Continental IO-520

{{short description|Family of flat-six piston aircraft engines}}

{{Refimprove|date=November 2012}}

{{Infobox Aircraft Begin

|name=O-520

|image=Continental IO-520 2.jpg

|caption=Preserved IO-520

}}{{Infobox Aircraft Engine

|type=Piston aircraft engine

|national origin=United States

|manufacturer= Teledyne Continental Motors

|first run= 1963

|produced= 1964-present

|major applications= Beechcraft Bonanza
Beechcraft Baron
Cessna 206
Cessna 210
Cessna 310
Cessna 340
Cessna 421

|number built =

|program cost =

|unit cost =

|developed from = Continental IO-346

|variants with their own articles =

|developed into = Continental IO-550

}}

The Continental IO-520 is a six-cylinder, horizontally opposed aircraft engine produced by Teledyne Continental Motors. First run in 1963 as a development of the IO-346, it has been produced in versions incorporating fuel injection (IO-520), turbo-charging (TSIO-520), and gearing (GTSIO-520).

Design and development

The IO-520 series engines normally produce {{convert|285|to|310|hp|-1}} and are used in numerous aircraft such as certain models of the Bellanca Viking 300 and Super Viking, the Beech Bonanza and Baron, and Cessna 185- 206-, 210-, 310-, and 400-series aircraft. The IO-520 remained in production in 2019.{{cite web|url = http://continentalmotors.aero/engines/500.aspx|title = 500 Series Engines|access-date = 8 November 2022|author=Continental Aerospace Technologies|author-link=Continental Aerospace Technologies|work = continentalmotors.aero|year=2022|archive-url= https://archive.today/20221108141454/http://www.continental.aero/engines/500.aspx|archive-date= 8 November 2022|url-status= live}}

The geared GTSIO-520's most common applications are the twin-engine Cessna 404 and 421, where it is rated at {{convert|375|hp|abbr=on}}. The 'G' prefix indicated the incorporation of propeller reduction gearing.

Variants

=IO-520=

;IO-520-A: 285 hp (213 kW){{cite web|url = https://drs.faa.gov/browse/excelExternalWindow/3915185C295FDD9686258846004F1E30.0001?modalOpened=true|title = Type Certificate Data Sheet No. E5CE Revision 27|access-date = 8 November 2022|author = Federal Aviation Administration|author-link = Federal Aviation Administration|date = 8 March 2022|archive-url= https://archive.today/20221108141653/https://drs.faa.gov/browse/excelExternalWindow/3915185C295FDD9686258846004F1E30.0001%3FmodalOpened%3Dtrue?modalOpened=true|archive-date= 8 November 2022|url-status= live}} (Meyers 200)

;IO-520-B: 285 hp (213 kW) (Beech 35-C33A Debonair, s35, model 36 Bonanza)

;IO-520-BA: 285 hp (213 kW)

;IO-520-BB: 285 hp (213 kW)

;IO-520-C: 285 hp (213 kW)

;IO-520-CB: 285 hp (213 kW)

;IO-520-D: 300 hp (224 kW)

;IO-520-E: 300 hp (224 kW)

;IO-520-F: 300 hp (224 kW)

;IO-520-J: 285 hp (213 kW)

;IO-520-K: 300 hp (224 kW) (Bellanca Viking)

;IO-520-L: 300 hp (224 kW)

;IO-520-M: 285 hp (213 kW)

;IO-520-MB: 285 hp (213 kW)

;IO-520-N: 300 hp (224 kW)

;IO-520-NB: 300 hp (224 kW)

;L/IO-520-P: {{convert|250|hp|kW|0|abbr=on}}

=TSIO-520=

;TSIO-520-A: {{convert|255|hp|kW|0|abbr=on}}{{cite web|url = https://drs.faa.gov/browse/excelExternalWindow/9E0F2A7C6E49173F86258543004495A0.0001?modalOpened=true|title = Type Certificate Data Sheet No. E8CE Revision 24|access-date = 8 November 2022|author = Federal Aviation Administration|author-link = Federal Aviation Administration|date = 6 April 2020|archive-url= https://archive.today/20221108142216/https://drs.faa.gov/browse/excelExternalWindow/9E0F2A7C6E49173F86258543004495A0.0001%3FmodalOpened%3Dtrue?modalOpened=true|archive-date= 8 November 2022|url-status= live}}

;TSIO-520-AE: {{convert|250|hp|kW|0|abbr=on}}

;LTSIO-520-AE: {{convert|250|hp|kW|0|abbr=on}}

;TSIO-520-AF: {{convert|310|hp|kW|0|abbr=on}}

;TSIO-520-B: 285 hp (213 kW)

;TSIO-520-BB: 285 hp (213 kW)

;TSIO-520-BE: {{convert|310|hp|kW|0|abbr=on}}

;TSIO-520-C: {{convert|265|hp|kW|0|abbr=on}}

;TSIO-520-CE: {{convert|325|hp|kW|0|abbr=on}}

;TSIO-520-D: 285 hp (213 kW)

;TSIO-520-DB: 285 hp (213 kW)

;TSIO-520-E: {{convert|300|hp|kW|0|abbr=on}}

;TSIO-520-EB: {{convert|300|hp|kW|0|abbr=on}}

;TSIO-520-G: 285 hp (213 kW)

;TSIO-520-H: {{convert|265|hp|kW|0|abbr=on}}

;TSIO-520-J: 310 hp (230 kW)

;TSIO-520-JB: 310 hp (230 kW)

;TSIO-520-K: 285 hp (213 kW)

;TSIO-520-KB: 285 hp (213 kW)

;TSIO-520-L: 310 hp (230 kW)

;TSIO-520-LB: 310 hp (230 kW)

;TSIO-520-M: 285 hp (213 kW)

;TSIO-520-N: 310 hp (230 kW)

;TSIO-520-NB: 310 hp (230 kW)

;TSIO-520-P: 310 hp (230 kW)

;TSIO-520-R: 310 hp (230 kW)

;TSIO-520-T: 310 hp (230 kW)

;TSIO-520-U: {{convert|300|hp|kW|0|abbr=on}}

;TSIO-520-UB: {{convert|300|hp|kW|0|abbr=on}}

;TSIO-520-VB: {{convert|325|hp|kW|0|abbr=on}}

;TSIO-520-WB: {{convert|325|hp|kW|0|abbr=on}}

=GTSIO-520=

;GTSIO-520-C: {{convert|340|hp|kW|0|abbr=on}}{{cite web|url = https://drs.faa.gov/browse/excelExternalWindow/37202859DA7B25CF862588C300651C09.0001|title = Type Certificate Data Sheet No. E7CE Revision 20|access-date = 8 November 2022|author = Federal Aviation Administration|author-link = Federal Aviation Administration|date = 8 September 2022|archive-url= https://archive.today/20221108135206/https://drs.faa.gov/browse/excelExternalWindow/37202859DA7B25CF862588C300651C09.0001%3FmodalOpened%3Dtrue?modalOpened=true|archive-date= 8 November 2022|url-status= live}}

;GTSIO-520-D: 375 hp (280 kW) (Cessna 421)

;GTSIO-520-F: {{convert|435|hp|kW|0|abbr=on}}

;GTSIO-520-H: 375 hp (280 kW) (Cessna 421B)

;GTSIO-520-K: {{convert|435|hp|kW|0|abbr=on}}

;GTSIO-520-L: 375 hp (280 kW) (Cessna 421C)

;GTSIO-520-M: 375 hp (280 kW) (Cessna 404)

;GTSIO-520-N: 375 hp (280 kW) (Cessna 421C)

;GTSIO-520-S: 375 hp (280 kW) (Tecnam P2012 Traveller)

Applications

Specifications (GTSIO-520-D)

{{pistonspecs|

|ref=Continental Motors.[http://www.tcmlink.com/EngSpecSheetDocs/GTSIO520D.pdf Product data sheet GTSIO-520-D] {{webarchive|url=https://web.archive.org/web/20060717002547/http://www.tcmlink.com/EngSpecSheetDocs/GTSIO520D.pdf |date=2006-07-17 }} Retrieved: 21 November 2012

|type=6-cylinder horizontally opposed aircraft engine

|bore={{cvt|5.25|in}}

|stroke={{cvt|4.00|in}}

|displacement={{cvt|520|cuin|L|1}}

|length=63.63 in (161.6 cm)

|diameter=

|width=34.04 in (86.5 cm)

|height=26.63 in (67.6 cm)

|weight=484 lb (219.5 kg) without accessories

|valvetrain=Overhead valve

|supercharger=

|turbocharger=

|fuelsystem=TCM fuel injection

|fueltype=100/130 Octane avgas

|oilsystem=

|coolingsystem=Air-cooled

|power=375 hp (280 kW) (Maximum continuous operation at 3,400 rpm)

|specpower=

|compression=7.5:1

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=0.77 hp/lb (1.27kW/kg)

|designer=

|reduction_gear=

|general_other=

|components_other=

|performance_other=

}}

See also

References

{{Reflist}}