2011 Leonardo Agusta AW139 - New

General

Seats

9

Avionics

• 1st PFD (Pilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display)
• 2nd PFD (Copilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display)
• 1st MFD (pilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display)
• 2nd MFD (Copilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display)
• One Electronic Standby Instrument System (ESIS)
• Two Attitude and Heading Reference Systems (AHRSs)
• Two Air Data Modules (ADMs)
• Two flux valves
• Two Display Controllers (DCs)
• Two Cursor Control Devices (CCDs)
• One Reversion Control Panel (RCP)
• One Display Dimming Control Panel (DCP)
• One Stability Augmentation System (SAS) control panel
• Two Remote Instrument Controllers (RICs)
• Two Modular Avionic Units (MAUs) together with major systems/functions
• Vehicle Monitoring System - VMS (dual)
• Monitor Warning System - MWS (dual)
• Aural Walling Generator - AWG (single)
• Central Maintenance Computer - CMC (single)
• 4-Axis Digital Automatic Flight Control System - DAFCS (dual) with auto trim function
• Provision for CVR/FDR data interface (single)
• Flight Director System (dual)
• Pilot and copilot microphone and headset
• Pilot and Copilot interphone control
• Left Modular Radio Cabinet (MRC) with modules
• One VHF Comm
• One Mode-S diversity transponder
• One VORILOC/GSIMB
• One ADF
• One 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)
• One Flight Guidance Controller
• Honeywell GPS module with Flight Plan Management System (FPMS)
• Pilot and copilot digital audio panels with remote ICS audio port
• Pilot clock (digital)
• Copilot clock (digital)
• One magnetic compass
• One Outside Air Temperature indicator
• Two Master Warning Lights (MWLs)
• Two Master Caution Lights (MCLs)
• Engine 1 Fire Light
• Engine 2 Fire Light
• Baggage compartment smoke detector light
• Dual electrical power connection for CVR/FDR
• Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)

Equipment

• Air conditioning
• Auxiliary fuel tank provision
• Auxiliary transversal fuel tanks – 132 gallons
• HEELS (Helicopter Emergency Exit Lighting System)
• HUMS (Health & Usage Monitoring System)
• Wire Strike Protection System (WSPS)
• Additional anti-collision light under fuselage
• TCAS I Bendix King fixed provisions
• TCAS I Bendix King KTA-970
• Weather radar (Primus 660) fixed provisions
• Weather radar (Primus 660)
• EGPWS (Enhanced Ground Proximity Warning System) fixed provisions
• Central approach plates chart holders with light
• Strobe light on the sponson/elevator
• External loudspeakers (400W) provision
• ADELT (2-frequency Automatic Deployable ELT w/GPS interface)
• VHF/FM NPX-138 NAT tactical radio