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2023 Airbus Helicopters H125

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S/N: 9395

Highlights

  • Cargo swing (1400 kg – 3,080 lb) – Fixed Parts/ Removable Parts
  • Emergency floatation gear – Fixed Parts

Details

    General

    • Certified with a pilot being on the right side
    • Delivered with right side controls and capabilities for the removable dual controls.
    • Fuselage comprising the cabin and 3 luggage hold, with floor tie-down nets and access doors
    • Tail boom with stabilizer, anti-torque rotor and fin with tail skid
    • High skid landing gear with long footsteps (on right side and on left side), capable of taking handling wheels.
    • Lifting points
    • Mooring fixtures
    • Structural reinforcement for cable cutter system
    • Structural reinforcement for RH external mirrors
    • Single color exterior painting
    • Internal paint: grey (prevailing colour)
    • Interior signs and marking

    Cockpit / Cabin

    • Cabin floor in light-alloy sheet-metal with tie-down rings
    • 2 pilot and copilot high-back energy-absorbing seats, adjustable in reach, removable, complete with cushions, safety belts and shoulder harnesses
    • 2 position rear bench-seats, foldable separately, complete with cushions, safety belts and shoulder harnesses
    • 2 pilot and copilot jettisonable doors each fitted with a sliding window and with improved side-visibility window.
      • 1 RH large front door
      • 1 LH front door
    • Hinged rear right door-extension for passengers and cargo
    • 1 rear left sliding door
    • Locks on every access to cabin and luggage compartments
    • Lock on fuel cap
    • 2 tinted upper panes
    • 1 ceiling housing the ventilation ducts and controls (ventilation controls, rotor brake and fuel cut-off)
    • Cabin heating
    • Demisting system for front windscreens
    • Ram air ventilation duct
    • Fixed parts for pilot and copilot windshield wipers
    • 1 pilot document holder
    • 1 fire-extinguisher
    • 1 Flight Manual
    • Interior harmony according to definition in force

    Instruments

    • 1 integrated Flight Display: Primary Flight Display / Navigation Display (PFD/ND)
      • Primary flight data display: airspeed, vertical speed, attitude, altitude, T&B, HSI with VOR
      • Navigation Display
        • Nav data, flight plan
        • High resolution helicopter dedicated terrain & obstacle database
    • 1 stop watch
    • 1 LCD dual RPM tachometer (rotor and free turbine)
    • 1 warning panel
    • 1 heated pilot head
    • 1 external side slip indicator
    • 1 control box for light and electrical generation
    • 1 ICS connection to audio warning issued from VEMD
    • 1 Cockpit imaging and flight data monitoring device
    • Standby instruments
      • 1 Eletronic Standby instrument (ESI)
      • 1 magnetic compass
    • 1 LCD Dual screen Vehicle and Engine multifunction Display (VEMD) providing the following information:
      • First Limit Indicator (FLI)
        • Torquemeter
        • Exhaust gas temperature (TOT)
        • Gas generator tachometer (N1)
      • Engine oil temperature/pressure
      • Fuel quantity
      • Fuel flow and estimated remaining time to fly
      • Ammeter, voltmeter, and battery temperature
      • Outside Air temperature (OAT)
      • Enhanced usage monitoring functions
        • IGE/OGE performance calculations
        • Engine cycle counting
        • Engine power check
        • Overlimit display
      • VEMD and peripheral maintenance information
      • Data downloading capability.

    Avionics

    • 1 Emergency Locator Transmitter
    • 1 VHF/VOR/LOC/GS
    • 1 VHF/VOR/LOC/GS/GPS
    • 1 ICS + passenger interphone
    • 1 transponder (mode S -ADSB-out)
    • 1 avionics master switch

    Power Plant

    • 1 Arriel 2 D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) with back-up control system that automatically controls the engine in case of a total failure of the 2 digital channels of the FADEC
    • 1 Crash Resistant Fuel System including 1 tank of 540 liters (143 US gal) total capacity
    • 1 twist grip on pilot side (for engine reduction in case of tail rotor failure and autorotation training)
    • 1 magnetic plug and 1 chip detector
    • 1 engine lubrication and oil cooling system
    • 1 fire detection system
    • 1 air-intake protection grids
    • 1 torque-measurement pick-up

    Transmission System

    • 1 main gearbox, anti-vibration mounted with oil sight gauge, chip detector, oil temperature and pressure switches, port for endoscope and self-sealing valve for oil sampling and draining.
    • 1 main gearbox oil cooling system
    • 1 engine to main gearbox coupling shaft
    • 1 rotor brake
    • 1 main rotor r.p.m sensor and high and low r.p.m warning device
    • 1 tail drive carried by five anti-friction bearings.
    • 1 tail gearbox with oil sight gauge, chip detector and port for endoscopic inspection

    Rotors and flight controls

    • 1 main rotor with 3 composite-material blades around a Starflex head fitted with spherical thrust bearings
    • 1 anti-torque rotor with 2 composite-material blades
    • 3 main rotor hydraulic servo units
    • 1 tail rotor hydraulic servo unit and load compensation systems

    Electrical Installation

    • One 150 A, 28 V DC starter generator
    • One 28 V DC cabin power outlet
    • One 15 A.h cadmium-nickel battery
    • 1 ground power receptacle
    • 3 position lights (LED)
    • 1 flashing anti-collision light (LED)
    • 2 fixed landing lights
    • 2 adjustable emergency/reading map lights for crew
    • 2 adjustable reading lights for passengers
    • 1 integrated instrument-panel lighting system
    • 1 integrated lighting in central console
    • 2 cockpit breaker panels
    • 1 USB charging dual outlet (instrument panel)

    Airborne Kit

    • 1 port plug (pitot)
    • 2 static port stoppers
    • 1 engine air-intake blanking cover
    • 1 exhaust pipe blank
    • 2 hydraulic ground handling wheels
    • 1 cargo net and rope
    • 2 upper mooring rings
    • 3 main-blade socks and pole
    • 1 tail rotor locking device.
    • 1 lifting ring
    • 1 document holder
    • 1 airborne kit stowage bag

    Avionics: Single/ Dual Pilot Day and night VFR Operations

    • Emergency locator transmitter – Kannad INTEGRA AP-H
    • VHF/VOR/LOC/GS – Garmin GNC 255A
    • Intercom system (ICS) – Garmin GMA 350H
    • Transponder (mode S) – Garmin GTX 335R
    • VHF/VOR/LOC/GS/GPS – Garmin GTN 650H
    • Avionics display system Garmin G500H Txi
    • 4 LCD Dual Screen Vehicle and Engine Multifunction Display (VEMD)

    Optional equipment

    • Tail rotor arch
    • Enhanced Engine Air Particle Separator
    • Dual controls
    • Starter-generator Skurka 200A, instead of Skurka 150A in baseline
    • RH side electric and de-iced external mirror – Fixed Parts/ Removable Parts
    • Cargo swing (1400 kg – 3,080 lb) – Fixed Parts/ Removable Parts
    • Capabilities for extended cargo swing
    • Emergency floatation gear – Fixed Parts
    • Left side two-place front bench seat (pilot on right side) – Fixed Parts
    • Headset – David Clark H10-13H (Q.ty 2)
    • Radio altimeter Thales AHV 16, remote controlled
    • Light Data Recorder (LDR)
    • VEMD Data download kit

    Interior Layout

    • 5 passengers seats

    Exterior

    • Complex exterior painting instead of standard painting
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