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Agusta AW139
Fotografías: aircraft24.com · Ver el anuncio original
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Agusta AW139

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Especificaciones

Año de fabricación
2011
Base
Leominster, Reino Unido
Anunciado por
Fly Q Limited

New Agusta AW139 - TT 0

Este modelo

La configuración habitual de este modelo. Esta aeronave puede diferir.

Homologación de tipo
EASA.R.006 — ficha de datos del certificado de tipo, EASA

Equipamiento

Lo que menciona el anuncio, a partir de la lista del vendedor de abajo.

  • GPS para aproximaciones IFR sí
  • Piloto automático sí
  • Cabina digital sí
  • ADS-B sí
  • Transpondedor sí

Tal como lo anunció el vendedor

  • 1st PFD (Pilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System
  • 2nd PFD (Copilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System
  • 1st MFD (pilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System
  • 2nd MFD (Copilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System
  • Electronic Standby Instrument System (ESIS)
  • Two Attitude and Heading Reference Systems (AHRSs)
46 elementos más
  • Two Air Data Modules (ADMs)
  • Two flux valves
  • Two Display Controllers (DCs)
  • Two Cursor Control Devices (CCDs)
  • Reversion Control Panel (RCP)
  • Display Dimming Control Panel (DCP)
  • Stability Augmentation System (SAS) control panel
  • Two Remote Instrument Controllers (RICs)
  • Two Modular Avionic Units (MAUs)
  • Vehicle Monitoring System - VMS (dual)
  • Monitor Warning System - MWS (dual)
  • Aural Warning Generator - AWG
  • Central Maintenance Computer - CMC
  • 4-Axis Digital Automatic Flight Control System - DAFCS (dual) with auto trim function
  • Flight Director System (dual)
  • VHF Comm
  • Mode-S diversity transponder
  • VORILOC/GSIMB
  • ADF
  • DME
  • Two pedestal mounted MCDUs (Multi Control Function Display Units)
  • 1st Radar Altimeter (RT - 300)
  • 2nd Radar Altimeter System (RT - 300)
  • Emergency Locator Transmitter (ELT)
  • Flight Guidance Controller
  • Honeywell GPS module with Flight Plan Management System (FPMS)
  • Pilot and copilot digital audio panels
  • Pilot clock (digital)
  • Copilot clock (digital)
  • Magnetic compass
  • Outside Air Temperature indicator
  • Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
  • TCAS I Bendix King KTA-970
  • Weather radar (Primus 660)
  • EGPWS (Enhanced Ground Proximity Warning System)
  • ADELT (2-frequency Automatic Deployable ELT w/GPS interface)
  • VHF/FM NPX-138 NAT tactical radio
  • Honeywell Autopilot
  • Dual VFR Transceivers
  • ATC Transponder
  • Dual VOR/ILS Receiver
  • ADF Receiver
  • DME Interrogator
  • VOR/MKR Receiver
  • Honeywell GPS
  • TCAS Computer

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