G-CMUV - 2024 LEONARDO AW109SP GRANDNEW

2024

LEONARDO

AW109SP GRANDNEW

22462

G-CMUV

Used

HIGHLIGHTS Delivery time 5 year Leonardo warranty Elite completion package Hangared near Heathrow Int Airport, UK

50

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 POWER PLANT & 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) -Two Submerged fuel boost pump -Airframe mounted easy access fuel filter --RH refuelling point Ground fuel drains TRANSMISSION DRIVE SYSTEM & 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 (1 RH + 1 LH) and landing lights (1 RH + 1 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

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, 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

PRATT & WHITNEY

PW207C

PCE-BH1137

50

SNEW

Landings: 9

PRATT & WHITNEY

PW207C

PCE-BH1139

50

SNEW

Landings: 9

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) 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 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 Genesys Aerosystems interfaced to EFIS/FMS Co-pilot GPS/SBAS Genesys Aerosystems 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 Dual controls WARNING / CAUTION ADVISORY & 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)

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 strake ADDITIONAL EQUIPMENT Airframe hourmeter Baggage compartment extension (2.3m) 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 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) CUSTOMER SELECTED EQUIPMENT -Painting Customized painting scheme, Premium Plus; up to 5 colours from selection, Premium finishing, Registration Marks and Logos (decal or painted) -Utility Equipment 213 USgal crash-resistant fuel system (in lieu of 152 USG) High-intensity white strobe lights on horizontal stabilizer Electrically operated passenger step (LH) -Avionic Equipment Traffic Advisory System TAS-620 Avydine (presented on EFIS) Weather radar RDR 2000 Bendix/King or equivalent model (presented on EFIS) iPad certified mount with USB charger point for USB A and C in cockpit (installed by Sloane post-delivery) 8.4” cockpit central display – provision Enhanced Vision System (EVS) Max-Viz 2300 – provision Cockpit Voice/Flight Data Recorder (CVR/FDR) Penny & Giles - provision

COMPLETION: GRANDNEW ELITE INTERIOR - 5 PLACES VIP Passenger Cabin, including: Super silent soundproofing Liners leather/leatherette covered Intercommunication system for passengers Two (2) cabin loudspeakers Reading lights, advisory lights, floor courtesy lights Upper and lower air vents VIP Cabin finishing VIP Cockpit package, including: Interseat console tray with 12 V power supply Multipurpose holder (with space provision for fire extinguisher) Right door pocket Two (2) headset hooks Cyclic and collective leather gators Curtains in cockpit on upper windows VIP Cockpit finishing Two (2) crashworthy fwd facing seats (aft bench) covered with leather, with Elite central cabinet Three (3) crashworthy aft facing seats (central bench) covered with leather, with see-through modification and with foldable armrest 4-point shoulder harness with inertial reels and safety belts for all passenger seats Cabin double layer acrylic windows (azure coloured) Five (5) Headset Bose ANR type Floor carpeting Leather headset straps in cabin Dual USB charger at central bench (RH) (A-C ports) Four coat hooks in passenger 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 TRIM Air conditioning ECS (Environment Control System) Primer finished cabin walls