OEABC - 2010 AIRBUS A318


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    Aircraft Summary


    General

    Year
    2010
    Manufacturer
    AIRBUS
    Model
    A318
    Serial Number
    1234
    Registration #
    OEABC
    Condition
    Used
    FlightRules
    IFR
    Description
    Green Delivery will be in November 2010. Outfitting is planned at Lufthansa Technik in Tulsa (duration 5 to 6 months). Interior changes are still possible. New Airbus A318Elite

    Engine Program

    Engine Program Notes
    CFM56-5B9/P

    Avionics

    Avionics/Radios
    * Flight Augmentation Computer: Thales, Avionics SA * Flight control unit: Thales, Avionics SA MCDU Honeywell * Flight Management Guidance Computer: Thales / Honeywell * VDR/COMM transceiver VHF-900B: Rockwell Collins * Radio Management Panel: Thales, Avionics SA * ADIRU: Honeywell * Standby altimeter: Thales, Avionics SA * Standby airspeed indicator: Thales, Avionics SA * Standby compass: SIRS Navigation * Standby horizon: Thales, Avionics SA * Multi-mode receiver: Rockwell Collins * Weather radar antenna: Honeywell * Weather radar antenna, dual mount: Honeywell * Weather radar dual control panel: Honeywell * Weather radar transceiver: Honeywell * Weather radar dual transceiver mount: Honeywell * Radio altimeter transceiver: Thales, Avionics SA * Enhanced Ground Proximity Warning Computer: Honeywell * DME interrogator, DME-900. Rockwell Collins * ATC transponder / DME antenna: Rayan * ATC/TCAS dual control panel: Thales, Avionics SA * ATC mode S transponder: Honeywell * ADF antenna: EAS * ADF receiver, ADF 900: Rockwell Collins * VOR antenna: Rayan * Marker antenna: Rayan * VOR/Marker receiver (VOR-900): Rockwell Collins * DDRMI :Thales, Avionics SA

    Additional Equipment

    Additional Equipment
    * 2 Additional Center Tanks are installed (can be removed easily) * Polar navigation function * Steep approach capability * EASA JAR 25 and compliance with JAR OPS1 – subpart K and L * Partial compliance with FAA type certificate requirement *Increased design weight to 66t MTOW *Operation on runways with reduced width Air conditioning • Floor panel heating for forward door area Auto Flight • Polar navigation function • Steep approach capability • Flight management kits Communications • Emergency Locator Transmitter • Dual HF system and activation of data link function • VHF data radio • Cockpit Voice Recorder • Radio Management Panel Electrical Power • Installation of additional electrical outlets 115V/60Hz in flight deck Equipment/furnishings • Fourth occupant seat in flight deck • Electrical foot warmers for pilots • Cargo Floor panels: Rubber seal & Reinforced for heavy bulk usage • Slide rafts at forward service and entry doors • Cabin configuration prior to outfitting (including G2 structural provisions)

    Exterior

    Year Painted
    2010
    Exterior Notes
    New Aircraft

    Interior

    Year Interior
    2010
    Number of Seats
    19
    Interior Notes
    Outfitting will be at Luftahnsa Technik in Tulsa, USA


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