Turbine Leonardo

Honeywell Primus Epic Avionics Suite 4-axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hovermode (HOV) Dual PFD Dual MFD Single ESIS Dual AHRS Dual ADM Dual Display Controllers Dual Cursor Control Devices Dual Modular Avionics Unit Dual VHF Radio Dual NAV Radio Single Mode-S Transponder Single ADF Single DME Dual pedestal mounted Multifunction Control Display Units (MCDU) Dual Radio Altimeter Single ELT Dual GPS (WAAS/SBAS) EGPWS TCAS II Weather Radar

Exterior
FIVE STAR Cabin Interior including: 3 VVIP / crashworthy armchairs leather covered-forward looking, (with inertial reels and safety belt, sliding inflight direction, reclining backrest) One Divan crashworthy seat leather covered (with inertial reels and 4 ea safety belts and understorage compartment ) 2 lateral covered armrests cabinets with metal cup holder, ICS control and multipurpose holder installed on the divan seat ) 2 additional standard crashworthy seats leather covered, including dedicated carpeting Headsets Bose ANR type with Bluetooth capable Multipurpose Cubby with sliding doors Night curtain cabin separator Passenger cabin hinged doors Air conditioning system (Enviro) ICS in the cabin for all passengers (ICS phone to speak with pilots) Passenger cabin thermo acoustic double layer tinted windows Two 115V AC power outlets in cabin and one 28V DC power outlet in cockpit VVIP Ultrasilent soundproofing Cockpit tinted upper windows (smoked colour) Co-pilot hinged window Pilot headset hooks (Qty 2) Approach plates chart holders with lights for pilot and co-pilot Metallic Paint (beige) with black and gold stripes.

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 Gross Weight - 7000 kg Auxilary Fuel Tanks (132 USgal) Emergency Floats provisions, removables and Kevlar covers) Camera on Tail Fin Under Belly Cameras (2 ea) Auxiliary heavy duty battery 27 Ah/28 Ah capable of paralled starting with 44Ah battery, in lieu of 13 Ah