2009 EMBRAER PHENOM 100


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    Aircraft Summary


    General

    Year
    2009
    Manufacturer
    EMBRAER
    Model
    PHENOM 100
    Serial Number
    TBD-2009
    Condition
    New
    Description
    New Position - Scheduled for Delivery August 2009

    Airframe

    Airframe Notes
    AIRFRAME 0 Hours POWERPLANT Pratt & Whitney – PW 617F 0 Hours SINCE New 0 Hours SINCE New ADDITIONAL • Takeoff thrust – 1,615 lb • FADEC controlled

    Avionics

    Avionics/Radios
    The EMBRAER Phenom 100 Executive Jet avionics will be Prodigy system wich is based on Garmin Avionics Platform. It will make extensive use of the latest technologies in a higly integrated and automated architeture. Designed with the "quiet and dark" cockipt concept, it will provide maximum safety, requiring adequate pilot workload while providing comfort during all flight phases. The main instrument panel will incorporate Three 12.4 inches Active Matrix Liquid Crystal Displays (AMLCD), one integrated Electronic Standby Instrument (IESI), two audio panels, one guidance panel and an additional panel for FMS (Flight Management System) control. The Prodigy will provide the following functions as baseline: Options Chosen: DME Transponder #2 Weather Radar Cockpit Flood Lights Sunshade and Sun Visor Life Vest Crew Portable Breathing Equipment Smoke Goggles Premium Pax Door

    Additional Equipment

    Additional Equipment
    • Display of attitude, heading, and slip/skid • Display of air data information • Display of engine parameters and system status / information (including synoptic) • Crew Alerting System (CAS) • Aural Warning (including Stall Warning Function) • Airborne Audio System • VHF Communication (COM) • Transponder functions including Traffic Information System (TIS) • VOR/ILS Navigation (NAV) • Satellite based positioning navigation (GPS-WAAS¹) • Flight Management System (FMS) including Required Navigation Performance (RNP) • Vertical Navigation (VNAV) • Satellite Weather and Radio Receiver² • Display of terrain information, including Terrain Awareness and Warning System, class B (TAWS-B) • Moving map for situational awareness • Flight Director (FD) • 3 Axis CAT I Automatic Flight Control System (AFCS) • Pitch and Mach Trim Computations • Center Maintenance Computer (CMC), including Health Monitoring Capability for Engines • Emergency Locator Transmiter (ELT) (1) WAAS capability is available in GPS WAAS coverage area. (2) Satellite Weather and Radio Receiver are available in XM service coverage area.

    Exterior

    Exterior Notes
    EXTERIOR To Be Determined

    Interior

    Interior Notes
    INTERIOR To be Determined


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