2016 AW169 VIP
$ Make Offer
AIRFRAME
Year Of Manufacture
Start Of Flight Operation
Total Time Since New
Total Landing Since New
HIGHLIGHTS
One Private Owner Since New
All Original Records since New
No Damage History / No Incidents
Fresh Annual Inspection c/w June, 2022
ENGINES
Model: Pratt & Whitney PW210A
ENGINE 1 ENGINE 2
Serial Numbers: PCE-BP0039 PCE-BP0012
Total Time Since New: 175.3 170.7
Total Cycles Since New: 325 303
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
Emergency Floats – Removable
External Life Raft on Sponson – Removable
INTERIOR
VIP “Diamond” Interior Layout 7 Pax (4+3)
Extended Cabin VIP Composite Liners leather/leatherette covered with enhanced soundproofing
Cabin ambient Mood Multicolor – LED lights, white LED reading light – 4 Coat Hooks
Environmental Control system (ECS) – Air Conditioning
Inter-Communication System for all passengers – Headsets are Bose ANR type (Qty. 7)
Customized Luxury cabin finishing and decoration trim with metal inserts
Handmade customised passenger carpet
Comfortable VIP seat leather covered sliding and with reclinable backrest (Aft Facing – Qty. 3)
Side Armrest Cabinets (RH / LH) for aft facing seats – Armchairs leather covered (w inertial reel & safety belts) (Qty. 2)
Central seat leather covered sliding and with reclinable and forward foldable backrest (Fwd facing)
Separation wall leather covered with manual sliding window and roll up curtain on pilots side
Basic Entertainment and Cabin Management System (CMS) including 4.3” Touch screen panel and one iPad mini for lighting system and ECS control
Cabin Active Comfort Enhancer VIP
COCKPIT EQUIPMENT
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
TCAS III
Moving map
ADS-B Out
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
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
Aux fuel tank equipment
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)