505:
31:
409:
477:
350 hp (261 kW) at 2600 rpm, dry weight 546 lb (248 kg). Similar to the TSIOL-550-A but with the exhaust system and turbocharger bracket from the TSIOL-550-B. The engine is modified to accept the AiResearch TA81 turbocharger. Neither oil nor coolant radiators are provided with the
470:
but with a new cylinder design that uses liquid cooling. The coolant manifold is on top of the cylinder head, with a coolant pump fitted to the starter adapter, driven by the propeller shaft using sheaves, the oil cooler is mounted on the airframe, not the engine. A coolant tank and coolant lines are
398:
315 hp (235 kW) at 2500 rpm, dry weight 522 lb (237 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-E with new oil sump and capacity, decreased maximum continuous power, increased turbo boost pressure, decreased engine speed rating and
455:
but with a new cylinder design that uses liquid cooling. The coolant manifold is on top of the cylinder head, with a coolant pump fitted to the starter adapter, driven by the starter adapter shaft and the oil cooler is mounted on the airframe, not the engine. The engine has an
371:
350 hp (261 kW) at 2700 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-A except with a 12 quart sump, sonic venturii removed and the two stage fuel pump replaced by a single stage fuel
391:
310 hp (231 kW) at 2700 rpm, dry weight 554 lb (251 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-E with smaller surface area intercoolers, different oil sump capacity and power
1045:
384:
350 hp (261 kW) at 2700 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to TSIO-550-C with the oil sump and maximum continuous power rating of the
1182:
1075:
437:
315 hp (235 kW) at 2500 rpm, dry weight 537.3 lb (243.7 kg) plus two turbochargers of 28.2 lb (12.8 kg) each. Similar to the TSIO-550-K but with FADEC fuel injection and ignition
211:
series, with the stroke increased from 4.00 to 4.25 inches, increasing the displacement to 552 in³ (9.05 L). The engine family covers a power range from 280 hp (209 kW) to 360 hp (268 kW).
420:
350 hp (261 kW) at 2600 rpm, dry weight 558 lb (253 kg) plus two turbochargers of 35.2 lb (16.0 kg) each. Similar to the TSIOF-550-J except the exhaust system and low voltage
1002:
942:
291:
310 hp (231 kW) at 2700 rpm, dry weight 439.5 lb (199.4 kg). Similar to the IO-550-N but with the oil sump, oil suction tube and mount legs from the IO-550-B. Certified 1 March 2000.
261:
300 hp (224 kW) at 2700 rpm, dry weight 437.1 lb (198.3 kg). Similar to the IO-550-A,B & C, with a top-mounted induction system and 12-quart oil sump. Certified 23 June 1988.
352:
310 hp (231 kW) at 2700 rpm, dry weight 470.5 lb (213.4 kg). Similar to the IO-550-R with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
346:
310 hp (231 kW) at 2700 rpm, dry weight 460.0 lb (208.7 kg). Similar to the IO-550-P with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
340:
310 hp (231 kW) at 2700 rpm, dry weight 460.0 lb (208.7 kg). Similar to the IO-550-N with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
334:
300 hp (224 kW) at 2700 rpm, dry weight 455.0 lb (206.4 kg). Similar to the IO-550-L with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
328:
300 hp (224 kW) at 2700 rpm, dry weight 460.1 lb (208.7 kg). Similar to the IO-550-F with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
322:
300 hp (224 kW) at 2700 rpm, dry weight 462.8 lb (209.9 kg). Similar to the IO-550-E with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
316:
300 hp (224 kW) at 2700 rpm, dry weight 455.0 lb (206.4 kg). Similar to the IO-550-D with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
310:
300 hp (224 kW) at 2700 rpm, dry weight 453.2 lb (205.6 kg). Similar to the IO-550-C with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
304:
300 hp (224 kW) at 2700 rpm, dry weight 447.1 lb (202.8 kg). Similar to the IO-550-B with an
Aerosance FADEC fuel and ignition control system. Certified 4 February 2002.
1049:
1460:
1186:
1079:
949:
427:
350 hp (261 kW) at 2600 rpm, dry weight 558 lb (253 kg) plus two turbochargers of 35.2 lb (16.0 kg) each. Similar to the TSIO-550-E except for
279:
310 hp (231 kW) at 2700 rpm, dry weight 429.97 lb (195.03 kg). Similar to the IO-550-G with increased power rating. Certified 16 August 1996.
1009:
431:
fuel injection and ignition control, turbochargers, tapered cylinder barrel fins, oil sump and capacity, maximum continuous speed and manifold pressure rating.
285:
310 hp (231 kW) at 2700 rpm, dry weight 429 lb (195 kg). Similar to the IO-550-N with oil sump from the IO-550-L. Certified 1 March 2000.
1581:
1535:
1332:
1274:
1252:
378:
310 hp (231 kW) at 2600 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each.
365:
360 hp (268 kW) at 2600 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each.
1247:
1602:
1612:
1267:
1283:
1124:
1282:
1260:
1178:
1071:
1041:
998:
938:
255:
300 hp (224 kW) at 2700 rpm, dry weight 450.50 lb (204.34 kg). Certified 20 December 1989.
243:
300 hp (224 kW) at 2700 rpm, dry weight 433.20 lb (196.50 kg). Certified 13 October 1983.
237:
300 hp (224 kW) at 2700 rpm, dry weight 421.61 lb (191.24 kg). Certified 13 October 1983.
231:
300 hp (224 kW) at 2700 rpm, dry weight 430.72 lb (195.37 kg). Certified 13 October 1983.
192:
There is no O-550 engine, which would be a carburetor-equipped variant, hence the base model is the IO-550.
267:
280 hp (209 kW) at 2500 rpm, dry weight 428.97 lb (194.58 kg). Certified 17 March 1989.
216:
163:
74:
273:
300 hp (224 kW) at 2700 rpm, dry weight 438.5 lb (198.9 kg). Certified 23 June 1988.
249:
300 hp (224 kW) at 2700 rpm, dry weight 437.1 lb (198.3 kg). Certified 23 June 1988.
219:, 1 February 1965 amendment, 33-8, 2 May 1977. The first IO-550 model was certified on 13 October 1983.
604:
1397:
868:
569:
685:
215:
The engines were first developed in the early 1980s and first certified on a regulatory basis of
1607:
1545:
1499:
158:
six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed for use in
1294:
831:
466:
325 hp (242 kW) at 2700 rpm, dry weight 557 lb (253 kg). Similar to the
451:
350 hp (261 kW) at 2700 rpm, dry weight 402 lb (182 kg). Similar to the
726:
663:
1157:
8:
1563:
1407:
751:
1102:
1517:
1512:
1507:
1465:
1455:
1450:
526:
457:
122:
1232:
1540:
1480:
1475:
1470:
1445:
1440:
1435:
1430:
1425:
1420:
1415:
1392:
1387:
1382:
1377:
1372:
1367:
1362:
1357:
1352:
1347:
1342:
1337:
1327:
1322:
822:
697:
574:
492:
467:
452:
208:
142:
609:
521:
118:
1317:
1286:
856:
742:
199:
series which are also six-cylinder engines with similar power output and weight.
196:
114:
52:
1284:
Continental Motors, Teledyne
Continental, and Continental Aerospace Technologies
851:
779:
584:
531:
159:
1596:
1527:
813:
733:
495:
covert reconnaissance aircraft, incorporating 3:2 gear reduction to 2267 rpm.
166:. The first IO-550 was delivered in 1983 and the type remains in production.
155:
64:
1131:
680:
658:
646:
594:
564:
182:
471:
added to the installation. The engine has an AiResearch TS06 turbocharger.
641:
599:
559:
504:
98:
94:
1208:
760:
668:
636:
631:
626:
589:
579:
554:
548:
542:
536:
508:
110:
106:
102:
39:
1573:
621:
30:
1555:
1235:, Disciples of Flight, 2/21/15, Aircraft Engine Upgrade section.
1177:
1070:
1040:
997:
937:
49:
408:
1299:
788:
428:
174:
491:
A special non-certified geared engine developed for the
1183:"Supplemental Type Certificate, STC Number: SA09133SC"
1076:"TYPE CERTIFICATE DATA SHEET NO. E00004NY, Revision 1"
1122:
207:
The IO-550 family of engines was developed from the
403:
1046:"TYPE CERTIFICATE DATA SHEET NO. E4SO Revision 1"
1594:
38:Continental TSIO-550-C engine installation in a
177:equipped version of the same basic engine, the
1268:
1158:"Designations Of U.S. Military Aero Engines"
943:"Type Certificate Data No. E3SO Revision 10"
703:
1100:
1003:"Type Certificate Data No. E5SO Revision 6"
1275:
1261:
716:
202:
1248:Continental Specification Sheet IO-550-N
503:
407:
1149:
1064:
993:
991:
989:
987:
933:
931:
929:
927:
925:
923:
921:
919:
917:
915:
913:
911:
909:
907:
905:
903:
442:
1595:
1171:
1155:
1116:
1036:
1034:
1032:
1030:
985:
983:
981:
979:
977:
975:
973:
971:
969:
967:
901:
899:
897:
895:
893:
891:
889:
887:
885:
883:
356:
1256:
1125:"MANDATORY SERVICE BULLETIN MSB94-4G"
1123:TELEDYNE CONTINENTAL (October 2005).
195:This engine family competes with the
1094:
154:engine is a large family of 9 liter
1027:
964:
880:
13:
14:
1624:
1241:
1156:Parsch, Andreas (February 2008).
712:Type Certificate Data Sheet E3SO.
482:
29:
1226:
1179:Federal Aviation Administration
1072:Federal Aviation Administration
1042:Federal Aviation Administration
999:Federal Aviation Administration
939:Federal Aviation Administration
499:
404:Turbocharged & FADEC models
295:
16:American piston aircraft engine
1201:
1103:"Schweizer RU-38A Twin Condor"
1101:Stoll, Alex (September 2001).
800:
1:
1603:1980s aircraft piston engines
874:
769:
539:(STC SA09133SC, modification)
399:tapered cylinder barrel fins.
1613:Continental aircraft engines
809:300 hp (224 kW) at 2,700 rpm
189:is a liquid-cooled variant.
7:
840:
222:
164:Teledyne Continental Motors
75:Teledyne Continental Motors
10:
1629:
605:Washington T-411 Wolverine
1572:
1554:
1526:
1498:
1406:
1308:
1293:
765:430.72 lb dry (195.37 kg)
704:Specifications (IO-550-A)
37:
28:
23:
869:List of aircraft engines
570:Freedom Aviation Phoenix
511:equipped with a TSIO-550
1500:Aircraft Diesel engines
836:0.70 hp/lb (1.15 kW/kg)
818:0.54 hp/in³ (24.6 kW/L)
717:General characteristics
686:Viper Aircraft Viperfan
1311:horsepower designation
1295:Opposed piston engines
729:aircraft piston engine
725:6-cylinder air-cooled
512:
413:
203:Design and development
832:Power-to-weight ratio
507:
411:
1233:Cessna 210 Centurion
1181:(November 4, 1999).
1137:on November 16, 2009
727:horizontally opposed
664:Cobalt Co50 Valkyrie
443:Liquid-cooled models
357:Turbocharged models
1556:Inverted-V engines
1189:on January 5, 2018
1082:on January 5, 2018
1052:on January 5, 2018
1015:on January 5, 2018
846:Comparable engines
747:4.25 in (108.0 mm)
738:5.25 in (133.4 mm)
527:Beechcraft Bonanza
513:
460:TA81 turbocharger.
414:
152:Continental IO-550
123:Beechcraft Bonanza
90:Major applications
1590:
1589:
1494:
1493:
823:Compression ratio
698:RU-38 Twin Condor
575:Lancair Barracuda
493:RU-38 Twin Condor
148:
147:
143:Continental O-520
1620:
1306:
1305:
1287:aircraft engines
1277:
1270:
1263:
1254:
1253:
1236:
1230:
1224:
1223:
1221:
1219:
1205:
1199:
1198:
1196:
1194:
1185:. Archived from
1175:
1169:
1168:
1166:
1164:
1153:
1147:
1146:
1144:
1142:
1136:
1130:. Archived from
1129:
1120:
1114:
1113:
1111:
1109:
1098:
1092:
1091:
1089:
1087:
1078:. Archived from
1068:
1062:
1061:
1059:
1057:
1048:. Archived from
1038:
1025:
1024:
1022:
1020:
1014:
1008:. Archived from
1007:
995:
962:
961:
959:
957:
948:. Archived from
947:
935:
756:552 in³ (9.05 L)
610:Yakovlev Yak-112
522:Beechcraft Baron
185:version and the
173:is an Aerosance
139:
119:Beechcraft Baron
91:
61:
33:
21:
20:
1628:
1627:
1623:
1622:
1621:
1619:
1618:
1617:
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1592:
1591:
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1568:
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1522:
1513:CD-200 (TD-300)
1490:
1408:By displacement
1402:
1310:
1297:
1289:
1281:
1244:
1239:
1231:
1227:
1217:
1215:
1213:Summit Aviation
1207:
1206:
1202:
1192:
1190:
1176:
1172:
1162:
1160:
1154:
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1140:
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1127:
1121:
1117:
1107:
1105:
1099:
1095:
1085:
1083:
1074:(August 2007).
1069:
1065:
1055:
1053:
1044:(August 1997).
1039:
1028:
1018:
1016:
1012:
1005:
996:
965:
955:
953:
952:on June 8, 2011
945:
936:
881:
877:
857:Lycoming IO-580
843:
803:
794:Cooling system:
772:
719:
706:
642:Velocity TXL-RG
502:
485:
445:
406:
359:
298:
225:
205:
197:Lycoming IO-580
137:
121:
117:
115:Bellanca Viking
113:
109:
105:
101:
97:
89:
60:National origin
59:
53:aircraft engine
17:
12:
11:
5:
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1566:
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1528:Radial engines
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1515:
1510:
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1242:External links
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1115:
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1026:
1001:(March 2010).
963:
941:(March 2007).
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871:
860:
859:
854:
852:Lycoming O-540
842:
839:
838:
837:
828:
819:
814:Specific power
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780:fuel injection
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600:Velocity XL-RG
597:
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585:Lancair Legacy
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551:(modification)
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545:(modification)
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532:Bellanca 17-30
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160:light aircraft
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138:Developed from
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1608:Boxer engines
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867:
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864:
863:Related lists
858:
855:
853:
850:
849:
848:
847:
835:
833:
829:
826:
824:
820:
817:
815:
811:
808:
807:Power output:
805:
804:
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773:
764:
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533:
530:
528:
525:
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494:
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487:
486:
483:Geared models
476:
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157:
156:fuel injected
153:
144:
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136:
135:
132:1983-present
131:
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120:
116:
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108:
104:
100:
96:
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73:
71:Manufacturer
70:
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66:
65:United States
63:
58:
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45:
44:
41:
36:
32:
27:
22:
19:
1485:
1398:Tiara series
1228:
1218:February 10,
1216:. Retrieved
1212:
1203:
1193:September 9,
1191:. Retrieved
1187:the original
1173:
1161:. Retrieved
1151:
1139:. Retrieved
1132:the original
1118:
1106:. Retrieved
1096:
1084:. Retrieved
1080:the original
1066:
1056:December 28,
1054:. Retrieved
1050:the original
1017:. Retrieved
1010:the original
956:December 28,
954:. Retrieved
950:the original
862:
861:
845:
844:
830:
821:
812:
806:
793:
784:
776:Fuel system:
775:
759:
752:Displacement
750:
741:
732:
722:
711:
708:
707:
681:Extra EA-400
659:Diamond DA50
647:Cirrus SR22T
637:Mooney M20TN
595:Seawind 300C
565:Cirrus VK-30
509:Lancair IV-P
500:Applications
296:FADEC models
214:
206:
194:
191:
186:
183:turbocharged
178:
170:
168:
151:
149:
18:
801:Performance
560:Cirrus SR22
474:TSIOL-550-C
468:TSIO-520-UB
463:TSIOL-550-B
453:TSIO-520-NB
448:TSIOL-550-A
434:TSIOF-550-K
424:TSIOF-550-J
417:TSIOF-550-D
412:TSIOF-550-D
385:TSIO-550-B.
99:Cirrus SR22
95:Velocity XL
1597:Categories
1574:Turboprops
1309:By company
1086:January 3,
875:References
796:Air-cooled
785:Fuel type:
770:Components
761:Dry weight
669:KAI KC-100
632:Lancair IV
627:Cessna 400
590:Mooney M20
580:Lancair ES
555:Cessna 350
549:Cessna 210
543:Cessna 206
537:Cessna 182
458:AiResearch
395:TSIO-550-K
388:TSIO-550-G
381:TSIO-550-E
375:TSIO-550-C
368:TSIO-550-B
362:TSIO-550-A
181:is a dual
111:Mooney M20
107:Cessna 185
103:Cessna TTx
81:First run
40:Cessna 400
709:Data from
675:TSIOL-550
653:TSIOF-550
622:Adam A500
488:GIO-550-A
349:IOF-550-R
343:IOF-550-P
337:IOF-550-N
331:IOF-550-L
325:IOF-550-F
319:IOF-550-E
313:IOF-550-D
307:IOF-550-C
301:IOF-550-B
187:TSIOL-550
129:Produced
1300:Gasoline
1163:July 14,
1141:July 14,
1019:June 21,
841:See also
616:TSIO-550
438:control.
421:harness.
288:IO-550-R
282:IO-550-P
276:IO-550-N
270:IO-550-L
264:IO-550-G
258:IO-550-F
252:IO-550-E
246:IO-550-D
240:IO-550-C
234:IO-550-B
228:IO-550-A
223:Variants
179:TSIO-550
1564:XI-1430
1209:"IO550"
1108:June 4,
692:GIO-550
478:engine.
392:rating.
171:IOF-550
24:IO-550
1582:TP-500
1518:CD-300
1508:CD-155
1486:IO-550
1466:IO-370
1461:IO-368
1456:IO-360
1451:IO-346
787:100LL
743:Stroke
516:IO-550
217:FAR 33
209:IO-520
50:Piston
1546:R-975
1541:R-670
1536:R-544
1481:O-526
1476:O-520
1471:O-470
1446:O-300
1441:O-280
1436:O-240
1431:O-205
1426:O-200
1421:O-190
1416:O-170
1135:(PDF)
1128:(PDF)
1013:(PDF)
1006:(PDF)
946:(PDF)
827:8.5:1
789:avgas
723:Type:
429:FADEC
372:pump.
175:FADEC
84:1983
46:Type
1393:E225
1388:E185
1383:E165
1378:C145
1373:C140
1368:C125
1363:C115
1220:2022
1195:2014
1165:2009
1143:2009
1110:2008
1088:2009
1058:2008
1021:2010
958:2008
778:TCM
734:Bore
169:The
150:The
1358:C90
1353:C85
1348:C75
1343:A80
1338:A75
1333:A70
1328:A65
1323:A50
1318:A40
162:by
1599::
1211:.
1029:^
966:^
882:^
1302:)
1298:(
1276:e
1269:t
1262:v
1222:.
1197:.
1167:.
1145:.
1112:.
1090:.
1060:.
1023:.
960:.
834::
825::
816::
763::
754::
745::
736::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
