N911EE - 2005 LANCAIR PROPJET


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    Aircraft Summary


    General

    Year
    2005
    Manufacturer
    LANCAIR
    Model
    PROPJET
    Registration #
    N911EE
    Serial Number
    LIV-550
    FlightRules
    IFR
    Condition
    Used
    Total Time
    50.0
    Number of Seats
    4
    Description
    This high powered turbine will fly you to incredible speeds of up to 370 mph with climb rates at 4000 FPM. The dream is now reality. Performance from the Ground Up PropJet. Fast Becomes Faster. Continental becomes Regional. At Lancair, performance is our one-word mission statement—one that combines speed, control, comfort and economy. And while all of these are easy to experience in the Lancair PropJet, speed is clearly at the controls. Powered by a Walter 601E turbine, this beauty propels you across country at upwards of 370 mph, with climb rates at 4000 FPM. Whether your cargo is a business presentation or a friend and a couple of sets of golf clubs, the destination is closer than you ever thought possible for an aircraft you have built, using our simple, intelligent, industry-renowned instructions, with your own hands. And the speed with which you get to your maiden PropJet flight is much faster as well, with on-site builder’s assistance programs, from one week to twenty-five weeks, that can dramatically cut the time to the first flight in your new Lancair PropJet. Specifications: Length .................................... 26 ft Wingspan .................................. 30.2 ft Wing Area ................................. 98 ft Aspect Ratio .............................. 9 : 1 Empty Weight .............................. 2200 lbs Gross Weight .............................. 3550 lbs Std. Fuel Capacity ........................ 125 gal Ext. Fuel Capacity ........................ 145 gal Useful Load ............................... 1350 lbs Baggage Capacity .......................... 150 lbs Trailering Width .......................... 100 in Cabin Area Seats ..................................... 4 Width (interior front) .................... 46 in Width (interior rear) ..................... 43 in Height (interior) ......................... 48 in Performance Cruise (typ @ 24,000 ft) .................. 370 mph Fuel Consumption (typ) .................... 33 gph Range (w/res) ............................. 1400 sm Endurance (w/res) ......................... 4 hrs Rate of Climb @ Sea Level Solo ...................................... 7000 fpm Gross ..................................... 4000 fpm Take Off Roll @ Sea Level ................. 1200 ft Landing Roll with Beta .................... 1400 ft Stall Speed VsO ........................... 74 mph Wing Loading .............................. 36 lbs/sq ft Power Loading ............................. 4.7 lbs/hp G loading (utility) ....................... +3.8, -1.9 Professional Built, Ready for Interior, 2 Chelton EFIS-SV, GMA 340, GNS 430, GTX 330, Apollo SL30

    Engine

    Engine Notes
    Walter 601E-11 Certified Turbine, 750 hp @ 2080 rpm

    Props

    Prop Notes
    Avia 3 Blades Constant Speed Propeller

    Modifications/Conversions

    Modifications/Conversions
    35 Gallon Belly Tank

    Avionics

    Avionics/Radios
    2 Chelton EFIS-SV, GMA 340, GNS 430, GTX 330, Apollo SL30

    Additional Equipment

    Additional Equipment
    Engine Monitor, Trutrak A/P, Co-Pilot Back-up Inst, EM O2 System, Oregon Aero Pilot/Co Pilot Seats

    Interior

    Interior Notes
    Ready for New Owner to Choose


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