Leonardo - Aw139

• Dual PFD (8” × 10” Pilot Primary Flight Display)
• Dual MFD (8” × 10” Pilot Multifunction Display)
• One Electronic Standby Instrument System (ESIS)
• 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 Warning Generator – AWG (single)
- Central Maintenance Computer – CMC (single)
- 3–Axis Digital Automatic Flight Control System – DAFCS (dual) with autotrim 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 VOR/LOC/GS/MB

• Right Modular Radio Cabinet (MRC) with the following modules:
— One VHF Comm
— One Mode–S diversity transponder
— One VOR/LOC/GS/MB
— 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 – 121.5/243/406 MHz)
• 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)

CORPORATE 12 seats interior configuration:
12-padded crashworthy comfortable seats fabric or leatherette covered (with inertial reels and safety belts) disposed on 3 rows

CORPORATE cabin basic arrangement:
• Air conditioning
• Silent soundproofing
• Standard roof liners with LED dome lights
• Composite liners leatherette covered
• Passenger carpet
• ICS panel, one position in passengers cabin (LH side)
• P.A. (Passenger Address) System (including loudspeakers and safety belts lights)
• Fixed steps for passenger cabin access

Additional Proposed Equipment:
• MGB Premium grade
• Mast Vibration absorber (MVA)
• Passenger cabin thermo acoustic double
layer tinted windows
• Ripple dampers

Standard Item / Equipment:
• Cabin, cockpit and baggage compartment utility finishing interior
• Pilot/ Copilot crashworthy seats (with inertial reels and safety belts)
• Cockpit dome/storm light
• Cockpit utility lights (2
• 28V DC cockpit/cabin power outlet
• Cockpit panel sun-glare shields
• Overhead cockpit windows sun shades
• Floor provisions for 15-seat configuration
• Fluorescent lighted emergency exit signs
• Cockpit map and data case in central console
• Two flash lights for pilot and copilot
• Map and data cases in pilot and copilot doors
• ICS panel with plug for one headset
• First aid kit
• Air ventilator system
• Limited 4-Axis DAFCS
• Moving map Sky Force Observer MKIII with std aeronautics charts
• Honeywell Primus 660 Weather radar
• Ice Detector
• Storm Window for the Copilot
• HUMS
• Additional Anti-Collision Light
• Strobe Lights
• Emergency Floating System (provision and removable parts)
• Kevlar rigid covers for Emergency Floats
• Pilot and co-pilot adjustable seats (in lieu of std seats)
• Customized leather covering for Pilot and co pilot seats (same color as interior)
• Heated Windshield
• Enhanced Ground Proximity Warning System (EGPWS) (provision and removable parts)
• TCAS I KTA-970 Honeywell Bendix/King (provision and removable parts)
• Approaches Plates chart holder with light for pilot and co-pilot
• Auxiliary Heavy Duty battery 27 Ah (in lieu of 13 Ah)
• Active Vibration Control System (AVCS) provision
• Active Vibration Control System (AVCS) installation