1513:
1511:
1509:
1505:
1499:
1496:
1495:
1493:
1491:
1487:
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1471:
1468:
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1411:
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1402:
1397:
1394:
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1379:
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1374:
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1367:
1364:
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1297:
1296:
1287:
1283:
1279:
1275:
1274:
1259:
1240:
1236:
1229:
1225:
1219:
1217:
1197:
1190:
1186:
1180:
1178:
1176:
1156:
1149:
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1139:
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1129:
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1125:
1123:
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987:
985:
983:
981:
979:
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972:
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954:
953:
952:
951:
950:Related lists
945:
942:
941:
940:
939:
933:
930:
929:
928:
927:
915:
913:
909:
906:
905:Power output:
903:
902:
893:
891:
887:
884:
881:
878:
875:
872:
869:
866:
863:
860:
856:
853:
851:
847:
846:
837:
835:
831:
828:
825:
822:
819:
816:
814:
810:
807:
805:
801:
798:
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789:
786:
785:
779:
777:
774:
762:
759:
758:
754:
753:
749:
746:
744:
741:
739:
736:
734:
731:
729:
726:
724:
721:
719:
718:Saab 91 Safir
716:
714:
711:
709:
706:
704:
701:
699:
698:Piaggio P.149
696:
694:
693:Piaggio P.148
691:
689:
688:Miles Aerovan
686:
684:
681:
679:
678:Kawasaki KH-4
676:
674:
671:
669:
666:
664:
661:
659:
656:
654:
651:
649:
646:
644:
643:Helio Courier
641:
639:
636:
634:
631:
629:
626:
624:
621:
619:
616:
614:
611:
609:
606:
604:
601:
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588:
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583:
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569:
568:
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560:
554:
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536:
533:
529:
526:
522:
519:
515:
512:
508:
505:
501:
498:
494:
491:
487:
484:
480:
477:
473:
470:
467:
464:
461:
460:
451:
448:
445:
441:
438:
434:
431:
427:
424:
420:
417:
413:
410:
406:
403:
399:
396:
392:
389:
388:
385:VO-435 models
378:
375:
371:
368:
364:
361:
357:
354:
350:
347:
343:
340:
336:
333:
329:
326:
322:
319:
315:
312:
309:
306:
302:
299:
298:
295:GO-435 models
288:
285:
282:
279:
275:
272:
268:
265:
261:
258:
254:
251:
247:
244:
240:
237:
234:
231:
227:
224:
220:
217:
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210:
207:
206:
200:
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184:
175:
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150:
141:
138:
133:
132:
128:
125:
124:
121:
117:
113:
109:
108:Helio Courier
105:
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98:
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84:
81:
78:
76:Manufacturer
75:
74:
70:
65:
64:
61:
57:
54:
51:
48:
47:
43:
38:
33:
30:
19:
1603:(Turboshaft)
1574:gas turbines
1412:
1286:000 470831-8
1277:
1270:Bibliography
1258:
1248:September 2,
1246:. Retrieved
1234:
1205:September 2,
1203:. Retrieved
1164:September 2,
1162:. Retrieved
1103:September 2,
1101:. Retrieved
1048:September 2,
1046:. Retrieved
949:
948:
937:
936:
925:
924:
910:
904:
894:Direct-drive
888:
882:
876:
870:
865:Fuel system:
864:
848:
832:
826:
820:
813:Displacement
811:
802:
793:
787:
775:
772:
771:
663:Kaman K-190A
543:Applications
466:Turbocharged
450:Turbocharged
203:O-435 models
192:
190:
181:
148:
146:
29:
1540:Turboshafts
899:Performance
877:Oil system:
738:UTVA Aero 3
723:Stinson 108
713:Ryan Navion
703:Pilatus P-4
683:LIBIS KB-11
668:Kaman K-225
638:Fokker S-11
633:Fokker F.25
527:TVO-435-G1B
520:TVO-435-G1A
513:TVO-435-F1A
506:TVO-435-E1A
499:TVO-435-D1B
492:TVO-435-D1A
485:TVO-435-C1A
478:TVO-435-B1B
462:TVO-435-A1A
446:TVO-435-A1A
348:GO-435-C2B2
341:GO-435-C2B1
327:GO-435-C2A2
1631:Categories
1536:Turboprops
962:References
871:Fuel type:
850:Valvetrain
843:Components
834:Dry weight
761:M22 Locust
582:AISA I-115
534:TVO-435-25
439:VO-435-B1A
432:VO-435-A1F
425:VO-435-A1E
369:GO-435-C2E
362:GO-435-C2D
355:GO-435-C2C
334:GO-435-C2B
320:GO-435-C2A
286:O-435-2-M1
164:helicopter
116:M22 Locust
86:First run
1508:Turbofans
1462:H engines
773:Data from
376:GO-435-D1
307:GO-435-A2
126:Produced
1609:See also
1601:T800-APW
1342:Lycoming
1239:Archived
1196:Archived
1155:Archived
1094:Archived
1039:Archived
921:See also
570:Aircraft
553:Bell 47G
345:8, 1955.
256:2, 1948.
232:O-435-A3
225:O-435-A2
197:magnetos
187:Variants
153:cylinder
1548:AGT1500
1498:DEL-120
1480:XH-2470
1475:XR-7755
1433:GSO-580
1428:TIO-541
1235:faa.gov
859:pushrod
827:Height:
743:UTVA 56
593:Bell 47
280:O-435-2
266:O-435-K
218:O-435-A
104:Bell 47
1526:LF 507
1448:O-1230
1443:IO-720
1438:IO-580
1408:IO-390
1371:IO-233
1284:
857:(OHV,
821:Width:
804:Stroke
776:Jane's
763:- tank
390:VO-435
300:GO-435
53:Piston
35:O-435
1582:TF-40
1470:R-680
1423:O-540
1418:O-480
1413:O-435
1396:O-360
1391:O-340
1386:O-320
1381:O-290
1376:O-235
1366:O-233
1361:O-145
1242:(PDF)
1231:(PDF)
1199:(PDF)
1192:(PDF)
1158:(PDF)
1151:(PDF)
1097:(PDF)
1090:(PDF)
1042:(PDF)
1035:(PDF)
967:Notes
916:7.5:1
788:Type:
755:Other
380:1953.
373:1956.
366:1956.
359:1956.
352:1956.
338:1952.
270:1951.
263:1948.
249:1943.
242:1950.
208:O-435
89:1939
49:Type
1516:PLF1
1460:and
1282:ISBN
1250:2022
1207:2022
1166:2022
1105:2022
1050:2022
795:Bore
162:and
147:The
58:and
56:tank
1563:T55
1558:T53
193:435
1633::
1599::
1237:.
1233:.
1215:^
1194:.
1187:.
1174:^
1153:.
1113:^
1092:.
1058:^
1037:.
975:^
199:.
174:.
155:,
1538:/
1403:)
1399:(
1334:e
1327:t
1320:v
1252:.
1209:.
1168:.
1107:.
1052:.
914::
892::
852::
836::
815::
806::
797::
778:.
589:,
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
