2012 AGUSTA A109SP


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    Aircraft Summary


    General

    Year
    2012
    Manufacturer
    AGUSTA
    Model
    A109SP
    Condition
    Used
    Description
    •Single Pilot IFR •LPV capable •4-axis dual duplex digital AFCS with integrated Flight Director •Moving map EURONAV V with 8.4” display •VIP interior completion 5 seats •Air conditioning ECS (Environment Control System) •Twin engine PW207C •Fresh yearly inspection August 2020 The aircraft is operating, why the condition and component times will be subject to changes depending upon such operations. Verification of the condition of the aircraft and its component times shall be the responsibility of the purchaser.

    Airframe

    Total Time
    1092

    Avionics

    Avionics/Radios
    •Pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP) in lieu of basic Pilot flight/navigation EFIS (1 display) slip indicator and Remote Bug Panel (RBP) •Co-pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP) •Electronic Standby Instrument System (ESIS) •Traffic Avoidance System TAS-620 Avydine (presented on EFIS) •Weather Radar (displayed on EFIS) •Reversionary Control Panel (RCP) •EFIS pilot/co-pilot naviagation synchronization switch (FMS data) •VOR/ILS/ADF NAV-4000 Collins •DME DME-4000 Collins •Radio altimeter ALT-4000 Collins •Pilot GPS/SBAS Chelton interfaced to EFIS/FMS •Co-pilot GPS/SBAS Chelton interfaced to EFIS/FMS •4-axis dual duplex digital AFCS with integrated Flight Director •ELT C406-N HM Artex (with Navigation Interface Module embedded) •Moving map EURONAV V with 8.4” Display •Enhanced Vision System (EVS) EVS-1500 Max-Viz •Second Radio Management System (RMS) RTU-4210 Collins •Second VHF/AM VHF-4000E Collins •Digital Audio Control System (DACS) NAT additional cockpit panel •Second electronic clock •Second magnetic compass indicator •Second Altitude Heading Reference System (AHRS) •Second Air Data unit (ADU)

    Additional Equipment

    Additional Equipment
    •Blade Tie Downs •Engine Air Intake Covers •Exhaust Covers •Towing bar •Crash-resistant pilot and co-pilot seat, fore and aft adjustable, with lap belts and headrest •Shoulder harness with inertial reels (pilot and co-pilot) •Active Noise Reduction (ANR) headsets (pilot and co- pilot) •Crew open door actuators •Reinforced windshields •Windshield wipers (pilot and co-pilot) •Retractable/rotating landing light (nose mounted) •Electrically Operated Passenger Step (LH & RH) •Engine compartment fire extinguishers (Qty 2) •Engine washing kit provisions •Rotor brake •Emergency floats (Fixed provision parts) •5 cells crash-resistant fuel system (213 US gal) with fuel drain electrical valves •Baggage compartment extension (2.3 m) •Baggage compartment lights •Tailboom strake •Fuel cap with key lock •Pulsed chip detectors (in lieu of quick disconnecting chip detectors) •Strobe Lights on Horizontal Stabilizers •Map Lights for Pilot/Co-Pilot •Dual controls •Pilot Multipurpose Holder •Pilot/Co-Pilot Console Tray •Airframe Hourmeter

    Exterior

    Exterior Notes
    Standard color scheme from Company paint selection, solid color

    Interior

    Interior Notes
    • Air conditioning ECS (Environment Control System) • Primer finished cabin walls • VIP interior completion 5 seats, 5 ANR headsets • Sheepskin Covers (crew seats) • Dome light cockpit • Set of 3 Drawers


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