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  • Alert Me Name: Airbus H130
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Airbus H130
Price: €2,890,000
  • YEAR
    2018
  • LOCATION
    Hong Kong, Asia
  • S/N
    861x
  • REG
  • TTAF
    6 H

Aircraft Highlights

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: available in either French or English.

 

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 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, available in either French or English ; Interior harmony according to definition in force.

 

1 Integrated Flight Display: Primary Flight Display/Navigation

Display ; 1 stop watch ;  1 Warning panel; 1 Magnetic compass; 1 Heated pitot tube; 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 ;

 

Back-up instruments:

1 airspeed indicator;1 altimeter;1 gyro-horizon;1 LCD dual RPM tachometer.

1 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).

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)

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)

 

1 avionics master switch;1 VHF/VOR/LOC/GS ;1 VHF/VOR/LOC/GS/GPS;1 transponder (Mode S);

1 emergency Locator Transmitter;1 ICS + passenger interphone.

 

1 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.

1 crashworthy 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 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 (FENESTRON) with 10 asymmetrical baldes, integrated in vertical fin.

3 main rotor hydraulic servo units 3 ,Integrated back-up control valve on each body of each duplex servo.

 

2 independent hydraulic systems feeding the duplex servos

 

One 150 A, 28 V DC 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 light ;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 panels; 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 wheels ;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 .

Airbus H130

Price: €2,890,000
  • YEAR
    2018
  • LOCATION
    Hong Kong, Asia
  • S/N
    861x
  • REG
  • TTAF
    6 H
User Image
Cong Li
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