Aircraft Details
- Year: 2023
- Make/Model: Leonardo AW169
- Number of Seats: 10
- Power: Turbo Shaft
- Engines: 2 Engines
- Flight Time: 0
- Listing ID: 3072774
- Partner ID: 6368
- Posted On: Jun 5, 2023
- Updated On: Mar 27, 2024
Description
Helicptero novo para ser entregue em Janeiro de 2024
General information:
To be delivered on January 2024
3 years or 2000 hours warranty
VIP Interior with full leather seats
VIP Layout "Pearl 4+2+2
Passenger cabin tinted windows
Electrically operated cabin dual step (RH+LH) (in lieu of standard step)
Increased Gross Weight (4800 kg MTOW)
Camera on the tail fin HD
Baggage compartment extension
4-axis autopilot
Enhanced Vision System (EVS) EVS-23000 Max-Viz
Engine(s):
Two Pratt &Whitney Canada PW210A1 turboshaft engines
APU mode on left hand side engine
Two anti icing fuel systems and two magnetic chip detectors (one per engine)
Two independent dual-channel FADEC systems (one per engine)
Avionics
Three Rockwell 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 (MW/L)
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)
Flight Control Computer (FCC)
One Flight Control System (FCS) Control Panel
Two VHF-AM radios
Two NAV (VOR/ILS/MB) receivers
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
Two flux valves
Two Air Data and Attitude Heading. Reference Systems
One Radar Altimeter
Pilot Clock integrated in the display
Co-Pilot Clock integrated in the display
One Standby magnetic Compass
Interior
Helicopter Comfort Package
Main Rotor Beanie
Environmental Control System (ECS) Dual Zone- Air Conditioning
Ripple Dampener Hydraulic System
VIP Interior with rear seats
VIP Composite Liners leather/leatherette covered with enhanced soundproofing extended for rear seats
Cabin ambient Mood Multicolor - LED lights, white LED reading light
Rear Cabin windows (left and right)
Coat hooks (Qty 4)
Inter-Communication System for all passengers
Entertainment and Cabin Management System (CMS)
Control of Cabin Lights, Environmental Control System, and ICS Communications through fixed Touch-screen panel and PEDs
USB data and power sockets
Manual window for separation wall
VIP Cabin Finishing
Cabin and Cockpit carpet
VIP Layout "Pearl 4+2+2"
Comfortable VIP Seat (18" Fixed) (Qtv 4)
Lower panel for fixed VIP seat (Qty 4)
Armchair (19") leather covered sliding and with reclinable backrest (forward facing) (Qty 2)
VIP Seats (18") in the rear cabin bay (Qty 2)
Headset Bose A20 with Active Noise Reduction (ANR) (Qty 8)
Electrically operated cabin dual step (RH+LH) (in lieu of standard step)
Passenger cabin tinted windows
Hinged passenger doors (in lieu of sliding doors with dedicated liners)
Additional Features
Additional Equipment:
ADS-B Out with provision for TCAS II
Health and Usage Monitoring System (HUMS)
Flight Data Monitoring system (FDM)
Helicopter Terrain Avoidance and Warning System (HTAWS)
Synthetic Vision System (SVS)
RNP Approach with LPV/LP minima
"RNP 0.3 navigation in al phase of flight" FMS capability
TCASII
Moving map
Weather Radar Rockwell Collins RTA-4112 MultiScan- Provision
Weather Radar Rockwell Collins RTA-4112 MultiScan Removable
