Description
- VIP 6 Passenger Interior
- Extremely Low Total Time (1650)
- Increased Gross Weight (6,800 Kg)
- Air Conditioning
- Auxiliary Fuel Tank
- Equipped with CVR, EGPWS, TCAS 1
- No Damage History / Complete Records
- Previously N & C Registered
ENGINES
•Pratt & Whitney PT6C-67C
•SN’s PCE-KB0089 / PCE-KB0092
•1,620.8 / 1,620.8 Total Time
•3,705 / 3,705 Total Cycles
•SN’s PCE-KB0089 / PCE-KB0092
•1,620.8 / 1,620.8 Total Time
•3,705 / 3,705 Total Cycles
Maintenance
Delivery through 2022 Canada Based (C reg)
2023 USA Based (N reg)
Currently Operated and Maintained by Leonardo authorized facility
2023 USA Based (N reg)
Currently Operated and Maintained by Leonardo authorized facility
Avionics
Honeywell Primus Epic System (Software Phase 4)
1” PFD Pilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display
2nd PFD Co-pilot display
1st MFD Pilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display
2nd MFD Co-pilot Multifunction Display
Electronic Standby Instrument System (ESIS) -Attitude, Airspeed, Altitude, Vertical speed, Compass and IT, S data
Two Attitude and Heading Reference Systems (AHRSs)
Two Air Data Modules (ADMs)
Two flux valves
Two Display Controllers (DCs)
Two Cursor Control Devices (CC Ds
Single Reversion Control Panel (RCP)
Single Display Dimming Control panel
Single Stability Augmentation System (SAS) control panel
Two Remote Instrument Controllers (RlCs)
Two Modular Avionic Units (MAUs)
Two pedestal mounted MCDUs (Multi Control Function Display Units) Dual Radar Altimeter (RT -300)
Emergency Locator Transmitter (ELT -122/243/406 MHz)
One Flight Guidance Controller
Honeywell GPS module with Flight Plan Management System (FPMS)
NOTABLE FEATURES
EGPWS
TCAS I Bendix King
Long Range Fuel Tank
MTOW 6,800 KG
Cockpit Voice & Data Recorder
Co-pilot Storm Window
Approach Plates Chart Holders Lighted for both pilot/copilot
Autopilot 4 Axis
Weather Search Radar “Primus 701” (Kit)
1” PFD Pilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display
2nd PFD Co-pilot display
1st MFD Pilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display
2nd MFD Co-pilot Multifunction Display
Electronic Standby Instrument System (ESIS) -Attitude, Airspeed, Altitude, Vertical speed, Compass and IT, S data
Two Attitude and Heading Reference Systems (AHRSs)
Two Air Data Modules (ADMs)
Two flux valves
Two Display Controllers (DCs)
Two Cursor Control Devices (CC Ds
Single Reversion Control Panel (RCP)
Single Display Dimming Control panel
Single Stability Augmentation System (SAS) control panel
Two Remote Instrument Controllers (RlCs)
Two Modular Avionic Units (MAUs)
Two pedestal mounted MCDUs (Multi Control Function Display Units) Dual Radar Altimeter (RT -300)
Emergency Locator Transmitter (ELT -122/243/406 MHz)
One Flight Guidance Controller
Honeywell GPS module with Flight Plan Management System (FPMS)
NOTABLE FEATURES
EGPWS
TCAS I Bendix King
Long Range Fuel Tank
MTOW 6,800 KG
Cockpit Voice & Data Recorder
Co-pilot Storm Window
Approach Plates Chart Holders Lighted for both pilot/copilot
Autopilot 4 Axis
Weather Search Radar “Primus 701” (Kit)
Exterior
Exterior base White
Additional Navy and gold accent stripes Last paint 2014
*
Additional Navy and gold accent stripes Last paint 2014
*
Additional Info
17” Flat Screen
9” Flat Screen
Aft Cabin Skylight Devore Lighting Electric Limo Window
Additional strobe light
Additional Transponder XS-856A, Honeywell
Air Conditioning System w/ separate cabin control switch in cockpit
Emergency Floats (provisions)
Emergency Floats (removable parts)
Engine Particle Separator
Five-point restraint Harness for Pilot and Co-pilot
Heated Windshield
High visibility main rotor blades
Moving Map “SEGEM”
PA System (on std. ICS)
RH/LH Electrically Operated Pax Steps (in lieu of fixed steps)
Tinted Window -Cabin
9” Flat Screen
Aft Cabin Skylight Devore Lighting Electric Limo Window
Additional strobe light
Additional Transponder XS-856A, Honeywell
Air Conditioning System w/ separate cabin control switch in cockpit
Emergency Floats (provisions)
Emergency Floats (removable parts)
Engine Particle Separator
Five-point restraint Harness for Pilot and Co-pilot
Heated Windshield
High visibility main rotor blades
Moving Map “SEGEM”
PA System (on std. ICS)
RH/LH Electrically Operated Pax Steps (in lieu of fixed steps)
Tinted Window -Cabin
