Descrição
AIRBUS H160 2024
FINANCIAMENTO DISPONÍVEL
O ÚNICO AIRBUS H160 À VENDA NO MUNDO
COM APENAS 62 HORAS TOTAIS
6 PASSAGEIROS
AERONAVE LANÇAMENTO E INOVAÇÃO HISTÓRICA DE TECNOLOGIA EMBARCADA E POTÊNCIA DOS MOTORES
GARANTIA DE FÁBRICA ATÉ JUNHO DE 2027
INSCRITO NOS PROGRAMAS SBH E HCARE
FLUTUADORES DE EMERGÊNCIA, HUMS
AVIÔNICOS E EQUIPAMENTOS ADICIONAIS:
- 4 reconfigurable smart 6×6-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:
- Main page: engine & vehicle status 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
- 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 Com- puter (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 n01 VHF/AM Collins VHF 4000 n02 VOR/ILS/MKR Collins NAV4500 n01 VOR/ILS/MKR Collins NAV4500 n02 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)
- 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
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
ROTORS & FLIGHT CONTROLS:
- 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)
