Leonardo AW139

- 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 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 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 Co-pilot Multi 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 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 co-pilot headsets
- Pilot and co 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
- 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)
- Two Air Data Modules (ADM)
- One magnetic compass
- One outside air temperature indicator
- Pilot and co co-pilot digital audio panels with remote ICS audio port for ground operation

- Forced fan ventilation
- Bleed air heater and defroster with air noise suppressions
- Cockpit air ventilation system
- Baggage compartment cargo tie tie-down fittings for increased load capacity (up to 300)
- Rotor brake
- 1st radar altimeter RT RT-300
- 2nd radar altimeter RT RT-30 0
- 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 ADSB-Out 1090 MHz) incorporated into the Modular Radio Cabinet (MRC)
- Cockpit Voice Recorder & Flight Data Recorder
(CVR/FDR) with Underwater Locator Beacon (ULB)
- Air conditioning system
(*) Accessory drive is required if the air conditioning system is installed in conjunction with FIPS
- Weather Radar Primus 660 Honeywell
- Cargo hook (2200 kg / 4850 lb ) - Provisions
(*) Including cargo hook monitoring cameras
- Emergency floats
- Rescue hoist (Breeze)
(*) Including light
(*) Including light Polycon(*) Including light (*) Including light(*) Including light (*) 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 7,000kg

HEMS/SARS/12 SEAT VIP CONFIGURATIONS AVAILABLE



- Pilot and co-pilot crashworthy seats (with inertias reels and safety belts)
- Cockpit dome/storm light
- Cockpit utility lights (2)
- 28 V DC cockpit/cabin power outlet
- Cockpit panel sun-glare shields
- Overhead cockpit windows sun shades
- Fluorescent emergency exit signs
- Cockpit map and data case in central console
- Two flash lights for pilot and co-pilot
- ICS panel with plug for one headset (LH side)
- First aid kit

Choice of Exterior Paint Work

- 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 co-pilot (*) Required for single pilot IFR operations. Alternative to
central approach plate chart holder