516:
42:
420:
488:
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
481:
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
409:
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
466:
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
382:
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
402:
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
1056:
395:
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
1193:
1086:
448:
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
222:
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).
431:
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
1013:
953:
302:
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.
272:
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.
363:
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.
357:
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.
351:
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.
345:
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.
339:
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.
333:
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.
327:
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.
321:
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.
315:
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.
1060:
1471:
1197:
1090:
960:
438:
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
290:
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.
1020:
442:
fuel injection and ignition control, turbochargers, tapered cylinder barrel fins, oil sump and capacity, maximum continuous speed and manifold pressure rating.
296:
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.
1592:
1546:
1343:
1285:
1263:
389:
310 hp (231 kW) at 2600 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each.
376:
360 hp (268 kW) at 2600 rpm, dry weight 442 lb (200 kg) plus two turbochargers of 28.2 lb (12.8 kg) each.
1258:
1613:
1623:
1278:
17:
1294:
1135:
1293:
1271:
1189:
1082:
1052:
1009:
949:
266:
300 hp (224 kW) at 2700 rpm, dry weight 450.50 lb (204.34 kg). Certified 20 December 1989.
254:
300 hp (224 kW) at 2700 rpm, dry weight 433.20 lb (196.50 kg). Certified 13 October 1983.
248:
300 hp (224 kW) at 2700 rpm, dry weight 421.61 lb (191.24 kg). Certified 13 October 1983.
242:
300 hp (224 kW) at 2700 rpm, dry weight 430.72 lb (195.37 kg). Certified 13 October 1983.
203:
There is no O-550 engine, which would be a carburetor-equipped variant, hence the base model is the IO-550.
278:
280 hp (209 kW) at 2500 rpm, dry weight 428.97 lb (194.58 kg). Certified 17 March 1989.
227:
174:
85:
284:
300 hp (224 kW) at 2700 rpm, dry weight 438.5 lb (198.9 kg). Certified 23 June 1988.
260:
300 hp (224 kW) at 2700 rpm, dry weight 437.1 lb (198.3 kg). Certified 23 June 1988.
230:, 1 February 1965 amendment, 33-8, 2 May 1977. The first IO-550 model was certified on 13 October 1983.
615:
1408:
879:
580:
696:
226:
The engines were first developed in the early 1980s and first certified on a regulatory basis of
1618:
1556:
1510:
169:
six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed for use in
1305:
842:
477:
325 hp (242 kW) at 2700 rpm, dry weight 557 lb (253 kg). Similar to the
462:
350 hp (261 kW) at 2700 rpm, dry weight 402 lb (182 kg). Similar to the
737:
674:
1168:
8:
1574:
1418:
762:
1113:
1528:
1523:
1518:
1476:
1466:
1461:
537:
468:
133:
1243:
1551:
1491:
1486:
1481:
1456:
1451:
1446:
1441:
1436:
1431:
1426:
1403:
1398:
1393:
1388:
1383:
1378:
1373:
1368:
1363:
1358:
1353:
1348:
1338:
1333:
833:
708:
585:
503:
478:
463:
219:
153:
620:
532:
129:
1328:
1297:
867:
753:
210:
series which are also six-cylinder engines with similar power output and weight.
207:
125:
63:
1295:
Continental Motors, Teledyne
Continental, and Continental Aerospace Technologies
862:
790:
595:
542:
170:
1607:
1538:
824:
744:
506:
covert reconnaissance aircraft, incorporating 3:2 gear reduction to 2267 rpm.
177:. The first IO-550 was delivered in 1983 and the type remains in production.
166:
75:
1142:
691:
669:
657:
605:
575:
193:
482:
added to the installation. The engine has an AiResearch TS06 turbocharger.
652:
610:
570:
515:
109:
105:
1219:
771:
679:
647:
642:
637:
600:
590:
565:
559:
553:
547:
519:
121:
117:
113:
50:
1584:
632:
41:
1566:
1246:, Disciples of Flight, 2/21/15, Aircraft Engine Upgrade section.
1188:
1081:
1051:
1008:
948:
60:
419:
1310:
799:
439:
185:
502:
A special non-certified geared engine developed for the
1194:"Supplemental Type Certificate, STC Number: SA09133SC"
1087:"TYPE CERTIFICATE DATA SHEET NO. E00004NY, Revision 1"
1133:
218:
The IO-550 family of engines was developed from the
414:
1057:"TYPE CERTIFICATE DATA SHEET NO. E4SO Revision 1"
1605:
49:Continental TSIO-550-C engine installation in a
188:equipped version of the same basic engine, the
1279:
1169:"Designations Of U.S. Military Aero Engines"
954:"Type Certificate Data No. E3SO Revision 10"
714:
1111:
1014:"Type Certificate Data No. E5SO Revision 6"
1286:
1272:
727:
213:
1259:Continental Specification Sheet IO-550-N
514:
418:
1160:
1075:
1004:
1002:
1000:
998:
944:
942:
940:
938:
936:
934:
932:
930:
928:
926:
924:
922:
920:
918:
916:
914:
453:
14:
1606:
1182:
1166:
1127:
1047:
1045:
1043:
1041:
996:
994:
992:
990:
988:
986:
984:
982:
980:
978:
912:
910:
908:
906:
904:
902:
900:
898:
896:
894:
367:
1267:
1136:"MANDATORY SERVICE BULLETIN MSB94-4G"
1134:TELEDYNE CONTINENTAL (October 2005).
206:This engine family competes with the
1105:
165:engine is a large family of 9 liter
1038:
975:
891:
24:
25:
1635:
1252:
1167:Parsch, Andreas (February 2008).
723:Type Certificate Data Sheet E3SO.
493:
40:
1237:
1190:Federal Aviation Administration
1083:Federal Aviation Administration
1053:Federal Aviation Administration
1010:Federal Aviation Administration
950:Federal Aviation Administration
510:
415:Turbocharged & FADEC models
306:
27:American piston aircraft engine
1212:
1114:"Schweizer RU-38A Twin Condor"
1112:Stoll, Alex (September 2001).
811:
13:
1:
1614:1980s aircraft piston engines
885:
780:
550:(STC SA09133SC, modification)
410:tapered cylinder barrel fins.
1624:Continental aircraft engines
820:300 hp (224 kW) at 2,700 rpm
200:is a liquid-cooled variant.
7:
851:
233:
175:Teledyne Continental Motors
86:Teledyne Continental Motors
10:
1640:
616:Washington T-411 Wolverine
1583:
1565:
1537:
1509:
1417:
1319:
1304:
776:430.72 lb dry (195.37 kg)
715:Specifications (IO-550-A)
48:
39:
34:
880:List of aircraft engines
581:Freedom Aviation Phoenix
522:equipped with a TSIO-550
1511:Aircraft Diesel engines
847:0.70 hp/lb (1.15 kW/kg)
829:0.54 hp/in³ (24.6 kW/L)
728:General characteristics
697:Viper Aircraft Viperfan
1322:horsepower designation
1306:Opposed piston engines
740:aircraft piston engine
736:6-cylinder air-cooled
523:
424:
214:Design and development
843:Power-to-weight ratio
518:
422:
1244:Cessna 210 Centurion
1192:(November 4, 1999).
1148:on November 16, 2009
738:horizontally opposed
675:Cobalt Co50 Valkyrie
454:Liquid-cooled models
368:Turbocharged models
18:Continental Voyager
1567:Inverted-V engines
1200:on January 5, 2018
1093:on January 5, 2018
1063:on January 5, 2018
1026:on January 5, 2018
857:Comparable engines
758:4.25 in (108.0 mm)
749:5.25 in (133.4 mm)
538:Beechcraft Bonanza
524:
471:TA81 turbocharger.
425:
163:Continental IO-550
134:Beechcraft Bonanza
101:Major applications
1601:
1600:
1505:
1504:
834:Compression ratio
709:RU-38 Twin Condor
586:Lancair Barracuda
504:RU-38 Twin Condor
159:
158:
154:Continental O-520
16:(Redirected from
1631:
1317:
1316:
1298:aircraft engines
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1196:. Archived from
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1153:
1147:
1141:. Archived from
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1120:
1109:
1103:
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1100:
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1089:. Archived from
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1059:. Archived from
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1031:
1025:
1019:. Archived from
1018:
1006:
973:
972:
970:
968:
959:. Archived from
958:
946:
767:552 in³ (9.05 L)
621:Yakovlev Yak-112
533:Beechcraft Baron
196:version and the
184:is an Aerosance
150:
130:Beechcraft Baron
102:
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44:
32:
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1524:CD-200 (TD-300)
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1419:By displacement
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1224:Summit Aviation
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1094:
1085:(August 2007).
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1066:
1064:
1055:(August 1997).
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1027:
1023:
1016:
1007:
976:
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964:
963:on June 8, 2011
956:
947:
892:
888:
868:Lycoming IO-580
854:
814:
805:Cooling system:
783:
730:
717:
653:Velocity TXL-RG
513:
496:
456:
417:
370:
309:
236:
216:
208:Lycoming IO-580
148:
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126:Bellanca Viking
124:
120:
116:
112:
108:
100:
71:National origin
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64:aircraft engine
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1539:Radial engines
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1012:(March 2010).
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863:Lycoming O-540
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874:Related lists
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818:Power output:
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584:
582:
579:
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569:
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544:
541:
539:
536:
534:
531:
530:
526:
525:
521:
517:
505:
501:
498:
497:
494:Geared models
487:
484:
480:
476:
473:
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461:
458:
457:
447:
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441:
437:
434:
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187:
183:
178:
176:
172:
168:
167:fuel injected
164:
155:
152:
147:
146:
143:1983-present
142:
139:
138:
135:
131:
127:
123:
119:
115:
111:
107:
104:
99:
98:
94:
91:
90:
87:
84:
82:Manufacturer
81:
80:
77:
76:United States
74:
69:
68:
65:
62:
59:
56:
55:
52:
47:
43:
38:
33:
30:
19:
1496:
1409:Tiara series
1239:
1229:February 10,
1227:. Retrieved
1223:
1214:
1204:September 9,
1202:. Retrieved
1198:the original
1184:
1172:. Retrieved
1162:
1150:. Retrieved
1143:the original
1129:
1117:. Retrieved
1107:
1095:. Retrieved
1091:the original
1077:
1067:December 28,
1065:. Retrieved
1061:the original
1028:. Retrieved
1021:the original
967:December 28,
965:. Retrieved
961:the original
873:
872:
856:
855:
841:
832:
823:
817:
804:
795:
787:Fuel system:
786:
770:
763:Displacement
761:
752:
743:
733:
722:
719:
718:
692:Extra EA-400
670:Diamond DA50
658:Cirrus SR22T
648:Mooney M20TN
606:Seawind 300C
576:Cirrus VK-30
520:Lancair IV-P
511:Applications
307:FADEC models
225:
217:
205:
202:
197:
194:turbocharged
189:
181:
179:
162:
160:
29:
812:Performance
571:Cirrus SR22
485:TSIOL-550-C
479:TSIO-520-UB
474:TSIOL-550-B
464:TSIO-520-NB
459:TSIOL-550-A
445:TSIOF-550-K
435:TSIOF-550-J
428:TSIOF-550-D
423:TSIOF-550-D
396:TSIO-550-B.
110:Cirrus SR22
106:Velocity XL
1608:Categories
1585:Turboprops
1320:By company
1097:January 3,
886:References
807:Air-cooled
796:Fuel type:
781:Components
772:Dry weight
680:KAI KC-100
643:Lancair IV
638:Cessna 400
601:Mooney M20
591:Lancair ES
566:Cessna 350
560:Cessna 210
554:Cessna 206
548:Cessna 182
469:AiResearch
406:TSIO-550-K
399:TSIO-550-G
392:TSIO-550-E
386:TSIO-550-C
379:TSIO-550-B
373:TSIO-550-A
192:is a dual
122:Mooney M20
118:Cessna 185
114:Cessna TTx
92:First run
51:Cessna 400
720:Data from
686:TSIOL-550
664:TSIOF-550
633:Adam A500
499:GIO-550-A
360:IOF-550-R
354:IOF-550-P
348:IOF-550-N
342:IOF-550-L
336:IOF-550-F
330:IOF-550-E
324:IOF-550-D
318:IOF-550-C
312:IOF-550-B
198:TSIOL-550
140:Produced
1311:Gasoline
1174:July 14,
1152:July 14,
1030:June 21,
852:See also
627:TSIO-550
449:control.
432:harness.
299:IO-550-R
293:IO-550-P
287:IO-550-N
281:IO-550-L
275:IO-550-G
269:IO-550-F
263:IO-550-E
257:IO-550-D
251:IO-550-C
245:IO-550-B
239:IO-550-A
234:Variants
190:TSIO-550
1575:XI-1430
1220:"IO550"
1119:June 4,
703:GIO-550
489:engine.
403:rating.
182:IOF-550
35:IO-550
1593:TP-500
1529:CD-300
1519:CD-155
1497:IO-550
1477:IO-370
1472:IO-368
1467:IO-360
1462:IO-346
798:100LL
754:Stroke
527:IO-550
228:FAR 33
220:IO-520
61:Piston
1557:R-975
1552:R-670
1547:R-544
1492:O-526
1487:O-520
1482:O-470
1457:O-300
1452:O-280
1447:O-240
1442:O-205
1437:O-200
1432:O-190
1427:O-170
1146:(PDF)
1139:(PDF)
1024:(PDF)
1017:(PDF)
957:(PDF)
838:8.5:1
800:avgas
734:Type:
440:FADEC
383:pump.
186:FADEC
95:1983
57:Type
1404:E225
1399:E185
1394:E165
1389:C145
1384:C140
1379:C125
1374:C115
1231:2022
1206:2014
1176:2009
1154:2009
1121:2008
1099:2009
1069:2008
1032:2010
969:2008
789:TCM
745:Bore
180:The
161:The
1369:C90
1364:C85
1359:C75
1354:A80
1349:A75
1344:A70
1339:A65
1334:A50
1329:A40
173:by
1610::
1222:.
1040:^
977:^
893:^
1313:)
1309:(
1287:e
1280:t
1273:v
1233:.
1208:.
1178:.
1156:.
1123:.
1101:.
1071:.
1034:.
971:.
845::
836::
827::
774::
765::
756::
747::
20:)
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