Description
Year: 2018
LEONARDO HELICOPTERS
Model: AW 169
Configuration: VIP PEARL INTERIOR 8 PAX
Total time: 733 tth
PHASE #6, #7 & #8 Performed
EW 3.516 Kgs
One owner since new
Maintenance
120 M INSPECTION 02/05/2026
48M INSPECTION 06/09/2028
24M INSPECTION 26/03/2026
12M INSPECTION 31/01/2026
3200HR/48M INSPECTION 06/09/2028
1600HR/48M INSPECTION 06/09/2028
48M INSPECTION 06/09/2028
24M INSPECTION 26/03/2026
12M INSPECTION 31/01/2026
3200HR/48M INSPECTION 06/09/2028
1600HR/48M INSPECTION 06/09/2028
Avionics
Full IFR Dual Single Pilot
Cockpit Display System (CDS)
- Three Rockwell Collins Display Units 10” X 8” colourful 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
■Four Axis Automatic Flight Control System (AFCS)
- Two Flight Control Computer (FCC)
- One Flight Control System (FCS) Control Panel
■Radio Comm and Navigation System
- 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)
■Interphone Communication System
- Two Audio Control Panels (Pilot and Co-pilot stations)
- One Audio Management Unit interfacing external transceivers
- One Passenger Intercom Amplifier
■Primary Flight Instruments
- Two flux valves
- Two Air Data and Altitude Heading Reference Systems (ADAHRS)
- One Radar Altimeter
- Pilot Clock
- Co-Pilot Clock
- One Standby magnetic Compass
■ Additional navigation and fleet management systems
- 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)
- Enhanced Vision System (EVS) EVS-Maxviz 1500
- Moving Map
- TCAS II (Rockwell Collins TTR 4000) – Provision
- TCAS II (Rockwell Collins TTR 4000) – Removable
- Weather Radar Rockwell/Collins RTA-4112 MultiScan
Cockpit Display System (CDS)
- Three Rockwell Collins Display Units 10” X 8” colourful 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
■Four Axis Automatic Flight Control System (AFCS)
- Two Flight Control Computer (FCC)
- One Flight Control System (FCS) Control Panel
■Radio Comm and Navigation System
- 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)
■Interphone Communication System
- Two Audio Control Panels (Pilot and Co-pilot stations)
- One Audio Management Unit interfacing external transceivers
- One Passenger Intercom Amplifier
■Primary Flight Instruments
- Two flux valves
- Two Air Data and Altitude Heading Reference Systems (ADAHRS)
- One Radar Altimeter
- Pilot Clock
- Co-Pilot Clock
- One Standby magnetic Compass
■ Additional navigation and fleet management systems
- 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)
- Enhanced Vision System (EVS) EVS-Maxviz 1500
- Moving Map
- TCAS II (Rockwell Collins TTR 4000) – Provision
- TCAS II (Rockwell Collins TTR 4000) – Removable
- Weather Radar Rockwell/Collins RTA-4112 MultiScan
Additional Info
EXTRA CONFIGUATION
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)
Emergency floatation provision
Engine particle separator provision
Hi Visibility Main and tail Rotor Blades
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)
Emergency floatation provision
Engine particle separator provision
Hi Visibility Main and tail Rotor Blades