Specifications
– 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 transparent windshield and side windows
– Acrylic transparent overhead windows
– Quick removable tail rotor drive shaft cover
– eparate 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
Engine(s)
– 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 – 152 USgal)
– Submerged fuel boost pump (2 each engine)
– Airframe mounted easy access fuel filter
– RH refuelling point
– Ground fuel drainsRotors 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
Avionics
-Traffic Advisory System TAS-620 Avydine (presented on EFIS)
– Weather radar RDR 2000 Bendix/King (presented on EFIS)
– ADS-B Out Capable Transponder TDR-94 Collins (in lieu of standard transponder)
– iPad certified mount with USB charger point for USB A and C in cockpit (installed by Sloane post-delivery)
Equipment
– Active Noise Reduction (ANR) headset (pilot and co-pilot)
– 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
– Shoulder harness with inertial reels (pilot and co-pilot)
– Tail boom strakeSingle 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 displays) with slip indicator and Remote Bug Panel (RBP)
(**) Data services subscription for the update of the Navigation databases from Jeppesen is under Customer’s responsibility
– 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-40000E Collins
– VOR/ILS/ADF NAV-4000 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) COBHAM 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
Additional Equipment
– 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
– Retractable/rotating landing light (nose mounted)
– Rotor brake
– Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
Utility Equipment
– 213 USgal crash-resistant fuel system (in lieu of 152 USG)
– 24 VDC 33Ah nickel-cadmium battery (20cells in lieu of 19 cells)
– Baggage compartment extension (2.3 m)
– High-intensity white strobe lights on horizontal stabilizer
Additional Equipment
– USB charger in passenger cabin (under LH or RH side rear facing seat)
– Electrically operated passenger step (LH)
– Single drawer in cabin (under aft bench)
– Mast Vibration Absorber
Transmission drive system and hydraulic system
– 960 shp for takeoff and 900 shp continuous operation main transmission
– Three-stage transmission
– Free wheeling units (2)
– Dual independent, redundant hydraulic systems
– Transmission mounted hydraulic pumps (2) with separate reservoir
– Ripple dampers (2)
– 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
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
– Interconnecting bus relays (2)
– External power relay
– Distribution buses (1 battery, 2 essential, 2 emergency, 2 main, 2 auxiliary)
– External power receptacle
– Position lights (NVG friendly – green, red, white)
– Taxing lights (2 RH + 2 LH) and landing lights (2 RH + 2 LH) on landing gear sponsors
– Anti collision lights (2) (NVG friendly)
– Cockpit utility lights (2)
– Instrument lights with dimming switch
– Radio master switch with ground function
Flight/navigation instruments
– Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP)
– Radio Management System (RMS) RTU-4210 Collins (1)
– VHF/AM VHF-4000E
– VOR/ILS NAV-4500 Collins
– Transponder (Mode S) TDR-94 Collins
– Attitude Heading Reference System (AHRS) (1) with one dual AHRS control panel
– Air Data Unit (ADU) (1)
– Digital Audio Control System (DACS) COBHAM with one cockpit panel
– Electronic clock (1)
– Magnetic compass indicator (1)
– Magnetic sensor unit
– Pitot tube right/left
Instrumentation (on IDS display)
– LCD Integrated Display System (IDS)
– Dual gas generator speed indicator (N1%)
– Dual turbine outlet temperature indicator (TOT°C)
– Dual torque meter indicator (TQ%)
– Dual power turbine speed indicator (N2%)
– Rotor speed indicator (NR%)
– Transmission oil pressure (PSI) and temperature (°C) indicator
– Two engine oil pressure (PSI) and temperature (°C) indicators
– Two fuel pressure indicators (PSI)
– Two fuel quantity indicators (Kg)
– Two fuel flow indicators (kg/hr)
– Two flight controls hydraulic system pressure indicators (PSI)
– Two utility hydraulic system pressure indicator (PSI)
– Outside air temperature indicators (°C)
– Two AC voltmeters (VAC)
– Two DC voltmeters (VDC)
– Two DC ammeters (Amp)
Warning/Caution Advisory and Maintenance System
– Master warning lights (2)
– Master caution lights (2)
– Warning, caution and advisory message (on IDS display)
– Aural warning generator system
– Engine fire detection system
– Exceedance recorder system (on IDS display)
– Warning horn (cabin)
Interior arrangement
– Crash-resistant pilot seat, fore and aft adjustable, with lap belts and headrest
– Aluminium alloy honeycomb reinforced floor with anti-skid finishing
– Ventilation ram air inlets
– Anti reflection instrument panel
Interior
– Air conditioning ECS (Environment Control System)
– Primer finished cabin wallsPassenger Cabin
– All seats crash-resistant covered with leather or fabric/leather
– 3 fwd facing seats (aft bench) with foldable armrest
– 3 aft facing seats (central bench) with see-through modification and with foldable armrest
– 4-point shoulder harness with inertial reels and safety belts for all passenger seats
– Super silent soundproofing
– Liners leather/Leatherette covered
– Cabin double layer acrylic windows (azure coloured)
– Decoration trim with metal inserts
– Intercommunication system for passengers
– Headset Bose ANR type (Qty 6)
– Cabin loudspeakers (Qty 2)
– Reading lights, advisory lights, floor courtesy lights
– Passenger hooks (Qty 4)
– Upper and lower air vents
– Floor carpeting with carpeting protection
– Seat covers
-Leather headset straps in cabin
Cockpit equipment
– Interseat 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
Exterior
– Finishing in accordance with manufacturer specification (NTA 893 A)
– Primer exterior paintingPainting
– Customized painting scheme, metallic colours
Remarks
– 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 retention straps)
Specifications and details are subject to verification upon inspection. Aircraft are offered
subject to prior sale or withdrawal from the market.