manufacturer
Leonardo
configuration
VIP
condition
Used
year
2006
time
1620
helicopter location
Argentina
serial number
31038
registration number
LV-KJB
listing ID
HT20627
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
avionics
• Honeywell Primus Epic System
• 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)
equipment
• 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)
• 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
