Leonardo AW109SP

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

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 & 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 & 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

Pratt & Whitney PW207C Turboshaft

S/N: PCE-BH1137
TSN: 10
Landings: 9

Pratt & Whitney PW207C Turboshaft

S/N: PCE-BH1139
TSN: 10
Landings: 9