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...

Avionics

ADSB

Multifunction Transponder ADS-B Out/TCAS II Coupled with AFCS

Traffic

TCAS II - 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

Fail Passive Dual Duplex Digital Automatic Flight Control System (4-axis type) Including Upper and Safety Modes (in Particular Auto Hover and Recovery Modes); 1 Automatic Pilot Control Panel (APCP)

Audio

DACS - Digital Communication System (DCAS) basic pack for pilot and copilot, two headset holders in cockpit, 2 DACS

Weather

Telephonic RDR1600 - Weather/Search Radar

PFD

4 Reconfigurable Smart 6x6-Inch Displays Providing Primary Flight Display (PFD), Navigation Display (ND), Automatic Flight Control System (AFCS), Fuel Data, First Limit Indicator (FLI), Rotor Speed and Free Turbine Rotation Speed, Crew Selectable Area, Alarms and Advisories

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

GPS

HR Smith Series 503 - Emergency Locator Transmitter (ELT) with Embedded GPS; ADELT HR with GPS Connection

Additional Equipment

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; Environment Control System (ECS) – Separate Cockpit / Cabin Ventilation & Heating and Air Conditioning, Cockpit Demisting

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

Emergency Floatation Gear

Emergency Floatation Gear with Automatic Percussion – Fixed Parts/Removable Parts; External Life Raft Installation with PLB Compart – Fixed Parts

Helicopter Emergency Egress Lighting (HEEL)

Cockpit Video Camera with Embedded Recorder

CVFDR

CVFDR – Solid State Cockpit and Flight Recorder

Flight Data Continuous Recorder (FDCR)

Flight Data Continuous Recorder (FDCR) for HFDM (Helicopter Flight Data Monitoring) (HELIONIX Suite)

Health Monitoring System (HMS)

Light HMS – Health Monitoring System

Helicopter Terrain Awareness Warning System

Helicopter Terrain Awareness Warning System (HELIONIX Suite)

Synthetic Vision System

Synthetic Vision System (HELIONIX Suite)

Enhanced Cargo Hold

Enhanced Corrosion Protection

Interior & Exterior

Interior Notes: COCKPIT / CABIN 2 removable pilot and co-pilot crashworthy high back-rest black covered seats, adjustable in height, forward and aft; each fitted with 5 points harness 1 windshield including sunshade in the upper area 2 lateral windows 2 nose windows 2 lockable hinged pilot and co-pilot doors providing each one: - Jettisonable window for emergency egress - 1 bad weather window - 1 lower window 2 external cockpit footsteps 1 first aid kit 2 tablet holders in cockpit Dual flight controls Windshield washer 2 windshield wipers 2 headset hooks on overhead panel 2 handles in cockpit (one on each side on upper frame of the canopy) Storage box in center console, on instrument panel and removal storage box on floor (pilot side) 4 jettisonable windows located in cabin 2 portable fire extinguishers, one in cockpit and one in cabin Handles in cabin (2 on each side of each cabin door) Dual zone air conditioning system with control in cockpit Standard key Capability to access the cargo compartment through cabin Emergency floatation gear with automatic percussion – Fixed Parts/Removable Parts External life raft installation with PLB compart – Fixed Parts Helicopter Emergency Egress Lighting (HEEL) ADELT HR SMITH series 503 with GPS connection – Fixed Parts/Removable Parts 2 enlarged cabin sliding doors 6-passenger ACH Line Lounge installation package (4+2) with one rear cabinet