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id="siteSub" class="noprint">From Wikipedia, the free encyclopedia</div> </div> <div id="contentSub"><div id="mw-content-subtitle"></div></div> <div id="mw-content-text" class="mw-body-content"><div class="mw-content-ltr mw-parser-output" lang="en" dir="ltr"><div class="shortdescription nomobile noexcerpt noprint searchaux" style="display:none">6-cylinder air-cooled aircraft engine</div> <p class="mw-empty-elt"> </p> <table class="infobox" style="width:25.5em;border-spacing:2px;"> <tbody><tr> <th colspan="2" style="text-align: center; font-size: 125%;">O-470 </th></tr> <tr> <td colspan="2" style="text-align: center;"><span typeof="mw:File"><a href="/wiki/File:Continental_O-470-13A.jpg" class="mw-file-description"><img src="//upload.wikimedia.org/wikipedia/commons/thumb/b/be/Continental_O-470-13A.jpg/300px-Continental_O-470-13A.jpg" decoding="async" width="300" height="191" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/b/be/Continental_O-470-13A.jpg 1.5x" data-file-width="431" data-file-height="274" /></a></span> </td></tr> <tr> <td colspan="2" style="border-bottom: 1px solid #aaa;text-align:center;">Preserved Continental O-470-13A </td></tr> <tr> <th>Type </th> <td><a href="/wiki/Piston" title="Piston">Piston</a> <a href="/wiki/Aircraft_engine" title="Aircraft engine">aero-engine</a> </td></tr> <tr> <th><span class="nowrap">National origin</span> </th> <td><a href="/wiki/United_States" title="United States">United States</a> </td></tr> <tr> <th>Manufacturer </th> <td><a href="/wiki/Teledyne_Continental_Motors" class="mw-redirect" title="Teledyne Continental Motors">Teledyne Continental Motors</a> </td></tr> <tr> <th>First run </th> <td>1950 </td></tr> <tr> <th><span class="nowrap">Major applications</span> </th> <td><a href="/wiki/Beechcraft_Bonanza" title="Beechcraft Bonanza">Beechcraft Bonanza</a><br /><a href="/wiki/Beechcraft_Baron" title="Beechcraft Baron">Beechcraft Baron</a><br /><a href="/wiki/Cessna_O-1_Bird_Dog" title="Cessna O-1 Bird Dog">Cessna Bird Dog</a> <br /><a href="/wiki/Cessna_180" class="mw-redirect" title="Cessna 180">Cessna 180</a><br /><a href="/wiki/Cessna_182" class="mw-redirect" title="Cessna 182">Cessna 182</a><br /><a href="/wiki/Cessna_185" class="mw-redirect" title="Cessna 185">Cessna 185</a><br /><a href="/wiki/Cessna_188" title="Cessna 188">Cessna 188</a><br /><a href="/wiki/Cessna_210" class="mw-redirect" title="Cessna 210">Cessna 210</a><br /><a href="/wiki/Cessna_310" title="Cessna 310">Cessna 310</a> </td></tr> <tr> <th>Produced </th> <td>1953–1986 </td></tr> </tbody></table> <p>The <b>Continental O-470</b> engine is a family of <a href="/wiki/Carburetor" title="Carburetor">carbureted</a> and <a href="/wiki/Fuel-injected" class="mw-redirect" title="Fuel-injected">fuel-injected</a> <a href="/wiki/Flat_six_engine" class="mw-redirect" title="Flat six engine">six-cylinder, horizontally opposed</a>, air-cooled aircraft engines that was developed especially for use in <a href="/wiki/Light_aircraft" title="Light aircraft">light aircraft</a> by <a href="/wiki/Teledyne_Continental_Motors" class="mw-redirect" title="Teledyne Continental Motors">Continental Motors</a>. Engines designated "IO" are fuel-injected.<sup id="cite_ref-E273_1-0" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-3E1_2-0" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup> </p><p>The family also includes the <b>E165</b>, <b>E185</b>, <b>E225</b> and the <b>E260</b> engines, and several specialty variants. It has been in production since 1950.<sup id="cite_ref-E273_1-1" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-3E1_2-1" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-E269_3-0" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-E281_4-0" class="reference"><a href="#cite_note-E281-4"><span class="cite-bracket">[</span>4<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-shanaberger470_5-0" class="reference"><a href="#cite_note-shanaberger470-5"><span class="cite-bracket">[</span>5<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-E267_6-0" class="reference"><a href="#cite_note-E267-6"><span class="cite-bracket">[</span>6<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-E246_7-0" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup> </p> <meta property="mw:PageProp/toc" /> <div class="mw-heading mw-heading2"><h2 id="Design_and_development">Design and development</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Continental_O-470&action=edit&section=1" title="Edit section: Design and development"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <p>The first engine in this series was the E165, a 471 cubic inch (7.7 L) engine producing 165 hp (123 kW), and was the first of the Continental's "E" series engines. Later versions were given the company designation of E185 (185 hp (138 kW) continuous) and E225 (225 hp (168 kW)). When the US military gave them all the designation of O-470 the company adopted the designation and future models were known as Continental O-470s.<sup id="cite_ref-shanaberger470_5-1" class="reference"><a href="#cite_note-shanaberger470-5"><span class="cite-bracket">[</span>5<span class="cite-bracket">]</span></a></sup> </p><p>The O-470 family of engines covers a range from 213 hp (159 kW) to 260 hp (194 kW). The engines were developed in the late 1940s and certification was applied for on 23 October 1950 on the regulatory basis of Part 13 of the US Civil Air Regulations effective 1 August 1949 as amended by 13-1. The first O-470 model was certified on 19 January 1951.<sup id="cite_ref-E273_1-2" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-3E1_2-2" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-E269_3-1" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-E281_4-1" class="reference"><a href="#cite_note-E281-4"><span class="cite-bracket">[</span>4<span class="cite-bracket">]</span></a></sup> </p> <div class="mw-heading mw-heading2"><h2 id="Variants">Variants</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Continental_O-470&action=edit&section=2" title="Edit section: Variants"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <div class="mw-heading mw-heading3"><h3 id="Carbureted_models">Carbureted models</h3><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Continental_O-470&action=edit&section=3" title="Edit section: Carbureted models"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <dl><dt>E165-2</dt> <dd>165 hp (123 kW) at 2050 rpm, dry weight 351 lb (159 kg), Marvel-Schebler MA-4-5 carburetor.<sup id="cite_ref-E246_7-1" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E165-3</dt> <dd>165 hp (123 kW) at 2050 rpm, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.<sup id="cite_ref-E246_7-2" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E165-4</dt> <dd>165 hp (123 kW) at 2050 rpm, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.<sup id="cite_ref-E246_7-3" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-1</dt> <dd>205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.<sup id="cite_ref-E246_7-4" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-2</dt> <dd>185 hp (138 kW) at 2300 rpm, dry weight 351 lb (159 kg), Marvel-Schebler MA-4-5 carburetor.<sup id="cite_ref-E246_7-5" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-3</dt> <dd>205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.<sup id="cite_ref-E246_7-6" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-5</dt> <dd>185 hp (138 kW) at 2300 rpm, dry weight 343 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.<sup id="cite_ref-E246_7-7" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-8</dt> <dd>205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor, identical to E185-1 but with revised starter drive with dog rather than gear type starter.<sup id="cite_ref-E246_7-8" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-9</dt> <dd>205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor, identical to E185-3 except for revised starter drive to accommodate dog rather than gear type starter.<sup id="cite_ref-E246_7-9" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-10</dt> <dd>205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor.<sup id="cite_ref-E246_7-10" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E185-11</dt> <dd>205 hp (153 kW) at 2600 rpm for five minutes, 185 hp (138 kW) at 2300 rpm continuous, dry weight 344 lb (156 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor, identical to E185-8 but with revised mounting brackets.<sup id="cite_ref-E246_7-11" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>E225-2</dt> <dd>225 hp (168 kW) at 2650 rpm, dry weight 359 lb (163 kg). Certified 19 July 1951.<sup id="cite_ref-E267_6-1" class="reference"><a href="#cite_note-E267-6"><span class="cite-bracket">[</span>6<span class="cite-bracket">]</span></a></sup></dd> <dt>E225-4</dt> <dd>225 hp (168 kW) at 2650 rpm, dry weight 355 lb (161 kg). Certified 5 July 1952.<sup id="cite_ref-E267_6-2" class="reference"><a href="#cite_note-E267-6"><span class="cite-bracket">[</span>6<span class="cite-bracket">]</span></a></sup></dd> <dt>E225-8</dt> <dd>225 hp (168 kW) at 2650 rpm, dry weight 347 lb (157 kg). Certified 12 July 1950.<sup id="cite_ref-E267_6-3" class="reference"><a href="#cite_note-E267-6"><span class="cite-bracket">[</span>6<span class="cite-bracket">]</span></a></sup></dd> <dt>E225-9</dt> <dd>225 hp (168 kW) at 2650 rpm, dry weight 363 lb (165 kg). Certified 30 October 1950.<sup id="cite_ref-E267_6-4" class="reference"><a href="#cite_note-E267-6"><span class="cite-bracket">[</span>6<span class="cite-bracket">]</span></a></sup></dd> <dt>GE260-2X</dt> <dd>260 hp (194 kW), flown in the <a href="/wiki/Robertson_Skylark_SRX-1" title="Robertson Skylark SRX-1">Robertson Skylark SRX-1</a></dd> <dt>O-470-2</dt> <dd>250 hp (186 kW) at 2600 rpm, dry weight 484 lb (220 kg), supercharged model. Certified 2 February 1955.<sup id="cite_ref-E281_4-2" class="reference"><a href="#cite_note-E281-4"><span class="cite-bracket">[</span>4<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-4</dt> <dd>225 hp (168 kW) at 2600 rpm, dry weight 415 lb (188 kg), previously designated 0-470-13B. It is identical to the Model 0-470-13A except for the Bendix-Stromberg Model PS-5CD carburetor in place of the PS-5C. Certified 19 January 1951.<sup id="cite_ref-E269_3-2" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-7</dt> <dd>Non-certified military engine, identical to E185-3, 205 hp (153 kW) at 2600 rpm, dry weight 352 lb (160 kg), Bendix-Stromberg PS-5C or PS-5CD carburetor. When equipped with 18 mm. spark plugs, it is designated 0-470-7A.<sup id="cite_ref-E246_7-12" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-11</dt> <dd>213 hp (159 kW) at 2600 rpm, dry weight 391 lb (177 kg), two sixth order dampers. Certified 19 January 1951.<sup id="cite_ref-E269_3-3" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-11B</dt> <dd>213 hp (159 kW) at 2600 rpm, dry weight 391 lb (177 kg), identical to the 0-470-11 but with 0-470-15 cylinders and pistons. Certified 19 January 1951.<sup id="cite_ref-E269_3-4" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-13</dt> <dd>225 hp (168 kW) at 2600 rpm, dry weight 415 lb (188 kg), one fifth and one sixth order dampers or two sixth order dampers. Certified 19 January 1951.<sup id="cite_ref-E269_3-5" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-13A</dt> <dd>225 hp (168 kW) at 2600 rpm, dry weight 415 lb (188 kg), identical to the 0-470-13 but with an additional tachometer drive through the camshaft gear and one fifth and one sixth order crankshaft damper. Certified 19 January 1951.<sup id="cite_ref-E269_3-6" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-15</dt> <dd>213 hp (159 kW) at 2600 rpm, dry weight 405 lb (184 kg), identical to the 0-470-11 except: four sixth order damper crankshaft, propeller control provisions, revised engine mounting brackets and long skirt pistons. Certified 19 January 1951.<sup id="cite_ref-E269_3-7" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-A</dt> <dd>225 hp (168 kW) at 2600 rpm, dry weight 378 lb (171 kg). Certified 4 December 1952.<sup id="cite_ref-E273_1-3" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt><style data-mw-deduplicate="TemplateStyles:r1238216509">.mw-parser-output .vanchor>:target~.vanchor-text{background-color:#b1d2ff}@media screen{html.skin-theme-clientpref-night .mw-parser-output .vanchor>:target~.vanchor-text{background-color:#0f4dc9}}@media screen and (prefers-color-scheme:dark){html.skin-theme-clientpref-os .mw-parser-output .vanchor>:target~.vanchor-text{background-color:#0f4dc9}}</style><span class="vanchor"><span id="O-470-B"></span><span class="vanchor-text">O-470-B</span></span></dt> <dd>240 hp (179 kW) at 2600 rpm, dry weight 410 lb (186 kg), similar to O-470-A except increased power, different damper configuration, incorporation of inclined valve cylinders, downdraft pressure carburetor and induction changes. Identical to E185-9. Certified 4 December 1952.<sup id="cite_ref-E273_1-4" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup><sup id="cite_ref-E246_7-13" class="reference"><a href="#cite_note-E246-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-E</dt> <dd>225 hp (168 kW) at 2600 rpm, dry weight 390 lb (177 kg), same as O-470-A except downdraft pressure carburetor. Certified 4 December 1952.<sup id="cite_ref-E273_1-5" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-G</dt> <dd>240 hp (179 kW) at 2600 rpm, dry weight 432 lb (196 kg), similar to O-470-M except crankshaft damper configuration, revised oil sump integral cast intake air passage and mounting brackets. Certified 4 December 1952.<sup id="cite_ref-E273_1-6" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-H</dt> <dd>240 hp (179 kW) at 2600 rpm, dry weight 495 lb (225 kg), same as O-470-B with an extension propeller shaft, approved for pusher installations. Certified 4 December 1952.<sup id="cite_ref-E273_1-7" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-J</dt> <dd>225 hp (168 kW) at 2550 rpm, dry weight 378 lb (171 kg), same as O-470-A except reduced max rpm and induction system risers, manifold and balance tube. Certified 4 December 1952.<sup id="cite_ref-E273_1-8" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-K</dt> <dd>230 hp (172 kW) at 2600 rpm, dry weight 404 lb (183 kg), similar to O-470-J except max rpm, crankshaft damper configuration, incorporation of shell-molded cylinder heads and revised mounting brackets. Certified 4 December 1952.<sup id="cite_ref-E273_1-9" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-L</dt> <dd>230 hp (172 kW) at 2600 rpm, dry weight 404 lb (183 kg), same as O-470-K except relocated carburetor, revised intake manifold oil sump. Certified 4 December 1952.<sup id="cite_ref-E273_1-10" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-M</dt> <dd>240 hp (179 kW) at 2600 rpm, dry weight 410 lb (186 kg), same as O-470-B except crankshaft damper configuration and incorporation of shell-molded cylinder heads. Certified 4 December 1952.<sup id="cite_ref-E273_1-11" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-N</dt> <dd>240 hp (179 kW) at 2600 rpm, dry weight 410 lb (186 kg), same as O-470-M except crankshaft damper configuration. Certified 4 December 1952.<sup id="cite_ref-E273_1-12" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-P</dt> <dd>240 hp (179 kW) at 2600 rpm, dry weight 432 lb (196 kg), identical to O-470-G except crankshaft damper configuration. Certified 4 December 1952.<sup id="cite_ref-E273_1-13" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-R</dt> <dd>230 hp (172 kW) at 2600 rpm, dry weight 401 lb (182 kg), same as O-470-L except crankshaft damper configuration. Certified 4 December 1952.<sup id="cite_ref-E273_1-14" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-S</dt> <dd>230 hp (172 kW) at 2600 rpm, dry weight 401 lb (182 kg), same as O-470-R except piston oil cooling and semi-keystone piston rings. Certified 4 December 1952.<sup id="cite_ref-E273_1-15" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-T</dt> <dd>230 hp (172 kW) at 2400 rpm, dry weight 410 lb (186 kg), similar to the O-470-S except crankcase design and max rpm. Certified 4 December 1952.<sup id="cite_ref-E273_1-16" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>O-470-U</dt> <dd>230 hp (172 kW) at 2400 rpm, dry weight 412 lb (187 kg), similar to the O-470-S except max rpm rating and crankshaft damper configuration. Certified 4 December 1952.<sup id="cite_ref-E273_1-17" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd></dl> <div class="mw-heading mw-heading3"><h3 id="Fuel-injected_models">Fuel-injected models</h3><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Continental_O-470&action=edit&section=4" title="Edit section: Fuel-injected models"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <dl><dt>IO-470-A</dt> <dd>240 hp (179 kW) at 2600 rpm, dry weight 432 lb (196 kg), equipped with a TCM 5580 fuel injector. Certified 4 December 1952.<sup id="cite_ref-E273_1-18" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-C</dt> <dd>250 hp (186 kW) at 2600 rpm, dry weight 410 lb (186 kg), equipped with a TCM 5620 or 5827 fuel injector. Certified 4 December 1952.<sup id="cite_ref-E273_1-19" class="reference"><a href="#cite_note-E273-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-D</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 14 October 1958.<sup id="cite_ref-3E1_2-3" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-E</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 26 November 1958.<sup id="cite_ref-3E1_2-4" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-F</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 3 December 1958.<sup id="cite_ref-3E1_2-5" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-G</dt> <dd>250 hp (186 kW) at 2600 rpm, dry weight 431 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 30 March 1959.<sup id="cite_ref-3E1_2-6" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-H</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 432 lb (196 kg), equipped with a TCM 5620-2 fuel injector. Certified 7 August 1959.<sup id="cite_ref-3E1_2-7" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-J</dt> <dd>225 hp (168 kW) at 2600 rpm, dry weight 400 lb (181 kg), equipped with a TCM 5612-1 fuel injector. Certified 31 July 1959.<sup id="cite_ref-3E1_2-8" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-K</dt> <dd>225 hp (168 kW) at 2600 rpm, dry weight 400 lb (181 kg), equipped with a TCM 5807 fuel injector. Certified 9 June 1960.<sup id="cite_ref-3E1_2-9" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-L</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 9 March 1960.<sup id="cite_ref-3E1_2-10" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-LO</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 26 September 1967.<sup id="cite_ref-3E1_2-11" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-M</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 428 lb (194 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 10 March 1960.<sup id="cite_ref-3E1_2-12" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-N</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 432 lb (196 kg), equipped with a TCM 5830 fuel injector. Certified 9 June 1960.<sup id="cite_ref-3E1_2-13" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-P</dt> <dd>250 hp (186 kW) at 2600 rpm, dry weight 472 lb (214 kg), equipped with a TCM 5648 fuel injector. Certified 31 March 1961.<sup id="cite_ref-3E1_2-14" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-R</dt> <dd>250 hp (186 kW) at 2600 rpm, dry weight 431 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 7 October 1960.<sup id="cite_ref-3E1_2-15" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-S</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 429 lb (195 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 10 May 1961.<sup id="cite_ref-3E1_2-16" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-T</dt> <dd>250 hp (186 kW) at 2600 rpm, dry weight 475 lb (215 kg), equipped with a TCM 5648 fuel injector. Certified 1 July 1963.<sup id="cite_ref-3E1_2-17" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-U</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 28 August 1963.<sup id="cite_ref-3E1_2-18" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-V</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Certified 15 June 1965.<sup id="cite_ref-3E1_2-19" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>IO-470-VO</dt> <dd>260 hp (194 kW) at 2625 rpm, dry weight 426 lb (193 kg), equipped with a TCM 5648, 5808 or 5832 fuel injector. Identical to a V but with a oil spray onto piston bottom for enhanced cooling. Certified 26 September 1967.<sup id="cite_ref-3E1_2-20" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>GIO-470-A</dt> <dd></dd> <dt>TSIO-470-B</dt> <dd></dd> <dt>LIO-470-A</dt> <dd>250 hp (186 kW) at 2600 rpm, dry weight 475 lb (215 kg), equipped with a TCM 6022 fuel injector. The same as an IO-470-T, except that the crankshaft turns in opposite direction for use on twin-engined aircraft. Certified 18 March 1964.<sup id="cite_ref-3E1_2-21" class="reference"><a href="#cite_note-3E1-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup></dd> <dt>FSO-470-A</dt> <dd>260 hp (194 kW) at 3000 rpm, dry weight 533 lb (242 kg), Supercharged model, specifically approved for helicopters. Certified 2 February 1955.<sup id="cite_ref-E281_4-3" class="reference"><a href="#cite_note-E281-4"><span class="cite-bracket">[</span>4<span class="cite-bracket">]</span></a></sup></dd></dl> <div class="mw-heading mw-heading2"><h2 id="Applications">Applications</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Continental_O-470&action=edit&section=5" title="Edit section: Applications"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <figure class="mw-default-size mw-halign-right" typeof="mw:File/Thumb"><a href="/wiki/File:Cessna182C-FVSO01.jpg" class="mw-file-description"><img src="//upload.wikimedia.org/wikipedia/commons/thumb/4/4b/Cessna182C-FVSO01.jpg/220px-Cessna182C-FVSO01.jpg" decoding="async" width="220" height="165" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/thumb/4/4b/Cessna182C-FVSO01.jpg/330px-Cessna182C-FVSO01.jpg 1.5x, //upload.wikimedia.org/wikipedia/commons/thumb/4/4b/Cessna182C-FVSO01.jpg/440px-Cessna182C-FVSO01.jpg 2x" data-file-width="750" data-file-height="563" /></a><figcaption><a href="/wiki/Cessna_182_Skylane" title="Cessna 182 Skylane">Cessna 182K</a> equipped with a Continental O-470R powerplant</figcaption></figure> <dl><dt>E165</dt></dl> <ul><li><a href="/wiki/Boisavia_Mercurey" title="Boisavia Mercurey">Boisavia Mercurey</a></li> <li><a href="/wiki/Luscombe_11" class="mw-redirect" title="Luscombe 11">Luscombe 11</a></li></ul> <dl><dt>E185</dt></dl> <ul><li><a href="/wiki/Beechcraft_Bonanza" title="Beechcraft Bonanza">Beechcraft Bonanza</a></li> <li><a href="/wiki/Macchi_M.B.320" title="Macchi M.B.320">Macchi M.B.320</a></li> <li><a href="/wiki/Muniz_Casmuniz_52" title="Muniz Casmuniz 52">Muniz Casmuniz 52</a></li> <li><a href="/wiki/Ryan_Navion" title="Ryan Navion">Ryan Navion</a></li></ul> <dl><dt>E225</dt></dl> <ul><li><a href="/wiki/Beechcraft_Bonanza" title="Beechcraft Bonanza">Beechcraft Bonanza</a></li> <li><a href="/wiki/Beechcraft_T-34_Mentor" title="Beechcraft T-34 Mentor">Beechcraft T-34 Mentor</a></li> <li><a href="/wiki/Fletcher_FD-25" title="Fletcher FD-25">Fletcher FD-25</a></li> <li><a href="/wiki/Fletcher_FL-23" title="Fletcher FL-23">Fletcher FL-23</a></li> <li><a href="/wiki/Ryan_Navion" title="Ryan Navion">Ryan Navion</a></li></ul> <dl><dt>E260</dt></dl> <ul><li><a href="/wiki/Robertson_SRX-1_Skyshark" class="mw-redirect" title="Robertson SRX-1 Skyshark">Robertson SRX-1 Skyshark</a></li></ul> <dl><dt>O-470</dt></dl> <ul><li><a href="/wiki/Associated_Air_Liberty_181" title="Associated Air Liberty 181">Associated Air Liberty 181</a></li> <li><a href="/wiki/Beechcraft_Bonanza" title="Beechcraft Bonanza">Beechcraft Bonanza</a></li> <li><a href="/wiki/Bellanca_14-13" title="Bellanca 14-13">Bellanca Cruisemaster</a></li> <li><a href="/wiki/Cessna_180" class="mw-redirect" title="Cessna 180">Cessna 180</a></li> <li><a href="/wiki/Cessna_182_Skylane" title="Cessna 182 Skylane">Cessna 182 Skylane</a></li> <li><a href="/wiki/Cessna_187" title="Cessna 187">Cessna 187</a></li> <li><a href="/wiki/Cessna_188" title="Cessna 188">Cessna 188</a></li> <li><a href="/wiki/Cessna_310" title="Cessna 310">Cessna 310</a></li> <li><a href="/wiki/DINFIA_IA_53" title="DINFIA IA 53">DINFIA IA 53</a></li> <li><a href="/wiki/Falconar_SAL_Mustang" title="Falconar SAL Mustang">Falconar SAL Mustang</a></li> <li><a href="/wiki/Fanaero-Chile_Chincol" title="Fanaero-Chile Chincol">Fanaero-Chile Chincol</a></li> <li><a href="/wiki/Fuji_KM-2" title="Fuji KM-2">Fuji KM-2</a></li> <li><a href="/wiki/HAL_Krishak" title="HAL Krishak">HAL Krishak</a></li> <li><a href="/wiki/Maestranza_Central_de_Aviaci%C3%B3n_HF_XX-02" title="Maestranza Central de Aviación HF XX-02">Maestranza Central de Aviación HF XX-02</a></li> <li><a href="/wiki/Meyers_200" title="Meyers 200">Meyers 200</a></li> <li><a href="/wiki/O-1_Bird_dog" class="mw-redirect" title="O-1 Bird dog">O-1 Bird dog</a></li> <li><a href="/wiki/PZL-104_Wilga" title="PZL-104 Wilga">PZL-104 Wilga</a></li> <li><a href="/wiki/SIAI-Marchetti_FN.333_Riviera" title="SIAI-Marchetti FN.333 Riviera">SIAI-Marchetti FN.333 Riviera</a></li> <li><a href="/wiki/St-Just_Cyclone" title="St-Just Cyclone">St-Just Cyclone</a></li> <li><a href="/wiki/Stinson_108" title="Stinson 108">Stinson 108</a> (modified under <a href="/wiki/Supplemental_Type_Certificate" class="mw-redirect" title="Supplemental Type Certificate">STC</a>)</li> <li><a href="/wiki/Taylorcraft_Ranch_Wagon" title="Taylorcraft Ranch Wagon">Taylorcraft Ranch Wagon</a></li> <li><a href="/wiki/Yeoman_Cropmaster" title="Yeoman Cropmaster">Yeoman Cropmaster</a></li></ul> <dl><dt>IO-470</dt></dl> <ul><li><a href="/wiki/Auster_AOP.9" title="Auster AOP.9">Auster AOP.9</a></li> <li><a href="/wiki/Beechcraft_Baron" title="Beechcraft Baron">Beechcraft Baron</a></li> <li><a href="/wiki/Beechcraft_Bonanza" title="Beechcraft Bonanza">Beechcraft Bonanza</a></li> <li><a href="/wiki/Cessna_185" class="mw-redirect" title="Cessna 185">Cessna 185</a></li> <li><a href="/wiki/Cessna_210" class="mw-redirect" title="Cessna 210">Cessna 210A</a></li> <li><a href="/wiki/Cessna_310" title="Cessna 310">Cessna 310</a></li> <li><a href="/wiki/Meyers_200" title="Meyers 200">Meyers 200</a></li> <li><a href="/wiki/Navion_G_Rangemaster" class="mw-redirect" title="Navion G Rangemaster">Navion G Rangemaster</a></li> <li><a href="/wiki/PAC_Fletcher" class="mw-redirect" title="PAC Fletcher">PAC Fletcher</a></li> <li><a href="/wiki/Procaer_Picchio" title="Procaer Picchio">Procaer Picchio</a></li> <li><a href="/wiki/Ryan_Navion" title="Ryan Navion">Ryan Navion</a></li> <li><a href="/wiki/A%C3%A9rotrain_01" class="mw-redirect" title="Aérotrain 01">Aérotrain 01</a> – experimental hover train project</li></ul> <div class="mw-heading mw-heading2"><h2 id="Specifications_(O-470-11)"><span id="Specifications_.28O-470-11.29"></span>Specifications (O-470-11)</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Continental_O-470&action=edit&section=6" title="Edit section: Specifications (O-470-11)"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <p style="font-size: 90%; margin:0; padding: .2em"><i>Data from</i> <i>Type Certificate Data Sheet E-269.</i><sup id="cite_ref-E269_3-8" class="reference"><a href="#cite_note-E269-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup></p> <div class="mw-heading mw-heading3"><h3 id="General_characteristics">General characteristics</h3></div> <ul><li><b>Type:</b> six-cylinder air-cooled <a href="/wiki/Horizontally_opposed" class="mw-redirect" title="Horizontally opposed">horizontally opposed</a> aircraft piston engine</li> <li><b><a href="/wiki/Bore_(engine)" title="Bore (engine)">Bore</a>:</b> 5.0 in (127.0 mm)</li> <li><b><a href="/wiki/Stroke_(engine)" title="Stroke (engine)">Stroke</a>:</b> 4.0 in (101.6 mm)</li> <li><b><a href="/wiki/Engine_displacement" title="Engine displacement">Displacement</a>:</b> 471 in<sup>3</sup> (7.7 L)</li> <li><b><a href="/wiki/Dry_weight" class="mw-redirect" title="Dry weight">Dry weight</a>:</b> 391 lb dry (177 kg)</li></ul> <div class="mw-heading mw-heading3"><h3 id="Components">Components</h3></div> <ul><li><b><a href="/wiki/Valvetrain" title="Valvetrain">Valvetrain</a>:</b> One intake and one exhaust valve per cylinder</li> <li><b>Fuel system:</b> Bendix-Stromberg Model PS-5C <a href="/wiki/Carburetor" title="Carburetor">carburetor</a></li> <li><b>Fuel type:</b> 80/87 <a href="/wiki/Avgas" title="Avgas">avgas</a></li> <li><b>Oil system:</b> dry sump</li> <li><b>Cooling system:</b> Air-cooled</li></ul> <div class="mw-heading mw-heading3"><h3 id="Performance">Performance</h3></div> <ul><li><b>Power output:</b> 213 hp (159 kW) at 2,575 rpm</li> <li><b><a href="/wiki/Power_density" title="Power density">Specific power</a>:</b> 0.45 hp/in³ (20.4 kW/L)</li> <li><b><a href="/wiki/Compression_ratio" title="Compression ratio">Compression ratio</a>:</b> 7.0:1</li> <li><b><a href="/wiki/Power-to-weight_ratio" title="Power-to-weight ratio">Power-to-weight ratio</a>:</b> 0.54 hp/lb (0.90 kW/kg)</li></ul> <div class="mw-heading mw-heading2"><h2 id="See_also">See also</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Continental_O-470&action=edit&section=7" title="Edit section: See also"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <p> <b>Comparable engines</b> </p> <ul><li><a href="/wiki/Lycoming_O-480" title="Lycoming O-480">Lycoming O-480</a></li></ul> <p><b>Related lists</b> </p> <ul><li><a href="/wiki/List_of_aircraft_engines" title="List of aircraft engines">List of aircraft engines</a></li></ul> <div class="mw-heading mw-heading2"><h2 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.cs1-maint{display:none;color:#085;margin-left:0.3em}.mw-parser-output .cs1-kern-left{padding-left:0.2em}.mw-parser-output .cs1-kern-right{padding-right:0.2em}.mw-parser-output .citation .mw-selflink{font-weight:inherit}@media screen{.mw-parser-output .cs1-format{font-size:95%}html.skin-theme-clientpref-night .mw-parser-output .cs1-maint{color:#18911f}}@media screen and (prefers-color-scheme:dark){html.skin-theme-clientpref-os .mw-parser-output .cs1-maint{color:#18911f}}</style><cite id="CITEREFFederal_Aviation_Administration1995" class="citation web cs1"><a href="/wiki/Federal_Aviation_Administration" title="Federal Aviation Administration">Federal Aviation Administration</a> (September 1995). <a rel="nofollow" class="external text" href="https://web.archive.org/web/20210805153142/http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/TcdsLookup/E-273_36">"TYPE CERTIFICATE DATA SHEET NO. 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E-246 Revision 20"</a>. Archived from <a rel="nofollow" class="external text" href="http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/TcdsLookup/E-246_20">the original</a> on 5 August 2021<span class="reference-accessdate">. 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title="Avgas">Gasoline</a>)</th><td class="navbox-list-with-group navbox-list navbox-odd hlist" style="width:100%;padding:0"><div style="padding:0 0.25em"></div><table class="nowraplinks navbox-subgroup" style="border-spacing:0"><tbody><tr><th scope="row" class="navbox-group" style="width:1%">By company<br />horsepower designation</th><td class="navbox-list-with-group navbox-list navbox-odd" style="width:100%;padding:0"><div style="padding:0 0.25em"> <ul><li><a href="/wiki/Continental_A40" title="Continental A40">A40</a></li> <li><a href="/wiki/Continental_O-170" title="Continental O-170">A50</a></li> <li><a href="/wiki/Continental_O-170" title="Continental O-170">A65</a></li> <li><a href="/w/index.php?title=Continental_A70&action=edit&redlink=1" class="new" title="Continental A70 (page does not exist)">A70</a></li> <li><a href="/wiki/Continental_O-170" title="Continental O-170">A75</a></li> <li><a href="/wiki/Continental_O-170" title="Continental O-170">A80</a></li> <li><a href="/wiki/Continental_O-190" title="Continental O-190">C75</a></li> <li><a href="/wiki/Continental_O-190" title="Continental O-190">C85</a></li> <li><a href="/wiki/Continental_O-200" title="Continental O-200">C90</a></li> <li><a href="/wiki/Continental_O-280" title="Continental O-280">C115</a></li> <li><a href="/wiki/Continental_O-280" title="Continental O-280">C125</a></li> <li><a href="/wiki/Continental_O-280" title="Continental O-280">C140</a></li> <li><a href="/wiki/Continental_O-300" title="Continental O-300">C145</a></li> <li><a class="mw-selflink selflink">E165</a></li> <li><a class="mw-selflink selflink">E185</a></li> <li><a class="mw-selflink selflink">E225</a></li> <li><a href="/wiki/Continental_Tiara_series" title="Continental Tiara series">Tiara series</a></li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Engine_displacement" title="Engine displacement">By displacement</a></th><td class="navbox-list-with-group navbox-list navbox-even" style="width:100%;padding:0"><div style="padding:0 0.25em"> <ul><li><a href="/wiki/Continental_O-170" title="Continental O-170">O-170</a></li> <li><a href="/wiki/Continental_O-190" title="Continental O-190">O-190</a></li> <li><a href="/wiki/Continental_O-200" title="Continental O-200">O-200</a></li> <li><a href="/wiki/Continental_O-200" title="Continental O-200">O-205</a></li> <li><a href="/wiki/Continental_O-240" title="Continental O-240">O-240</a></li> <li><a href="/wiki/Continental_O-280" title="Continental O-280">O-280</a></li> <li><a href="/wiki/Continental_O-300" title="Continental O-300">O-300</a></li> <li><a href="/wiki/Continental_IO-346" title="Continental IO-346">IO-346</a></li> <li><a href="/wiki/Continental_IO-360" title="Continental IO-360">IO-360</a></li> <li><a href="/w/index.php?title=Continental/Rolls-Royce_IO-368&action=edit&redlink=1" class="new" title="Continental/Rolls-Royce IO-368 (page does not exist)">IO-368</a></li> <li><a href="/wiki/Continental_IO-370" title="Continental IO-370">IO-370</a></li> <li><a class="mw-selflink selflink">O-470</a></li> <li><a href="/wiki/Continental_O-520" class="mw-redirect" title="Continental O-520">O-520</a></li> <li><a href="/wiki/Continental_O-526" title="Continental O-526">O-526</a></li> <li><a href="/wiki/Continental_IO-550" title="Continental IO-550">IO-550</a></li></ul> </div></td></tr></tbody></table><div></div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Aircraft_Diesel_engine" class="mw-redirect" title="Aircraft Diesel engine">Aircraft Diesel engines</a></th><td class="navbox-list-with-group navbox-list navbox-odd hlist" style="width:100%;padding:0"><div style="padding:0 0.25em"> <ul><li><a href="/wiki/Thielert_Centurion" title="Thielert Centurion">CD-155</a></li> <li><a href="/wiki/Continental_CD-230" title="Continental CD-230">CD-200 (TD-300)</a></li> <li><a href="/wiki/Thielert_Centurion" title="Thielert Centurion">CD-300</a></li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Radial_engine" title="Radial engine">Radial engines</a></th><td class="navbox-list-with-group navbox-list navbox-even hlist" style="width:100%;padding:0"><div style="padding:0 0.25em"> <ul><li><a href="/w/index.php?title=Continental_A70&action=edit&redlink=1" class="new" title="Continental A70 (page does not exist)">R-544</a></li> <li><a href="/wiki/Continental_R-670" title="Continental R-670">R-670</a></li> <li><a href="/wiki/Wright_R-975_Whirlwind" title="Wright R-975 Whirlwind">R-975</a></li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/V_engine" title="V engine">Inverted-V engines</a></th><td class="navbox-list-with-group navbox-list navbox-odd hlist" style="width:100%;padding:0"><div style="padding:0 0.25em"> <ul><li><a href="/wiki/Continental_XI-1430" title="Continental XI-1430">XI-1430</a></li></ul> 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