Leonardo AW109SP

GRAND NEW IFR STANDARD CONFIGURATION STANDARD EQUIPMENT
- ACTIVE NOISE REDUCTION (ANR) HEADSETS (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 & CO-PILOT)
- TAIL BOOM STRIKE

SINGLE PILOT DUAL CONTROLS IFR AVIONIC PACKAGE
- PILOT FLIGHT/NAVIGATION EFIS (2 DISPLAYS) WITH EMBEDDED FMS, SYNTHETIC VISION (SVS), HTAWS (HELICOPTER TERRAIN AWARE-NESS AND WARNING SYSTEM),
- 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) EFIS PILOT/CO-PILOT NAVIGATION SYNCHRONISATION
- 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)
- 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)
- 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)

- AIRFRAME HOURMETER
- BAGGAGE COMPARTMENT EXTENSION (2.3M)
- ENGINE COMPARTMENT FIRE EXTINGUISHERS (X2)
- FUEL CAP WITH KEY LOCK
- PULSED CHIP DETECTORS
- REINFORCED WINDSHIELDS (PILOT & CO-PILOT) RETRACTABLE/ROTATING LANDING
- LIGHT (NOSE MOUNTED) ROTOR BRAKE
- WINDSHIELD WIPERS (PILOT & CO-PILOT) WITH WIPER SWITCH ON CYCLIC GRIPS
- 8.4” COCKPIT CENTRAL DISPLAY
- FDR/CVR
- WEATHER RADAR RDR 2000 BENDIX/KING
- DIGITAL MAP EURONAV V EUROAVIONICS
- 213 USG CRASH RESISTANT FUEL SYSTEM (IN LIEU OF 152 USG)
- LH ELECTRICALLY OPERATED PASSENGER STEP
- TAS (TAS-620 AVYDINE)
- TINTED OVERHEAD COCKPIT WINDOWS
- EXTRA DOOR HANDLE ON LEFT HAND CO-PILOT SIDE CENTRE PILLAR, JUST ABOVE
- THE EMERGENCY DOOR HANDLE RELEASE
- HIGH-INTENSITY STROBE LIGHTS ON HORIZONTAL STABILIZER

MISCELLANEOUS/GROUND EQUIPMENT:
- AIR INTAKE/EXHAUST COVERS
- GROUND TOOLS KIT (INCLUDING TOW BAR, LIFTING TOOL, WHEEL CHOCKS)
- ROTORCRAFT FLIGHT MANUAL (RFM) AND TECHNICAL PUBLICATIONS
- TIE-DOWN FITTINGS (MAIN ROTOR AND TAIL ROTOR RETENTION STRAPS)

- VIP INTERIOR (INCLUDING CUSTOMER FITTED OPTIONS)
- AIR CONDITIONING ECS (ENVIRONMENT CONTROL SYSTEM) PRIMER FINISHED CABIN WALLS
- ALL SEATS CRASH-RESISTANT COVERED WITH LEATHER OR FABRIC/LEATHER
- 3 FWDFACING SEATS (AFT BENCH) WITH FOLDABLE ARMREST AND GLASS HOLDER
- 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 CORPORATE CABIN FINISHING DECORATION TRIM WITH METAL INSERTS INTERCOMMUNICATION SYSTEM FOR PASSENGERS HEADSET BOSE
- ANR TYPE (X6)
- CABIN LOUDSPEAKERS (X2)
- READING LIGHTS, EMERGENCY LIGHTS, FLOOR COURTESY LIGHTS
- PASSENGER HOOKS (X4)
- UPPER AND LOWER AIR VENTS
- FLOOR CARPETING
- CARPETING PROTECTION
- SEAT COVERS
- INTERSEATCONSOLE TRAY WITH 12V POWER SUPPLY
- MULTIPURPOSE HOLDER (WITH SPACE PROVISION FOR FIRE EXTINGUISHER)
- RIGHT DOOR POCKET

INTERIOR ARRANGEMENT
- CRASH-RESISTANT PILOT SEAT, FORE AND AFT ADJUSTABLE, WITH LAP BELTSAND HEADREST ALUMINIUM ALLOY HONEYCOMB - REINFORCED FLOOR WITH ANTI-SKID FINISHING VENTILATION RAM AIR INLETS
- ANTI REFLECTION INSTRUMENT PANEL
- HEADSET HOOKS (X2)
- CYCLIC AND COLLECTIVE LEATHER GATORS
- CURTAINS IN COCKPIT ON UPPER WINDOWS

- CUSTOMISED METALLIC PAINT SCHEME WITH WHITE BODY, DARK BLUE UNDERCARRIAGE, STRIPING DETAIL AND COWLING
- FINISHING IN ACCORDANCE WITH MANUFACTURER SPECIFICATION (NTA 893 A) PRIMER EXTERIOR PAINTING)

- 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 USGAL)
- SUBMERGED FUEL BOOST PUMP (2)
- AIRFRAME MOUNTED EASY ACCESS FUEL FILTER
- RH REFUELLING POINT & GROUND FUEL DRAINS

TRANSMISSION DRIVE SYSTEM AND HYDRAULIC SYSTEM
- 960 SHPFOR TAKEOFFAND 900 SHPCONTINUOUS 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
- TAXING LIGHTS (2) AND LANDING LIGHTS (2) ON LANDING GEAR SPONSONS
- ANTI COLLISION LIGHTS (2)
- 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)