2016 AgustaWestland AW169
Description
The AgustaWestland AW169 is a twin-engine, multirole helicopter produced by Leonardo (formerly AgustaWestland, now Leonardo Helicopters Division). It is designed for a variety of roles including emergency medical services, search and rescue, law enforcement, and offshore transportation. The AW169 can carry up to 8 passengers, and has a maximum cruise speed of 150 knots (173 mph). It is equipped with advanced avionics and a full digital flight control system. It was first flight in 2011 and entered service in 2014. It have been selected by many customer worldwide, as well as military and government agencies.
Features
- Total Time: 170
- 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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