16 Hrs TT

Corporate 6 place passenger cabin

All seats crash-resistant covered with leather or fabric/leather
Air Conditioning ECS (Environmental Control System)
3 fwd & aft facing seats with foldable armrest and glass holders
3 aft facing seats (central bench) with see-through modification and with foldable armrest and glass holder
Forward facing side arm rests
4-point shoulder harness with inertial reels and safety belts for all passenger seats
Super silent soundproofing
Liners leather
Acoustic screen around doors
Cabin double layer acrylic windows
Customised Corporate cabin finishing
Decoration trim with metal inserts
Intercommunication system for passengers
Seat covers
Headset Bose ANR type (Qty 6)
Cabin loudspeakers (Qty 2)
Reading lights, emergency lights, floor courtesy lights
Passenger hooks (Qty 4)
Upper and lower air vents
Floor carpeting & carpeting protection

Cockpit equipment

Inter seat console tray with 12 V power supply
Multipurpose holder (with space provision for fire extinguisher)
Right door pocket, Headset hooks (Qty 2)
Cyclic and collective leather gators
Curtains in cockpit on upper windows

Single Pilot Dual Controls IFR Avionic Package

Pilot flight/navigation EFIS (2 displays) with embedded FMS
Synthetic Vision (SVS)
HTAWS (Helicopter Terrain Awareness and Warning System)
Slip indicator and Remote Bug Panel (RBP)
(*) In lieu of basic Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP)
Co-pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS)
HTAWS (Helicopter Terrain Awareness and Warning System)
Slip indicator and Remote Bug Panel (RBP)Reversionary Control Panel (RCP)
EFIS pilot/co-pilot navigation synchronization switch (FMS data)
Electronic Standby Instrument System (ESIS)
Second Radio Management System (RMS) RTU-4210 Collins
Second VHF/AM VHF-4000E Collins
VOR/ILS/ADF NAV-4000 Collins
Transponder (Mode S) TDR-94 Collins
DME DME-4000 Collins
Radio altimeter ALT-4000 Collins
Second Attitude Heading Reference System (AHRS)
Second Air Data Unit (ADU)
Pilot GPS/SBAS Chelton interfaced to EFIS/FMS
Co-pilot GPS/SBAS Chelton interfaced to EFIS/FMS
Digital Audio Control System (DACS) NAT additional cockpit panel
4-axis dual duplex digital AFCS with integrated Flight Director
Second electronic clock
Second magnetic compass indicator
ELT C406-N HM Artex (with Navigation Interface Module embedded)
Dual controls

Installed Additional Equipment

Customised painting scheme, metallic colours from Company selection
213 USgal crash-resistant fuel system (in lieu of 152 USgal)
Baggage compartment extension (2.3 m)
Stormscope Lightning Detection System WX-500 L3 (presented on EFIS)
Traffic Advisory System TAS-620 Avydine (presented on EFIS)
Weather radar RDR 2000 Bendix/King (presented on EFIS)
Mast Vibration Absorber
Provision for 8.4’’ display and provision for DMG
Electrically operated passenger steps (RH) -provision only
Electrically operated passenger steps (LH) -removable only
Airframe hour meter
Baggage compartment extension (1.9 m)
Engine compartment fire extinguishers (Qty 2)
Fuel cap with key-lock
Pulsed chip detectors (in lieu of quick disconnecting chip detectors)
Reinforced windshields (pilot and co-pilot)
Retractable/rotating landing light (nose mounted)
Rotor brake
Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips

Miscellaneous/Ground Equipment

Air intake/exhaust covers
Ground tools kit (including tow bar, lifting tool, wheel chocks)
Pitot tubes covers
Rotorcraft Flight Manual (RFM) and technical publications
Tie-down fittings (main rotor and tail rotor retention straps)