2024 Airbus H160

General

Manufacturer

AIRBUS

Model

H160

Serial Number

1047

Registration #

LX-HGB

Condition

Used

Airframe

Total time

95

Power distribution system

- 2 primary bus bars

Lighting system

- 1 red/white tail fin anti-collision / strobe light

• 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

• 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
• 1 Fenestron type tail rotor with 10 composite material blades built into vertical fin
• 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)

• 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

• 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 1maintenance external ICS jack
• 1 breaker panel in nose
• 2 breaker panels in cockpit
• 1 emergency breaker panel in cockpit
• 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
• 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)

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

Avionics

Main page

engine & vehicle status

• STANDARD AVIONICS PACKAGE BASED ON HELIONIX SUITE
• Cockpit video camera with embedded recorder
• Tail fin video camera
• CVFDR – Solid State Cockpit and Flight Recorder
• Flight Data Continuous Recorder (FDCR) for HFDM (Helicopter Flight Data Monitoring) (HELIONIX SUITE)
• 2 duplex Aircraft Management Computer (AMC) (HELIONIX SUITE)
• Usage Monitoring System (HELIONIX SUITE)
• Light HMS – Health Monitoring System
• Emergency Locator Transmitter (ELT) with embedded GPS
• Radio altimeter AVH1600
• Dual Flight Management System installation with LPV approach function, search patterns and auto hover mode
• Digital Audio Communication System (DCAS) basic pack for pilot and copilot, two headset holders in cockpit
• Passenger address NAT 251
• VHF/AM Collins VHF 4000 n 1
• VHF/AM Collins VHF 4000 n 2
• VOR/ILS/MKR Collins NAV4500 n 1
• VOR/ILS/MKR Collins NAV4500 n 2
• VHF/FM NAT NPX 138 – Fixed Parts
• Collins DME 4000
• Multifunction transponder ADSB-Out/TCAS II coupled with AFCS
• Weather/Search Radar Telephonic RDR1600
• Digital MAP (HELIONIX SUITE)
• Helicopter Terrain Awareness Warning System (HELIONIX SUITE)
• Synthetic Vision System (HELIONIX SUITE)

• 4 reconfigurable smart 6x6-inch displays providing following functions:
• Flight Navigation Display page including:
• Primary Flight Display (PFD)
• Navigation Display (ND)
• Parameter tuning
• Automatic Flight Control System (AFCS)
• Fuel data
• First Limit Indicator (FLI)
• Rotor speed and free turbine rotation speed
• Crew selectable area (clock, etc.)
• Alarms and advisories
• Vehicle Monitoring Display (VMD) pages including:
• Fuel page
• Electrical system page
• Hydraulic / landing gear page
• Transmission page
• Enhanced usage monitoring page
• External video sources (when optional equipment is fitted)
• 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
• Stand-by compass
• Integrated Electronic Stand-by Instrument (IESI)
• 1 storage box

• 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

• 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

Equipment

• 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

Interior

• 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

Registration

Registration

LX-HGB