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Agusta - Aw139, 2020

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Agusta - Aw139, 2020

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13 February 2021
85

Avionics:

Standard Avionics Package
  • 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
  • Emergency Floats -Provision
  • Rescue Hoist (Breeze) –Provision (*) Including: ICS AV-900 Honeywell and Wireless ICS Polycon
  • Rescue Hoist (Breeze) –Removable (*) Including Light
  • Strobe Lights on the Winglets
  • Bubble Cabin Window (LH and RH) (*) not Compatible with Passenger Cabin Vertical Sliding Windows on Fixed Windows
  • Increased Gross Weight 7,000 Kg
  • Power Outlet 110V
  • Cabin Door Lighting
  • Ice Detector (RAD)
  • Standard Roof Liners with Dome Lights
  • Composite Liners –Painted(no soundproofing)
  • Rail Floor
  • Qty 3 Foldable Passenger Seats –3rd Row
  • Qty 1 Lightweight Crashworthy Passenger Seat –1st Row
  • 4-axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hover Mode (HOV)
  • Auxiliary Transversal Fuel Tanks 132 US gal Provision
  • Auxiliary Transversal Fuel Tanks 132 US gal Removable
  • Engine Wash Kit
  • HF Radio
Miscellaneous / Ground Equipment
  • Cargo Net in Baggage Compartment for Increased Load Capacity (up to 300 kg)
  • Covers and Flags: Engine Exhaust Pipes (2), Engine Air Inlets (2) and Pitot Tubes (2), Battery Connector Warning Flag (1)
  • Manuals: Aircraft Log, Engines Operations, Flight and Maintenance and Overhaul, Illustrated Parts Catalogue
  • Tie-down Assemblies for Main Rotor Blades (5)
  • Tail Rotor Blades Flapping Block (1)
  • Main Rotor Blades Sock Pole (1)
  • Main Landing Gear Wheel Chocks (2)
  • Main Rotor Balance and Tracking Chart, Tail Rotor Balance Chart
  • Nose Landing Gear Centrepin (1) and Landing Gear Handle Locking Pin (1)
  • Jacking Dome Assy(1)
  • Tow Bar (1)
  • Loose Equipment Bag (1)
Other aircraft Agusta - Aw139 (32)

Basic information:

Category: Helicopter
Manufacturer: Agusta
Model: Aw139
Year: 2020

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