N473PS - 1994 DORNIER 328 100


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    Aircraft Summary


    General

    Year
    1994
    Manufacturer
    DORNIER
    Model
    328-100
    Serial Number
    3010
    Condition
    Used
    Registration #
    N473PS
    Description
    5 Tube DU-870 EFIS Displays, Dual 855B Radio Management Units (RMU)

    Airframe

    Total Time
    20242.0
    Airframe Notes
    Total Airframe Hours Since New : 20,242.7 Total Airframe Cycles Since New : 23,919

    Engine Program

    Engine Program Notes
    Pratt & Whitney PW-119C Engine Position: #1 Engine Serial: 116022 TSN 18919.2 CSN 21829 TSO 8799.1 CSO 8972 TSHSI 8799.1 CSHSI 8972

    Props

    Prop Notes
    #1 Propeller Serial: HL454 TSN 5079.5 #2 Propeller Serial: HL43 TSN 5752.6 CSN N/A TSO 565.4 CSO N/A

    Avionics

    Avionics/Radios
    Flight Director: Built into the Integrated Avionics Computer (IAC) Auto-Pilot: Built into the Integrated Avionics Computer (IAC) COMMS: Dual Honeywell Units NAVS: Dual Honeywell Units ADF: Integrated into the Honeywell NAV Units DME: Integrated into the Honeywell NAV Units XPONDER: Mode “S” diversity transponder RADAR: Primus 650 Weather Radar TCAS: Honeywell RT-910 TCAS EGPWS: Honeywell Mark VI EGPWS RMI: Built into the Multi-Function Displays (MFD) HSI: Built into the Multi-Function Displays (MFD) ALTIMETER: Built into the Multi-Function Displays (MFD) RAD ALT: Dual Honeywell RT-300 CVR/FDR: Honeywell CVR & FDR

    Additional Equipment

    Additional Equipment
    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) Single AHZ-800 Attitude Heading Reference System (AHRS) with Single Inertial Reference System (IRS) Dual ADZ-840 Air Data Computers AI-330K Standby Horizon AV-850A Audio Control Panel JETPACK Emergency Power Supply PS-835C 115 Cubic Foot Oxygen Bottle Curtain for Passenger Door Cockpit Observer Seat Propeller Reverse Standby Compass

    Exterior

    Exterior Notes
    This aircraft was painted in 2004.

    Interior

    Interior Notes
    Aircraft is currently configured for 30 passenger seats, but can be configured for 32 seats.

    Inspection Status

    Inspection Status
    Current Operational Weights Operating Weight (with crew, galley, lav) : 20,550 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. Inspection Items Hourly Interval Last Performed Next Due Inspections Line Check 60 20241.7 20301.7 A1 400 19912.1 20312.1 A2 800 19581.5 20381.5 A3 1200 20094.3 21294.3 A4 1600 N/A N/A A5 2000 18663.5 20663.5 C1 4000 19357.2 23357.2 C2 8000 17883.0 25883.0 C3 12000 17349.4 29349.4 C4 16000 18972.6 34972.6 Calendar Interval Last Performed Next Due Inspections Line Check 15 days 8/01/2008 8/16/2008 C1 24 mth 7/05/2007 7/31/2009 C2 48 mth 9/01/2005 9/30/2009 C3 72 mth 8/13/2004 8/31/2010 C4 96 mth 2/07/2007 2/28/2015 Structure Interval Last Performed Next Due Inspections SSI/CP2 24 mth 7/05/2007 7/31/2009 SSI/CP25 30 mth 4/11/2008 10/31/2010 CP4 48 mth 9/01/2005 9/30/2009 SSI/CP5 60 mth 9/01/2005 9/30/2010 SSI/CP10 120 mth 3/20/2002 3/31/2012 Gear Status Description Limit Remaining NLG LEG 120 mth 104 mth NLG BRACE 120 mth 101 mth RH MLG LEG 120 mth 32 mth RH MLG BRACE 120 mth 101 mth LH MLG LEG 120 mth 26 mth LH MLG BRACE 120 mth 101 mth


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