2024 LEONARDO AW169
Aircraft Summary
General
Year
2024
Manufacturer
LEONARDO
Model
AW169
Serial Number
69173
Condition
New
Description
Aircraft based and registered in Brazil – We can deliver worldwide.
Recently delivered by Leonardo.
Only one owner.
Equipped w/ EVS, Synthetic Vision, ADSB, Autopilot 4 axis, soundproofing, etc.
Executive interior configured for 9 passengers + 1 pilot.
Approved IFR Single Pilot.
Airframe
Total Time
40
Airframe Notes
New! Recently delivered. Only 40 hours.
Engine 1
Engine 1 Time
40
Engine 1 Time Since
SNEW
Engine 1 Notes
PW210A
Engine 2
Engine 2 Time
40
Engine 2 Time Since
SNEW
Engine 2 Notes
PW210A
Avionics
ADS-B Equipped
Yes
SVT
Yes
Auto Pilot
Yes
Avionics/Radios
Three Collins Display Units 10” X 8” colour AMLCD with LED backlight and NVIS
compatibility: 2 Primary Flight Displays (PFD) and 1 Multi Function Display (MFD)
One Integrated Standby Instrument System (ISIS)
Two Display Control Panels (DCP)
Two Cursor Control devices (CCD)
One Reversionary Control Panel (RCP)
One Display Dimming Panel
Two Master Caution Lights (MCL)
Two Master Warning Lights (MWL)
Two Avionics Full Duplex Ethernet (AFDX) switches
Aircraft Monitoring and Management System (AMMS)
Two Aircraft Monitoring & Management Computers (AMMC)
One Data Transfer Device (DTD)
Two touch screen control panels
Weather Radar Rockwell Collins RTA-4112 MultiScan – Provision and Removable
Four Axis Automatic Flight Control System (AFCS)
Two Flight Control Computer (FCC)
One Flight Control System (FCS) Control Panel
Two VHF-AM radios
Two NAV (VOR/ILS/MB) receivers
One ADF
One DME
One Transponder with Enhanced Surveillance Mode (Mode S)
First SBAS GNSS (GPS)
Second SBAS GNSS (GPS)
Two Audio Control Panels (Pilot and Co-pilot stations)
One Audio Management Unit interfacing external transceivers
One Passenger Intercom Amplifier
TCAS II Rockwell Collins TCAS 4100 – Provision and Removable
Moving map
Additional Equipment
Dual Controls
Yes
A/C
Yes
Baggage Compartment
Yes
Additional Equipment
SATCOM Iridium Skytrack ISAT 200 A integrated – Provisions
EVS MaxViz
Two flux valves
Two Air Data and Altitude Heading Reference Systems (ADAHRS)
One Radar Altimeter
Pilot Clock
Co-Pilot Clock
One Standby magnetic Compass
Cockpit compartment utility finishing interior
Cockpit panel sun-glare shields
Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
28V DC cockpit/cabin power outlet
Baggage compartment utility finishing interior
Baggage smoke sensor
Pilot / copilot headsets
ADS-B Out (Automatic Dependent Surveillance – Broadcast)
Health and Usage Monitoring System (HUMS)
Flight Data Monitoring system (FDM)
Helicopter Terrain Avoidance and Warning System (HTAWS)
Synthetic Vision System (SVS)
Steps for cockpit / cabin access
Rotor brake system
Second radar altimeter
One solid state Cockpit and Voice Flight Data Recorder with ULB
One Emergency Locator Transmitter (ELT – 3 frequencies) (fixed)
Overhead cockpit windows sun shades
First aid kit (as per JAR OPS 3)
One cockpit and one cabin fire extinguisher (as per JAR OPS 3)
Approach plates chart holders with lights for pilot and co-pilot
Co-pilot hinged window (storm window)
Exterior
Year Painted
2024
Interior
Year Interior
2024
Number of Seats
10
Soundproofing
Yes
Interior Notes
9 Passengers + 1 Pilot
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