Air conditioning ECU Garret
Emergency floats provision
Structural provision for utility equipment (emergency floats, rescue hoist, cargo hook)
Reinforced windshield
213 US gall. Fuel system
Baggage compartment extension (to 1.9 m)
Engine compartment fire extinguishers
Baggage compartment extension (2,3 mt)
Baggage compartment light
Pilot and copilot shoulder harness with inertia reel
Crew open door actuators
Quick disconnecting chip detectors
Pulsed chip detector
Fuel drain electrical valves
Tail boom strake
Airframe hour meter provision
Dual control
Rotor brake
450 W Retractable/Rotating landing light
Pilot and copilot windshield wipers
Wiper switch on pilot cyclic grip
Rotorcraft Flight Manual and technical publications
Hook for Jacket (nr. 2) right and left in pax cabin
Locking fuel cap & Ground fuel drains
Airframe mounted easy access fuel filter
Engine oil chip detectors (one per engine)
Two independent fuel systems with cross-feeding valve and control panel
3-cell crash-resistant fuel system (460 kg – 152 USG)
Submerged fuel boost pump (one per system)
RH refueling point
High-intensity strobe lights on horizontal stabilizer
Ground tools kit (including tow bar. lifting tool. wheel chocks)
Air intake/exhaust covers
Pitot tubes covers
Tie-down fittings
Portable fire extinguisher
First aid kit
Fuel cup with key-lock
Six (6) Active Noise Reduction (ANR) headsets