Opis:

Full Anti Ice System - FIPS 6800 kgs, Increased Weight Option. 600 hour Inspection complied with at AW Yeovil.
Agusta Westland maintained since new.

Engine Specs:
2 x Pratt & Whitney Canada PT6C-67C - 589 hours TT.
------------
Avionics/Radios:
1st PFD (Pilot Primary Flight Display 8" x 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" x 10" colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data.
1st MFD (pilot Multifunction Display 8" x 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 Multifunction Display 8" x 10" colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data.

Central Maintenance Computer - CMC (single)
Two VHF Comm
One Mode-S Diversity Transponder
One VORILOC/GSIMB - One ADF One DME
Two pedestal mounted MCDUs (Multi Control Function Display Units)
Pilot and co-pilot interphone control (cyclic grip and floor switches)
1st Radar Altimeter (RT - 300) 2nd Radar Altimeter System (RT - 300)
Emergency Locator Transmitter (ELT)
One Flight Guidance Controller
Honeywell GPS module with Flight Plan Management System (FPMS)
Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation
Pilot clock (digital) Co-pilot clock (digital)
Magnetic compass Outside
Air Temperature indicator
Two (2) Master Warning Lights (MWLs)
Two (2) Master Caution Lights (MCLs)
Engine 1 Fire Light — Engine 2 Fire Light

Two (2) Master Warning Lights (MWLs), Two (2) 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)
One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data)
Two (2) Attitude and Heading Reference Systems (AHRSs)
Two (2) Air Data Modules (ADMs)
Two (2) flux valves Two (2) Display Controllers (DCs)
Two (2) Cursor Control Devices (CCDs)
Reversion Control Panel (RCP)
Display Dimming Control Panel (DCP)
Stability Augmentation System (SAS) control panel
Two (2) Remote Instrument Controllers (RICs)
4-Axis Digital Automatic Flight Control System - DAFCS (dual) with auto trim function CVR/FDR
Flight Director System (dual) , Pilot and co-pilot microphone and headset
Two Modular Avionic Units (MAUs
Monitor Warning System - MWS (dual) Aural Walling Generator - AWG (single)
------------
Additional Equipment:
IFR Configured
Auxiliary fuel tank provision
Air conditioning
Emergency floats
Additional anti-collision light under fuselage
TCAS I Bendix King fixed provisions
TCAS I Bendix King KTA-970
Weather radar (Primus 660) fixed provisions
Baggage Load Capacity Increase to 300 kg
Central Approach Plates Chart Holders with Light
Strobe Light on the Sponson/Elevator
VHF/FM NPX-138 NAT Tactical Radio
Aircell Satphone.

Approach plates chart holders with lights for pilot and co-pilot
5th display in cockpit
(moving map EuroNav V with standard aeronautical charts)
Auxiliary heavy duty battery 27 Ah (in lieu of 13 Ah)
4 axis autopilot (no hover mode)
DMU (Data Management Unit)
Enhanced Ground Proximity Warning System (EGPWS)
Lightning Sensor System Honeywell LSZ-860
TCAS 1 KTA-970
Transponder 2nd unit
Emergency floats
Emergency floats Kevlar covers
Strobe lights on the winglets
Auxiliary transversal fuel tanks 132 USgal
SATCOM Iridium ST3100 Aircell
(ICS integrated with cabin handset in fashion cabinet)
Accessory drive MGB required by the installation of FIPS in conjunction with ECS
EVS (Enhanced Vision System) EVS-1500 MaxViz (dual field of view and image processing)
Full Ice Protection System (FIPS) fully upgraded to the latest modification standard,
Including heated glass windshield and ice detector system
------------
Interior:
VIP interior - Six seat cabin layout:
Passenger cabin thermo acoustic tinted double layer windows
Hydraulic pulsation dampeners
Active Vibration Control System (AVCS) complete installation
MGB Premium grade
Cyclic and collective leather gators (same colour as cabin interior)
Cabin vertical handles metal finished on doorposts (Qty 2)
Alternate Current (AC) power outlet (28V/115V 50 Hz) (Qty 4)
Coat hooks (Qty 4)
Passenger cabin hinged doors
Pilot and co-pilot adjustable leather covered seats.
Pilot headset hooks (Qty 2)
7th seat (captains seat) in lieu of fashion cabinet.