2024 Airbus Helicopters H125

• H125 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

• 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 dual-strap shoulder harnesses
• 2 place rear bench-seats, foldable separately, complete with cushions, safety belts and single-strap 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

• 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 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 connected to aural warning issued from VEMD
  • 1 cockpit imaging and flight data monitoring device
  • Standby instruments
    • 1 Electronic Standby Instrument (ESI)
    • 1 magnetic compass
  • Wireless Airborne Communication System (WACS)
  • 1 LCD Dual screen Vehicle and Engine Multifunction Display (VEMD) providing the following information:
    • First Limitation Indicator (FLI)
      • Torque meter
      • Exhaust gas temperature (TOT)
      • Gas generator tachometer (N1)
    • Engine oil temperature/pressure
    • Fuel quantity
    • Fuel flow and estimated remaining time to fly
    • Ammeter and voltmeter and battery temperature
    • Outside Air temperature (OAT)
    • Enhanced usage monitoring functions
      • IGE/OGE performance calculations
      • Engine cycles counting
      • Engine power check
      • Over-limit display
    • VEMD and peripheral maintenance information
    • Data downloading capability

• 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

• 1 Arriel 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 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

• 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

• 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 a load compensation system

• One 150A, 28 V DC starter-generator
• One 28 V DC cabin power outlet
• One 15 amp.hr 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)

• 1 pitot head cover
• 2 static port stoppers
• 1 engine air-intake blanking cover
• 1 exhaust pipe blank
• 2 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 VFR Day and night Package, with Integrated Flight Display with Garmin G500H TXi included in Baseline definition.  

• Emergency locator transmitter – Kannad INTEGRA 406 AP-H
• VHF/VOR/LOC/GS – Garmin GNC 255A
• Intercom system (ICS) – Garmin GMA 350H
• Transponder (mode S) – Garmin GTX 335R-ADS-B out
• VHF/VOR/LOC/GS/GPS – Garmin GTN 650Xi
• Avionics display system Garmin G500H TXi

Including:

• Display-PFD RH unit
• Air Data, Attitude and heading Reference System Unit (ADAHRS)
• Magnetometer Unit
• Outside Air Temperature probe

• ICS Installation compatible with Bose Aviation X headset
• Light Data Recorder (LDR)
• Hour meter
• Supply six (6) Bose A20 Bluetooth Aviation headsets compatible with the ICS installation

• Genesys HeliSAS 2 axis Autopilot kit HELI-0009 in accordance with EASA STC 10041971
• Kit to increase Internal Gross Weight to 2370 k, 5,225 lb), including the Dual hydraulic circuit
• First Aid kit
• High visibility paint scheme on main rotor blades (white, red or yellow stripes)
• Tinted windows for standard and optional door configuration
• Bulged window on right and left rear door
• Pilot windshield wiper
• Dual controls
• Lean Instrument Panel (LIP) in place of the baseline Instrument Panel
• Cargo swing (1400 kg – 3,080 lb) – Fixed Parts
• LH landing Light (swiveling in elevation and azimuth)
• Emergency floatation gear – Fixed Parts
• Tablet holder on Lean Instrument Panel (LIP) L/R side

• Comfort lay-out 5 passengers seats

• Complex exterior painting instead of standard painting