Agusta AW139 - YOM 2012
Air conditioning | Auxiliary fuel tank provision | Auxiliary transversal fuel tanks – 132 gallons | Emergency floats provisions | Emergency floats removable | HEELS (Helicopter Emergency Exit Lighting System) | HUMS Provision | 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 | Baggage load capacity increase to 300 kg | Separate 4 points seatbelts (15 seats) | Central approach plates chart holders with light | Cargo hook (2200 kg/4850 lb) provision | Life Rafts (Qty 2) up to 17 passengers each | Strobe light on the sponson/elevator | ADELT (2-frequency Automatic Deployable ELT w/GPS interface) in lieu of standard ELT | Rescue Hoist single (Goodrich) provision | VHF/FM NPX-138 NAT tactical radio
1st PFD (Pilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data | 2nd PFD (Copilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data | 1st MFD (pilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data | 2nd MFD (Copilot Multifunction Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data | One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data) | 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) incorporating the following major subsystems and/or 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 (cyclic grip and floor switches) | Left Modular Radio Cabinet (MRC) with the following 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 for ground operation | 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 (FAA requirement compliant) | Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
Helicopter not as shown in the Picture.
