2016 WESTLAND LEONARDO AW169

Specifiche

Cellula

Motore ed elica

Descrizione

2016 AW169 VIP-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

Avionica e attrezzature

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
Co-pilot hinged window (storm window)

Other Equipment:
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 extinguisher (as perJAR OPS 3)
Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)

Cellula

Airframe:
Year of Manufacture: September, 2016
Entry Into Service: March, 2017
Total Hours Since New: 170.7
Total Landings Since New: 417