2021 Leonardo AW139 for sale, England, United Kingdom

- 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)

- 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 PAINTWORK

- AgustaWestland painting scheme, metallic color from Company selection
- Main rotor blades high visibility painting
- 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)

- 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
- 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 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
- Adelt