1st PFD (Pilot Primary Flight Display) 8" ×10" (external) Color Active Matrix Liquid Crystal Display as Part of Honeywell Primus Epic System for Visualization of Flight and Navigation Data
2nd PFD (Co-pilot Primary Flight Display) 8" ×10" (external) Color Active Matrix Liquid Crystal Display as Part of Honeywell Primus Epic System for Visualization of Flight and Navigation Data
1st MFD (Pilot Multi-Function Display) 8" ×10" (external) Color Active Matrix Liquid Crystal Display as Part of Honeywell Primus Epic System for Visualization of Flight and Navigation Data
2nd MFD (Co-pilot Multi-Function Display) 8" ×10" (external) 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 (AHRS)
Two Air Data Modules (ADM)
Two Flux Valves
Two Display Controllers (DC)
Two Cursor Control Devices (CCD)
One Reversion Control Panel (RCP)
One Display Dimming Control Panel (DCP)
One Stability Augmentation System (SAS) Control Panel
Two Remote Instrument Controllers (RIC)
Pilot and Co-pilot Headsets
Pilot and Co-pilot Interphone Control (cyclic grip and floor switches)
Pilot Clock (digital)
Co-pilot Clock (digital)
Two Modular Avionic Units (MAU) Incorporating the Following Major Subsystems and/or Functions:
Vehicle Monitoring System (VMS) Dual
Monitor Warning System (MWS) Dual
Aural Warning Generator (AWG) Single
Central Maintenance Computer (CMC) Single
Provision for CVR/FDR Data Interface (single)
Left Modular Radio Cabinet (MRC) with the Following Modules:
One VHF COMM
One VOR/LOC/GS/MB
Right Modular Radio Cabinet (MRC) with the Following Modules:
One VHF COMM
One VOR/LOC/GS/MB
One ADF
One DME
Two Pedestal Mounted Multifunction Control Display Units (MCDU)
Emergency Locator Transmitter (ELT)
One Flight Guidance Controller
Pilot and Co-pilot Digital Audio Panels with Remote ICS Audio Port for Ground Operation
One Magnetic Compass
One Outside Air Temperature Indicator
Two Master Warning Lights (MWL)
Two Master Caution Lights (MCL)
Engine 1 Fire Light
Engine 2 Fire Light
Baggage Compartment Smoke Detector Light
Dual Electrical Power Connection for CVR/FDR (FAA requirement compliant)
Equipment:
AW139 Standard Equipment
Forced Fan Ventilation
Bleed Air Heater and Defroster with Air Noise Suppressions
Cockpit Air Ventilation System
Baggage Compartment Cargo Tie-down Fittings for Increased Load Capacity (up to 300 kg)
Rotor Brake
1st Radar Altimeter RT-300
2nd Radar Altimeter RT-300
4-axis Dual Digital Automatic Flight Control System (DAFCS) Basic Incorporated into Modular Avionic Units (MAUs)
Flight Director System (dual) Incorporated into the Modular Avionic Unit (MAU)
Two Honeywell GPS Modules (GNSS/SBAS –Global Navigation Satellite System/Satellite Based Augmentation System) with Flight Plan Management System (FPMS)
One Mode S Diversity Transponder with Extended Squitter (ADSB-Out 1090 MHz) Incorporated into the Modular Radio Cabinet (MRC)
Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
Health & Usage Monitoring System (HUMS)
Increased Payload Package -Increased Gross Weight -6,800 kg
Additional Optional Equipment
AgustaWestland Painting Scheme, Metallic Color from Company Selection
Main Rotor Blades High Visibility Painting
Cockpit Tinted Upper Window (*)Smoked Color
Co-pilot Hinged Window (storm window)
Approach Plates Chart Holders with Lights for Pilot and Co-pilot (*) Required for Single Pilot IFR Operations. Alternative to Central Approach Plate Chart Holder
Air Conditioning System (*) Accessory Drive is Required if the Air Conditioning System is Installed in Conjunction with FIPS
Weather Radar Primus 660 Honeywell -Provision
Weather Radar Primus 660 Honeywell -Removable
Cargo Hook (2200 kg / 4850 lb) –Provision (*) Including Cargo Hook Monitoring Cameras Provision
