Dual Digital Automatic Flight Control System. ( Sperry SPZ – 7000 )

Electronic Flight INSTRUMENT system. ( Sperry EDZ – 705 )

Standby attitude indicator. ( Sfena H321 AFM with J.E.T. battery pack )

Dual compass system. ( Sperry C – 14 A )

Dual digital electric clocks. ( Davtron 877 )

Cabin air temperature digital display in cockpit..

Density – altitude / five – function indicator. ( Davtron 655 – 2 )

Radio altimeter ( Collins ALT – 50A ) with dual expanded – scale indicators.

Dual VHF communications radios. ( Collins VHF – 22A )

Dual VOR navigation radios with ILS, Glideslope, and Marker Beacon. (Collins VIR – 32A )

Dual DME. ( Collins DME – 42 )

Transponder Collins TDR-94D (Mode S) P/N.622-9210-006

Single ADF. ( Collins ADF – 60A with CTL – 62 control head )

Provisions for Microwave Landing System. ( Bendix MLS – 21 )

Navigation Management System ( Universal UNS – 1A ) with GPS and Loran C sensor and fuel management )

Weather radar ( Sperry Primus – 500 with EFIS interface )

Data Nav III ( Sperry ) with checklist function

Stormscope ( 3M – Ryan WX – 11J )

Moving map display ( Argus – 5000 )

Cockpit audio system ( Baker ) with LED annuciators, cockpit ICS footswitches, and cabin ICS jack

Cabin paging and chime system ( Baker )

Cabin audio interphone system with four headsets ( Airman – 750 Telex )

Cockpit voice recorder ( Fairchild / Loral GA100 )

Moving Terrain installed in Cockpit and 12” Display unit in Cabin by  Wiking Helikopter in Germany on December 2007

Emergency Locator Transmitter : 406Mhz. Artex C406-1 HM P/N. 455 – 5016 S/N. 170 - 08612 installed by Wiking Helikopter in Istanbul on 16-04-2009

Two Pratt & Whitney Canada PT6B – 36A turboshaft engines.

Engine air particle separator system. ( EAPS )

Engine fire detection and extinguishing systems.

Two gravity-filled fuel tanks ( 281 us, gallons total capacity )

Hinged/Lockable fuel filler caps.

Dual independent suction fuel systems with crossfeed capability.

High – visibility main rotor blade paint.

Provisions for main rotor tracker and tail rotor balancer.

Inspection lights for intermediate and tail gearbox sight gauges.

Manually – actuated rotor brake system.

Hinged cockpit and cabin doors.

Retractable passenger boarding steps at left and right cabin doors.

Cockpit-controlled electric cabin door locks.

Key. locks for cockpit. cabin and baggage compartments doors.

Miscellaneous cockpit storage containers.

Executive interior with ultrasuede covering on sidewalls and ceiling and leather trim.

Two executive seats with pull-up headrests and drop-down armrests. (These  two seats can be removed and a 4 place aft facing seat installed)

Four-place forward-facing executive divan with fold-down table.

Cabin / cockpit divider bulkhead with magazine racks.

Floor-to-ceiling refreshment credenza with hot liquid containers. ice and miscellaneous storage.

Airborne telephone ( Wulfsberg Flitefone VI ) with pilot call bell.

Therapeutic oxygen bottle ( portable )

Portable litter kit installation (Keystone STC)

Quiet Main Gear Box P/N. 76351-09600-045 installed on December 2007

Cabin / cockpit bleed-air heating and ventilation system.

Heated cockpit foot pads.

Ram-air ventilation system.

Freon air conditioning system. ( parker – Hannifen )

Heated glass windshields.

Two independent 3000 PSI flight control hydraulic systems with Quick disconnect fittings for ground hydraulic system connection.

Retractable tricycle landing gear with self-centering and castering nose wheel and main wheel brakes.

Pneumatic emergency landing gear extension system.

Emergency flotation system.

Auxiliary Fuel Tank provisions installed on Oct. 1995 by Air Hanson in England  (50 gallon tank available)

Two 200VA DC starter / generators.

DC external power receptacle with overvoltage protection.

Dual 22 ampere-hour batteries. ( nose – mounted )

Dual digital battery temperature indicator. ( foxtronics )

AC electric system with 10 KVA generator and dual static inverters.

Cabin emergency lighting system with battery power supply.

Nose – mounted controllable searchlight.

3 – position strobe lights.

Forward – facing recognition lights.

Landing lights on left and right main landing gear.

Underfuselage high intensity LED strobe.

Rotor disk recognition light.

Pulselite system.