1995 BELL 412EP


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    Aircraft Summary


    General

    Year
    1995
    Manufacturer
    BELL
    Model
    412EP
    Condition
    Used
    FlightRules
    IFR

    Airframe

    Total Time
    7095
    Max Takeoff Weight
    11,898.35 lb
    Basic Empty Weight
    7,806.57 lb
    Airframe Notes
    YOM August 1995 Total time 7,095 hours/7,431 landings Configuration Multirole Engine 2x PT6T-3DF Flight rule SP/DP IFR Registration FAA Highlights: •4,500 lbs/2,041 kgs cargo hook fixed parts •DART Simplex 375 gallon fire tank fixed parts •Litter fixed parts •600 lbs/272 kgs hoist fixed parts •SX16 search light fixed parts •Cargo mirror fixed parts •Wire strike protection system •TCAS II, GPWS •3 axis dual digital AFCS •Satellite tracking and communication •Air conditioning

    Rotor

    Main Rotor Blade Time Remaining
    338
    Main Rotor Hub Time Remaining
    339
    Main Rotor Gearbox Time Remaining
    3839
    Tail Rotor Blade Time Remaining
    896
    Tail Rotor Gearbox Time Remaining
    896

    Engine 1

    Engine 1 Manufacturer
    PRATT & WHITNEY
    Engine 1 Time
    156
    Engine 1 Time Since
    SOH
    Engine 1 TBO
    4000
    Engine 1 Notes
    Engine model Pratt & Whitney PT6T-3DF Engine 1 TT 7,925

    Engine 2

    Engine 2 Manufacturer
    PRATT & WHITNEY
    Engine 2 Time
    156
    Engine 2 Time Since
    SOH
    Engine 2 TBO
    4000
    Engine 2 Notes
    Engine model Pratt & Whitney PT6T-3DF Engine 2 TT 8,850

    Avionics

    Artificial Horizon
    Yes
    Radar Altimeter
    Yes
    Single Pilot Operation
    Yes
    Auto Pilot
    Yes
    ELT
    Yes
    Airborne Weather Radar
    Yes
    Traffic Avoidance System
    Yes
    Wire Strike Protection System
    Yes
    Avionics/Radios
    •3 axis dual digital AFCS •NAV/COM x2 •VHF VOR/LOC 108-118 MHz x2 •DME •ADF Bendix King •Marker receiver 75 MHz •Transponder with altitude reporting transmitter •Audio amplifier for COMM and NAV audio •Turn indicator •Artifical horizon x2 •Slaved direction gyro •Altimeters with barometric scales in milibars x2 •Chronometer x2 •Airspeed indicator x2 •Inertial lead vertical speed indicator x2 •Alternate static source •ELT 406 MHz •Weather radar •TCAS II •GPWS •Radio altimeter •Multi channel SSB HF 1-21 MHz •Dual GPS coupled to HSI •Satellite tracking and communication •NAT audio panel AMS 43 & AMS 44

    Additional Equipment

    Dual Controls
    Yes
    A/C
    Yes
    Additional Equipment
    •4,500 lbs/2,041 kgs cargo hook fixed parts •DART Simplex 375 gallon fire tank fixed parts •Litter fixed parts •600 lbs/272 kgs hoist fixed parts •SX16 search light fixed parts •Wide opening doors accomodating forklift loading •Cabin flat floor with 51 cargo restraint points •Additional baggage space in tail boom 0.8 m^3 •Landing light x2 •Dimmer for instrument light •Passengers compartment light •Seats and anchor points capable of lied stresses up to 9 ‘’G’’ •Cargo mirror fixed parts •Wire strike protection system •LED pulse lights •First aid kit •Air conditioning

    Exterior

    Door Type
    Sliding

    Interior

    Configuration
    Passenger / Utility
    Number of Seats
    13


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