Description:

Delivery Time Only
Enhanced Vision System (EVS)
HTAWS
4 Axis Digital Auto Pilot
VIP 6 Seats
Full Manufacturer Warranties

(Currently located at Lodrino Airport, Switzerland)

Airframe:
AIRFRAME
Aluminium alloy / composite material and bonded panel fuselage
Semi-monocoque aluminium alloy tail boom
Three-wheeled retractable landing gear
Two hinged jettisonable crew doors (LH and RH)
Two sliding passenger doors (LH and RH), 1.40 m opening, with jettisonable windows
Acrylic windshield and side windows
Acrylic overhead windows
Quick removable tail rotor drive shaft cover
Separate baggage compartment with hinged door
Removable fairing and cowlings, for complete accessibility to the controls
and drive components
Swivelling front wheel with tow bar attachment
Quick opening hinged inspection doors, to allow Visual check of engine oil levels and
maintenance inspection points
Grounding points
Jacking and hoisting points

ELECTRICAL SYSTEM
24 V DC 33 Ah nickel-cadmium battery with temperature probe
200 A self-cooled starter generators (2)
Voltage regulators (2)
Battery relay
lnterconnecting bus relays (2)
Extemal power relay
Distribution buses (I battery, 2 essential, 2 emergency, 2 main)
External power receptacle
Position lights
Taxing lights (2) and landing lights (2) on landing gear sponsons
Anti-collision lights (2)
Cockpit utility lights (2)
Instrument lights with dimming switch
Radio master switch with ground function
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Engine Specs:
Power plant and fuel system
Two Pratt & Whitney Canada PW207C turbo-shaft engines
Two independent electronic control systems (FADEC) with normal emergency and training
operation modes and auto-start
Engine mounted fuel pump and filter assembly
Engine mounted oil pump and filter assembly
Engine mounted fuel control and governor
Lubrication and cooling system
Engine oil chip detectors (2)
Engine control panel
Two independent fuel systems with cross-feeding valve and control panel
3-cell crash-resistant fuel system (575 l - 152 USgal)
Submerged fuel boost pump (2)
Airframe mounted easy access fuel filter
RH refuelling point
Ground fuel drains

Rotors and controls
Titanium main rotor hub, corrosion protected, fully articulated with four composite grips,
four elastomeric bearings, four individually interchangeable composite material blades,
swept tips, and dampers
Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite
blades, individually interchangeable
Cyclic and collective controls powered by two hydraulic systems
Hydraulically powered anti-torque system
Adjustable friction devices on cyclic and collective system
Force trim and artificial feel system
Adjustable directional control pedals
Flapping and droop restraint mechanism
Co-Pilot brake controls (in addition to the Pilot standard ones)

Transmission drive system and hydraulic system
960 shp for takeoff and 900 shp continuous operation main transmission
Three-stage transmission
Freewheeling units (2)
Transmission mounted hydraulic pumps (2) with separate reservoir
Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter
Transmission oil chip detectors (2)
Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detector
Transmission cooling and lubrication system
Transmission shafts
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Avionics/Radios:
3 SINGLE PILOT IFR (EASA) AVIONIC PACKAGE
(Chelton Flight Systems)
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)
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)
EFIS pilot/co-pilot navigation synchronization switch
Electronic Standby Instrument System (ESIS)
Radio Management System (RMS) RTU-4210 Collins (Qty 2)
VHF/AM #1 VHF-4000B Collins
VHF/AM #2 VHF-4000B Collins
VOR #l/ILS/ADF NAV-4000 Collins
VOR #2/ILS NAV-4500 Collins
DME DME-4000 Collins
Transponder (mode S) TDR-94 Collins
Radio altimeter ALT- 4000 Collins
Attitude Heading Reference System (AHRS) (Qty 2) with one dual AHRS control panel
Air Data Unit (ADU) (Qty 2) A
Pilot GPS Chelton (SBAS) interfaced to EFIS
Co-pilot GPS Chelton (SBAS) interfaced to EFIS
Digital lCS (two cockpit panels and Audio Management Unit)
4-axis dual duplex digital AFCS with integrated Flight Director
Electronic clocks (Qty 2)
Magnetic compass indicators (Qty 2)
BLT C406-N HM Artex (with Navigation Interface Module embedded)
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Additional Equipment:
STANDARD EQUIPMENT
Active Noise Reduction (ANR) headsets (pilot and co-pilot)
Airframe hour meter
Baggage compartment extension (1.9 m)
Baggage compartment lights
Crash-resistant co-pilot seat, fore and aft adjustable, with lap belts and headrest
Crew open door actuators
First aid kit
Fuel drain electrical valves
Internal structural provisions for utility equipment
Portable fire extinguisher
Quick disconnecting chip detectors
Shoulder harness with inertial reels (pilot and co-pilot)
Tail boom strake

ADDTIONAL EQUIPMENT
Dual controls
Engine compartment fire extinguishers (2)
Fuel cap with key-lock
Pulsed chip detectors
Reinforced windshield
Retractable/rotating landing light
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
Tie-down fittings provisions
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Exterior:
Standard colour scheme from Company paint selection, solid colour
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Interior:
VIP Interior 6 places including:
Super Silent soundproofing
Leatherette covered liners
Cabin double layer acrylic windows
All seats crash-resistant covered with leather or fabric/leather
3 aft facing seats (central bench) with see-through modification and
with foldable armrest and glass holder
3 fwd facing seats (aft bench) with foldable armrest and glass holder
4-point shoulder harness with inertial reels and safety belts for all seats
Seats covers
Advisory, reading and floor courtesy lights
Leather bellows on flight controls
Cabin loudspeakers
6 Active Noise Reduction (ANR) headsets
Floor carpeting
Carpeting protection
Customized finishing from VIP available selections

EQUIPMENT
Single central refrigerated drawer
Single drawer (qty 2)
Pilot and Co-pilot aft holders
Curtains in cockpit (upper windows)
Weather Radar RDR 2000 Bendix/King (presented on EFIS)
Traffic Avoidance System TAS-620 Avydine (presented on EFIS)
Euroavionics Euronav V digital map interfaced to FMS (presented on 8.4” display)
Cockpit central monitor 8.4” display for digital map
Enhanced Vision System (EVS) MaxViz 1500
213 USG crash resistant fuel systems (in lieu of 152 US gall)
Baggage compartment extension (2.30 m)
Emergency floats provision
Customized painting scheme, metallic colours from Company selection

- Air conditioning ECS (Environment Control System)
- Passive vibration absorber
- Primer finished cabin walls
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Inspection Status:
(The offer for sale of this aircraft is subject to contract and the aircraft may at any time be withdrawn from the market without prior notice. Specification is always subject to verification by the purchaser)