1990 BEECHCRAFT 1900C 1


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    Aircraft Summary


    General

    Year
    1990
    Manufacturer
    BEECHCRAFT
    Model
    1900C-1
    Serial Number
    UC-171
    Condition
    Used
    Description
    Fresh Phase I-VI inspection, New paint to customer specifications, other engine available with times from 23K to 26K! Financing Available

    Airframe

    Total Time
    23481.0

    Engine Program

    Engine Program Notes
    P&W PT6A-65B Reverse flow, free turbine engines Flat rated at 1,1,, SHP each Engine fire detection system w/ fire extinguishers Left: Gas Generator S/N: 32565 Time Since Overhaul: 4107.7 Time Since HSI: 1039 Power Section S/N: 32078 Time since Overhaul: 2566.2 Right: Gas Generator S/N: 32062 Time Since Overhaul: 3509.2 Time Since HSI: 1562.1 Power Section S/N: 32463 Time since Overhaul: 4313.9

    Engine 1

    Engine 1 Time
    4107
    Engine 1 Time Since
    SOH
    Engine 1 Time Since HSI/MPI/Mid-Life
    1039

    Engine 2

    Engine 2 Time
    3509
    Engine 2 Time Since
    SOH
    Engine 2 Time Since HSI/MPI/Mid-Life
    1562

    Props

    Prop Notes
    Hartzell HC-B4MP-3A four bladed propellers Auto feathering with reverse pitch Propeller synchrophaser with synch scope 0/397.5 Time since overhaul

    Avionics

    Avionics/Radios
    Comm 1: Collins VHF-22A Transceiver with CTL-22 Control & Antenna Comm 2: Collins CHF-22A Transceiver with CTL-22 Control & Antenna Nav 1: Collins VIR-32 with Collins EFD-74 EHSI Indicator Nav 2: Collins VIR-32 with Collins 331A-3G HSI Indicator ADF: Collins ADF-60A iwht CTL-62 Control and ANT-60 Antenna Transponder: Dual Collins TDR-90's w/ Single CTL-92 Control and Antennas DME: Collins DME-42 with CTL 42 Control (Active/Preset) DME 2: Collins DME-42 with CTL 42 Control (Active/Hold) RMI: Dual Collins RMI-30's (pilot) VOR-1/ADF and VOR-2/ADF Switching Compass System #1: Honeywell/Sperry C-14A-43 with Servo Amplifier Compass System #2: Honeywell/Sperry C-14A Altitude Alerter: Bendix King KAS-297A Inverters: Dual Flight Tronics PC-250's (250 VA) Pilot's Altimeter: Bendix King KEA-346 Encoding Altimeter Copilot's Altimeter: IDC Kollsman Standard Audio System: Dual Beech Systems in Edge Lighted Panel Dual Cockpit Speakers Dual Audio Switches CVR: Fairchild A100S GPWS Sundstrand Mark VI Radar Altimeter: Collins ALT-55 Weather Radar: Collins WXR-270 TCAS: King CAS-66A with Radar Display Cabin Briefer: Heads up technologies momolingual, pedestal mounted Pilot's Horizon Indicator: Collins ADI-84 Pilot's Directional Indicator: Collins EFD-74 EHSI Copilot's Horizon Indicator: Collins EFD-74 EHSI Copilot's Directional Indicator: Collins 331A-3G HSI Avionics Master Switch Front Mounted Instruments Flight Hour Meter Microphone Key in Pilot and Copilot Control Wheels Emergency Locator Transmitter

    Additional Equipment

    Additional Equipment
    Landing Gear and Brakes: Hydraulically actuated tricycle landing gear Aircraft Braking system: Multiple Disc Brakes on each Main wheel Main Wheel Tire Size: 22 x 6.75-10 (Tubeless 10 ply rating, high flotation) Nose Wheel Tire Size: 19 x 6.75-8 (Tubeless 8 ply rating, high flotation) Systems and Controls Complete Anti-icing and De-icing includes: Surface Deicing Boots Electric Propeller Anti-icing Engine Anti-Icing Dual Electrically Heated Windshields Electrically heated pitot tubes 152 Cu. Ft. Oxygen system with Outlets for Two Cre and Occupants Yaw Damp & Rudder Boost Equipped Electric Elevator Trim System with Manual Wheel Flight Instruments: Two Airspeed Indicators Two Sensitive Altimeters Two Instantaneous Vertical Speed Indicators Compass(Standby Magnetic) Outside Air Temperature Indicator Vacuum Gauge Deice Pressure Gauge Flap Position Indicator Cabin Rate of Climb Indicator Cabin Altitude and Differential Pressure Indicator Oxygen Pressure Indicator Two Fuel Quantity Indicators Electrical 28 Volt DC System: Two Engine Starter/Generators (250 AMP-28 Volt) Triple Fed Bus System with Automatic Load Shedding Air cooled Nickel-Cadmium Battery(34 Ampere Hour Rate) Battery Charging Current Sensor (Safety Sentinel) Solid State Generator Controllers External Power Receptavle with Cockpit Annunciation and Overvoltage Protection Automatic Solid State Master Warning and Annunciator control Panel System with Self Test and Dimmer System Voltmeter/Ammeter Propeller Anti-Ice Ammeter All Electrical Circuits have Circuit Protective Devices

    Exterior

    Exterior Notes
    New to Customer specifications

    Interior

    Interior Notes
    Custom Commuter/Corporate Quick Change

    Inspection Status

    Inspection Status
    Fresh Phase I through Phase VI inspection....All life limited airframe components mid time or better


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