2012 DEHAVILLAND DHC 6 400


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    Aircraft Summary


    General

    Year
    2012
    Manufacturer
    DEHAVILLAND
    Model
    DHC-6-400
    Condition
    Used
    FlightRules
    IFR

    Airframe

    Total Time
    893.0
    Airframe Notes
    Configuration and Construction: All metal, non pressurized, high-wing monoplane with fixed tricycle (steerable nose) landing gear.

    Engine Program

    Engine Program Notes
    Two, Pratt & Whitney Aircraft of Canada Limited, PT6A-34, single stage, freeturbine engines.

    Props

    Prop Notes
    Two Hartzell HC-B3TN three bladed reversible pitch, constant speed, fully feathering propellers.

    Avionics

    Avionics/Radios
    Dual DME Dual Mode S EHS Transponders with ADS-B Out Capability Radar Altimeter Class AT errain Warning (Honeywell MK VI EGPWS) TCAS I Traffic Advisory System Honeywell RDR 2000 Weather Radar Crew Intercom Dual David Clark Noise Cancelling Headsets Jacks for Third (Observer) Headset at Flight Compartment Cabin Public Address System 406 Mhz ELT with Latitude and Longitude Transmission L3 Electronic Integrated Standby Instrument System Thommen Chronometer Eye Height Reference Device Integrated Central Maintenance Computer Function 4 Channel CVR Dual14 Volt Convenience Outlets in Flight Compartment Flight Director (delayed

    Additional Equipment

    Additional Equipment
    CVR, FDR, HF RADIO, DUAL GPS Installation, ELT with navigation interface and remote switch, Dual Audio Panels, Vertical Depiction of Terrain on Route Ahead, Mk 6 Class A TAWS, Radar Altimeter, TCAS

    Exterior

    Year Painted
    2012
    Exterior Notes
    NEW

    Interior

    Year Interior
    2012
    Number of Seats
    19
    Interior Notes
    NEW


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