STANDARD EQUIPMENT
• Active Noise Reduction (ANR) headsets (pilot and co-pilot)
• Baggage compartment lights
• Crew open door actuators
• First aid kit
• Fuel drain electrical valves
• Portable fire extinguisher
• Quick disconnecting chip detectors
• Shoulder harness with inertial reels (pilot and co-pilot)
• Tail boom strake
ADDITIONAL AVIONIC EQUIPMENT
• AC power supply system (two [2] inverters)
• AFCS 3-axis duplex SP-711 Honeywell
• Emergency Locator Transmitter
MISCELLANEOUS / GROUND EQUIPMENT
• Air intake / exhaust covers
• Ground tools kit (including tow bar, ground wheels, lifting tool)
• Pitot tube cover
• Rotorcraft Flight Manual (RFM) (hard copy) and technical publications (soft copy)
• Tie-down fitting (main rotor retention straps)
ELECTRICAL SYSTEM
• 28 Ah nickel-cadmium battery with temperature probe
• 200 A self-cooled starter generator
• Voltage regulator
• Battery relay
• Interconnecting bus relay
• External power relay
• Distribution buses (2)
• External power receptacle Position lights
• Two (2) LED landing lights
• Two (2) anti-collision lights
• Two (2) cockpit utility lights
• Instrument lights
• Radio master switch
SYSTEMS DATA (on PFD/MFD)
• Inter turbine gas temperature indicator (ITT°C) (on MFD)
• Power index (on PFD)
• Engine torque indicator (TQ%) (on MFD)
• Compressor speed indicator (N1%) (on MFD)
• Turbine speed indicator (N2%)
• Rotor speed indicator (NR%)
• Transmission oil pressure (PSI) and temperature (°C) indicator
• Engine oil pressure (PSI) and temperature (°C) indicator
• Fuel pressure (PSI) and fuel quantity (kg) indicator
• Two (2) hydraulic pressure system indicators (PSI)
• Outside air temperature indicator (°C) (on PFD)
• DC voltmeter (VDC)
• DC ammeter (Amp)
UTILITY EQUIPMENT
• 1X-K-151-3CM: Air conditioning
• 1X-K-101-6CM: 230 USgal fuel system In lieu of 160 USgal
• 1X-K-103-6CM: Baggage compartment extension (2.3 m)