ADDITIONAL STANDARD EQUIPMENT
-Second radar altimeter system
-Flight plan management system (FPMS) and GPS module with MCDU
-Dual flight director system integrated with MAU
-Steps for passenger cabin access and cockpit access
-Rotor brake
-ELT
-Air conditioning and heating
-EAPS - Engine Air Particle Separator
-Slope Operation Envelope Extension to 10º
-Cargo hook and cargo camera provision
-Aux Fuel Tank
ROTORS & CONTROLS
-Fully-articulated main rotor with five composite blades, five elastomeric bearings and five hydraulic dampers
-Rotating main rotor flight controls
-Three main dual servo actuators
-Fully-articulated tail rotor with four composite blades, four elastomeric bearings and four elastomeric dampers
-Rotating tail rotor flight controls
-One tail rotor dual servo actuator
-Force trim system
-Pilot fixed flight controls (cyclic, collective, rudder)
-Co-pilot fixed flight controls (cyclic, collective, rudder – provisions for)
-Engine mechanical back-up control (2)
-Dual digital three-axis linear actuators (6)
ELECTRICAL SYSTEMS
-DC primary power generation: 28-volt DC regulated voltage provided by two independent 300-amp starter generators
-DC external power receptacle
-One nickel-cadmium battery 40 Ah plus one 13 Ah auxiliary battery
-DC starter generator control unit (2)
-Manual engine start and ignition system (2)
-Navigation lights
-Anti-collision lights
-Landing light/search light
-Utility lights
-Pilot cabin dome light
-PAX cabin lights (dome or reading lights according to interior configuration)
-Tritium-lighted emergency exit signs
-Seatbelt/no smoking signs
-Baggage compartment light & fire/smoke sensor
-AC static inverters system (provisions for)
TRANSMISSION / DRIVE SYSTEM & HYDRAULIC SYSTEM
-Main transmission with chip detectors/debris collectors with burning capability
-Four strut rods for upper deck attachment and anti-torque plate
-Intermediate gearbox (sight gage and magnetic drain plug/chip detector)
-Tail gearbox (sight gage and magnetic drain plug/chip detector)
-Two hydraulic power control modules (PCMs)
-Three hydraulic mechanical pumps for controls (2 independent sys) and one electrical pump for controls check on ground (engines off)
-Upper-deck cowlings
-Provisions for BCS compressor
POWER PLANT & FUEL SYSTEM
-Two Pratt & Whitney Canada PT6C-67C engines
-EEC (Electronic Engine Control)
-Overriding clutches
-Two magnetic chip detectors
-Two integrated and independent engine oil coolers
-Separate firewall protection for each engine
-Fire detecting system
-Cowlings
-Engine exhausts and ejectors
-Two independent crashworthy fuel cells
-Pumps on engines (2) and submerged in fuel tanks (2)
-Fuel filter assembly