AIRBUS H160 2024

AIRBUS H160 2024

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Status da aeronave: Disponivel

Consulte!

Faixa de preço: acima de R$35 milhões (over US$7mi)

Detalhes da aeronave:

Localização da aeronave: -
Ano de fabricação da aeronave: 2024
Horas totais de célula: 62
Horas totais do(s) motor(es): 62
Horas após revisão geral do(s) motor(es): -
Horas disponíveis até a próxima revisão do(s) motor(es): (Programa SBH e HCARE)
Todas as cadernetas desde novo: Sim
Total (crew + pax): 8 (2+6)
Seguro RETA: Em dia
Seguro CASCO: Em dia

Descrição da aeronave:

HELICÓPETO AIRBUS H160 2024 À VENDA

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)

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