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    Pratt & Whitney’s JT8D-219 is the latest version of the popular JT8D engine family. More

    than 350 operators use JT8Ds to power approximately 12 percent of the world’s

    commercial airline fleet. The -200 series covers the 18,500- to 21,700-pound thrust range,

    and it is the exclusive power plant for the MD-80 aircraft and the Super 27 re-engining

    program for the B727 aircraft. Since starting revenue service in 1980, more than 2,900

    JT8D-200 engines have been produced, logging more than 110 million hours of flight. Pratt & Whitney

    and Seven Q Seven have entered into a joint venture (JV) to re-engine B707-model aircraft with

    JT8D-219 engines for commercial and military applications. The JV is under contract to Northrop

    Grumman to begin re-engining the United States Air Force (USAF) E-8C Joint STARS aircraft.

    The JT8D-219 is a dual-spool, low-bypass-ratio turbofan with a service-proven design. The -219

    builds on the JT8D family’s excellent reputation for high reliability and low maintenance cost. For

    B707s with JT3D engines, re-engining with JT8D-219 offers excellent performance and cost-saving

    opportunities, including higher thrust and a 19% reduction in fuel burn (typical mission) for attractive

    gains in payload and range. The JT8D-219 also reduces perceived noise by approximately 50%, while

    reducing smoke, carbon monoxide and unburned hydrocarbons by 85% or more.

    The latest version of the JT8D-219 incorporates reliability improvements that will further extend

    time on-wing and reduce maintenance costs. It also features the capability for higher power

    extraction to meet the increased power requirements for state-of-the-art military avionics and

    surveillance equipment as well as for commercial onboard electrical needs.

    Pratt & Whitney. It’s in our power.TM

    JT8D-219 CharacteristicsTakeoff thrust rating (SLS) 21,000 pounds (93.4 kN)

    Climb thrust (35k/0.8 Mn) 5,530 pounds (24.6 kN)Flat-rated temperature 84°F (28.9°C)Dry weight 4,741 pounds (2,150 kg)Length 154 inches (3.91 m)Fan tip diameter 49.2 inches (1.25 m)Bypass ratio 1.74Fan pressure ratio 1.91Overall pressure ratio 19.4

    JT8D-219 Military ApplicationsJoint STARS; AWACS and other B707 tanker/transport aircraft (potential future applications)

    JT8D-219 Commercial ApplicationsMD80, Super 27 and Seven Q Seven

    Product Facts 

    Program MilestonesNovember 1996 Commercial re-engine program startedFebruary 1999 Delivery of first flight-test enginesJuly 1999 First commercial demonstration flightAugust 2001 Fully re-engined demonstration flightsJanuary 2007 Selected by Northrop Grumman for USAF Joint STARS re-enginingMay 2008 Contract awarded to re-engine two Joint STARS aircraftDecember 2008 First flight of Joint STARS E-8C with JT8D-219 enginesJuly 2010 FAA B707 Supplemental Type Certificate awarded to Seven Q Seven2012 Begin Joint STARS fleet re-engining with JT8D-219

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    JT8D-219 Turbofan Engine

    Cost-Effective, Off-the-Shelf Commercial Re-Engining

    www.pw.utc.com 

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