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Aircraft > Turbine Helicopter > Agusta > LV-GYK: Agusta AW169

LV-GYK: Agusta AW169

Last Updated
March 25, 2025

LV-GYK: Agusta AW169

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Details

Registration #
LV-GYK
Status
For Sale
Year
2016
Make
Agusta
Model
AW169
Serial Number
69025
TTAF
225
Engine 1 Time
175
Location
Uruguay

Price History

March 25, 2025
6,895,000

Listings

Site
Price
Status
Updated
None
Removed
June 9, 2022
None
For Sale
June 14, 2022
None
For Sale
June 20, 2022
6,895,000
For Sale
March 25, 2025

Description

-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
  

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
•
  

Airframe

Year of Manufacture: September, 2016
Entry Into Service: March, 2017
Total Hours Since New: 170.7
Total Landings Since New: 417
Home Base: Montevideo, Uruguay
  

Engines / Mods

Model: Pratt & Whitney PW210A
ENGINE 1 ENGINE 2
Serial Numbers: PCE-BP0039 PCE-BP0012
Total Hours Since New: 175.3 170.7
Total Cycles Since New: 325 303
  

Interior / Exterior

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 Ea. Coat Hooks
Environmental Control system (ECS) - Air Conditioning
Inter-Communication System for all passengers
Bose ANR type Headset Plugs (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 pilot’s 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

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
  

Remarks

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 extingisher (as perJAR OPS 3)
• Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
  

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