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Aircraft Overview
Garmin G1000, Hartzell 3-Blade Constant Speed Prop. Factory new demonstrator.
Airframe
Engines
Teledyne Continental Gold Standard Edition six cylinder IO-550-B fuel injected engine rated at 300 horsepower. Prop(s): Hartzell three blade, aluminum alloy, 80" diameter, constant speed propeller with polished spinner.
APU
Garmin G1000 fully integrated avionics glass panel fl ight deck with a large-format, high-resolution display system consisting of:Dual high defi nition color LCD displays - GDU 1040 10.4" primary flight display (PFD) and 1045 multi-function display (MFD) with XGA (1024 x 768 pixels) resolution, wide viewing angles, adjustable backlighting and clear sunlight readability.GPS/Comm 1 - Garmin GIA 63W IFR oceanic, WAAS enabled TSO C145a approved GPS receiver LPV/LNAV/VNAV with 16-watt communications transceiver (118.000 to 136.992 MHz with 8.33 KHz channel increments).GPS/Comm 2 - Garmin GIA 63W IFR oceanic, WAAS enabled TSO C145a approved GPS receiver LPV/LNAV/VNAV with 16-watt communications transceiver (118.000 to 136.992 MHz with 8.33 KHz channel increments).Nav 1 - Garmin GIA 63W VOR/ILS/LOC receiver tuning (108.00 to 117.95 MHz).Nav 2 - Garmin GIA 63W VOR/ILS/LOC receiver tuning (108.00 to 117.95 MHz).Transponder - GTX 33 ES integrated transponder with ADS-B.AHRS 1 - Garmin GRS 77 integrated solid-state attitude heading and reference system, and GMU 44 magnetometer.ADC 1 - GDC 74A MOD 1 integrated digital air data computer.
Audio/marker system - GMA 1347; audio control panel and sixplace stereo intercom system with associated aural tones and digital clearance recording/playback.TAWS B - integrated Class-B terrain awareness and warning system (TAWS) with worldwide terrain or domestic terrain and obstacle database displayed on the MFD.TAS - GTS 820 Traffic Advisory System with dual directional antennas.EIS engine indication advisories - function of MFD or PFD in reversionary mode.GEA 71 engine airframe data concentrator displayed on MFD.AFCS - GFC 700 three-axis, WAAS integrated automatic fl ight control system (AFCS) with LPV approach coupled VNAV, (VNAV on descent only) altitude alert, fl ight level change, pitch hold, and go around mode; Flight director (FD) provides pitch and roll guidance and the GSA 81 autopilot servos perform internal calculations for optimum performance.WX data link - GDL 69A.XM Satellite - weather and radio reception with wireless two-way remote control [Applicable to North America Only].Garmin SafeTaxi (US Only) and Garmin FliteCharts provide electronic display of airport and fl ight navigation charts on the PFD (Subscription services are required at the buyers cost).
Hand-held microphone (mounted on end of armrest betweenpilot's and copilot's chair).Synthetic Vision Technology.Cockpit speaker.Static wicks.Avionics master switch.Avionics cooling fan.Emergency Locator Transmitter (ELT) - Artex ME406 operating on 121.5 and 406 MHz with cockpit switch.
Exterior high solids polyurethane paint. Complete internal polyamide epoxy corrosion proofi ng. Quick removable fuel tank caps. Stainless steel cabin assist step. 74 gallon usable fuel tanks (total).
Headliner: TBD Vertical Trim: TBD Horizontal Trim: Foothill Aspen Sidewall; Sidewall Armrest Pad: TBD Floor Covering: TBD Seat - Center Insert; Side Insert; Seat Trim: TBD Seat Belts: TBD Instrument Panel: Nextel-Suede: Dark Anthracite
Paint Scheme Paint Design: TBD #1 Color (Overall): Matterhorn White #2 Color: TBD #3 Color: TBD
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Year: 2012 | S/N: E-3982 | TTAF: New
Hawker Beechcraft Pre-Owned
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