Copilot flight/navigation instruments (LCD EADI and EHSI, barometric altimeter, airspeed indicator, VSI)
Gyrocompass C14 Honeywell
Vertical gyro #1 46060-11 Flightline System
Vertical gyro #2 VG-208 JET Electronics
3-axis duplex AFCS SP711 Honeywell
ADF KR 87 Bendix/King
Transponder (mode S) KT 73 Bendix/King
VHF#1 COM/NAV/GPS GNS 530 Garmin
VHF#2 COM/NAV/GPS GNS 430 Garmin
DME KDM 706A Bendix/King
Marker beacon KMR 675 Bendix/King
Pilot ICS (including pilot/copilot control panel. mode controller. audio cabin control)
AC power supply system (two inverters)
Copilot flight/navigation instruments (LCD EADI and EHSI. barometric altimeter airspeed indicator. VSI)
Flight director FZ 702 Honeywell with autotrim
Radio altimeter AA 300 Honeywell
ELT C406-2HM Artex
Moving map KMD 550 Bendix/King
Radio master switch with ground function
EFIS pilot/copilot in command switch
Moving Map MKII Observer (Sky Force)
TCAS SKY 791 (BF Goodrich)
Weather Radar presented on pilot/copilot EHSI RDR 2000 Bendix/King.
2 independent electronic control systems (FADEC) w/ emergency & training operation modes & auto start
Airspeed indicator
Instantaneous vertical speed indicator
Barometric encoding altimeter
Magnetic compass indicator
Clock. 8 days and elapsed time
LC Integrated Display System (IDS)
Master Warning & Caution lights
Engine fire detection system
Aural Warning Generator system
Exceedance recorder system (on IDS display)

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

Soundproofing PAULSTRA VIP Interior (5 places) including leatherette covered or painted liners. 3 seats aft facing central bench and see-through with foldable armrest and 2 seats aft bench fwd facing with central cabinet/bar. All seats crash-resistant and include 4 points shoulder harness with inertial reels and safety belts on all seats. Additional amenities include advisory, reading and floor courtesy light, Floor carpeting, Cabin double glass windows, Two individual crash-resistant pilot seats fore and aft adjustable with lap belts, Aluminum alloy honeycomb reinforced floor with anti-skid finishing, Ventilation ram air inlets, passive vibration absorber.

Overall White with Red & Blue Accent Striping.