Description:

Delivery June 2015. EMS, SAR, Law Enforcement, VIP or Offshore

Airframe:
Maximum Take-Off Weight: 4,500 kg
Empty Aircraft Weight: 2,700 kg
Useful Load: 1,800 kg (+-4%)
Fuel Consumption / hour: 290 kg ~ 310 kg
Maximam Speed: 168 ~ 169 kt/h = 311 ~ 313 km/h
Cruising Speed:
- 140 kt/h = 259 km/h (with fixed landing gear)(+-4%)
- 150 kt/h = 277km/h (with retractable landing gear)(+-4%)
Range (without additional tank):
- 460 nm = 852 km (with fixted landing gear)
- 500 nm = 926 km (with retractable landing gear)
Maximum Endurance (without additional tank):
- 2.96 ~ 3.17 Hrs
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Engine Specs:
Two Pratt & Whitney Canada 210A turboshaft engines (1,000 shp x 2 units)
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)
Engine Control Panel
Engine bay group (engine mounts, firewalls, cowlings, drains, exhausts)
Fire detection system
Fire extinguisher system
Fire Detection and Extinguisher Control Panel (1)

Electrical System
DC primary power generation system: 28 V DC provided by two independent 300 starter generators
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Avionics/Radios:
STANDARD AVIONICS PACKAGE

Cockpit Display System (CDS)
- Three Rockwell Collins Display Units 10? X 8? colour AMLDC with LED backlight and NVIS compatibility (2 normally used as Primary Flight Displays (PFD) and 1 used as 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)
- Two Master Caution Lights (MCL)
- Two Master Warning Lights (MWL)
- Two Avionics Full Duplex Ethernet (AFDX) switches

Aircraft Monitoring and Management System (AMMS)
- Two Aircraft Monitoring & Management Computers (AMMS)
- One Data Transfer Device (DTD)
- Two touch screen control panels

Four Axis automatic Flight Control System (AFCS)
- Two Flight Contol Computer (FCC)
- One Flight Control System (FCS) Control Panel

Radio Comm and Navigation System
- Two VHF-AM radios
- Two NAV (VOR/ILS/MB) receivers
- One ADF
- One DME
- One Transponder with Enhanced Surveillance Mode (Mode S)
First SBAS GNSS (GPS) / Second SBAS GNSS (GPS)

Interphone Communication System
- Two Audio Control Panels (Pilot and Co-pilot stations)
- One Audio Management Unit interfacing external transceivers
- One Passenger Intercom Amplifier
- One ELT

Primary Flight Instruments
- Two flux valves
- Two Air Data and Altitude Heading Reference System (ADAHRS)
- One Rader Altimeter
- Two Clocks
- One Standby magnetic Compass
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Additional Equipment:
Covers and flags for engines, pitot and connectors
Manuals and parts catalogue
Tie-down assemblies for main rotor blades
Tail rotor blaes flapping block (1)
Main rotor blades sock pole (1)
Main landing gear wheel chocks (2)
Main rotor balance and trancking chart, tail rotor balance chart
Nose landing gear centre pin (1) and landing gear handle locking pin (1)
Jacking dome assy
Tow bar (1)
Loose equipment bag (1)
Baggage compartment cargo net
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Interior:
Cockpit compartment utility finishing interior
Cockpit panel sun-glare shields
Pilot / Co-pilot crashworthy adjustable seats (with inertial reels and separate 5 points safety belts)
28V DC cockpit/cabin power outlet
Baggage compartment utility finishing interior
Baggage smoke sensor
Pilot / Co-pilot headsets