Nov. 2025 H130 immediately available for sale in France
Highlights:
IBF, Enhanced Air conditioning system, Cargo sling fixed parts, Dual external mirror etc.
manufacturer
Airbus
model
H130
configuration
Utility
condition
undefined
year
2025
time
5
helicopter location
France
serial number
TBD
registration number
TBD
listing ID
HT25695
Description
avionics
INSTRUMENTS
• Integrated Flight Display: Primary Flight Display/Navigation Display
• Stop watch
• Warning panel
• Magnetic compass
• Heated pitot tube
• External side slip indicator
• Control box for light and electrical generation
• ICS connection to audio warning issued from VEMD
• Cockpit imaging and flight data monitoring device
• Back-up instruments:
• Airspeed indicator
• Altimeter
• Gyro-horizon
• LCD dual RPM tachometer
• LCD dual screen vehicle and Engine Multifunction Display (VEMD) providing the
• following information:
• First limitation 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 cycles counting
• Engine power check
• Overlimits display
• VEMD and peripheral maintenance information
• Data downloading capability (software and connection wire are optional)
AVIONICS
• Avionics master switch
• VHF/VOR/LOC/GS
• VHF/VOR/LOC/GS/GPS
• Transponder (Mode S)
• Emergency Locator Transmitter
• ICS + passenger interphone
• Integrated Flight Display: Primary Flight Display/Navigation Display
• Stop watch
• Warning panel
• Magnetic compass
• Heated pitot tube
• External side slip indicator
• Control box for light and electrical generation
• ICS connection to audio warning issued from VEMD
• Cockpit imaging and flight data monitoring device
• Back-up instruments:
• Airspeed indicator
• Altimeter
• Gyro-horizon
• LCD dual RPM tachometer
• LCD dual screen vehicle and Engine Multifunction Display (VEMD) providing the
• following information:
• First limitation 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 cycles counting
• Engine power check
• Overlimits display
• VEMD and peripheral maintenance information
• Data downloading capability (software and connection wire are optional)
AVIONICS
• Avionics master switch
• VHF/VOR/LOC/GS
• VHF/VOR/LOC/GS/GPS
• Transponder (Mode S)
• Emergency Locator Transmitter
• ICS + passenger interphone
equipment
Enhanced Engine Air Particle Filter
Heavy Duty blade pins
Dual controls
ST/GEN 200a
Enhanced Air Conditioning System
Dual external mirror for cargo sling operation
Cargo sling (1500kg - 3307lb) - Fixed parts
Heavy Duty blade pins
Dual controls
ST/GEN 200a
Enhanced Air Conditioning System
Dual external mirror for cargo sling operation
Cargo sling (1500kg - 3307lb) - Fixed parts
engine 1
POWERPLANT
• Turbomeca ARRIEL 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 back-up fuel control box that automatically controls the engine in case of total failure of the 2 digital channels of the FADEC
• Crashworthy fuel system including 1 tank of 540 liters (143 US gal) total capacity
• Twist grip on pilot side (for engine reduction in case of tail rotor failure and autorotation training)
• Magnetic plug and 1 chip detector
• Engine lubrication and oil cooling system
• Fire detection system
• Air-intake protection grids
• Torque-measurement pick-up
• Turbomeca ARRIEL 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 back-up fuel control box that automatically controls the engine in case of total failure of the 2 digital channels of the FADEC
• Crashworthy fuel system including 1 tank of 540 liters (143 US gal) total capacity
• Twist grip on pilot side (for engine reduction in case of tail rotor failure and autorotation training)
• Magnetic plug and 1 chip detector
• Engine lubrication and oil cooling system
• Fire detection system
• Air-intake protection grids
• Torque-measurement pick-up
