N543AE - 2012 EUROCOPTER EC145


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    Aircraft Summary


    General

    Year
    2012
    Manufacturer
    EUROCOPTER
    Model
    EC145
    Serial Number
    9514
    Registration #
    N543AE
    Condition
    Used
    FlightRules
    IFR
    Based at
    KGPM
    Description
    Aka BK117C2. Aircraft Manufactured in the USA under Production Certificate PC343CE and Conforms to Type Certificate Data Sheet EASA.R.101 and FAA H13EU R12. Airbus Helicopters Maintained and Operated. Dual Pilot IFR (Not WAAS Certified), Utility Configured with Standard Production Release Avionics. Cabin interior adapted to BAE Crew and standard 8-Pax .

    Airframe

    Total Time
    2670
    Complete Logs
    Yes
    Airframe Notes
    See Sales Brochure under Service Logs Drop down Menu. Total Time Since New: ≈2,670 hours Projected Time at Delivery: Not To Exceed 2,700 Hours Dedicated Mission: Basic Utility Delivery: As Is/Where Is, Location: FOB Grand Prairie, TX Training, at AHI: 1 Pilot Transition/1 Technician.

    Rotor

    Main Rotor Blade Time Remaining
    22387
    Main Rotor Hub Time Remaining
    4760
    Main Rotor Gearbox Time Remaining
    2330
    Anti-Torque System
    Tail Rotor
    Tail Rotor Blade Time Remaining
    6654
    Tail Rotor Gearbox Time Remaining
    680
    Rotor Notes
    Tail Rotor and Intermediate Gearboxes can be extended by 300 hours. Intermediate Gearbox has 334 hours remaining before overhaul; may be extended to 634 hours TBO. T/R Gearbox has 680 hours remaining before overhaul; may be extended to 980 hours TBO.

    Modifications/Conversions

    Modifications/Conversions
    See Sales Brochure under Service Log Drop down Menu. CENTRAL PANEL • Central Panel Display System (CPDS) consisting of two LCD displays • Cautions and Advisories Display (CAD) with digital indication of: Caution and advisory information Fuel quantity indication • Vehicle and Engine Multifunction Display (VEMD) with digital indication of: Engine parameters (engine oil pressure, engine oil temperature) FLI (First Limit Indicator) for TQ, TOT,rN1 as analogue display Main gear box parameters (oil pressure, oil temperature) Dual amp meter for generator; ampere meter for battery Dual voltmeter Outside Air Temperature (OAT) Mast moment indicator • Back-up conventional instruments (2”) • Clock • Stand-by-horizon • Triple (rotor and engines) RPM-indicator • Warning unit • Engine fire warning with fuel emergency shut-off • Warning lights • Aural warning (for each warning, rotor RPM, fire warning) • Fire extinguishing system warning • Master caution light • Main switch panel • DC power control • VARTOMS control • Start switches • Magnetic compass AIR DATA • Dual pitot static system (electrically heated pitot tube and static port) • 2 ADC MEGHAS sensors STANDARD INSTRUMENTS (SINGLE PILOT) • Air speed indicator (3”) • Vertical speed indicator (3”) • Encoding altimeter (3”) • Artificial horizon (4”) • Gyro magnetic heading with horizontal situation ind. (3”)

    Avionics

    ADS-B Equipped
    Yes
    Artificial Horizon
    Yes
    Radar Altimeter
    Yes
    Single Pilot Operation
    Yes
    Auto Pilot
    Yes
    Wire Strike Protection System
    Yes
    Avionics/Radios
    See Sales Brochure under Service Logs Drop down Menu. Garmin GTX 330 Transponder Dual Garmin 430 GPS/COMM/NAV DME, CDM-451 *Wulfsberg C5000 V/UHF AM/FM System *Dual Wulfsberg UHF-FM P2000 System (STC SR00036MC-D) Marker Beacon Installation, KR 21 Radar Altimeter, KRA405B Nav/ILS/LPV Approach Switching for SMD 45 Displays Thales (4x) SMD 45 Displays Pilot, Copilot Rear Station Becker ACU 6100 Audio Controls *NVG/NVIS Lighting System (STC SR09303RC-D), Aircraft NVG Radios/Instrumentation NOTE: Items Marked with “*” may be ITAR Restricted if Aircraft is to be Sold outside USA.

    Additional Equipment

    Dual Controls
    Yes
    Cargo Hook
    Yes
    A/C
    Yes
    Heater
    Yes
    Baggage Compartment
    Yes
    Additional Equipment
    See Sales Brochure under Service Logs Drop down Menu Standard Gear with Full Length Steps Standby Attitude Gyro Engine Fire Detection and Extinguishing System Fuel Flow Display Cargo Sling System Fixed Provisions Fixed Provisions Hoist, Right Side Cable Cutter System (Wire Strike) Rotor Brake System 3-Axis Autopilot with Yaw SAS Controllable Landing/Search Light, 200W/400W External Lashing Points, 60 Knots Anti Collision LED Light (STC SR09303RC-D) Position LED Lights (STC SR09302RC-D) 44 AH Lead Acid Battery (STC SR09298RC-D) Dual Windshield Wiper System Carbide Skid Protectors, Brauer (STC SR03936AT)

    Exterior

    Year Painted
    2012
    Door Type
    Hinged and Sliding
    Exterior Notes
    Very Good Condition

    Interior

    Year Interior
    2012
    Configuration
    Passenger / Utility
    Interior Notes
    See Sales Brochure under Service Logs Drop down Menu Pilot & Copilot Energy Absorbing Height Adjustable BAE Seats (STC SR01938LA). 8-Passengers Standard Energy Absorbing Seats that can be configured from One to Eight independent seating arrangements. Alternate Nine (9) Passenger Utility BAE Troop Seats (can be negotiated), Loincoin Cabin Flooring Tinted Overhead Sunshades Slant and XL Center Consoles Freon Air Conditioning, Air Comm (STCSR00601DE) Dual Controls Cockpit Ventilation and Cabin Heat Crew & Cabin Door Window Vents (STC SR09308RC-D)

    Inspection Status

    Inspection Status
    CURRENTLY IN WORK and At 2650 hours total time: (1) Airframe 4800 hour/6 year Main rotor head inspection; (2) Airframe 800 hour/36 month Periodical completed; (3) Main Rotor Blades refurbished and processed through AHI Blade Shop.
    Airworthy
    Yes


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