2016 AW109SP GrandNew – G-KLNH

2016 AW109SP GrandNew – G-KLNH

2016 AW109SP GrandNew – G-KLNH

2016 AW109SP GrandNew – G-KLNH

2016 AW109SP GrandNew – G-KLNH

Specifications

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 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)

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 – 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

Avionic Equipment
-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

Standard 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

Interior Trim
– 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

Exterior finishing
– Finishing in accordance with manufacturer specification (NTA 893 A)
– Primer exterior paintingPainting
– Customized painting scheme, metallic colours

Remarks

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 retention straps)

Specifications and details are subject to verification upon inspection. Aircraft are offered
subject to prior sale or withdrawal from the market.

Specifications and details are subject to verification upon inspection. Aircraft are offered
subject to prior sale or withdrawal from the market.