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Airbus H130
Please Call
  • YEAR
    2019
  • LOCATION
    Europe, Turkey
  • S/N
    TBD
  • REG
  • TTAF
    Delivery Time Only

Aircraft Highlights

June 2019 delivery ACH130

  • VFR day and night package with Integrated Flight Display Garmin G500H , included in baseline definition
  • First Aid Kit - Stylence® layout
  • Engine flushing device without removal of cowlings
  • Enhanced Engine Air Particle Separator
  • Tinted windows for front windscreens
  • Sun protected upper windows
  • Dual controls
  • Enhanced Air conditioning system
  • Cargo Sling (1500kg) Fixed Parts
  • Landing light adjustable in site and azimuth
  • Emergency floatation gear - Fixed Parts
  • Stylence® layout - Silk Harmony
  • ICS installation compatible with Bose headset
  • Bose headset
  • Independent battery for back up for Stand-by gyro horizon Thales H321EGM (included in standard package)
• Avionics master switch
• 1 gyro-horizon
• 1 gyro-compass with - 1 horizontal Situation Indicator
• 1 turn and bank indicator
• 1 VHF/VOR/LOC/GS
• 1 VHF/VOR/LOC/GS/GPS
• 1 transponder (mode S)
• 1 altitude encoder
• 1 Emergency Locator Transmitter
• 1 ICS + passenger interphone

POWER PLANT
• 1 Turbomeca ARRI EL 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 a total failure of the 2 digital channels of the FADEC
• 1 crashworthy fuel system including 1 tank of 540 liters (143 US gal.) total capacity






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 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 rotor 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




• Cabin floor in light-alloy sheet-metal
• 1 pilot high-back energy-absorbing seat, adjustable in reach, removable, complete with cushions, safety belts and shoulder harnesses
• 6 passengers high-back energy-absorbing seats, removable, complete with cushions safety belts and shoulder harnesses:
• 2 front right, including for 1 copilot (copilot controls are optional)
• 4 rear row
• 2 cockpit jettisonable hinged doors
• 1 LH front door fitted with a sliding window
• 1 RH front door compatible with 8 seat layout
• 1 LH rear sliding door
• 1 RH rear sliding door
• Locks on every access to cabin and luggage compartments
• Lock on fuel cap
• Lateral and upper tinted windows (windscreen excluded)
• 1 ceiling housing the cabin lighting, 7 air ventilation outlets and controls (rotor brake and fuel cut-off)
• Dynamic ventilation system
• Cabin heating
• Demisting system for front windscreens
• 2 pilot document holders
• Door map case in LH and RH front doors
• Rear bulkhead and lateral rear upholstery
• 1 fire-extinguisher
• 1 Flight Manual in English

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 (FENESTRON) with 10 asymmetrical blades, integrated in vertical fin
• 3 main rotor hydraulic servo units (duplex servos)
• Integrated back-up control valve on each body of each duplex servo

HYDRAULIC GENERATION
• 2 independent hydraulic systems feeding the duplex servos

ELECTRICAL INSTALLATION
• One 150 A, 28 VDC starter-generator
• 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 cabin light sets, each with 2 reading lights for 2 rear passengers and 1 dome light
• 1 integrated instrument panel lighting system
• Integrated lighting in central console
• 1 reading map light on upper canopy strut for pilot
• 1 cockpit breaker panel
• One 28 V DC cabin power outlet

• 1 pitot head cover
• 2 static port stoppers
• 1 engine air-intake blanking cover
• 1 exhaust pipe blank
• 2 hydraulic ground handling bogies
• 1 cargo net and rope
• 1 lifting ring
• 2 upper mooring rings
• 3 main-blade socks and pole
• 1 document holder
• 1 airborne kit stowage bag
• 1 front air-intake blanking cover
• 1 fuel tank bleeding
• 3 ballast plates

• H130 Baseline Aircraft
• VFR day and night package with Integrated Flight Display Garmin GS00H , included in baseline definition
• First Aid Kit - Stylence® layout
• Engine flushing device without removal of cowlings
• Enhanced Engine Air Particle Separator
• Tinted windows for front windscreens
• Sun protected upper windows
• Dual controls
• Enhanced Air conditioning system
• Cargo Sling (1500kg) Fixed Parts
• Landing light adjustable in site and azimuth
• Emergency floatation gear - Fixed Parts
• Stylence® layout - Silk Harmony
• ICS installation compatible with Bose headset
• Bose headset (x2)
• Independent battery for back up for Stand-by gyro horizon Thales H321EGM (included in standard package)

• The H130® is certified with a pilot being on the left side
• The baseline aircraft is delivered with left side controls and capabilities for the removable dual controls (copilot controls are optional)
• Anti-Vibration Control System with 1 controller, actuators and accelerometers
• Fuselage comprising the cabin and 3 luggage holds, with floor tie-down nets and access doors
• Tail boom with stabilizer, FENESTRON® type anti torque rotor, and tail skid
• Tubular skid landing gear, with replaceable skid shoes, with long footsteps (on right and on left side), profiler on rear tube, capable of taking handling wheels
• Lifting points
• Mooring fixtures
• Single color exterior painting
• Internal paint: light grey (prevailing colour)
• Interior signs and markings in English

INSTRUMENTS
• 1 altimeter
• 1 vertical speed indicator
• 1 LCD dual RPM tachometer (rotor and free turbine)
• 1 stop watch
• 1 warning panel
• 1 magnetic compass
• 1 heated pitot 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
• 1 LCD dual screen Vehicle and Engine Multifunction Display (VEMD) providing the following information:
• First Limit Indicators {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 and 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 as option)

Airbus H130

Please Call
  • YEAR
    2019
  • LOCATION
    Europe, Turkey
  • S/N
    TBD
  • REG
  • TTAF
    Delivery Time Only
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Mehmet Yuksel Hocaoglu
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