40:
265:
397:"4-cylinder, air-cooled, naturally aspirated, horizontally opposed, fuel-injected, spark ignition, four-stroke, direct drive. The engine incorporates a full authority digital electronic control (FADEC) system to control the ignition and fuel injection functions."
571:
233:
Dual ignition, 130 hp (97 kW) at 2800 rpm, dry weight 246 lb (112 kg) including starter and generator. Uses a Marvel-Schebler MA-3SPA IO 5067 carburetor. Certified 7 July 1971
736:
611:
578:
217:
system to control the ignition and fuel injection systems. The engine was not selected to power any production North
American-manufactured aircraft until the
714:
1064:
1074:
729:
39:
745:
708:
645:
255:
system controls the ignition and fuel injection systems, 125 hp (93 kW) at 2800 rpm, dry weight 255 lb (116 kg)
722:
607:
567:
245:
Dual ignition, 125 hp (93 kW) at 2800 rpm, dry weight 246 lb (112 kg), uses a TCM 639231A34 fuel injector
239:
Dual ignition, 125 hp (93 kW) at 2800 rpm, dry weight 246 lb (112 kg), uses a TCM 639231A27 fuel injector
144:
engine is a four-cylinder, horizontally opposed, air-cooled aircraft engine that was developed in the late 1960s for use in
661:
332:
78:
922:
310:
859:
529:
149:
210:
IO-240-A and -B were introduced in 1993. The A and B versions differ only in the type of fuel injector used.
1069:
1007:
961:
1043:
756:
509:
173:
172:. The O-240 delivers 30% more power than the O-200 while it weighs only 12% more. It may be mounted in
997:
794:
364:
320:
177:
98:
1025:
869:
419:
342:
188:
979:
974:
969:
947:
927:
917:
912:
161:
1002:
942:
937:
932:
907:
902:
892:
887:
882:
877:
854:
849:
844:
839:
834:
829:
824:
819:
814:
809:
804:
799:
789:
784:
704:
641:
500:
347:
191:
and was used to power the Reims-Cessna FRA150 Aerobat, a more powerful aerobatic model of the
165:
132:
299:
17:
779:
748:
524:
410:
304:
58:
203:
under license. Rolls-Royce acquired the rights to the O-240, but not the IO-240 in 1977.
160:
The 130 hp (97 kW) O-240 was a new engine design derived from the six-cylinder
315:
282:
207:
200:
184:
145:
106:
1058:
989:
491:
401:
352:
293:
337:
102:
264:
746:
Continental Motors, Teledyne
Continental, and Continental Aerospace Technologies
369:
269:
218:
110:
665:
444:
428:
287:
192:
164:
and introduced in 1971. It is generally similar in overall dimensions to the
1035:
213:
The IOF-240 is similar to the IO-240-B except that it employs an
Aerosance
1017:
168:, but with a higher 8.5:1 compression ratio, designed to run on 100/130
196:
55:
761:
466:
456:
263:
252:
214:
169:
718:
703:. Cambridge, England. Patrick Stephens Limited, 1989.
221:
entered production in 2006 powered by the IOF-240-B.
1034:
1016:
988:
960:
868:
770:
755:
612:"TYPE CERTIFICATE DATA SHEET NO. E11EU Revision 4"
572:"TYPE CERTIFICATE DATA SHEET NO. E7SO Revision 4"
638:Engines for Homebuilt Aircraft & Ultralights
272:is equipped with a Continental IOF-240-B engine.
152:The first O-240 was certified on 7 July 1971.
730:
655:
653:
449:One intake and one exhaust valve per cylinder
8:
183:The O-240 was produced under license in the
767:
737:
723:
715:
632:
630:
602:
600:
598:
546:
290:("R" meaning a Rolls-Royce-built O-240)
562:
560:
558:
556:
554:
552:
550:
29:
27:1970s American aircraft piston engine
7:
384:TYPE CERTIFICATE DATA SHEET NO. E7SO
701:World Encyclopedia of Aero Engines
25:
640:, pages 58-59. TAB Books, 1983.
38:
608:Federal Aviation Administration
568:Federal Aviation Administration
1:
1065:1970s aircraft piston engines
660:Shanaberger, Kenneth (2008).
1075:Continental aircraft engines
333:American Homebuilts John Doe
487:125 hp (93 kW) at 2,800 rpm
288:Reims Cessna FRA150 Aerobat
79:Teledyne Continental Motors
18:Teledyne Continental IO-240
1091:
376:Specifications (IOF-240-B)
311:St Croix Pietenpol Aerial
46:
37:
32:
530:List of aircraft engines
150:Continental Motors, Inc.
962:Aircraft Diesel engines
514:0.49 hp/lb (0.80 kW/kg)
496:0.52 hp/in (23.66 kW/L)
389:General characteristics
773:horsepower designation
757:Opposed piston engines
273:
156:Design and development
510:Power-to-weight ratio
267:
365:Issoire APM 40 Simba
321:Warner Revolution II
178:pusher configuration
99:Issoire APM 40 Simba
47:Continental IO-240B
685:Gunston 1989, p.42.
662:"Continental O-240"
406:4.438 in (112.7 mm)
343:Eagle Aircraft 150B
189:Rolls-Royce Limited
1018:Inverted-V engines
415:3.875 in (98.4 mm)
274:
94:Major applications
1052:
1051:
956:
955:
501:Compression ratio
348:Rans S-16 Shekari
283:AESL Airtourer T3
166:Continental O-200
162:Continental O-360
142:Continental O-240
138:
137:
133:Continental O-360
16:(Redirected from
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749:aircraft engines
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664:. Archived from
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583:
577:. Archived from
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300:Practavia Sprite
129:
122:1993-Today (IO)
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67:
42:
30:
21:
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1083:
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1080:
1079:
1055:
1054:
1053:
1048:
1030:
1012:
984:
975:CD-200 (TD-300)
952:
870:By displacement
864:
772:
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751:
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713:
699:Gunston, Bill.
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525:Lycoming IO-233
521:
481:
472:Cooling system:
440:
433:255 lb (116 kg)
424:240 in (3.93 L)
391:
378:
338:Diamond DA20-C1
305:Rollason Condor
262:
227:
195:constructed in
158:
127:
121:
109:
105:
103:Diamond DA20-C1
101:
93:
66:National origin
65:
28:
23:
22:
15:
12:
11:
5:
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990:Radial engines
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636:Christy, Joe:
626:
610:(March 2007).
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570:(March 2007).
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492:Specific power
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316:Tri-R KIS TR-1
313:
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296:(front engine)
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261:
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237:
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201:Reims Aviation
185:United Kingdom
157:
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146:light aircraft
136:
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128:Developed from
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118:
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107:AESL Airtourer
96:
90:
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70:United States
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53:
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26:
24:
14:
13:
10:
9:
6:
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2:
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1070:Boxer engines
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709:1-85260-163-9
706:
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668:on 2008-10-10
667:
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646:0-8306-2347-7
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584:on 2016-01-31
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485:Power output:
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353:Roko Aero NG4
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294:Rutan Voyager
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208:fuel-injected
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75:Manufacturer
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36:
31:
19:
897:
860:Tiara series
700:
693:Bibliography
681:
670:. Retrieved
666:the original
637:
618:. Retrieved
586:. Retrieved
579:the original
508:
499:
490:
484:
471:
462:
453:Fuel system:
452:
443:
427:
420:Displacement
418:
409:
400:
394:
383:
380:
379:
260:Applications
212:
205:
182:
159:
141:
139:
479:Performance
370:Liberty XL2
270:Liberty XL2
219:Liberty XL2
120:1971-Today,
111:Liberty XL2
59:aero-engine
1059:Categories
1036:Turboprops
771:By company
672:2008-12-18
620:2008-12-27
588:2008-12-18
536:References
474:Air-cooled
463:Fuel type:
455:Aerosance
445:Valvetrain
438:Components
429:Dry weight
251:Aerosance
193:Cessna 150
85:First run
381:Data from
359:IOF-240-B
248:IOF-240-B
117:Produced
762:Gasoline
519:See also
242:IO-240-B
236:IO-240-A
225:Variants
1026:XI-1430
230:O-240-A
174:tractor
1044:TP-500
980:CD-300
970:CD-155
948:IO-550
928:IO-370
923:IO-368
918:IO-360
913:IO-346
707:
644:
465:100LL
459:system
411:Stroke
327:IO-240
307:(D62C)
197:France
56:Piston
33:O-240
1008:R-975
1003:R-670
998:R-544
943:O-526
938:O-520
933:O-470
908:O-300
903:O-280
898:O-240
893:O-205
888:O-200
883:O-190
878:O-170
615:(PDF)
582:(PDF)
575:(PDF)
541:Notes
505:8.5:1
467:avgas
457:FADEC
395:Type:
277:O-240
253:FADEC
215:FADEC
170:avgas
88:1971
52:Type
855:E225
850:E185
845:E165
840:C145
835:C140
830:C125
825:C115
705:ISBN
642:ISBN
402:Bore
268:The
206:The
140:The
820:C90
815:C85
810:C75
805:A80
800:A75
795:A70
790:A65
785:A50
780:A40
199:by
187:by
176:or
148:by
1061::
652:^
629:^
597:^
549:^
180:.
764:)
760:(
738:e
731:t
724:v
675:.
623:.
591:.
512::
503::
494::
447::
431::
422::
413::
404::
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
