N328ST - 1997 DORNIER 328 110


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    Aircraft Summary


    General

    Year
    1997
    Manufacturer
    DORNIER
    Model
    328-110
    Serial Number
    3086
    Condition
    Used
    Registration #
    N328ST
    FlightRules
    IFR
    Description
    After reviewing aircraft records, FAA FORM 337’s, the aircraft does not appear to have any damage history. Current Operational Weights Empty Weight: 19,655 lbs. Max Gross Taxi Weight:31,019 lbs. Max Takeoff Weight: 30,843 lbs. Max Landing Weight: 29,167 lbs. Max Zero Fuel Weight: 27,800 lbs.

    Airframe

    Total Time
    6232.0
    Airframe Notes
    Current Times TAT 6693.7 TAC 7453 APU 4558.0

    Engine Program

    Engine Program Notes
    ENGINE LT TSO/TSN 5857.1 LT CSO/CSN 5473 RT TSO/TSN 4264.8 RT CSO/CSN 4986 Engine Manufacturer: Pratt & Whitney Model: PW119B Engine #1 Serial Number: AB0065 Engine #2 Serial Number: PC-E116011 APU Serial Number: P-135 Propeller #1 Serial Number: HL306 Propeller #2 Serial Number: HL241

    Props

    Prop Notes
    PROPELLER LT TSO/TSN 4338.9 RT TSO 514.9 RT TSN 5859.1

    Avionics

    Avionics/Radios
    Honeywell Primus 2000 Integrated Avionics Suite which includes the following: FLIGHT DIRECTOR: Integrated avionics computer (IAC) AUTO PILOT: Integrated avionics computer (IAC) COMMS:Dual Honeywell RCZ-851/RCZ-851C NAVS: Dual Honeywell RNZ-851 ADF Integrated NAV units (RNZ-851) DME: Integrated NAV units (RNZ-851) TDR: Mode “S” Xpndr; built into the Honeywell RCZ-851C RADAR:Primus 650 by Honeywell TCAS: TCAS RT-910 GPS: Honeywell GR-500 HF Radios: Dual Honeywell KTR-953 RMI: Built into the multi-function displays HSI:Built into the multi-function displays ALT: Built into the multi-function displays RAD ALT: Dual Honeywell RT-300 CVR/FDR: CVR-A100 / FDR-800 EGPWS:Honeywell P/N 065-1190-020 Passenger Address System:PBS250-1

    Additional Equipment

    Additional Equipment
    Features: 5 Tube DU-870 EFIS Displays Dual 855B Radio Management Units (RMU) Dual Honeywell DA-800 Data Acquisition Units Dual Honeywell IC-800 Integrated Avionics Computer (IAC) Dual AHZ-800 Attitude Heading Reference System (AHRS) Dual ADZ-840 Air Data Computers AI-330K Standby Horizon AV-850A Audio Control Panel 77 Cubic Foot Oxygen Bottle Curtain for Passenger Door Cockpit Observer Seat Propeller Reverse Standby Compass High Frequency Radios Auxiliary Power Unit

    Exterior

    Year Painted
    2010

    Interior

    Year Interior
    2009

    Inspection Status

    Inspection Status
    Needs Phase 2 and Phase 6 Low Utilization Maintenance Program Time Life Limited Systems AD’s Current: 12/12 ASC / SB Current: 12/12


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