{{Short description|Turbofan engine}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{infobox aero engine |name= PW800 |image= File:PW800.png |caption= |engine_type= Turbofan |national_origin= Canada |manufacturer= Pratt & Whitney Canada |first_run= April 2012 |major_applications= {{ubl | Gulfstream G400/G500/G600 | Dassault Falcon 6X }}
|produced= |number_built= |developed_from= |variants_with_their_own_articles= }}
The '''Pratt & Whitney Canada PW800''' is a series of turbofan engines in the {{convert|10,000|-|20,000|lbf|kN|abbr=on}} thrust class, manufactured by Pratt & Whitney Canada. Intended for the regional jet and business jet market, the gear-less PW800 shares a common core with the larger, geared PW1000G. The first variants were certified on February 15, 2015, to power the new Gulfstream G500/G600. A later variant was certified in 2021 for the Dassault Falcon 6X.
== Development ==
The development of the PW800 stretches back to demonstration projects in 1999, soon after the development of the PW600 very light engine and the PW300 business jet engine.<ref>{{cite news |author= Guy Norris |url= http://aviationweek.com/awin/five-engine-companies-chase-same-bizjet-market-changes-are-underway |title= Five Engine Companies Chase The Same Bizjet Market, But Changes Are Underway |journal= Aviation Week & Space Technology |date= 6 Oct 2008}}{{subscription required}}</ref> After the Advanced Technology Fan Integrator demonstrator first ran on March 17, 2001, which became the PW1000G, Pratt & Whitney Canada was searching for a launch customer for the initially geared PW800, in the {{convert|10,000|-|19,000|lbf|kN|abbr=on}} thrust range, bridging the gap between P&WC's PW300 and P&W's PW6000, intended for the regional- and business-jet engine market.<ref>{{cite news |url= https://www.flightglobal.com/news/articles/pratt-whitney-canadas-geared-turbofan-seeks-launc-128579/ |title= Pratt & Whitney Canada's geared turbofan seeks launch customer |work= Flight Global |date= 10 April 2001}}</ref>
The PW800 core was to be the basis for the Pratt & Whitney Canada '''PW180''', a {{convert|12000|hp|kW|adj=pre|shaft|abbr=off}} turboprop engine proposed for the Airbus A400M Atlas.<ref>{{cite magazine |title=Profit margins in A400M engine program will be thin, official says |date=8 May 2003 |page=5 |magazine=Aerospace Daily |volume=206 |number=28 |given1=John |surname1=Fricker |given2=Rich |surname2=Tuttle |issn=0193-4546}}</ref> However the Europrop TP400 was selected instead.<ref>{{cite news |url= https://www.flightglobal.com/news/articles/usa-blasts-a400m-engine-choice-165396/ |title= USA blasts A400M engine choice |work= Flight International |date= 13 May 2003}}</ref>
Pratt & Whitney Canada showcased at the 2007 Paris Air Show its PW-10X engine development, within the 10,000-pound-thrust-class among the Rolls-Royce RB282, General Electric CF34 successor which became the General Electric Passport, Snecma Silvercrest and Honeywell pushing its HTF10000 development of the HTF7000.<ref>{{cite news |url= http://www.ainonline.com/aviation-news/business-aviation/2007-06-19/pwc-going-green-pw-10x |title= PWC is going green on PW-10X |author= Julian Moxon |date= June 19, 2007 |work= Aviation International News}}</ref>
=== PW810 for the Citation Columbus ===
In 2008, the PW810 variant was announced as the engine for the Cessna Citation Columbus business jet with an anticipated first flight of 2011.<ref name="citation">{{cite news |url= https://www.flightglobal.com/news/articles/cessna39s-columbus-launches-second-new-10k-engine-221374/ |title= Cessna's Columbus launches second new 10K engine |work= Flight International |date= 11 Feb 2008}}</ref> However Cessna canceled the program in 2009, which halted the PW810 program, but Pratt & Whitney continued the PW800 series development.<ref>{{cite news |url= http://www.flyingmag.com/news/textron-pulls-plug-cessnas-columbus-project |title= Textron Pulls the Plug on Cessna's Columbus Project |author= Mark Phelps |publisher= Flying Magazine |date= July 16, 2009}}</ref>
Pratt & Whitney announced that the core high pressure spool with eight compressor and two turbine stages should start testing before the end of 2009.<ref name=FG091009>{{Cite news |author= Niall O'Keefe |url= https://www.flightglobal.com/news/articles/pw800-core-tests-imminent-pratt-whitney-333302/ |title= PW800 core tests imminent: Pratt & Whitney |work= Flight International |date= 9 Oct 2009}}</ref> In December 2009, PWC announced that the core testing had begun.<ref>{{cite press release |url= http://prattwhitney.mwnewsroom.com/press-release/Pratt-Whitney-Begins-Testing-of-Advanced-Core-for-PurePower-Engine-Family-1094166?lang=en-US |archive-url= https://web.archive.org/web/20160816035647/http://prattwhitney.mwnewsroom.com/press-release/Pratt-Whitney-Begins-Testing-of-Advanced-Core-for-PurePower-Engine-Family-1094166?lang=en-US |url-status= usurped |archive-date= August 16, 2016 |title= Pratt & Whitney Begins Testing of Advanced Core for PurePower(R) Engine Family |date= 21 Dec 2009 |publisher= Pratt & Whitney Canada}}</ref> It made its first run in April 2012 and first flew in April 2013.<ref>{{cite news |url= http://aviationweek.com/ebace-2016/pw800-gulfstream-g600-progresses |title= PW800 For Gulfstream G600 Progresses |date= May 26, 2016 |author= Guy Norris |work= Aviation Week}}</ref>
=== PW814/815 for the Gulfstream G500/G600===
thumb|PW815 on a Gulfstream G600
On October 20, 2014, the engine was selected by Gulfstream for its new Gulfstream G500/G600.<ref>{{cite news |url= http://aviationweek.com/nbaa2014/gulfstreams-pratt-whitney-choice-challenges-rolls-royces-dominance |title= Gulfstream's Pratt & Whitney Choice Challenges Rolls-Royce's Dominance |work= Aviation Week |date= Oct 20, 2014 |author= Guy Norris}}</ref> Pratt & Whitney Canada (P&WC) announced on February 17, 2015, that it had received Transport Canada type certification for its PW814GA and PW815GA engines, which will power the new Gulfstream G500 (5,300 nmi range) and G600 (6,600 nmi range) business jets, respectively.<ref name="PWPressMar15">{{cite press release |url= http://prattwhitney.mwnewsroom.com/press-releases/pratt-whitney-canada-s-purepowerr-pw814ga-and-pw815ga-engines-receive-type-cer-201502170992558001?lang=en-US |archive-url= https://archive.today/20150423104528/http://prattwhitney.mwnewsroom.com/press-releases/pratt-whitney-canada-s-purepowerr-pw814ga-and-pw815ga-engines-receive-type-cer-201502170992558001?lang=en-US |url-status= usurped |archive-date= April 23, 2015 |title= Pratt & Whitney Canada's PurePower® PW814GA And PW815GA Engines Receive Type Certification To Power New Gulfstream Business Jets |publisher= Pratt & Whitney Canada |date= Feb 17, 2015}}</ref>
On May 18, 2015, the Gulfstream G500 took its first flight using the PW814A engine after the PW800 engine family has surpassed 3,600 hours of full engine testing, including rigorous endurance testing that simulates a multitude of aircraft missions and environments, and more than 470 hours on P&WC's 747 Flying Test Bed.<ref>{{cite press release |url= http://prattwhitney.mwnewsroom.com/press-releases/successful-gulfstream-g500-first-flight-a-new-milestone-for-purepower-pw800-eng-201505181007831001?lang=en-US |archive-url= https://web.archive.org/web/20150530075315/http://prattwhitney.mwnewsroom.com/press-releases/successful-gulfstream-g500-first-flight-a-new-milestone-for-purepower-pw800-eng-201505181007831001?lang=en-US |url-status= usurped |archive-date= May 30, 2015 |title= Successful Gulfstream G500 First Flight: A New Milestone for PurePower® PW800 Engines |publisher= Pratt & Whitney Canada |date= May 18, 2015}}</ref>
The United States Federal Aviation Administration validated the PW814GA and PW815GA type certificate on February 24, 2017.<ref name=FAATCDS>{{cite web |url= http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/661da79be985d04e862580d4007a4325/$FILE/E00093EN_Rev_0.pdf |title= PW814GA, PW815GA type certificate data sheet |publisher= FAA |date= February 24, 2017}}</ref><ref>[http://www.ainonline.com/aviation-news/business-aviation/2017-03-15/us-faa-gives-nod-g500-g600-pwc-engines U.S. FAA Gives Nod to G500, G600 P&WC Engines]</ref> In May 2017, 13,000h of testing were completed, including 3,500h in flight.<ref>{{cite news |url= https://www.flightglobal.com/news/articles/ebace-rivals-for-power-in-the-business-aviation-eng-437181/ |title= Rivals for power in the business aviation engine market |date= 19 May 2017 |work= Flight Global |author= Murdo Morrison }}</ref> In October this rose to 16,600 hours and 16,800 cycles, the first shop visit is scheduled at 10,000 hours and it needs 20% fewer inspections and 40% lower on-wing maintenance than its competitors<ref>{{cite news |url= https://www.ainonline.com/aviation-news/business-aviation/2017-10-09/purepower-pw800-nearing-entry-service |title= PurePower PW800 Nearing Entry Into Service |author= Matt Thurber |date= October 9, 2017 |work= AIN}}</ref>
In September 2018, the first Gulfstream G500 was delivered with the 14,000 lbf (62.3 kN) PW814.<!--ref name=Flight20may2019/--> The Gulfstream G600 should be first delivered in June 2019, powered by the {{cvt|15,000|lbf|kN}} PW815.<ref name=Flight20may2019/>
=== PW812 for the Falcon 6X ===
The {{cvt|12,000-13,000|lbf|kN}} PW812D variant was selected for the Dassault Falcon 6X, replacing the cancelled 5X after troubles with its Safran Silvercrest engines, expecting a 2022 service entry.<!--ref name=Flight20may2019/--> By May 2019, five test engines were tested over 1,000 h, including bird strikes, ice issues and blade off testing.<ref name=Flight20may2019>{{cite news |url= https://www.flightglobal.com/news/articles/pwc-on-track-with-falcon-6x-engine-testing-458377/ |title= P&WC on track with Falcon 6X engine testing |date= 22 May 2019 |author= Jon Hemmerdinger |work= Flightglobal}}</ref> By December 2021, a type certificate was issued by Transport Canada after more than 4,900h of testing, including more than 1,150h of flight testing, to allow the 6X to enter service on schedule in late 2022.<ref>{{cite news |url= https://www.flightglobal.com/engines/canadian-regulators-certificate-falcon-6xs-pw812d-engine/146682.article |title= Canadian regulators certificate Falcon 6X's PW812D engine |author= Jon Hemmerdinger |date= 1 December 2021 |work= Flightglobal}}</ref>
== Design ==
The PW800 was originally going to be a geared turbofan like the PW1000G.<ref>{{cite news |url= http://www.ainonline.com/aviation-news/2007-10-16/two-new-contenders-vie-power-future-rjs |title= Two new contenders vie to power future RJs |author= Thierry Dubois |date= October 16, 2007 |work= Aviation International News}}</ref> While the PW814/PW815 shares the core of the PW1500G (powering the Airbus A220)<!--ref name=Flight20may2019/--> and the PW812D shares the core of the PW1200G (powering the Mitsubishi MRJ),<ref name=Flight20may2019/> neither model ultimately incorporated the reduction gear system.<ref name="janes">{{cite news |title= P&WC PW800 |work= Jane's Aero Engines |date= 13 Oct 2009}}</ref>
The engine will feature the Technology for Advanced Low NOx (TALON) X combustor, allowing it to exceed International Civil Aviation Organization (ICAO) standards for NOx by 50%, Carbon monoxide (CO) by 35% and that the engine should meet upcoming stage IV aircraft noise requirements.<ref>{{cite news |url= http://airinsight.com/2016/05/23/pwcs-pw800-leading-next-generation-business-aircraft-engine-market/ |title= Leading the next-generation business aircraft engine market |date= May 23, 2016 |publisher= Air Insight}}</ref> A previous version of the TALON combustor is in service with the Pratt & Whitney PW4000.
MTU Aero Engines has a 15% share in the program, developing and producing various stage of the high-pressure compressor and the low-pressure turbine.<ref>{{cite web |url= http://www.mtu.de/engines/commercial-aircraft-engines/business-jets/pw800/ |title= PW800 |publisher= MTU Aero Engines }}</ref>
==Variants== ;PW810 * was to produce 8,830 lbf (39 kN) thrust to power the cancelled Cessna Citation Columbus.<ref name="citation"/> ;PW812D * powers the Dassault Falcon 6X business jet. ;PW812GA * powers the Gulfstream G400 business jet. ;PW814GA * powers the Gulfstream G500 business jet.<ref name="PWPressMar15"/> ;PW815GA * powers the Gulfstream G600 business jet.<ref name="PWPressMar15"/>
==Applications== * Cessna Citation Columbus (cancelled) * Dassault Falcon 6X * Gulfstream G400 * Gulfstream G500 * Gulfstream G600
==Specifications (PW810)== {{jetspecs <!-- If you do not understand how to use this template, please ask at Wikipedia talk:WikiProject Aircraft. Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> . --> |ref=FAA<ref name=FAATCDS/> |type=Twin spool Turbofan<!--also in <ref name=AW141101>--> |length= {{convert|105.8|in|cm|abbr=on}} (flange to flange) / {{convert|130.44|in|cm|abbr=on}} (fan spinner face to aft tail cone) |diameter= {{convert|50|in|cm|abbr=on}} fan case<!--also in <ref name=AW141101/>--> |weight={{convert|3,135.7|lb|kg}} (dry) |compressor= 24-blade, single-piece Single-stage fan, 2-stage LP and 8-stage HP compressor<!--also in <ref name=EASATCDS>{{cite web |url= https://www.easa.europa.eu/system/files/dfu/EASA%20TCDS%20IM%20E96_PW814GA-PW815GA_01.pdf |title= PW814GA, PW815GA type certificate data sheet |publisher= EASA |date= August 31, 2017}}</ref>--> |combustion= |turbine=2 stage HP and 5 stage LP turbine<!--also in <ref name=EASATCDS>--> LP: max 6,240 rpm, HP: max 24,043 rpm |fueltype= |oilsystem= |power= |thrust=PW814GA: {{convert|15,429|lbf|kN|abbr=on}}, PW815GA: {{convert|16,011|lbf|kN|abbr=on}} (33°C flat rated) |compression= |bypass=5.5:1 (approx)<ref name=AW141101>{{cite news |url= http://aviationweek.com/bca/gulfstream-unveils-g500-and-g600 |title= Gulfstream Unveils G500 and G600 |date= Nov 1, 2014 |author= Fred George |work= Business & Commercial Aviation |publisher= Aviation Week}}</ref> |aircon= |turbinetemp= 965 °C / 1769 °F (ITT) |fuelcon= |specfuelcon= |power/weight= |thrust/weight= {{#expr:15429/3135.7round2}} - {{#expr:16011/3135.7round2}} }}
==See also== {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related= *Pratt & Whitney PW1000G |similar engines= *Rolls-Royce Pearl *Rolls-Royce RB282 *General Electric Passport *Snecma Silvercrest |lists= }}
==References== {{Reflist|30em}}
==External links== *{{Official website|http://www.pw800.com/}}
{{Pratt & Whitney Canada aeroengines}}
{{DEFAULTSORT:Pratt and Whitney Canada PW800}} Category:2010s turbofan engines Category:Pratt & Whitney Canada aircraft engines