G-MLAP: Agusta AW169

Details

Listings

Description

• One owner from New
• VIP ‘’Pearl’’ Interior 3+2+2
• Conversion kit for 4+2+2 interior
• Soundproofing
• Removable Emergency Floats
• Removable External Life Raft on Sponson
• Tail Fin Camera
• ADS-B
• SVS
• JAR Ops 3 / EASA IFR Equipped
• Increased Gross Weight (4800 kg MTOW)
  

Avionics

• Three Rockwell Collins Display Units 10” X 8” colour 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)
• One Radar Altimeter
• Pilot Clock/Co-Pilot Clock
• TCAS II Rockwell Collins TCAS-4100 -
• Moving map
• Weather Radar Rockwell Collins RTA-4112 MultiScan
• SATCOM Iridium Skytrack ISAT 200 A integrated
• 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)
• Second radar altimeter
• 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)
  

Airframe

Year of Manufacture: 2016
Entry Into Service: 2017
Total Time Since New: 255 Hours
Total Landings Since New: 606
  

Engines / Mods

Model: PW210A
ENGINE 1 ENGINE 2
Serial Number: PCE-BP0039 PCE-BP0012
Total Time Since New: 255 Hours 255 Hours
Total Cycles Since New: 606 606
  

Interior / Exterior

• VIP “Pearl” 3+2+2 Interior Layout
• Conversion Kit to achieve Pearl 4+2+2
• VIP Composite Liners leather/leatherette covered with enhanced soundproofing extended for rear seats
• Rear Cabin windows (left and right)
• Cabin ambient Mood Multicolor - LED lights, white LED reading light
• Environmental Control system (ECS) - Air Conditioning
• Inter-Communication System for all passengers inc. Headsets ANR type (Qty. 7)
• Handmade customised passenger carpet
• Comfortable VIP seat leather covered sliding and with reclinable backrest x 3
• Extra wide armchairs leather covered sliding and with reclinable backrest x 2
• VIP Seats in the rear cabin bay x 2
• Basic Entertainment and Cabin Management System inc. 4.3” Touch screen panel and one iPad mini for lighting system and ECS control
• Window and roll up curtain on pilots’ side
• Cabin Active Comfort Enhancer VIP
• Hinged passenger doors in lieu of sliding doors with dedicated liners
• 28V DC cabin power outlet
• Electrical ‘limo’ window for the separation wall
Cockpit – Interior
• Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
• 28V DC cockpit power outlet
• First aid kit (as per JAR OPS 3)
• One cockpit and one cabin fire extinguisher (as per JAR OPS 3)

• Upper areas painted in white and lower areas in mid blue
• Silver 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
• Tail Fin Camera
• Strobe lighting
  

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 refuelling (on left hand side)
• Dual independent, redundant hydraulic system
• Retractable swivelling Landing / taxiing lights (2)
  

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