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  • Alert Me Name: Leonardo AW109SP Grand New
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Leonardo AW109SP Grand New
Make Offer
  • YEAR
    2013
  • LOCATION
    Europe, Russian Federation
  • S/N
    22314
  • REG
    RA01986
  • TTAF
    620

Aircraft Highlights

URGENT SALE

Looks just like accepted from the factory

Email: bjetsale@gmail.com

Cell: +79629207390

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 transparent windshield and side windows – Acrylic transparent 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 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 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 US gal) – Submerged fuel boost pump (2)– Airframe mounted easy access fuel filter – RH refuelling point – Ground fuel drains Transmission drive system and hydraulic system – 960 shp for take-off and 900 shp continuous operation main transmission – Three-stage transmission – Freewheeling units (2) – Dual independent, redundant hydraulic systems – 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 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) – Taxing lights (2) and landing lights (2) on landing gear sponsons – 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) NAT with one cockpit panel – Electronic clock (1) – Magnetic compass indicator (1) 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 indicators (PSI) – Outside air temperature indicator (°C) – Two AC voltmeters (VAC) – Two DC voltmeters (VDC) – Two DC ammeters (Amp) Warning/caution advisory and maintenance system – Master warning lights – Master caution lights – Warning, caution and advisory messages (on IDS display) – Aural warning generator system – Engine fire detection system – Exceedance recorder system (on IDS display) 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 Exterior finishing – Finishing in accordance with manufacturer specification (NTA 893 A) – Primer exterior painting 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)

ENGINES

2 * PW207C
620 fh each
Year inspection in progress and will be finalized in 2 weeks
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 – 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 controlsADDITIONAL EQUIPMENT – Airframe hourmeter – 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 windshield – Retractable/rotating landing light (nose mounted) – Rotor brake – Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips INTERIOR – Air conditioning ECS (Environment Control System) – Primer finished cabin walls
"Elite" interior - 5 places Passenger cabin – All seats crash-resistant covered with leather or fabric/leather – 2 fwd. facing seats (aft bench) with Elite central cabinet – 3 aft facing seats (central bench) with see-through modification and with foldable armrest and glass holder – Forward facing side armrests – 4-point shoulder harness with inertial reels and safety belts for all passenger seats – Super silent soundproofing – Liners leather/Leatherette covered – Acoustic screen around doors – Cabin double layer acrylic windows – Customised Elite finishing– Decoration trim with metal inserts – Intercommunication system for passengers – Headset Bose ANR type (Qty 5) – Cabin loudspeakers (Qty 2) – Reading lights, emergency lights, floor courtesy lights – Passenger hooks (Qty 4) – Upper and lower air vents – Floor carpeting – Carpeting protection – Seat covers 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
Very nice painting scheme
– 213 USG crash-resistant fuel system (in lieu of 152 USG) – Baggage compartment extension (2.3 m) – Single central drawer – High intensity strobe lights on horizontal stabilizers – Euroavionics Euronav V digital map interfaced to FMS (presented on cockpit central 8.4" display) – Cockpit central monitor 8.4" for digital map, FLIR and EVS – Traffic Advisory System TAS-620 Avydine (presented on EFIS) – Weather radar RDR 2000 Bendix/King (presented on EFIS), provision & removable – Snow skis/slump protection pads provision – Russian certification kit – Mast vibration absorber – Satcom Iridium – Entertainment system – Electrically operated step (RH)
Need Urgent deal

Leonardo AW109SP Grand New

Make Offer
  • YEAR
    2013
  • LOCATION
    Europe, Russian Federation
  • S/N
    22314
  • REG
    RA01986
  • TTAF
    620
User Image
Roman Zuykin
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