2021 AgustaWestland AW139 Leonardo
Description
The AgustaWestland AW139 is a twin-engine, medium-sized utility helicopter manufactured by Leonardo. It has been in service since 2005 and is widely used for various purposes, such as passenger transport, search and rescue, law enforcement, and corporate/VIP transport. It is capable of carrying up to 16 passengers, with a cruise speed of up to 140 knots (259 km/h) and a maximum range of over 600 nm (1110 km). The AW139 is powered by two Pratt & Whitney PW207C engines, each providing up to 1,800 horsepower. It is equipped with the latest avionics, including a four-axis autopilot, dual digital flight controls, and a four-axis digital avionics suite. The AW139 has been certified for single-pilot operations, making it an ideal choice for corporate and VIP transport.
Features
- Total Time: NEW!!!
- Avionics
- Standard Avionics Package
- - 1st PFD (Pilot Primary Flight Display) 8" × 10" (external) color Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for
- visualization of flight and navigation data
- - 2nd PFD (Co-pilot Primary Flight Display) 8" × 10" (external) color Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for
- visualization of flight and navigation data
- - 1st MFD (Pilot Multi-Function Display) 8" × 10" (external) color Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for
- visualization of flight and navigation data
- - 2nd MFD (Co-pilot Multi-Function Display) 8" × 10" (external) color Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for
- visualization of flight and navigation data
- - One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data)
- - Two Attitude and Heading Reference Systems (AHRS)
- - Two Air Data Modules (ADM)
- - Two flux valves
- - Two Display Controllers (DC)
- - Two Cursor Control Devices (CCD)
- - One Reversion Control Panel (RCP)
- - One Display Dimming Control Panel (DCP)
- - One Stability Augmentation System (SAS) control panel
- - Two Remote Instrument Controllers (RIC)
- - Pilot and co-pilot headsets
- - Pilot and co-pilot interphone control (cyclic grip and floor switches)
- - Pilot clock (digital)
- - Co-pilot clock (digital)
- - Two Modular Avionic Units (MAU) incorporating the following major subsystems and/or functions:
- - Vehicle Monitoring System (VMS) dual
- - Monitor Warning System (MWS) dual
- - Aural Warning Generator (AWG) single
- - Central Maintenance Computer (CMC) single
- - Provision for CVR/FDR data interface (single)
- - Left Modular Radio Cabinet (MRC) with the following modules:
- - One VHF Comm.
- - One VOR/LOC/GS/MB
- - Right Modular Radio Cabinet (MRC) with the following modules:
- - One VHF Comm.
- - One VOR/LOC/GS/MB
- - One ADF
- - One DME
- - Two pedestal mounted Multifunction Control Display
- Features/Options
- - Two Modular Avionic Units (MAU) incorporating the following major subsystems and/or functions:
- - Vehicle Monitoring System (VMS) dual
- - Monitor Warning System (MWS) dual
- - Aural Warning Generator (AWG) single
- - Central Maintenance Computer (CMC) single
- - Provision for CVR/FDR data interface (single)
- - Left Modular Radio Cabinet (MRC) with the following modules:
- - One VHF Comm.
- - One VOR/LOC/GS/MB
- - Right Modular Radio Cabinet (MRC) with the following modules:
- - One VHF Comm.
- - One VOR/LOC/GS/MB
- - One ADF
- - One DME
- - Two pedestal mounted Multifunction Control Display Units (MCDU)
- - Emergency Locator Transmitter (ELT)
- - One flight guidance controller
- - Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation
- - One magnetic compass
- - One outside air temperature indicator
- - Two Master Warning Lights (MWL)
- - Two Master Caution Lights (MCL)
- - Engine 1 fire light
- - Engine 2 fire light
- - Baggage compartment smoke detector light
- - Dual electrical power connection for CVR/FDR (FAA requirement compliant)
Location
