manufacturer
Leonardo
configuration
VIP
condition
Used
year
2011
time
1476
helicopter location
Switzerland
listing ID
HT19027
Description
Single Pilot IFR - 4 Axis Auto-Pilot
VIP Configuration
Garret ECS Air Conditioner
avionics
DUAL EFIS & FMS
SYNTHETIC VISION WITH TAWS
SLIP INDICATOR AND REMOTE BUG PANEL
EFIS PILOT/CO-PILOT NAVIGATION SYNCHRONISATION SWITCH
ELECTRONIC STANDBY INSTRUMENT SYSTEM (ESIS)
SECOND RADIO MANAGEMENT SYSTEM (RMS) RTU-4210 COLLINS SECOND VHF/AM
VHF-4000E COLLINS
VOR/ILS/ADF NAV-4000 COLLINS
DME DME-4000 COLLINS
RADIO ALTIMETER ALT-4000 COLLINS
SECOND ATTITUDE HEADING REFERENCE SYSTEM (AHRS) SECOND AIR DATA UNIT
CO-PILOT GPS/SBAS CHELTONINTERFACED TO EFIS/FMS
DIGITAL AUDIO CONTROL SYSTEM (DACS) NAT ADDITIONAL COCKPIT PANEL 4-AXIS AUTO PILOT
DUAL DUPLEX DIGITAL AFCS WITH INTEGRATED FLIGHT DIRECTOR
ELECTRONIC CLOCK
SECOND MAGNETIC COMPASS INDICATOR
ELT-C406-N HM ARTEX
equipment
ANR HEADSETS (PILOT AND CO-PILOT)
BAGGAGE COMPARTMENT LIGHTS
CRASH-RESISTANT SEATS, DUAL ADJUSTABLE, WITH LAP BELTS & HEADRESTS
CREW OPEN DOOR ACTUATORS
INTERNAL STRUCTURAL PROVISIONS FOR UTILITY EQUIPMENT
DUAL SHOULDER HARNESS WITH INERTIAL REELS
TAIL BOOM STRIKE KIT
GARRET ECS AIR CONDITIONER
OTHER EQUIPMENT
EFIS (1 DISPLAY) WITH SLIP INDICATOR AND REMOTE BUG PANEL (RBP)
RADIO MANAGEMENT SYSTEM (RMS) RTU-4210 COLLINS (1)
VHF/AM VHF-4000E
VOR/ILS NAV-4500 COLLINS
TRANSPONDER (MODE S) TDR-94 COLLINS
ATTITUDE HEADING REFERENCE SYSTEM (AHRS) (1) WITH ONE DUAL AHRS
CONTROL PANEL
AIR DATA UNIT (ADU) (1)
DIGITAL AUDIO CONTROL SYSTEM (DACS) NAT WITH ONE COCKPIT PANEL
ELECTRONIC CLOCK (1)
MAGNETIC COMPASS
engine 1
TWO PRATT & WHITNEY CANADA PW207C TURBO-SHAFT ENGINES
TIME SINCE NEW: 1,476 HOURS
TBO: 2,524 HOURS
- TWO INDEPENDENT ELECTRONIC CONTROL SYSTEMS (FADEC) WITH NORMAL
- EMERGENCY AND TRAINING OPERATION MODES AND AUTO-START
- ENGINE MOUNTED FUEL PUMP AND FILTER ASSEMBLY
- ENGINE MOUNTED OIL PUMP AND FILTER ASSEMBLY
- ENGINE MOUNTED FUEL CONTROL AND GOVERNOR
- LUBRICATION AND COOLING SYSTEM
- ENGINE OIL CHIP DETECTORS (2)
- ENGINE CONTROL PANEL
- TWO INDEPENDENT FUEL SYSTEMS WITH CROSS-FEEDING VALVE AND CONTROL PANEL
- 3-CELL CRASH-RESISTANT FUEL SYSTEM (575 L –152 USGAL)
- SUBMERGED FUEL BOOST PUMP (2)
- AIRFRAME MOUNTED EASY ACCESS FUEL FILTER
- RH REFUELLING POINT & GROUND FUEL DRAINS
inspection details
HOURS REMAINING:
MGB: 3,324
TGB: 1,524
TRB: 8,524
MRB: 7,324
TRANSMISSION DRIVE SYSTEM AND HYDRAULIC SYSTEM
- 960 SHPFOR TAKEOFFAND 900 SHPCONTINUOUS OPERATION MAIN TRANSMISSION
- THREE-STAGE TRANSMISSION
- FREE WHEELING UNITS (2)
- DUAL INDEPENDENT, REDUNDANT HYDRAULIC SYSTEMS
- TRANSMISSION MOUNTED HYDRAULIC PUMPS (2) WITH SEPARATE RESERVOIR
- RIPPLE DAMPERS (2)
- INTERNAL DRY SUMP TRANSMISSION LUBRICATION WITH PRESSURE AND
- SCAVENGE PUMP AND OIL FILTER
- TRANSMISSION OIL CHIP DETECTORS (2)
- SINGLE STAGE, BEVEL GEAR T/R 90°GEAR BOX INCLUDING OIL LEVEL SIGHT
- GLASS AND CHIP DETECTOR TRANSMISSION COOLING AND LUBRICATION SYSTEM TRANSMISSION SHAFTS
ELECTRICAL SYSTEM
- 24 V DC 33 AH NICKEL-CADMIUM BATTERY WITH TEMPERATURE PROBE
- 200 A SELF-COOLED STARTER GENERATORS (2)
- VOLTAGE REGULATORS (2)
- BATTERY RELAY
- INTERCONNECTING BUS RELAYS (2)
- EXTERNAL POWER RELAY
- DISTRIBUTION BUSES (1 BATTERY, 2 ESSENTIAL, 2 EMERGENCY, 2 MAIN, 2 AUXILIARY)
- EXTERNAL POWER RECEPTACLE
- POSITION LIGHTS
- TAXING LIGHTS (2) AND LANDING LIGHTS (2) ON LANDING GEAR SPONSONS
- ANTI COLLISION LIGHTS (2)
- COCKPIT UTILITY LIGHTS (2)
- INSTRUMENT LIGHTS WITH DIMMING SWITCH
- RADIO MASTER SWITCH WITH GROUND FUNCTION
FLIGHT/NAVIGATION INSTRUMENTS
- PILOT FLIGHT/NAVIGATION EFIS (1 DISPLAY) WITH SLIP INDICATOR AND REMOTE
- BUG PANEL (RBP) RADIO MANAGEMENT SYSTEM (RMS) RTU-4210 COLLINS (1)
- VHF/AM VHF-4000E
- VOR/ILS NAV-4500 COLLINS
- TRANSPONDER (MODE S) TDR-94 COLLINS
- ATTITUDE HEADING REFERENCE SYSTEM (AHRS) (1) WITH ONE DUAL AHRS
- CONTROL PANEL
- AIR DATA UNIT (ADU) (1)
- DIGITAL AUDIO CONTROL SYSTEM (DACS) NAT WITH ONE COCKPIT PANEL
- ELECTRONIC CLOCK (1)
- MAGNETIC COMPASS INDICATOR (1)
