For more information contact Robbie Merrigan Phone: + 353 1 8138817 Web site: www.mach.ie e-mail: info@mach.ie
Avionics
Honeywell Primus Epic System
Two 8" X 10" LCD Primary Flight Display
Two 8" X 10" LCD Multifunction Displays
One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass and ILS data)
Two Altitude and Heading Reference Systems (AHRS)
Two Air Data Modules (ADM)
Two Display Controllers (DC)
Two Cursor Control Devices (CCD)
One Reversion Control Panel (RCP)
One Display Dimming Control Panel (DCP)
One Stability Augmentation System (SAS) control panel
Two Remote Instrument Controllers (RIC)
Two Modular Avionics Units (MAU) incorporating the following major subsystems and/or functions:
Vehicle Monitoring System - VMS (dual)
Monitor Warming System MWS (dual)
Aural Warning Generator - AWG
Central Maintenance Computer - CMC
3-Axis Digital Automatic Flight Control System - DAFCS (dual) with autotrim function
Provision for CVR/FDR data interface
Flight Director System (dual)
Pilot and copilot microphone and headset, and 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)
Two Radar Altimeters (RT - 300)
Emergency Locator Transmitter (ELT - 121.5/243/406 MHZ)
One Flight Guidance Computer
Honeywell GPS module with Flight Plan Management System (FPMS)
Pilot & copilot digital audio panels with remote ICS audio port for ground operation
Digital pilot & copilot clocks
One magnetic compass
One outside air temperature indicator
Two Master Warning Lights (MWL)
Two Master Caution Lights (MCL)
Engine Fire Lights
Baggage compartment smoke detector
Dual electrical power connection for CVR/FDR (FAA requirement compliant)
Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
Additional Equipment
Autopilot 4 axis DAFCS
Additional Anti collision strobe lights under fuselage
Air conditioning system
Auxiliary fuel Tank provisions and equipment 132 USG
EGPWS provisions and kit equipment
RH and LH electrically operated passenger steps and step lights
TCAS
Weather Radar Primus 660
Interior
Passenger Cabin hinged doors in lieu of Sliding doors
Super silent Soundproofing
“Elite” passenger cabin Ceiling
Composite leather liners
Separation Wall cockpit/ passenger cabin electrically operated with curtains on pilot’s side
ANR headset battery powered
Armchair control panel for separation wall and entertainment system
SATCOM
CD and DVD system with 15” display
Passenger cabin handles
Passenger cabin thermo acoustic double layer tinted windows
Air conditioning system with control panel in passenger cabin
Super Silent Main Gearbox
3rd anti vibration mass in passenger area
Customized carpets
Dome lights
External Camera System with Two Views
8 Seat VIP configuration
Emergency Floats Kevlar Covers
Pilot/Co Pilot approach plate chart holders with Light
Auxiliary heavy duty battery 27 A/H
Heated glass windshield
Baggage Floor Carpet
Baggage Load increase to 300Kg
Light and heavy duty tow bars.
Don't forget to mention you spotted the aircraft online at International Aviation Sales
