2023 Airbus Helicopters H125
SoldS/N: 9395
Highlights
- Cargo swing (1400 kg – 3,080 lb) – Fixed Parts/ Removable Parts
- Emergency floatation gear – Fixed Parts
Details
- 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 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
- 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.
- First Limit Indicator (FLI)
- 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 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
- 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 load compensation systems
- 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)
- 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
- 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)
- 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
- 5 passengers seats
- Complex exterior painting instead of standard painting
General
Cockpit / Cabin
Instruments
Avionics
Power Plant
Transmission System
Rotors and flight controls
Electrical Installation
Airborne Kit
Avionics: Single/ Dual Pilot Day and night VFR Operations
Optional equipment
Interior Layout
Exterior
Photo Gallery 2023 Airbus Helicopters H125
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