This 2024 Airbus H160, registration LX-HGB, serial number 1047, is a used turbine helicopter located in Le Castellet, Provence-Alpes-Côte d'Azur, France. The airframe shows just 95 total hours. The aircraft is described with no damage history. It is enrolled in SBH and Hcare, and retains a factory warranty until June 2027. The listing highlights a VIP Lounge configuration, emergency floats, HUMS, CVFDR, an ADELT HR Smith with GPS connection, an extended cargo hold, and enhanced corrosion protection. The airframe is described as crashworthy, with a front fuselage housing the cockpit and nose avionics bay, an intermediate fuselage with a cabin...
ADSB
Multifunction transponder ADS-B Out/TCAS II coupled with AFCS
Traffic
Multifunction transponder ADS-B Out/TCAS II coupled with AFCS
Comms
NAT 251 - NAT VHF/AM, VHF VHF/AM, VHF VOR/ILS/MKR, VOR/ILS/MKR, VHF/FM, NAT NPX Fixed Parts, DME
AP
Dual Duplex Digital Automatic Flight Control System (4-axis type) including upper and safety modes (in particular Auto Hover and recovery modes)
Audio
DACS - Digital Audio Communication System (DCAS) basic pack for pilot and copilot, two headset holders in cockpit, 2 DACS Audio Control Panels
Weather
Telephonic RDR1600 - Weather/Search Radar
PFD
4 reconfigurable smart 6x6-inch displays providing Primary Flight Display (PFD) and Navigation Display (ND)
MFD
4 reconfigurable smart 6x6-inch displays providing Vehicle Monitoring Display (VMD) pages including Main page, Fuel page, Electrical system page, Hydraulic / landing gear page, Transmission page, Enhanced usage monitoring page, and External video sources
Cockpit Video Camera
Cockpit video camera with embedded recorder
Tail Fin Video Camera
Cockpit Voice and Flight Data Recorder
CVFDR – Solid State Cockpit and Flight Recorder, Flight Data Continuous Recorder (FDCR) for HFDM (Helicopter Flight Data Monitoring)
Health Monitoring System
Light HMS – Health Monitoring System
Emergency Locator Transmitter
Emergency Locator Transmitter (ELT) with embedded GPS
Radio Altimeter
AVH1600 - Radio altimeter
Flight Management System
Dual Flight Management System installation with LPV approach function, search patterns and auto hover mode
Emergency Floats
Emergency floatation gear with automatic percussion – Fixed Parts/Removable Parts
Life Raft
External life raft installation with PLB compart – Fixed Parts
Emergency Egress Lighting
HR Smith series 503 - Helicopter Emergency Egress Lighting (HEEL) ADELT HR with GPS connection Fixed Parts/Removable Parts
Air Conditioning
Dual zone air conditioning system with control in cockpit
Crashworthy Airframe
Crashworthy airframe comprising Front fuselage (cockpit & nose avionics bay), Intermediate fuselage including Cabin Luggage compartment with 2 lockable doors (LH & RH sides), Rear fuselage tail boom with Canted Fenestron & horizontal stabilizer, Cowlings and fairings, Built-in footsteps & handles to access upper deck for maintenance, Tricycle-type & electrically controlled retractable landing gear, Jacking, hoisting & mooring points
Main Rotor System
1 main rotor with 5 Blue Edge concept blades, 1 SPHERIFLEX motor head, 1 rotor mast fitted with rotor Top and Nr sensors, 5 interblade elastomeric dampers, Upper coning stop
Tail Rotor System
1 Fenestron type tail rotor with 10 composite material blades built into vertical fin
Flight Control System
1 Flight Control System (FCS) fitted with 3 dual-chamber /dual body main servo-units (on cyclic and collective pitch channels) and 1 dual-chamber / dual body rear servo-unit (on tail rotor pitch control channel), 1 “fail passive” Dual Duplex Digital Automatic Flight Control System (4-axis type) including upper and safety modes (in particular Auto Hover and recovery modes)
Transmission System
1 main gearbox with low oil level switch, oil pressure and temperature sensors, access to ports for endoscope and oil sampling, 4 chip detectors and oil cooling system, 2 free wheels integrated to the main gearbox, 1 dual lubrication system with 1 main pump and 1 emergency pump, 2 engine / main gearbox coupling devices (shaft and torque tube), 1 rotor brake system, 1 tail rotor drive shaft, 1 splash lubricated tail gearbox with 1 temperature sensor and 1 chip detector
Hydraulic System
2 independent hydraulic systems feeding main rotor and tail rotor actuators including level probes and sight gauges in oil tanks, 1 electro-hydraulic pump (on LH side) for ground assistance, Self-sealing hydraulic ports on each side for ground hydraulic power bench connection
Electrical System
1 DC power generation system: 2 starters / generators (300 A, 28 VDC), 2 electrical master boxes, 2 nickel-cadmium batteries 15 Ah including thermal switch and temperature probe, 1 DC emergency electrical generator, 1 external receptacle with 28 VDC power connector and 1 maintenance external ICS jack, 1 breaker panel in nose, 2 breaker panels in cockpit, 1 emergency breaker panel in cockpit. Power distribution system: 2 primary bus bars, 2 essential bus bars, 4 high load contactors (150 A), 2 USB (5V/2A) power supply plug on instrument panel, Cabin power supplies at rear console. Lighting system: 1 red/white tail fin anti-collision / strobe light, 3 position lights (red, green, white), 2 exterior emergency lights, Instrument panel, interseat console and overhead panel adjustable lightings, 2 flashlights, 1 dome light and 2 reading lights in cockpit, Cabin lights (including emergency lighting), 1 luggage retractable and swiveling front central landing light (must be replaced by optional equipment to be compliant with NVIS system). Radio on ground based on batteries (autonomous electrical power supply on ground)
Instruments
IESI - Stand-by compass, Integrated Electronic Stand-by Instrument (IESI), 3 Attitude and Heading Reference Systems (AHRS), 2 three-axis Magnetic Sensor Units (MSU) connected to AHRS, 3 heated pitot heads, 2 Air Data Units (ADU), 2 Temperature Probe Units (TPU), Wireless data device with SD card
Instrument Panel
4 reconfigurable smart 6x6-inch displays, 1 common control panel: Landing gear maneuver and position indicators, Windshield wiper and washer controls, Parking brake and nose wheel control panel, Capabilities for optional controls, Stand-by Instruments, 1 storage box
Interseat Console
APCP - 1 Automatic Pilot Control Panel (APCP), 1 Environment Control System (ECS) separate cockpit cabin ventilation heating and air conditioning, cockpit demisting, 1 lighting control panel, 1 ELT remote control panel, 1 radar control panel, 2 Advanced Flight Management and Control Display Units, 2 DACS Audio Control Panels
Overhead Panel
Electrical function and emergency cut-off controls, Fire detection / extinguishing controls, Engine controls, Engine auxiliary controls (training and chip burning), Hydraulics control, Pre-flight test and lamp test control, Rotor brake control grip, Capabilities for optional controls
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Le Castellet, Provence-Alpes-Côte D'azur, France
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Le Castellet, Provence-Alpes-Côte D'azur, France
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