2016 AgustaWestland AW169 Leonardo
Description
The AgustaWestland AW169 is a twin-engine, multi-role helicopter developed by Leonardo. The AW169 is powered by two Pratt & Whitney Canada PW210 engines, each delivering 1,000 shp (746 kW). It has a maximum cruise speed of 152 knots (282 km/h) and a maximum range of 544 nautical miles (1,004 km). The AW169 is capable of performing a wide range of missions, including EMS/SAR, VIP/corporate transport, offshore transport, and law enforcement. It is equipped with the latest avionics and safety features, such as digital flight control systems, a four-axis autopilot, and a full-glass cockpit with a four-screen display. The AW169 also features a cargo hook and an underslung load system for external loads up to 4,000 kg (8,818 lb).
Features
- AIRFRAME
- Year of Manufacture: September, 2016
- Entry Into Service: March, 2017
- Total Hours Since New: 170.7
- Total Landings Since New: 417
- Home Base: Buenos Aires, Argentina
- ENGINES
- Model: Pratt & Whitney PW210A
- ENGINE 1 ENGINE 2
- Serial Numbers: PCE-BP0039 PCE-BP0012
- Total Hours Since New: 175.3 170.7
- Total Cycles Since New: 325 303
- COCKPIT EQUIPMENT
- Three Rockwell Collins Display Units 10” X 8” color 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)
- Dual Radar Altimeter
- Pilot Clock/Co-Pilot Clock
- Moving map
- 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 – MaxViz EVS-1500
- TCAS III
- ADS-B Out
- 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)
- OTHER EQUIPMENT
- 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 liters of usable fuel)
- Filler port for gravity refueling (on left hand side)
- Dual independent, redundant hydraulic system
- Retractable swiveling Landing / taxiing lights (2)
- Provisions Only for Weather Radar
- Steps for cockpit / cabin access
- Overhead cockpit window sun shades
- First aid kit (as per JAR OPS 3)
- One cockpit and one cabin fire extinguisher (as per JAR OPS 3)
- Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
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