Airbus H130

AVIONICS
1 Emergency Locator Transmitter
1 VHFNOR/LOC/GS - Garmin GNC255A
1 VHFNOR/LOC/GS/GPS - Garmin G650Xi
1 ICS + passenger interphone - Garmin GMA350H
1 transponder (mode S - ADSB-out) - Garmin GTX335R
1 avionics master switch

INSTRUMENTS
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 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

Standby instruments:
• 1 Electronic Standby Instrument (ESI)
• 1 magnetic compass
1 LCD dual screen Vehicle and Engine Multifunction Display (VEMD) providing the following information:
• First Limit lndicators (FU) - 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 cycle counting, engine power check & overlimit display
• VEMD and peripheral maintenance information
• Data downloading capability (software and connection wire as option)

- Anti-Vibration Control System with 1 controller, actuators and accelerometers
- Fuselage comprising 3 luggage holds with floor tie-down nets, the cabin and access doors
- Tail boom with stabilizer, Fenestron® type anti torque rotor and tail skid
- Lifting points
- Mooring fixtures
- Tinted windows for front windscreens
- Dual controls
- Enhance Air conditioning system

SAFRAN ARRIEL 2D
Engine 1:
S/N: 53870
TSN: 50