2008 EUROCOPTER EC225


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    Aircraft Summary


    General

    Year
    2008
    Manufacturer
    EUROCOPTER
    Model
    EC225
    Condition
    Used
    Description
    This EC225 /H225 is equipped with state-of-the art technology such as navigation precision equipment (sensors, inertia reference system, etc) and detection devices (FLIR, RADAR). Equipped with a rotor de-icing system and Multi Purpose Air Intake fly in all-weather conditions and still offers a contained landing footprint.

    Airframe

    Total Time
    0
    Airframe Notes
    Full SAR Superior Mode navigation with 4-axis coupled autohover and hoist operator joystick and drift control. UNIQUE SAR CAPABILITIES Fully automatic transition to hover Less than 1 m hover accuracy with redundant sensors (dual GPS or Inertial navigation System) capabilities. Fully automatically set up a search pattern Unique automatic fly-away in case of engine failure during hoisting. Return to service with fresh 16-year airframe major inspection and all EASA AD ASB to be performed during 12 months with possible delivery mid-2024. During RTS, engines and components will be optimized for required flight hours and calendar potential.

    Engine 1

    Engine 1 Manufacturer
    SAFRAN
    Engine 1 Notes
    Makila 2A1 fresh from shop. Details available on request.

    Engine 2

    Engine 2 Manufacturer
    SAFRAN
    Engine 2 Notes
    Makila 2A1 fresh from shop. Details available on request.

    Modifications/Conversions

    Modifications/Conversions
    This EC225 /H225 is equipped with state-of-the art technology such as navigation precision equipment (sensors, inertia reference system, etc) and detection devices (FLIR, RADAR). This EC225 is also equipped with a rotor de-icing system and Multi Purpose Air Intake fly in all-weather conditions and still offers a contained landing footprint. Full SAR Superior Mode navigation with 4-axis coupled autohover and hoist operator joystick and drift control. UNIQUE SAR CAPABILITIES Fully automatic transition to hover Less than 1 m hover accuracy with redundant sensors (dual GPS or Inertial navigation System) capabilities. Fully automatically set up a search pattern Unique automatic fly-away in case of engine failure during hoisting. Return to service with fresh 16-year airframe major inspection and all EASA AD ASB to be performed during 12 months with possible delivery mid-2024. During RTS, engines and components will be optimized for required flight hours and calendar potential.

    Avionics

    Avionics/Radios
    AUTOPILOT SAR MODE PA APM 2000 HOIST MAN CONSOLE WITH JOYSTICK FMS CANADIAN MARCONI CMA 9000 WITH SAR MODE A V A D AUTOMATIC VOICE ALARM DEVICE VHF- AM COLLINS 422A PILOT VHF- AM COLLINS 422A COPILOT TRANSPONDER COLLINS TDR ADF COLLINS ADF 462 PILOT DME COLLINS DME 442 VOR / ILS / MKR COLLINS VIR 432 PILOT VOR / ILS / MKR COLLINS VIR 432 COPILOT RADIO ALTIMETER AHV 16 N° 1 RADIO ALTIMETER THALES AHV 16 N° 2 VHF/FM MARINE NAT NPX138 N (PILOT) BAKER M1060 PUBLIC ADRESS SYSTEM CHELTON SYSTEM 7 - (121,5) VHF/AM BI-FREQUENCY) RADAR TELEPHONICS 1600C WEATHER RADAR DISPLAY ON AHCAS GPS FREEFLIGHT TNL 2101 APPROACH + STAND ALONE GPS CANADIAN MARCONI CMA 3024 CONNECTED WITH FMS RADAR DOPPLER MARCONI ANV-353 CVFDR, RECORDER AR-204C CHRONOMETER NVG INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)


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