Description
-Only 225 Hours since New
-stunning VIP Interior and Custom Paint
-Two Owners since New, Leonardo Service Center Maintained
-no damage / no incidents
-Phase 4 Upgrade Complied With, Phase 6 Underway
-Can be Exported and Delivered Anywhere Worldwide
ENGINES
Model: Pratt & Whitney PW210A
ENGINE 1 ENGINE 2
Serial Numbers: PCE-BP0039 PCE-BP0012
Total Hours Since New: 175.3 170.7
Total Cycles Since New: 325 303
ENGINE 1 ENGINE 2
Serial Numbers: PCE-BP0039 PCE-BP0012
Total Hours Since New: 175.3 170.7
Total Cycles Since New: 325 303
Avionics
• Three Rockwell Collins Display Units 10” X 8” color AMLCD with LED backlight and NVIS
compatibility:
• 2 Primary Flight Displays and 1 Multi-Function Display
• Integrated Standby Instrument System (ISIS)
• Two Display / cursor Control Panels/Devices (DCP/CCD)
• Reversionary Control Panel (RCP)
• Two Master Caution / Warning Lights (MCL/MWL)
• Two Avionics Full Duplex Ethernet (AFDX) switches
• Two Aircraft Monitoring & Management Computers (AMMC)
• Data Transfer Device (DTD)
• Two touch screen control panels
• Four Axis Automatic Flight Control System (AFCS)
• Two Flight Control Computer (FCC)
• Flight Control System (FCS) Control Panel
• Two VHF-AM radios
• Two NAV (VOR/ILS/MB) receivers
• One ADF / DME
• Transponder with Enhanced Surveillance Mode (Mode S)
• First SBAS GNSS (GPS)
• Second SBAS GNSS (GPS)
• Two Audio Control Panels (Pilot and Co-pilot stations)
• Audio Management Unit interfacing external transceivers
• Passenger Intercom Amplifier
• Two flux valves
• Two Air Data and Altitude Heading Reference Systems (ADAHRS)
• Dual Radar Altimeter
• Pilot Clock/Co-Pilot Clock
• Moving map
• Health and Usage Monitoring System (HUMS)
• Flight Data Monitoring system (FDM)
• Helicopter Terrain Avoidance and Warning System (HTAWS)
• Synthetic Vision System (SVS)
• Enhanced Vision System – MaxViz EVS-1500
• TCAS III
• ADS-B Out
• Rotor brake system
• One solid state Cockpit and Voice Flight Data Recorder with ULB
• One Emergency Locator Transmitter (ELT – 3 frequencies) (fixed)
• Approach plates chart holders with lights for pilot and co-pilot
•
compatibility:
• 2 Primary Flight Displays and 1 Multi-Function Display
• Integrated Standby Instrument System (ISIS)
• Two Display / cursor Control Panels/Devices (DCP/CCD)
• Reversionary Control Panel (RCP)
• Two Master Caution / Warning Lights (MCL/MWL)
• Two Avionics Full Duplex Ethernet (AFDX) switches
• Two Aircraft Monitoring & Management Computers (AMMC)
• Data Transfer Device (DTD)
• Two touch screen control panels
• Four Axis Automatic Flight Control System (AFCS)
• Two Flight Control Computer (FCC)
• Flight Control System (FCS) Control Panel
• Two VHF-AM radios
• Two NAV (VOR/ILS/MB) receivers
• One ADF / DME
• Transponder with Enhanced Surveillance Mode (Mode S)
• First SBAS GNSS (GPS)
• Second SBAS GNSS (GPS)
• Two Audio Control Panels (Pilot and Co-pilot stations)
• Audio Management Unit interfacing external transceivers
• Passenger Intercom Amplifier
• Two flux valves
• Two Air Data and Altitude Heading Reference Systems (ADAHRS)
• Dual Radar Altimeter
• Pilot Clock/Co-Pilot Clock
• Moving map
• Health and Usage Monitoring System (HUMS)
• Flight Data Monitoring system (FDM)
• Helicopter Terrain Avoidance and Warning System (HTAWS)
• Synthetic Vision System (SVS)
• Enhanced Vision System – MaxViz EVS-1500
• TCAS III
• ADS-B Out
• Rotor brake system
• One solid state Cockpit and Voice Flight Data Recorder with ULB
• One Emergency Locator Transmitter (ELT – 3 frequencies) (fixed)
• Approach plates chart holders with lights for pilot and co-pilot
•
Exterior
Customized Paint Scheme - Overall Metallic Silver Paint
Blue and Black accent stripes
Retractable Landing Gear
Electrically operated cabin dual step
Baggage Compartment extension - Baggage smoke sensor
Blue and Black accent stripes
Retractable Landing Gear
Electrically operated cabin dual step
Baggage Compartment extension - Baggage smoke sensor
Additional Info
Anti-icing fuel systems and two magnetic chip detectors (one per engine)
• Independent dual-channel FADEC systems (one per engine)
• Fire detection / extinguisher system
• Crashworthy fuel cells (1140 litres of usable fuel)
• Filler port for gravity refueling (on left hand side)
• Dual independent, redundant hydraulic system
• Retractable swiveling Landing / taxiing lights (2)
• Provisions Only for Weather Radar
• Steps for cockpit / cabin access
• Overhead cockpit window sun shades
• First aid kit (as per JAR OPS 3)
• One cockpit and one cabin fire extingisher (as perJAR OPS 3)
• Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
• Independent dual-channel FADEC systems (one per engine)
• Fire detection / extinguisher system
• Crashworthy fuel cells (1140 litres of usable fuel)
• Filler port for gravity refueling (on left hand side)
• Dual independent, redundant hydraulic system
• Retractable swiveling Landing / taxiing lights (2)
• Provisions Only for Weather Radar
• Steps for cockpit / cabin access
• Overhead cockpit window sun shades
• First aid kit (as per JAR OPS 3)
• One cockpit and one cabin fire extingisher (as perJAR OPS 3)
• Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
