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style="display:none">Turboprop aircraft engine family</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%;">AE 2100 </th></tr> <tr> <td colspan="2" style="text-align: center;"><span typeof="mw:File"><a href="/wiki/File:RR_AE_2100_of_C-27J.jpg" class="mw-file-description"><img src="//upload.wikimedia.org/wikipedia/commons/thumb/b/b4/RR_AE_2100_of_C-27J.jpg/300px-RR_AE_2100_of_C-27J.jpg" decoding="async" width="300" height="200" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/thumb/b/b4/RR_AE_2100_of_C-27J.jpg/450px-RR_AE_2100_of_C-27J.jpg 1.5x, //upload.wikimedia.org/wikipedia/commons/thumb/b/b4/RR_AE_2100_of_C-27J.jpg/600px-RR_AE_2100_of_C-27J.jpg 2x" data-file-width="3648" data-file-height="2432" /></a></span> </td></tr> <tr> <td colspan="2" style="border-bottom: 1px solid #aaa;text-align:center;">The Rolls-Royce AE 2100 D2A on a <a href="/wiki/C-27J" class="mw-redirect" title="C-27J">C-27J</a> </td></tr> <tr> <th>Type </th> <td><a href="/wiki/Turboprop" title="Turboprop">Turboprop</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/Allison_Engine_Company" title="Allison Engine Company">Allison Engine Company</a> <br /> <a href="/wiki/Rolls-Royce_plc" class="mw-redirect" title="Rolls-Royce plc">Rolls-Royce plc</a> </td></tr> <tr> <th><span class="nowrap">Major applications</span> </th> <td><a href="/wiki/Alenia_C-27J_Spartan" title="Alenia C-27J Spartan">Alenia C-27J Spartan</a> <br /> <a href="/wiki/Lockheed_Martin_C-130J_Hercules" class="mw-redirect" title="Lockheed Martin C-130J Hercules">Lockheed Martin C-130J Hercules</a> <br /> <a href="/wiki/Saab_2000" title="Saab 2000">Saab 2000</a> <br /> <a href="/wiki/ShinMaywa_US-2" title="ShinMaywa US-2">ShinMaywa US-2</a> </td></tr> <tr> <th><span class="nowrap">Number built</span> </th> <td>2,300+<sup id="cite_ref-2300engines_1-0" class="reference"><a href="#cite_note-2300engines-1"><span class="cite-bracket">[</span>1<span class="cite-bracket">]</span></a></sup> </td></tr> <tr> <th><span class="nowrap">Developed from</span> </th> <td><a href="/wiki/Rolls-Royce_T406" title="Rolls-Royce T406">Rolls-Royce T406</a> </td></tr> </tbody></table> <p>The <b>Rolls-Royce AE 2100</b> is a <a href="/wiki/Turboprop" title="Turboprop">turboprop</a> developed by <a href="/wiki/Allison_Engine_Company" title="Allison Engine Company">Allison Engine Company</a>, now part of <a href="/wiki/Rolls-Royce_North_America" title="Rolls-Royce North America">Rolls-Royce North America</a>. The engine was originally known as the GMA 2100, when Allison was a division of former corporate parent <a href="/wiki/General_Motors" title="General Motors">General Motors</a>. </p> <meta property="mw:PageProp/toc" /> <div class="mw-heading mw-heading2"><h2 id="Development">Development</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Rolls-Royce_AE_2100&action=edit&section=1" title="Edit section: Development"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <p>On July 11, 1989, <a href="/wiki/Saab-Scania" title="Saab-Scania">Saab-Scania</a> A.B. selected the GMA 2100 to power its new <a href="/wiki/Saab_2000" title="Saab 2000">Saab 2000</a>, a 50-seat stretch of the <a href="/wiki/Saab_340" title="Saab 340">Saab 340</a> turboprop, in a US$500 million deal.<sup id="cite_ref-NYT19890712_2-0" class="reference"><a href="#cite_note-NYT19890712-2"><span class="cite-bracket">[</span>2<span class="cite-bracket">]</span></a></sup> In July 1990, Industri Pesawat Terbang Nusantara (IPTN) of Indonesia picked the GMA 2100 as the engine for the twin-engine <a href="/wiki/IPTN_N-250" title="IPTN N-250">N-250</a> regional airliner.<sup id="cite_ref-FI19900718_3-0" class="reference"><a href="#cite_note-FI19900718-3"><span class="cite-bracket">[</span>3<span class="cite-bracket">]</span></a></sup> <a href="/wiki/Flight_testing" class="mw-redirect" title="Flight testing">Flight testing</a> with a 13 ft 6 in diameter (4.11 m) Dowty R373 propeller on a <a href="/wiki/Lockheed_P-3_Orion" title="Lockheed P-3 Orion">Lockheed P-3 Orion</a> <a href="/wiki/Testbed_aircraft" title="Testbed aircraft">testbed aircraft</a> began on August 23, 1990, and finished after over 50 hours of flight and ground testing.<sup id="cite_ref-DowtyNews199102_4-0" class="reference"><a href="#cite_note-DowtyNews199102-4"><span class="cite-bracket">[</span>4<span class="cite-bracket">]</span></a></sup> </p><p>The GMA 2100D3 became the powerplant for the <a href="/wiki/Lockheed_Martin_C-130J_Super_Hercules" title="Lockheed Martin C-130J Super Hercules">Lockheed Martin C-130J Super Hercules</a>. It made its first <a href="/wiki/Test_flight" class="mw-redirect" title="Test flight">test flight</a> on March 19, 1994,<sup id="cite_ref-DODAppropriations1995_5-0" class="reference"><a href="#cite_note-DODAppropriations1995-5"><span class="cite-bracket">[</span>5<span class="cite-bracket">]</span></a></sup> which was conducted by Marshall Aerospace on a <a href="/wiki/Lockheed_C-130K_Hercules" class="mw-redirect" title="Lockheed C-130K Hercules">Lockheed C-130K Hercules</a> testbed leased from the <a href="/wiki/Royal_Air_Force" title="Royal Air Force">Royal Air Force</a>. Testing ended in June 1994 after 47 flight hours.<sup id="cite_ref-FI19940831_6-0" class="reference"><a href="#cite_note-FI19940831-6"><span class="cite-bracket">[</span>6<span class="cite-bracket">]</span></a></sup> The engine powered the initial flight of the C-130J aircraft on April 5, 1996.<sup id="cite_ref-FG19960416_7-0" class="reference"><a href="#cite_note-FG19960416-7"><span class="cite-bracket">[</span>7<span class="cite-bracket">]</span></a></sup> By April 1997, the D3 variant had received <a href="/wiki/Federal_Aviation_Administration" title="Federal Aviation Administration">Federal Aviation Administration</a> (FAA) type certification.<sup id="cite_ref-DD19970410_8-0" class="reference"><a href="#cite_note-DD19970410-8"><span class="cite-bracket">[</span>8<span class="cite-bracket">]</span></a></sup> 2,000 of the D3 variants have been delivered as of 2018.<sup id="cite_ref-2thousandD3engines_9-0" class="reference"><a href="#cite_note-2thousandD3engines-9"><span class="cite-bracket">[</span>9<span class="cite-bracket">]</span></a></sup> </p><p>The engine's C variant was certified on December 20, 1993.<sup id="cite_ref-CRAN19940221_10-0" class="reference"><a href="#cite_note-CRAN19940221-10"><span class="cite-bracket">[</span>10<span class="cite-bracket">]</span></a></sup> It powered the N-250 prototype's first flight on August 10, 1995,<sup id="cite_ref-FG19950815_11-0" class="reference"><a href="#cite_note-FG19950815-11"><span class="cite-bracket">[</span>11<span class="cite-bracket">]</span></a></sup> but the N-250 aircraft program was postponed indefinitely in the late 1990s due to the <a href="/wiki/Asian_financial_crisis" class="mw-redirect" title="Asian financial crisis">Asian financial crisis</a>.<sup id="cite_ref-AIN200110_12-0" class="reference"><a href="#cite_note-AIN200110-12"><span class="cite-bracket">[</span>12<span class="cite-bracket">]</span></a></sup> </p><p>In June 1997, the AE 2100 was selected by <a href="/wiki/Lockheed_Martin" title="Lockheed Martin">Lockheed Martin</a> and <a href="/wiki/Alenia_Aeronautica" title="Alenia Aeronautica">Alenia</a> to power the <a href="/wiki/C-27J_Spartan" class="mw-redirect" title="C-27J Spartan">C-27J Spartan</a> <a href="/wiki/Tactical_airlifter" class="mw-redirect" title="Tactical airlifter">tactical airlifter</a>.<sup id="cite_ref-DD19970620_13-0" class="reference"><a href="#cite_note-DD19970620-13"><span class="cite-bracket">[</span>13<span class="cite-bracket">]</span></a></sup> In October 2015, Alenia announced plans to use a 5,100-horsepower (3,800-kilowatt) uprated version of the AE 2100 as the baseline engine by 2017.<sup id="cite_ref-FG20151019_14-0" class="reference"><a href="#cite_note-FG20151019-14"><span class="cite-bracket">[</span>14<span class="cite-bracket">]</span></a></sup> </p> <div class="mw-heading mw-heading2"><h2 id="Design">Design</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Rolls-Royce_AE_2100&action=edit&section=2" title="Edit section: Design"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <figure class="mw-default-size mw-halign-left" typeof="mw:File/Thumb"><a href="/wiki/File:C-130_Hercules_over_Santa_Cruz_Island.jpg" class="mw-file-description"><img src="//upload.wikimedia.org/wikipedia/commons/thumb/0/0a/C-130_Hercules_over_Santa_Cruz_Island.jpg/220px-C-130_Hercules_over_Santa_Cruz_Island.jpg" decoding="async" width="220" height="176" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/thumb/0/0a/C-130_Hercules_over_Santa_Cruz_Island.jpg/330px-C-130_Hercules_over_Santa_Cruz_Island.jpg 1.5x, //upload.wikimedia.org/wikipedia/commons/thumb/0/0a/C-130_Hercules_over_Santa_Cruz_Island.jpg/440px-C-130_Hercules_over_Santa_Cruz_Island.jpg 2x" data-file-width="1024" data-file-height="819" /></a><figcaption><a href="/wiki/C-130J_Hercules" class="mw-redirect" title="C-130J Hercules">C-130J Hercules</a> with six-bladed props</figcaption></figure> <p>A derivative of the Allison AE 1107C-Liberty (<a href="/wiki/Rolls-Royce_T406" title="Rolls-Royce T406">Rolls-Royce T406</a>) <a href="/wiki/Turboshaft_engine" class="mw-redirect" title="Turboshaft engine">turboshaft engine</a>, the AE 2100 shares the same high-pressure core as that engine, as does the <a href="/wiki/Rolls-Royce_AE_3007" title="Rolls-Royce AE 3007">Rolls-Royce AE 3007</a> <a href="/wiki/Turbofan" title="Turbofan">turbofan</a>. This core is capable of powering turboprops of up to 10,000 shp (7,500 kW).<sup id="cite_ref-CAI199111p19_15-0" class="reference"><a href="#cite_note-CAI199111p19-15"><span class="cite-bracket">[</span>15<span class="cite-bracket">]</span></a></sup> The AE 2100 is a two-shaft design,<sup id="cite_ref-MilTech201002_16-0" class="reference"><a href="#cite_note-MilTech201002-16"><span class="cite-bracket">[</span>16<span class="cite-bracket">]</span></a></sup><sup class="reference nowrap"><span title="Pages: 83–84">: 83–84 </span></sup> and it was the first<sup class="noprint Inline-Template" style="white-space:nowrap;">[<i><a href="/wiki/Wikipedia:Manual_of_Style/Dates_and_numbers#Chronological_items" title="Wikipedia:Manual of Style/Dates and numbers"><span title="The time period mentioned near this tag is ambiguous. (May 2020)">when?</span></a></i>]</sup> to use dual <a href="/wiki/FADEC" title="FADEC">FADECs</a> (full authority digital engine control) to control both engine and <a href="/wiki/Propeller_(aeronautics)" title="Propeller (aeronautics)">propeller</a>,<sup id="cite_ref-Dowty80_17-0" class="reference"><a href="#cite_note-Dowty80-17"><span class="cite-bracket">[</span>17<span class="cite-bracket">]</span></a></sup> allowing both to be adjusted with a single lever.<sup id="cite_ref-MilTech201002_16-1" class="reference"><a href="#cite_note-MilTech201002-16"><span class="cite-bracket">[</span>16<span class="cite-bracket">]</span></a></sup><sup class="reference nowrap"><span title="Pages: 83–84">: 83–84 </span></sup> There are four production variants of the engine: the civil AE 2100A, and the military variants which include the AE 2100D2/D2A, AE 2100D3, AE 2100J and AE 2100P. </p><p>The AE 2100 inherited the <a href="/wiki/Allison_T56" title="Allison T56">Allison T56</a>'s 14-stage <a href="/wiki/Axial_compressor" title="Axial compressor">axial compressor</a> design, but the inlet and the <a href="/wiki/Stator" title="Stator">stator</a> for the first five stages have variable blades. The <a href="/wiki/Annular_combustor" class="mw-redirect" title="Annular combustor">annular combustor</a> has 16 air-blast fuel injection nozzles. The turbine that drives the compressor has two stages, with the first stage using single-crystal blades. A <a href="/wiki/Free-turbine_turboshaft" title="Free-turbine turboshaft">free power turbine</a> with two stages drives the propeller through an inner shaft and a gearbox.<sup id="cite_ref-MilTech201002_16-2" class="reference"><a href="#cite_note-MilTech201002-16"><span class="cite-bracket">[</span>16<span class="cite-bracket">]</span></a></sup><sup class="reference nowrap"><span title="Pages: 83–84">: 83–84 </span></sup> The engine has replaceable steel blades and vanes, which are more reliable but heavier than <a href="/wiki/Titanium" title="Titanium">titanium</a>.<sup id="cite_ref-CAI199111p19_15-1" class="reference"><a href="#cite_note-CAI199111p19-15"><span class="cite-bracket">[</span>15<span class="cite-bracket">]</span></a></sup> </p><p>The AE 2100 engine and <a href="/wiki/Gearbox" class="mw-redirect" title="Gearbox">gearbox</a> are rated at 6,000 shaft horsepower (4,500 kilowatts), but was derated to 4,200, 4,590, and 3,600 shp (3,130, 3,420, and 2,680 kW) for the <a href="/wiki/Saab_2000" title="Saab 2000">Saab 2000</a>, <a href="/wiki/Lockheed_Martin_C-130J_Super_Hercules" title="Lockheed Martin C-130J Super Hercules">Lockheed Martin C-130J Super Hercules</a>, and <a href="/wiki/IPTN_N-250" title="IPTN N-250">IPTN N-250</a>, respectively.<sup id="cite_ref-Interavia199410p16_18-0" class="reference"><a href="#cite_note-Interavia199410p16-18"><span class="cite-bracket">[</span>18<span class="cite-bracket">]</span></a></sup> The engine uses six-bladed, all-composite blade <a href="/wiki/Dowty_Rotol" class="mw-redirect" title="Dowty Rotol">Dowty</a> propellers, including the model R381 on the Saab 2000, R414 on the <a href="/wiki/ShinMaywa_US-2" title="ShinMaywa US-2">ShinMaywa US-2</a>,<sup id="cite_ref-Dowty80_17-1" class="reference"><a href="#cite_note-Dowty80-17"><span class="cite-bracket">[</span>17<span class="cite-bracket">]</span></a></sup> R384 on the IPTN N-250,<sup id="cite_ref-CRAN19941114_19-0" class="reference"><a href="#cite_note-CRAN19941114-19"><span class="cite-bracket">[</span>19<span class="cite-bracket">]</span></a></sup> and R391 on the C-130J military transport<sup id="cite_ref-FI19960828_20-0" class="reference"><a href="#cite_note-FI19960828-20"><span class="cite-bracket">[</span>20<span class="cite-bracket">]</span></a></sup> and the <a href="/wiki/Lockheed_Martin_LM-100J" class="mw-redirect" title="Lockheed Martin LM-100J">LM-100J</a> civil-certified version of the C-130J.<sup id="cite_ref-AADT_LM-100J_21-0" class="reference"><a href="#cite_note-AADT_LM-100J-21"><span class="cite-bracket">[</span>21<span class="cite-bracket">]</span></a></sup> The gearbox has a reduction ratio of about 14 and a mean time before unscheduled removal (MTBUR) of over 35,000 hours.<sup id="cite_ref-CAI199111p12_22-0" class="reference"><a href="#cite_note-CAI199111p12-22"><span class="cite-bracket">[</span>22<span class="cite-bracket">]</span></a></sup> </p> <div class="mw-heading mw-heading2"><h2 id="Variants_and_applications">Variants and applications</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Rolls-Royce_AE_2100&action=edit&section=3" title="Edit section: Variants and applications"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <dl><dt>AE 2100A</dt></dl> <ul><li><a href="/wiki/Lockheed_P-3_Orion" title="Lockheed P-3 Orion">Lockheed P-3 Orion</a> (testbed)</li> <li><a href="/wiki/Saab_2000" title="Saab 2000">Saab 2000</a></li></ul> <dl><dt>AE 2100C</dt></dl> <ul><li><a href="/wiki/IPTN_N-250" title="IPTN N-250">IPTN N-250</a> (prototype only)</li></ul> <dl><dt>AE 2100D2A</dt></dl> <ul><li><a href="/wiki/Alenia_C-27J_Spartan" title="Alenia C-27J Spartan">Alenia C-27J Spartan</a></li></ul> <dl><dt>AE 2100D3</dt></dl> <ul><li><a href="/wiki/Lockheed_C-130K_Hercules" class="mw-redirect" title="Lockheed C-130K Hercules">Lockheed C-130K Hercules</a> (testbed)</li> <li><a href="/wiki/Lockheed_Martin_C-130J_Super_Hercules" title="Lockheed Martin C-130J Super Hercules">Lockheed Martin C-130J Super Hercules</a></li> <li><a href="/wiki/Lockheed_Martin_LM-100J" class="mw-redirect" title="Lockheed Martin LM-100J">Lockheed Martin LM-100J</a></li></ul> <dl><dt>AE 2100F</dt> <dd>A variant proposed in 1995 and paired with Dowty R394 propellers to retrofit the <a href="/wiki/Allison_T56" title="Allison T56">Allison T56</a>-powered <a href="/wiki/Lockheed_C-130" class="mw-redirect" title="Lockheed C-130">Lockheed C-130</a> models E through H and <a href="/wiki/Lockheed_L-100-30" class="mw-redirect" title="Lockheed L-100-30">Lockheed L-100-30</a>, at a price after engine/propeller trade-in of USD$11 million per aircraft.<sup id="cite_ref-FG19951212_23-0" class="reference"><a href="#cite_note-FG19951212-23"><span class="cite-bracket">[</span>23<span class="cite-bracket">]</span></a></sup></dd> <dt>AE 2100G</dt> <dd>A variant offered in 1994 for the proposed <a href="/wiki/ATR_72" title="ATR 72">ATR 82</a>, a twin-turboprop airliner seating up to 86 passengers and requiring about 5,000 hp (3,700 kW) of power.<sup id="cite_ref-JPRS-EST-94-017_24-0" class="reference"><a href="#cite_note-JPRS-EST-94-017-24"><span class="cite-bracket">[</span>24<span class="cite-bracket">]</span></a></sup></dd> <dt>AE 2100H</dt> <dd>A variant offered in 1996 for <a href="/wiki/Dassault_Aviation" title="Dassault Aviation">Dassault Aviation</a>'s proposed <a href="/wiki/Dassault_Atlantic" class="mw-redirect" title="Dassault Atlantic">Atlantic Third Generation</a> (ATL3G) <a href="/wiki/Maritime_patrol_aircraft" title="Maritime patrol aircraft">maritime patrol aircraft</a> (MPA).<sup id="cite_ref-FG19960521_25-0" class="reference"><a href="#cite_note-FG19960521-25"><span class="cite-bracket">[</span>25<span class="cite-bracket">]</span></a></sup></dd> <dt>AE 2100J</dt> <dd>A hybrid of the AE 2100A and AE 2100D3, sporting the torque-meter and interconnecting struts from the AE 2100A and the gearbox-mounted accessory gearbox from the AE 2100D3; also uses a stronger reduction gearbox, a Dowty six-bladed propeller for higher loads, and modified inlet and bypass section positioning to mitigate seawater ingestion;<sup id="cite_ref-FI19970820_26-0" class="reference"><a href="#cite_note-FI19970820-26"><span class="cite-bracket">[</span>26<span class="cite-bracket">]</span></a></sup> powers the <a href="/wiki/ShinMaywa_US-2" title="ShinMaywa US-2">ShinMaywa US-2</a>.</dd> <dt>AE 2100P</dt></dl> <ul><li><a href="/wiki/Saab_2000_AEW%26C" class="mw-redirect" title="Saab 2000 AEW&C">Saab 2000 AEW&C</a></li></ul> <dl><dt>AE 2100SD-7</dt> <dd>A variant proposed in 1994 for the European <a href="/wiki/Future_Large_Aircraft" class="mw-redirect" title="Future Large Aircraft">Future Large Aircraft</a><sup id="cite_ref-JPRS-EST-94-014-L_27-0" class="reference"><a href="#cite_note-JPRS-EST-94-014-L-27"><span class="cite-bracket">[</span>27<span class="cite-bracket">]</span></a></sup> (which eventually became the <a href="/wiki/Airbus_A400M" class="mw-redirect" title="Airbus A400M">Airbus A400M</a>), with the required power increase from 6,000 to 10,000 shp (4,500 to 7,500 kW) estimated to cost USD$600 million.<sup id="cite_ref-Interavia199410p14_28-0" class="reference"><a href="#cite_note-Interavia199410p14-28"><span class="cite-bracket">[</span>28<span class="cite-bracket">]</span></a></sup></dd></dl> <div class="mw-heading mw-heading2"><h2 id="Specifications_(AE_2100D3)"><span id="Specifications_.28AE_2100D3.29"></span>Specifications (AE 2100D3)</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Rolls-Royce_AE_2100&action=edit&section=4" title="Edit section: Specifications (AE 2100D3)"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <figure class="mw-default-size" typeof="mw:File/Thumb"><a href="/wiki/File:Rolls-Royce_AE_2100D3_turboprops_of_a_C-130J_2010.jpg" class="mw-file-description"><img src="//upload.wikimedia.org/wikipedia/commons/thumb/b/bf/Rolls-Royce_AE_2100D3_turboprops_of_a_C-130J_2010.jpg/220px-Rolls-Royce_AE_2100D3_turboprops_of_a_C-130J_2010.jpg" decoding="async" width="220" height="151" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/thumb/b/bf/Rolls-Royce_AE_2100D3_turboprops_of_a_C-130J_2010.jpg/330px-Rolls-Royce_AE_2100D3_turboprops_of_a_C-130J_2010.jpg 1.5x, //upload.wikimedia.org/wikipedia/commons/thumb/b/bf/Rolls-Royce_AE_2100D3_turboprops_of_a_C-130J_2010.jpg/440px-Rolls-Royce_AE_2100D3_turboprops_of_a_C-130J_2010.jpg 2x" data-file-width="472" data-file-height="324" /></a><figcaption>The AE 2100D3 engines of a <a href="/wiki/US_Air_Force" class="mw-redirect" title="US Air Force">US Air Force</a> C-130J Hercules ready for inspection at <a href="/wiki/Ramstein_Air_Base" title="Ramstein Air Base">Ramstein Air Base</a>, Germany</figcaption></figure> <figure class="mw-default-size mw-halign-right" typeof="mw:File/Thumb"><a href="/wiki/File:JMSDF_US-2_Rolls-Royce_AE2100J_turboprop_engine_left_side_view_at_MCAS_Iwakuni_May_5,_2019.jpg" class="mw-file-description"><img src="//upload.wikimedia.org/wikipedia/commons/thumb/d/d4/JMSDF_US-2_Rolls-Royce_AE2100J_turboprop_engine_left_side_view_at_MCAS_Iwakuni_May_5%2C_2019.jpg/220px-JMSDF_US-2_Rolls-Royce_AE2100J_turboprop_engine_left_side_view_at_MCAS_Iwakuni_May_5%2C_2019.jpg" decoding="async" width="220" height="147" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/thumb/d/d4/JMSDF_US-2_Rolls-Royce_AE2100J_turboprop_engine_left_side_view_at_MCAS_Iwakuni_May_5%2C_2019.jpg/330px-JMSDF_US-2_Rolls-Royce_AE2100J_turboprop_engine_left_side_view_at_MCAS_Iwakuni_May_5%2C_2019.jpg 1.5x, //upload.wikimedia.org/wikipedia/commons/thumb/d/d4/JMSDF_US-2_Rolls-Royce_AE2100J_turboprop_engine_left_side_view_at_MCAS_Iwakuni_May_5%2C_2019.jpg/440px-JMSDF_US-2_Rolls-Royce_AE2100J_turboprop_engine_left_side_view_at_MCAS_Iwakuni_May_5%2C_2019.jpg 2x" data-file-width="5568" data-file-height="3712" /></a><figcaption>A side view of the AE 2100J engine without its casing, on display at <a href="/wiki/Marine_Corps_Air_Station_Iwakuni" title="Marine Corps Air Station Iwakuni">Marine Corps Air Station Iwakuni</a> in 2019</figcaption></figure> <p style="font-size: 90%; margin:0; padding: .2em"><i>Data from</i> <i>FAA type certificate data sheet no. TE1CH.</i><sup id="cite_ref-FAA_TCDS_29-0" class="reference"><a href="#cite_note-FAA_TCDS-29"><span class="cite-bracket">[</span>29<span class="cite-bracket">]</span></a></sup></p> <div class="mw-heading mw-heading4"><h4 id="General_characteristics">General characteristics</h4></div> <ul><li><b>Type:</b> <a href="/wiki/Free-turbine_turboshaft" title="Free-turbine turboshaft">Free-turbine</a> <a href="/wiki/Turboprop" title="Turboprop">turboprop</a> <a href="/wiki/Aircraft_engine" title="Aircraft engine">engine</a></li> <li><b>Length:</b> 124.12 in (315.3 cm)</li> <li><b>Diameter:</b> 28.71 in (72.9 cm)</li> <li><b>Dry weight:</b> 1,740 lb (790 kg)</li></ul> <div class="mw-heading mw-heading4"><h4 id="Components">Components</h4></div> <ul><li><b>Compressor:</b> 14-stage <a href="/wiki/Axial_compressor" title="Axial compressor">axial</a></li> <li><b><a href="/wiki/Combustor" title="Combustor">Combustors</a>:</b> <a href="/wiki/Annular_combustor" class="mw-redirect" title="Annular combustor">Annular</a></li> <li><b><a href="/wiki/Turbine" title="Turbine">Turbine</a>:</b> 2-stage <a href="/wiki/Gas_generator" title="Gas generator">HP</a>, 2-stage <a href="/wiki/Free-turbine_turboshaft" title="Free-turbine turboshaft">PT</a></li></ul> <div class="mw-heading mw-heading4"><h4 id="Performance">Performance</h4></div> <ul><li><b>Maximum power output:</b> 4,637 <a href="/wiki/Horsepower#Shaft_horsepower" title="Horsepower">shp</a> (3,458 <a href="/wiki/Kilowatt" class="mw-redirect" title="Kilowatt">kW</a>)</li> <li><b><a href="/wiki/Overall_pressure_ratio" title="Overall pressure ratio">Overall pressure ratio</a>:</b> 16.6:1</li> <li><b>Air mass flow:</b> 36 lb/s (16.3 kg/s)<sup id="cite_ref-MilTech201002_16-3" class="reference"><a href="#cite_note-MilTech201002-16"><span class="cite-bracket">[</span>16<span class="cite-bracket">]</span></a></sup><sup class="reference nowrap"><span title="Pages: 83–84">: 83–84 </span></sup></li> <li><b><a href="/wiki/Thrust_specific_fuel_consumption" class="mw-redirect" title="Thrust specific fuel consumption">Specific fuel consumption</a>:</b> <i>Takeoff</i>: 0.460 lb/(hp⋅h) (0.209 kg/(hp⋅h); 0.280 kg/kWh)<sup id="cite_ref-NRC2007_30-0" class="reference"><a href="#cite_note-NRC2007-30"><span class="cite-bracket">[</span>30<span class="cite-bracket">]</span></a></sup></li> <li><b><a href="/wiki/Power-to-weight_ratio" title="Power-to-weight ratio">Power-to-weight ratio</a>:</b> 2.76 shp/lb (4.54 kW/kg)<sup id="cite_ref-HectoPressure_31-0" class="reference"><a href="#cite_note-HectoPressure-31"><span class="cite-bracket">[</span>31<span class="cite-bracket">]</span></a></sup></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=Rolls-Royce_AE_2100&action=edit&section=5" title="Edit section: See also"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <style data-mw-deduplicate="TemplateStyles:r1266661725">.mw-parser-output .portalbox{padding:0;margin:0.5em 0;display:table;box-sizing:border-box;max-width:175px;list-style:none}.mw-parser-output .portalborder{border:1px solid var(--border-color-base,#a2a9b1);padding:0.1em;background:var(--background-color-neutral-subtle,#f8f9fa)}.mw-parser-output .portalbox-entry{display:table-row;font-size:85%;line-height:110%;height:1.9em;font-style:italic;font-weight:bold}.mw-parser-output .portalbox-image{display:table-cell;padding:0.2em;vertical-align:middle;text-align:center}.mw-parser-output .portalbox-link{display:table-cell;padding:0.2em 0.2em 0.2em 0.3em;vertical-align:middle}@media(min-width:720px){.mw-parser-output .portalleft{margin:0.5em 1em 0.5em 0}.mw-parser-output .portalright{clear:right;float:right;margin:0.5em 0 0.5em 1em}}</style><ul role="navigation" aria-label="Portals" class="noprint portalbox portalborder portalright"> <li class="portalbox-entry"><span class="portalbox-image"><span class="noviewer" typeof="mw:File"><span><img alt="" src="//upload.wikimedia.org/wikipedia/commons/thumb/6/68/Aviacionavion.png/28px-Aviacionavion.png" decoding="async" width="28" height="28" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/thumb/6/68/Aviacionavion.png/42px-Aviacionavion.png 1.5x, //upload.wikimedia.org/wikipedia/commons/thumb/6/68/Aviacionavion.png/56px-Aviacionavion.png 2x" data-file-width="1600" data-file-height="1600" /></span></span></span><span class="portalbox-link"><a href="/wiki/Portal:Aviation" title="Portal:Aviation">Aviation portal</a></span></li></ul> <p> <b>Related development</b> </p> <ul><li><a href="/wiki/Allison_T56" title="Allison T56">Allison T56</a></li> <li><a href="/wiki/Rolls-Royce_AE_3007" title="Rolls-Royce AE 3007">Rolls-Royce AE 3007</a></li> <li><a href="/wiki/Rolls-Royce_T406" title="Rolls-Royce T406">Rolls-Royce T406</a></li></ul> <p> <b>Comparable engines</b> </p> <ul><li><a href="/wiki/General_Electric_GE38" title="General Electric GE38">General Electric GE38</a></li> <li><a href="/wiki/Pratt_%26_Whitney_Canada_PW150" class="mw-redirect" title="Pratt & Whitney Canada PW150">Pratt & Whitney Canada PW150</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 id="References">References</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Rolls-Royce_AE_2100&action=edit&section=6" title="Edit section: References"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <style data-mw-deduplicate="TemplateStyles:r1239543626">.mw-parser-output .reflist{margin-bottom:0.5em;list-style-type:decimal}@media screen{.mw-parser-output .reflist{font-size:90%}}.mw-parser-output .reflist .references{font-size:100%;margin-bottom:0;list-style-type:inherit}.mw-parser-output .reflist-columns-2{column-width:30em}.mw-parser-output .reflist-columns-3{column-width:25em}.mw-parser-output .reflist-columns{margin-top:0.3em}.mw-parser-output .reflist-columns ol{margin-top:0}.mw-parser-output .reflist-columns li{page-break-inside:avoid;break-inside:avoid-column}.mw-parser-output .reflist-upper-alpha{list-style-type:upper-alpha}.mw-parser-output .reflist-upper-roman{list-style-type:upper-roman}.mw-parser-output .reflist-lower-alpha{list-style-type:lower-alpha}.mw-parser-output .reflist-lower-greek{list-style-type:lower-greek}.mw-parser-output .reflist-lower-roman{list-style-type:lower-roman}</style><div class="reflist"> <div class="mw-references-wrap mw-references-columns"><ol class="references"> <li id="cite_note-2300engines-1"><span class="mw-cite-backlink"><b><a href="#cite_ref-2300engines_1-0">^</a></b></span> <span class="reference-text"><style data-mw-deduplicate="TemplateStyles:r1238218222">.mw-parser-output cite.citation{font-style:inherit;word-wrap:break-word}.mw-parser-output .citation q{quotes:"\"""\"""'""'"}.mw-parser-output .citation:target{background-color:rgba(0,127,255,0.133)}.mw-parser-output .id-lock-free.id-lock-free a{background:url("//upload.wikimedia.org/wikipedia/commons/6/65/Lock-green.svg")right 0.1em center/9px no-repeat}.mw-parser-output .id-lock-limited.id-lock-limited a,.mw-parser-output .id-lock-registration.id-lock-registration a{background:url("//upload.wikimedia.org/wikipedia/commons/d/d6/Lock-gray-alt-2.svg")right 0.1em center/9px no-repeat}.mw-parser-output .id-lock-subscription.id-lock-subscription a{background:url("//upload.wikimedia.org/wikipedia/commons/a/aa/Lock-red-alt-2.svg")right 0.1em center/9px no-repeat}.mw-parser-output .cs1-ws-icon a{background:url("//upload.wikimedia.org/wikipedia/commons/4/4c/Wikisource-logo.svg")right 0.1em center/12px no-repeat}body:not(.skin-timeless):not(.skin-minerva) .mw-parser-output .id-lock-free a,body:not(.skin-timeless):not(.skin-minerva) .mw-parser-output .id-lock-limited a,body:not(.skin-timeless):not(.skin-minerva) .mw-parser-output .id-lock-registration a,body:not(.skin-timeless):not(.skin-minerva) .mw-parser-output .id-lock-subscription a,body:not(.skin-timeless):not(.skin-minerva) .mw-parser-output .cs1-ws-icon a{background-size:contain;padding:0 1em 0 0}.mw-parser-output .cs1-code{color:inherit;background:inherit;border:none;padding:inherit}.mw-parser-output .cs1-hidden-error{display:none;color:var(--color-error,#d33)}.mw-parser-output .cs1-visible-error{color:var(--color-error,#d33)}.mw-parser-output .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 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National Academies Press. pp. 29–<a rel="nofollow" class="external text" href="https://www.nap.edu/read/11837/chapter/5#33">33</a>. <a href="/wiki/Doi_(identifier)" class="mw-redirect" title="Doi (identifier)">doi</a>:<a rel="nofollow" class="external text" href="https://doi.org/10.17226%2F11837">10.17226/11837</a>. <a href="/wiki/ISBN_(identifier)" class="mw-redirect" title="ISBN (identifier)">ISBN</a> <a href="/wiki/Special:BookSources/978-0-309-10399-2" title="Special:BookSources/978-0-309-10399-2"><bdi>978-0-309-10399-2</bdi></a>. <a href="/wiki/OCLC_(identifier)" class="mw-redirect" title="OCLC (identifier)">OCLC</a> <a rel="nofollow" class="external text" href="https://search.worldcat.org/oclc/934667552">934667552</a>.</cite><span title="ctx_ver=Z39.88-2004&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Abook&rft.genre=book&rft.btitle=Improving+the+efficiency+of+engines+for+large+nonfighter+aircraft&rft.pages=29-33&rft.pub=National+Academies+Press&rft.date=2007&rft_id=info%3Aoclcnum%2F934667552&rft_id=info%3Adoi%2F10.17226%2F11837&rft.isbn=978-0-309-10399-2&rft.au=National+Research+Council&rft_id=https%3A%2F%2Fwww.nap.edu%2Fread%2F11837%2Fchapter%2F5%2329&rfr_id=info%3Asid%2Fen.wikipedia.org%3ARolls-Royce+AE+2100" class="Z3988"></span></span> </li> <li id="cite_note-HectoPressure-31"><span class="mw-cite-backlink"><b><a href="#cite_ref-HectoPressure_31-0">^</a></b></span> <span class="reference-text"><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1238218222" /><cite id="CITEREFKaiserDonnerhackLundbladhSeitz2015" class="citation conference cs1">Kaiser, Sascha; Donnerhack, Stefan; Lundbladh, Anders; Seitz, Arne (27–29 July 2015). "A composite cycle engine concept with hecto-pressure ratio". <i>51st AIAA/SAE/ASEE Joint Propulsion Conference</i>. AIAA/SAE/ASEE Joint Propulsion Conference (51st ed.). <a href="/wiki/Doi_(identifier)" class="mw-redirect" title="Doi (identifier)">doi</a>:<a rel="nofollow" class="external text" href="https://doi.org/10.2514%2F6.2015-4028">10.2514/6.2015-4028</a>. <a href="/wiki/ISBN_(identifier)" class="mw-redirect" title="ISBN (identifier)">ISBN</a> <a href="/wiki/Special:BookSources/978-1-62410-321-6" title="Special:BookSources/978-1-62410-321-6"><bdi>978-1-62410-321-6</bdi></a>.</cite><span title="ctx_ver=Z39.88-2004&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Abook&rft.genre=conference&rft.atitle=A+composite+cycle+engine+concept+with+hecto-pressure+ratio&rft.btitle=51st+AIAA%2FSAE%2FASEE+Joint+Propulsion+Conference&rft.edition=51st&rft.date=2015-07-27%2F2015-07-29&rft_id=info%3Adoi%2F10.2514%2F6.2015-4028&rft.isbn=978-1-62410-321-6&rft.aulast=Kaiser&rft.aufirst=Sascha&rft.au=Donnerhack%2C+Stefan&rft.au=Lundbladh%2C+Anders&rft.au=Seitz%2C+Arne&rfr_id=info%3Asid%2Fen.wikipedia.org%3ARolls-Royce+AE+2100" class="Z3988"></span></span> </li> </ol></div></div> <div class="mw-heading mw-heading2"><h2 id="Bibliography">Bibliography</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a href="/w/index.php?title=Rolls-Royce_AE_2100&action=edit&section=7" title="Edit section: Bibliography"><span>edit</span></a><span class="mw-editsection-bracket">]</span></span></div> <style data-mw-deduplicate="TemplateStyles:r1239549316">.mw-parser-output .refbegin{margin-bottom:0.5em}.mw-parser-output .refbegin-hanging-indents>ul{margin-left:0}.mw-parser-output .refbegin-hanging-indents>ul>li{margin-left:0;padding-left:3.2em;text-indent:-3.2em}.mw-parser-output .refbegin-hanging-indents ul,.mw-parser-output .refbegin-hanging-indents ul li{list-style:none}@media(max-width:720px){.mw-parser-output .refbegin-hanging-indents>ul>li{padding-left:1.6em;text-indent:-1.6em}}.mw-parser-output .refbegin-columns{margin-top:0.3em}.mw-parser-output .refbegin-columns ul{margin-top:0}.mw-parser-output .refbegin-columns li{page-break-inside:avoid;break-inside:avoid-column}@media screen{.mw-parser-output .refbegin{font-size:90%}}</style><div class="refbegin" style=""> <ul><li><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1238218222" /><cite id="CITEREFLeyes_IIWilliam_A._Fleming1999" class="citation book cs1">Leyes II, Richard A.; William A. Fleming (1999). <a rel="nofollow" class="external text" href="https://books.google.com/books?id=V0SnFt8JGokC&pg=frontcover"><i>The History of North American Small Gas Turbine Aircraft Engines</i></a>. Washington, DC: Smithsonian Institution. <a href="/wiki/ISBN_(identifier)" class="mw-redirect" title="ISBN (identifier)">ISBN</a> <a href="/wiki/Special:BookSources/1-56347-332-1" title="Special:BookSources/1-56347-332-1"><bdi>1-56347-332-1</bdi></a>. <a href="/wiki/OCLC_(identifier)" class="mw-redirect" title="OCLC (identifier)">OCLC</a> <a rel="nofollow" class="external text" href="https://search.worldcat.org/oclc/247550535">247550535</a>.</cite><span title="ctx_ver=Z39.88-2004&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Abook&rft.genre=book&rft.btitle=The+History+of+North+American+Small+Gas+Turbine+Aircraft+Engines&rft.place=Washington%2C+DC&rft.pub=Smithsonian+Institution&rft.date=1999&rft_id=info%3Aoclcnum%2F247550535&rft.isbn=1-56347-332-1&rft.aulast=Leyes+II&rft.aufirst=Richard+A.&rft.au=William+A.+Fleming&rft_id=https%3A%2F%2Fbooks.google.com%2Fbooks%3Fid%3DV0SnFt8JGokC%26pg%3Dfrontcover&rfr_id=info%3Asid%2Fen.wikipedia.org%3ARolls-Royce+AE+2100" class="Z3988"></span></li> <li><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1238218222" /><cite id="CITEREFMoxonWinnElliottBarrie1991" class="citation magazine cs1">Moxon, Julian; Winn, Allan; Elliott, Simon; Barrie, Douglas (11 December 1991). "Quiet revolution". <i><a href="/wiki/Flight_International" title="Flight International">Flight International</a></i>. Vol. 140, no. 4297. pp. S10+. <a href="/wiki/ISSN_(identifier)" class="mw-redirect" title="ISSN (identifier)">ISSN</a> <a rel="nofollow" class="external text" href="https://search.worldcat.org/issn/0015-3710">0015-3710</a>. <link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1238218222" /><a href="/wiki/Gale_(identifier)" class="mw-redirect" title="Gale (identifier)">Gale</a> <a rel="nofollow" class="external text" href="https://go.gale.com/ps/anonymous?id=GALE%7CA11714309">A11714309</a>.</cite><span title="ctx_ver=Z39.88-2004&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.jtitle=Flight+International&rft.atitle=Quiet+revolution&rft.volume=140&rft.issue=4297&rft.pages=S10%2B&rft.date=1991-12-11&rft.issn=0015-3710&rft.aulast=Moxon&rft.aufirst=Julian&rft.au=Winn%2C+Allan&rft.au=Elliott%2C+Simon&rft.au=Barrie%2C+Douglas&rfr_id=info%3Asid%2Fen.wikipedia.org%3ARolls-Royce+AE+2100" class="Z3988"></span></li> <li><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1238218222" /><cite id="CITEREFKandebo1990" class="citation magazine cs1">Kandebo, Stanley W. (19 February 1990). <span class="id-lock-subscription" title="Paid subscription required"><a rel="nofollow" class="external text" href="https://archive.aviationweek.com/issue/19900219/#!&pid=36">"Allison plans flight tests of turboprop GMA 2100"</a></span>. Cover story. <i><a href="/wiki/Aviation_Week_%26_Space_Technology" title="Aviation Week & Space Technology">Aviation Week & Space Technology</a></i>. Vol. 132, no. 8. pp. <span class="nowrap">36–</span>38. <a href="/wiki/ISSN_(identifier)" class="mw-redirect" title="ISSN (identifier)">ISSN</a> <a rel="nofollow" class="external text" href="https://search.worldcat.org/issn/0005-2175">0005-2175</a>.</cite><span title="ctx_ver=Z39.88-2004&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.jtitle=Aviation+Week+%26+Space+Technology&rft.atitle=Allison+plans+flight+tests+of+turboprop+GMA+2100&rft.volume=132&rft.issue=8&rft.pages=%3Cspan+class%3D%22nowrap%22%3E36-%3C%2Fspan%3E38&rft.date=1990-02-19&rft.issn=0005-2175&rft.aulast=Kandebo&rft.aufirst=Stanley+W.&rft_id=https%3A%2F%2Farchive.aviationweek.com%2Fissue%2F19900219%2F%23%21%26pid%3D36&rfr_id=info%3Asid%2Fen.wikipedia.org%3ARolls-Royce+AE+2100" class="Z3988"></span></li></ul> </div> <div class="mw-heading mw-heading2"><h2 id="External_links">External links</h2><span class="mw-editsection"><span class="mw-editsection-bracket">[</span><a 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style="width:1px;padding:0 0 0 2px"><div><span typeof="mw:File"><a href="/wiki/File:Allison_engines_logo.png" class="mw-file-description"><img src="//upload.wikimedia.org/wikipedia/commons/thumb/6/6f/Allison_engines_logo.png/120px-Allison_engines_logo.png" decoding="async" width="120" height="46" class="mw-file-element" srcset="//upload.wikimedia.org/wikipedia/commons/thumb/6/6f/Allison_engines_logo.png/180px-Allison_engines_logo.png 1.5x, //upload.wikimedia.org/wikipedia/commons/thumb/6/6f/Allison_engines_logo.png/240px-Allison_engines_logo.png 2x" data-file-width="306" data-file-height="118" /></a></span></div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Turbojet" title="Turbojet">Turbojets</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="/wiki/Allison_J33" title="Allison J33">J33</a></li> <li><a href="/wiki/Allison_J35" title="Allison J35">J35</a></li> <li><a href="/wiki/Allison_J71" title="Allison J71">J71</a></li> <li><a href="/wiki/Allison_J102" title="Allison J102">J102</a></li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Turbofan" title="Turbofan">Turbofans</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/Rolls-Royce_AE_3007" title="Rolls-Royce AE 3007">AE 3007</a></li> <li><a href="/wiki/Rolls-Royce_Spey" title="Rolls-Royce Spey">AR.168R</a>†</li> <li><a href="/wiki/Allison_TF32" title="Allison TF32">TF32</a></li> <li><a href="/wiki/Allison_TF41" title="Allison TF41">TF41</a></li> <li><a href="/wiki/General_Electric/Rolls-Royce_F136" title="General Electric/Rolls-Royce F136">F136</a>†</li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Turboprop" title="Turboprop">Turboprops</a>/<a href="/wiki/Turboshaft" title="Turboshaft">Turboshafts</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="/wiki/Allison_Model_250" title="Allison Model 250">250/T63</a></li> <li><a class="mw-selflink selflink">AE 2100</a></li> <li><a href="/wiki/Allison_T38" title="Allison T38">T38</a></li> <li><a href="/wiki/Allison_T38" title="Allison T38">T39</a></li> <li><a href="/wiki/Allison_T40" title="Allison T40">T40</a></li> <li><a href="/wiki/Allison_T40" title="Allison T40">T44</a></li> <li><a href="/wiki/Allison_T40" title="Allison T40">T54</a></li> <li><a href="/wiki/Allison_T56" title="Allison T56">T56</a> (<a href="/wiki/Allison_T56_variants" title="Allison T56 variants">variants</a>)</li> <li><a href="/wiki/Allison_T61" title="Allison T61">T61</a></li> <li><a href="/wiki/Allison_T78" title="Allison T78">T78</a></li> <li><a href="/wiki/Rolls-Royce_T406" title="Rolls-Royce T406">T406</a></li> <li><a href="/wiki/Allison_T701" class="mw-redirect" title="Allison T701">T701</a></li> <li><a href="/wiki/LHTEC_T800" title="LHTEC T800">T800</a>†</li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Propfan" title="Propfan">Propfan</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/Pratt_%26_Whitney/Allison_578-DX" title="Pratt & Whitney/Allison 578-DX">578-DX</a>†</li></ul> </div></td></tr><tr><td class="navbox-abovebelow" colspan="3"><div>† <a href="/wiki/Template:Joint_development_aeroengines" title="Template:Joint development aeroengines">Joint development aeroengines</a></div></td></tr></tbody></table></div> <div class="navbox-styles"><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1129693374" /><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1236075235" /></div><div role="navigation" class="navbox" aria-labelledby="Rolls-Royce_Holdings_aero_engines_and_aircraft483" style="padding:3px"><table class="nowraplinks hlist mw-collapsible autocollapse navbox-inner" style="border-spacing:0;background:transparent;color:inherit"><tbody><tr><th scope="col" class="navbox-title" colspan="2"><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1129693374" /><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1239400231" /><div class="navbar plainlinks hlist navbar-mini"><ul><li class="nv-view"><a href="/wiki/Template:Rolls-Royce_plc_aeroengines" title="Template:Rolls-Royce plc aeroengines"><abbr title="View this template">v</abbr></a></li><li class="nv-talk"><a href="/wiki/Template_talk:Rolls-Royce_plc_aeroengines" title="Template talk:Rolls-Royce plc aeroengines"><abbr title="Discuss this template">t</abbr></a></li><li class="nv-edit"><a href="/wiki/Special:EditPage/Template:Rolls-Royce_plc_aeroengines" title="Special:EditPage/Template:Rolls-Royce plc aeroengines"><abbr title="Edit this template">e</abbr></a></li></ul></div><div id="Rolls-Royce_Holdings_aero_engines_and_aircraft483" style="font-size:114%;margin:0 4em"><a href="/wiki/Rolls-Royce_Holdings" title="Rolls-Royce Holdings">Rolls-Royce Holdings</a> <a href="/wiki/Aircraft_engines" class="mw-redirect" title="Aircraft engines">aero engines</a> and aircraft</div></th></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Turbofan" title="Turbofan">Turbofans</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="/w/index.php?title=Rolls-Royce_Advance_2&action=edit&redlink=1" class="new" title="Rolls-Royce Advance 2 (page does not exist)">Advance 2</a></li> <li><a href="/w/index.php?title=Rolls-Royce_Advance_3&action=edit&redlink=1" class="new" title="Rolls-Royce Advance 3 (page does not exist)">Advance 3</a></li> <li><a href="/wiki/Rolls-Royce_AE_3007" title="Rolls-Royce AE 3007">AE 3007</a>†</li> <li><a href="/wiki/Rolls-Royce_BR700" title="Rolls-Royce BR700">BR700</a>‡</li> <li><a href="/wiki/Eurojet_EJ200" title="Eurojet EJ200">EJ200</a>‡</li> <li><a href="/wiki/General_Electric/Rolls-Royce_F136" title="General Electric/Rolls-Royce F136">F136</a>‡</li> <li><a href="/wiki/Rolls-Royce_RB.183_Tay" title="Rolls-Royce RB.183 Tay">RB183</a></li> <li><a href="/wiki/Rolls-Royce_RB282" title="Rolls-Royce RB282">RB282</a></li> <li><a href="/wiki/Rolls-Royce_RB401" title="Rolls-Royce RB401">RB401</a></li> <li><a href="/wiki/Rolls-Royce/JAEC_RJ500" title="Rolls-Royce/JAEC RJ500">RJ500</a>‡</li> <li><a href="/wiki/Rolls-Royce_RB.183_Tay" title="Rolls-Royce RB.183 Tay">Spey Junior</a></li> <li><a href="/wiki/Rolls-Royce_RB.183_Tay" title="Rolls-Royce RB.183 Tay">Tay</a></li> <li><a href="/wiki/Rolls-Royce_Trent" title="Rolls-Royce Trent">Trent series</a> (<a href="/wiki/Rolls-Royce_Trent_500" title="Rolls-Royce Trent 500">Trent 500</a></li> <li><a href="/wiki/Rolls-Royce_Trent_700" title="Rolls-Royce Trent 700">Trent 700</a></li> <li><a href="/wiki/Rolls-Royce_Trent_800" title="Rolls-Royce Trent 800">Trent 800</a></li> <li><a href="/wiki/Rolls-Royce_Trent_900" title="Rolls-Royce Trent 900">Trent 900</a></li> <li><a href="/wiki/Rolls-Royce_Trent_1000" title="Rolls-Royce Trent 1000">Trent 1000</a></li> <li><a href="/wiki/Rolls-Royce_Trent_XWB" title="Rolls-Royce Trent XWB">Trent XWB</a></li> <li><a href="/wiki/Rolls-Royce_Trent_7000" title="Rolls-Royce Trent 7000">Trent 7000</a>)</li> <li><a href="/wiki/IAE_V2500" title="IAE V2500">V2500</a>‡</li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Turboprop" title="Turboprop">Turboprops</a>/<a href="/wiki/Turboshaft" title="Turboshaft">Turboshafts</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="/wiki/Allison_T56" title="Allison T56">501</a> (<a href="/wiki/Allison_T56_variants" title="Allison T56 variants">variants</a>)†</li> <li><a class="mw-selflink selflink">AE 2100</a>†</li> <li><a href="/wiki/Allison_Model_250" title="Allison Model 250">M250</a>†</li> <li><a href="/wiki/MTR_MTR390" title="MTR MTR390">MTR390</a>‡</li> <li><a href="/wiki/Rolls-Royce_RR300" title="Rolls-Royce RR300">RR300</a></li> <li><a href="/wiki/Rolls-Royce_RR500" title="Rolls-Royce RR500">RR500</a></li> <li><a href="/wiki/Allison_T56" title="Allison T56">T56</a>†</li> <li><a href="/wiki/Rolls-Royce_T406" title="Rolls-Royce T406">T406</a>†</li> <li><a href="/wiki/LHTEC_T800" title="LHTEC T800">T800</a>‡</li> <li><a href="/wiki/Europrop_TP400" title="Europrop TP400">TP400</a>‡</li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%">Other fan-type engines</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/Rolls-Royce_RB529_Contrafan" title="Rolls-Royce RB529 Contrafan">RB529</a></li> <li><a href="/wiki/Rolls-Royce_RB3011" title="Rolls-Royce RB3011">RB2011</a></li> <li><a href="/wiki/Rolls-Royce_RB3011" title="Rolls-Royce RB3011">RB3011</a></li> <li><a href="/wiki/Rolls-Royce_LiftSystem" title="Rolls-Royce LiftSystem">LiftSystem</a></li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%">Aero-derivative industrial <br />and marine <a href="/wiki/Gas_turbine" title="Gas turbine">gas turbines</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="/wiki/Rolls-Royce_MT30" title="Rolls-Royce MT30">MT30</a></li> <li><a href="/wiki/Rolls-Royce_T406" title="Rolls-Royce T406">MT7</a></li> <li><a href="/wiki/Rolls-Royce_WR-21" title="Rolls-Royce WR-21">WR-21</a>‡</li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%">Aircraft</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/Rolls-Royce_ACCEL" title="Rolls-Royce ACCEL">ACCEL</a></li></ul> </div></td></tr><tr><td class="navbox-abovebelow" colspan="2"><div> <ul><li>Symbol † indicates <a href="/wiki/Allison_Engine_Company" title="Allison Engine Company">Allison</a> engines</li> <li>Symbol ‡ indicates <a href="/wiki/Template:Joint_development_aeroengines" title="Template:Joint development aeroengines">Joint development aero engines</a></li> <li>See also <a href="/wiki/Template:Rolls-Royce_aeroengines" title="Template:Rolls-Royce aeroengines">Rolls-Royce Limited aero engines</a> and <a href="/wiki/Rolls-Royce_Heritage_Trust" title="Rolls-Royce Heritage Trust">Rolls-Royce Heritage Trust</a></li></ul> </div></td></tr></tbody></table></div> <div class="navbox-styles"><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1129693374" /><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1236075235" /></div><div role="navigation" class="navbox" aria-labelledby="United_States_military_gas_turbine_aircraft_engine_designation_system251" style="padding:3px"><table class="nowraplinks mw-collapsible autocollapse navbox-inner" style="border-spacing:0;background:transparent;color:inherit"><tbody><tr><th scope="col" class="navbox-title" colspan="2"><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1129693374" /><link rel="mw-deduplicated-inline-style" href="mw-data:TemplateStyles:r1239400231" /><div class="navbar plainlinks hlist navbar-mini"><ul><li class="nv-view"><a href="/wiki/Template:US_military_gas_turbine_aeroengines" title="Template:US military gas turbine aeroengines"><abbr title="View this template">v</abbr></a></li><li class="nv-talk"><a href="/wiki/Template_talk:US_military_gas_turbine_aeroengines" title="Template talk:US military gas turbine aeroengines"><abbr title="Discuss this template">t</abbr></a></li><li class="nv-edit"><a href="/wiki/Special:EditPage/Template:US_military_gas_turbine_aeroengines" title="Special:EditPage/Template:US military gas turbine aeroengines"><abbr title="Edit this template">e</abbr></a></li></ul></div><div id="United_States_military_gas_turbine_aircraft_engine_designation_system251" style="font-size:114%;margin:0 4em"><a href="/wiki/United_States_Department_of_Defense" title="United States Department of Defense">United States military</a> gas turbine aircraft engine <a href="/wiki/United_States_military_aircraft_engine_designations" title="United States military aircraft engine designations">designation system</a></div></th></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Turbojet" title="Turbojet">Turbojets</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/Westinghouse_J30" title="Westinghouse J30">J30</a></li> <li><a href="/wiki/General_Electric_J31" title="General Electric J31">J31</a></li> <li><a href="/wiki/Westinghouse_J32" title="Westinghouse J32">J32</a></li> <li><a href="/wiki/Allison_J33" title="Allison J33">J33</a></li> <li><a href="/wiki/Westinghouse_J34" title="Westinghouse J34">J34</a></li> <li><a href="/wiki/Allison_J35" title="Allison J35">J35</a></li> <li><a href="/wiki/De_Havilland_Goblin" title="De Havilland Goblin">J36</a></li> <li><a href="/wiki/Lockheed_J37" title="Lockheed J37">J37</a></li> <li><a href="/wiki/West_Engineering_XJ38" title="West Engineering XJ38">XJ38</a></li> <li><a href="/wiki/General_Electric_J31" title="General Electric J31">J39</a></li> <li><a href="/wiki/Westinghouse_J40" title="Westinghouse J40">J40</a></li> <li><a href="/wiki/Packard_XJ41" title="Packard XJ41">XJ41</a></li> <li><a href="/wiki/Rolls-Royce_Nene" title="Rolls-Royce Nene">J42</a></li> <li><a href="/wiki/Westinghouse_J30" title="Westinghouse J30">J43</a></li> <li><a href="/wiki/Fairchild_J44" title="Fairchild J44">J44</a></li> <li><a href="/wiki/Westinghouse_J34" title="Westinghouse J34">J45</a></li> <li><a href="/wiki/Westinghouse_J46" title="Westinghouse J46">J46</a></li> <li><a href="/wiki/General_Electric_J47" title="General Electric J47">J47</a></li> <li><a href="/wiki/Pratt_%26_Whitney_J48" title="Pratt & Whitney J48">J48</a></li> <li><a href="/wiki/Packard_XJ49" title="Packard XJ49">XJ49</a></li> <li><a href="/w/index.php?title=Wright_J51&action=edit&redlink=1" class="new" title="Wright J51 (page does not exist)">J51</a></li> <li><a href="/wiki/Pratt_%26_Whitney_J52" title="Pratt & Whitney J52">J52</a></li> <li><a href="/w/index.php?title=General_Electric_J53&action=edit&redlink=1" class="new" title="General Electric J53 (page does not exist)">J53</a></li> <li><a href="/wiki/Rolls-Royce_Avon" title="Rolls-Royce Avon">J54</a></li> <li><a href="/wiki/Flader_J55" title="Flader J55">J55</a></li> <li><a href="/w/index.php?title=Allison_J56&action=edit&redlink=1" class="new" title="Allison J56 (page does not exist)">J56</a></li> <li><a href="/wiki/Pratt_%26_Whitney_J57" title="Pratt & Whitney J57">J57</a></li> <li><a href="/wiki/Pratt_%26_Whitney_J58" title="Pratt & Whitney J58">J58</a></li> <li><a href="/w/index.php?title=Wright_J59&action=edit&redlink=1" class="new" title="Wright J59 (page does not exist)">J59</a></li> <li><a href="/wiki/Pratt_%26_Whitney_JT12" title="Pratt & Whitney JT12">J60</a></li> <li><a href="/w/index.php?title=Wright_J61&action=edit&redlink=1" class="new" title="Wright J61 (page does not exist)">J61</a></li> <li><a href="/w/index.php?title=Fairchild_J63&action=edit&redlink=1" class="new" title="Fairchild J63 (page does not exist)">J63</a></li> <li><a href="/wiki/Wright_J65" title="Wright J65">J65</a></li> <li><a href="/wiki/Rolls-Royce_Olympus" title="Rolls-Royce Olympus">J67</a></li> <li><a href="/wiki/Teledyne_CAE_J69" title="Teledyne CAE J69">J69</a></li> <li><a href="/wiki/Allison_J71" title="Allison J71">J71</a></li> <li><a href="/wiki/General_Electric_J73" title="General Electric J73">J73</a></li> <li><a href="/wiki/Pratt_%26_Whitney_J75" title="Pratt & Whitney J75">J75</a></li> <li><a href="/wiki/General_Electric_J79" title="General Electric J79">J79</a></li> <li><a href="/wiki/Rolls-Royce_Soar" title="Rolls-Royce Soar">J81</a></li> <li><a href="/wiki/Fairchild_J83" title="Fairchild J83">J83</a></li> <li><a href="/wiki/General_Electric_J85" title="General Electric J85">J85</a></li> <li><a href="/wiki/General_Electric_J87" title="General Electric J87">J87</a></li> <li><a href="/w/index.php?title=Allison_J89&action=edit&redlink=1" class="new" title="Allison J89 (page does not exist)">J89</a></li> <li><a href="/w/index.php?title=Pratt_%26_Whitney_J91&action=edit&redlink=1" class="new" title="Pratt & Whitney J91 (page does not exist)">J91</a></li> <li><a href="/wiki/General_Electric_YJ93" title="General Electric YJ93">YJ93</a></li> <li><a href="/w/index.php?title=Teledyne_LJ95&action=edit&redlink=1" class="new" title="Teledyne LJ95 (page does not exist)">J95</a></li> <li><a href="/wiki/General_Electric_J97" title="General Electric J97">J97</a></li> <li><a href="/w/index.php?title=Rolls-Royce_J99&action=edit&redlink=1" class="new" title="Rolls-Royce J99 (page does not exist)">J99</a></li> <li><a href="/wiki/Teledyne_CAE_J69" title="Teledyne CAE J69">J100</a></li> <li><a href="/wiki/General_Electric_YJ101" title="General Electric YJ101">YJ101</a></li> <li><a href="/wiki/Allison_J102" title="Allison J102">J102</a></li></ul> <ul><li><a href="/wiki/Williams_J400" title="Williams J400">J400</a></li> <li><a href="/w/index.php?title=Garrett_J401&action=edit&redlink=1" class="new" title="Garrett J401 (page does not exist)">J401</a></li> <li><a href="/wiki/Teledyne_CAE_J402" title="Teledyne CAE J402">J402</a></li> <li><a href="/wiki/Microturbo_TRI_60" title="Microturbo TRI 60">J403</a></li></ul> <ul><li><a href="/wiki/Teledyne_CAE_J700" title="Teledyne CAE J700">J700</a></li></ul> </div></td></tr><tr><th scope="row" class="navbox-group" style="width:1%"><a href="/wiki/Turboprop" title="Turboprop">Turboprops</a>/<br /><a href="/wiki/Turboshaft" title="Turboshaft">Turboshafts</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="/wiki/Westinghouse_T30" class="mw-redirect" title="Westinghouse T30">T30</a></li> <li><a href="/wiki/General_Electric_T31" title="General Electric T31">T31</a></li> <li><a href="/wiki/Flader_J55" title="Flader J55">T33</a></li> <li><a href="/wiki/Pratt_%26_Whitney_T34" title="Pratt & Whitney T34">T34</a></li> <li><a href="/wiki/Lockheed_J37" title="Lockheed J37">T35</a></li> <li><a href="/wiki/Chrysler_T36D" title="Chrysler T36D">T36</a></li> <li><a href="/wiki/Northrop-Hendy_XT37" title="Northrop-Hendy XT37">T37</a></li> <li><a href="/wiki/Allison_T38" title="Allison T38">T38</a></li> <li><a href="/wiki/Allison_T38" title="Allison T38">T39</a></li> <li><a href="/wiki/Allison_T40" title="Allison T40">T40</a></li> <li><a href="/wiki/General_Electric_T31" title="General Electric T31">T41</a></li> <li><a href="/w/index.php?title=De_Laval_T42&action=edit&redlink=1" class="new" title="De Laval T42 (page does not exist)">T42</a></li> <li><a href="/w/index.php?title=Wright_T43&action=edit&redlink=1" class="new" title="Wright T43 (page does not exist)">T43</a></li> <li><a href="/wiki/Allison_T40" title="Allison T40">T44</a></li> <li><a href="/w/index.php?title=Pratt_%26_Whitney_T45&action=edit&redlink=1" class="new" title="Pratt & Whitney T45 (page does not exist)">T45</a></li> <li><a href="/wiki/Fairchild_T46" class="mw-redirect" title="Fairchild T46">T46</a></li> <li><a href="/wiki/Wright_T47" class="mw-redirect" title="Wright T47">T47</a></li> <li><a href="/w/index.php?title=Pratt_%26_Whitney_T48&action=edit&redlink=1" class="new" title="Pratt & Whitney T48 (page does not exist)">T48</a></li> <li><a href="/wiki/Wright_T49" class="mw-redirect" title="Wright T49">T49</a></li> <li><a href="/wiki/Boeing_T50" title="Boeing T50">T50</a></li> <li><a href="/wiki/Continental_T51" title="Continental T51">T51</a></li> <li><a href="/w/index.php?title=Pratt_%26_Whitney_T52&action=edit&redlink=1" class="new" title="Pratt & Whitney T52 (page does not exist)">T52</a></li> <li><a href="/wiki/Lycoming_T53" title="Lycoming T53">T53</a></li> <li><a href="/wiki/Allison_T40" title="Allison T40">T54</a></li> <li><a href="/wiki/Honeywell_T55" title="Honeywell T55">T55</a></li> <li><a href="/wiki/Allison_T56" title="Allison T56">T56</a> (<a href="/wiki/Allison_T56_variants" title="Allison T56 variants">variants</a>)</li> <li><a href="/wiki/Pratt_%26_Whitney_XT57" title="Pratt & Whitney XT57">T57</a></li> <li><a href="/wiki/General_Electric_T58" title="General Electric T58">T58</a></li> <li><a href="/wiki/Boeing_T60" title="Boeing T60">T60</a></li> <li><a href="/wiki/Allison_T61" title="Allison T61">T61</a></li> <li><a href="/wiki/Solar_T62" title="Solar T62">T62</a></li> <li><a href="/wiki/Allison_Model_250" title="Allison Model 250">T63</a></li> <li><a href="/wiki/General_Electric_T64" title="General Electric T64">T64</a></li> <li><a href="/wiki/Continental_T51" title="Continental T51">T65</a></li> <li><a href="/wiki/Solar_T62" title="Solar T62">T66</a></li> <li><a href="/wiki/Continental_T51" title="Continental T51">T67</a></li> <li><a href="/w/index.php?title=Rolls-Royce_T68&action=edit&redlink=1" class="new" title="Rolls-Royce T68 (page does not exist)">T68</a></li> <li><a href="/w/index.php?title=Teledyne_CAE_T69&action=edit&redlink=1" class="new" title="Teledyne CAE T69 (page does not exist)">T69</a></li> <li><a href="/wiki/Westinghouse_T70" class="mw-redirect" title="Westinghouse T70">T70</a></li> <li><a href="/w/index.php?title=Allison_T71&action=edit&redlink=1" class="new" title="Allison T71 (page does not exist)">T71</a></li> <li><a href="/wiki/Continental_T51" title="Continental T51">T72</a></li> <li><a href="/wiki/Pratt_%26_Whitney_JT12" title="Pratt & Whitney JT12">T73</a></li> <li><a href="/wiki/Pratt_%26_Whitney_Canada_PT6" title="Pratt & Whitney Canada PT6">T74</a></li> <li><a href="/wiki/Garrett_TPE331" class="mw-redirect" title="Garrett TPE331">T76</a></li> <li><a href="/wiki/Allison_T78" title="Allison T78">T78</a></li> <li><a href="/w/index.php?title=Allison_T80&action=edit&redlink=1" class="new" title="Allison T80 (page does not exist)">T80</a></li></ul> <ul><li><a href="/w/index.php?title=Sunstrand_T100&action=edit&redlink=1" class="new" title="Sunstrand T100 (page does not exist)">T100</a></li> <li><a href="/wiki/Pratt_%26_Whitney_Canada_PT6#PT6A" title="Pratt & Whitney Canada PT6">T101</a></li></ul> <ul><li><a href="/wiki/Pratt_%26_Whitney_Canada_PT6T" title="Pratt & 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href="/wiki/Williams_F107" title="Williams F107">F107</a></li> <li><a href="/wiki/CFM_International_CFM56" title="CFM International CFM56">F108</a></li> <li><a href="/wiki/Garrett_F109" title="Garrett F109">F109</a></li> <li><a href="/wiki/General_Electric_F110" title="General Electric F110">F110</a></li> <li><a href="/wiki/Williams_F112" title="Williams F112">F112</a></li> <li><a href="/wiki/Rolls-Royce_Spey" title="Rolls-Royce Spey">F113</a></li> <li><a href="/wiki/Pratt_%26_Whitney_PW2000" title="Pratt & Whitney PW2000">F117</a></li> <li><a href="/wiki/General_Electric_F118" title="General Electric F118">F118</a></li> <li><a href="/wiki/Pratt_%26_Whitney_F119" title="Pratt & Whitney F119">F119</a></li> <li><a href="/wiki/General_Electric_YF120" title="General Electric YF120">YF120</a></li> <li><a href="/wiki/Williams_F121" title="Williams F121">F121</a></li> <li><a href="/wiki/Williams_F122" class="mw-redirect" title="Williams F122">F122</a></li> <li><a href="/wiki/Honeywell/ITEC_F124" title="Honeywell/ITEC F124">F124</a></li> <li><a href="/wiki/Honeywell/ITEC_F124" title="Honeywell/ITEC F124">F125</a></li> <li><a href="/wiki/Rolls-Royce_RB.183_Tay" title="Rolls-Royce RB.183 Tay">F126</a></li> <li><a href="/wiki/General_Electric_F404" title="General Electric F404">F127</a></li> <li><a href="/wiki/General_Electric_F404" title="General Electric F404">F128</a></li> <li><a href="/wiki/Williams_FJ44" title="Williams FJ44">F129</a></li> <li><a href="/wiki/Rolls-Royce_BR700" title="Rolls-Royce BR700">F130</a></li> <li><a href="/wiki/Pratt_%26_Whitney_F135" title="Pratt & Whitney F135">F135</a></li> <li><a href="/wiki/General_Electric/Rolls-Royce_F136" title="General Electric/Rolls-Royce F136">F136</a></li> <li><a href="/wiki/Rolls-Royce_AE_3007" title="Rolls-Royce AE 3007">F137</a></li> <li><a href="/wiki/General_Electric_CF6" title="General Electric CF6">F138</a></li></ul> <ul><li><a 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