Specifications

Description

Details Baseline configuration is composed of Airframe Rotors and controls Power plant and fuel system Transmission drive system and hydraulic system Electrical system Standard avionic Package (reported here under) Interior (reported here under) Painting (reported here under) Avionic Premium Equipment (reported here under) Optional Equipment Inlet Barrier Filter Provisions Electrically operated step (Left & Right) with boarding lights Auxiliary transversal fuel tanks 132 US gallon (FP& RP) Emergency floats FP Kevlar covers 1 X Camera on tail fin and 2 X Belly cameras Increased Gross weight 7.000 kg Liferaft provisions Auxiliary heavy-duty battery 28 Ah in lieu of 13 Ah Strobe lights Pilot & Copilot Glass windshields Main rotor tracking signal connector in cockpit AVCS Active Vibration Control System Pilot/ Co-pilot adjustable seats with sheep shin covers Interior Completion VIP Transport: Five Star Customized cabin Five Star Interior Layout – 7 seats 3 X VVIP crashworthy armchairs leather covered-forward looking, 4 X VIP crashworthy armchairs leather covered. 2 X additional aft facing Comfortable seat leather covered installed in the central raw (not installed) Air Conditioning System Mast Vibration Absorber (MVA) VVIP ultra silent soundproofing Night curtain separator Headsets Bose ANR type with Bluetooth capable (X 2) Multipurpose cubby with hinged cabin Night curtain cabin separator Passenger cabin hinged doors ICS in the cabin for all passengers (ICS phone to speak with pilots) Passenger cabin thermos acoustic double layer tinted windows Cockpit tinted upper windows (smoked colour) Co-pilot hinged window 2 X Pilot headset hooks Approach plates chart holders with lights for pilot and co-pilot Cockpit air ventilation system 02 X 115V AC power outlets in cabin and one 28V DC power outlet in cockpit Baggage compartment cargo tie-down fittings (up to 300 kg) Avionic Package: Single Pilot Configuration Night VFR/IFR (EASA/ FAA) Epic Primus Avionics Suite Software Phase 7 1st PFD (Pilot Primary Flight Display 8″ × 10″ colour 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″ colour 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″ colour 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″ colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data 1 X Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data) 2 X Attitude and Heading Reference Systems (AHRS) 2 X Air Data Modules (ADM) 2 X flux valves 2 X Display Controllers (DC) 2 X Cursor Control Devices (CCD) 1 X Reversion Control Panel (RCP) 1 X Display Dimming Control Panel (DCP) 1 X Stability Augmentation System (SAS) control panel 2 X Remote Instrument Controllers (RIC) 2 X 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) Pilot and co-pilot headsets Pilot and co-pilot interphone control (cyclic grip and floor switches) Left Modular Radio Cabinet (MRC) with the following modules: 1 X VHF Comm. 1 X VOR/LOC/GS/MB Right Modular Radio Cabinet (MRC) with the following modules: 1 X VHF Comm. 1 X VOR/LOC/GS/MB 1 X ADF 1 X DME 2 X pedestal mounted Multi-function Control Display Units (MCDU) Emergency Locator Transmitter (ELT) 1 X flight guidance controller Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation Pilot clock (dig