AW139 G-VIPG

Aircraft Details:

Interior: Three armchairs leather covered forward-looking (with inertial reels and safety belts, sliding inflight direction, reclining backrest), with the middle armchair foldable forward and the two lateral armchairs with foldable table,  Comfortable seat leather covered (x4) (with safety belts, storage compartment under the seats and the under-seat skirts), Two lateral covered armrests cabinets with metal cup holder, ICS Control, Multipurpose Cubby with 3 sliding doors, Super Silent Soundproofing, Electrically Operated Pax Steps (RH & LH), Customised VIP Cabin finishing, Ripple Dampers, Active Vibration Control System (AVCS)

Exterior: Immaculate white paintwork with navy accent stripes running nose to tail and to cowling

Additional Equipment: EGPWS Particle Separator Provisions, TCAS, Secondary Swiveling Landing Light, Weather Radar Honeywell Primus 660, Auxiliary Fuel Tanks (132 Usgal), EVS-1500 Max Viz, Auxiliary Heavy Duty Battery 27 Ah, Camera on Tail Fin, Emergency Float Provisions

Avionics: Honeywell Primus Epic System v 7.14, (Dual MFD & Dual PFD), Electronic Standby Instrument System (ESIS), Dual AHRS, Two Air Data Modules (ADMs), Dual Cursor Control Devices (CCD), Single Reversion Control Panel (RCP), Single Stability Augmentation System (SAS) control panel, Dual Remote Instrument Controllers (RICs), Dual Modular Avionic Units (Vehicle Monitoring System (VMS) dual, Monitor Warning System (MWS) dual, Aural Warning Generator (AWG) single, Central Maintenance Computer (CMC) single, 4-axis dual Digital Automatic Flight, Control System (DAFCS) Enhanced with Hover Mode (HOV), Provision for CVR/FOR data interface, Flight Director System (dual)), Dual VHF Comm, Dual VOR/LOC/GS/MB, Single Mode S Diversity Transponder, Single ADF, Single DME, Dual Radio Altimeter RT-300, Emergency Locator Transmitter (ELT), Dual Honeywell GPS module with Flight Plan Management System (FPMS), Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR} with Underwater Locator Beacon