2016 Leonardo AW109SP GrandNew Turbine Helicopter For Sale (G-KLNH)

Description

Airframe

Aluminium alloy/composite material & 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 & side windows
Acrylic transparent overhead windows
Quick removable tail rotor drive shaft cover
Separate baggage compartment with hinged door
Removable fairing & cowlings, for complete accessibility to the controls & drive components
Swivelling front wheel with tow bar attachment
Quick opening hinged inspection doors, to allow visual check of engine oil levels & maintenance inspection points
Grounding points
Jacking & hoisting points

Engine(s)

Power plant & fuel system:
Two Pratt & Whitney Canada PW207C turbo-shaft engines
Two independent electronic control systems (FADEC) with normal emergency & training operation modes & auto-start
Engine mounted fuel pump & filter assembly
Engine mounted oil pump & filter assembly
Engine mounted fuel control & governor
Lubrication & cooling system
Engine oil chip detectors (2)
Engine control panel
Two independent fuel systems with cross-feeding valve & 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 drains

Rotors & controls:
Titanium main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite material blades, swept tips & dampers
Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite blades, individually interchangeable
Cyclic & collective controls powered by two hydraulic systems
Hydraulically powered anti-torque system
Adjustable friction devices on cyclic & collective system
Force trim & artificial feel system
Adjustable directional control pedals
Flapping & 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 & C in cockpit (installed by Sloane post-delivery)

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 & remote Bug Panel (RBP)
(*) In lieu of basic Pilot flight/navigation EFIS (1 displays) with slip indicator & 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 & Warning System), slip indicator & 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

Equipment

Standard Equipment:
Active Noise Reduction (ANR) headset (pilot & co-pilot)
Baggage compartment lights
Crash-resistant co-pilot seat, fore & aft adjustable, with lap belts & 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 & co-pilot)
Tail boom strake

Additional Equipment:
Airframe hour meter
Baggage compartment extension (1.9 m)
Electrically operated passenger step (LH)
Engine compartment fire extinguishers (Qty 2)
Fuel cap with key-lock
Mast Vibration Absorber
Pulsed chip detectors (in lieu of quick disconnecting chip detectors)
Reinforced windshields
Retractable/rotating landing light (nose mounted)
Rotor brake
Single drawer in cabin (under aft bench)
USB charger in passenger cabin (under LH or RH side rear facing seat)
Windshield wipers (pilot & 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

Transmission drive system & hydraulic system:
960 shp for takeoff & 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 & scavenge pump & oil filter
Transmission oil chip detectors (2)
Single stage, bevel gear T/R 90° gear box including oil level sight glass & chip detector
Transmission cooling & 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) & 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 & 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) & temperature (°C) indicator
Two engine oil pressure (PSI) & 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 & Maintenance System:
Master warning lights (2)
Master caution lights (2)
Warning, caution & 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 & aft adjustable, with lap belts & 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 walls
Passenger 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 & with foldable armrest
4-point shoulder harness with inertial reels & 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 & 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 & collective leather gators
Curtains in cockpit on upper windows

Exterior

Exterior finishing:
Finishing in accordance with manufacturer specification (NTA 893 A)
Primer exterior painting

Painting:
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) & technical publications
Tie-down fittings (main rotor retention straps)