Low Aircraft Total Time
Six (6) Passenger VIP Interior
Mast Vibration Absorber
Enhanced Flight Vision System (EVS)
Inlet Barrier Filters System (IBF)
Air conditioning ECS (Environment Control System)
4 Axis Autopilot

Airframe:
Total Time: 800

Engines:
PRATT & WHITNEY PW207C
Time: 824/806

Single pilot IFR certified, fully dual pilot IFR configured
4-axis dual duplex digital AFCS with integrated Flight Director
Weather radar RDR 2000 Bendix/King
Dual pilot flight/nav EFIS displays with FMS
HTAWS Helicopter Terrain Avoidance Warning System
Dual AHRS Attitude heading reference systems
Electronic Standby Instrument System
Reversionary Control Panel (RCP))
Dual Radio Management System (RMS) RTU-4210 Collins
Dual VHF/AM VHF-4000E Collins
Dual VOR/ILS/ADF NAV-4500 Collins
Transponder (Mode S) TDR-94 Collins ADS-B out
Radar Altimeter ALT 4000 Collins
TCAS: TAS 620 Avidyne
EuroNav Digital Map Display
Enhanced Vision System (EVS)
Dual ADU Air Data Units
Dual digital clocks
Dual magnetic compass indicators
ELT Artex C408-N HM

2011

2011

Modifications / Conversions:
Engine compartment fire extinguishers (Qty 2)
High Intensive strobe lights
Baggage compartment extension
USB Charger - cockpit
Locking fuel cap
Pulsed chip detectors
Reinforced windshields
Retractable/rotating landing light (nose mounted)
Rotor brake
Windshield wipers with switch on cyclic grip
Air conditioning ECS (Environment Control System)
5 Cell Fuel System (213 US gal)