2011 Agusta A 109 SP Grand New Turbine Helicopter For Sale

This beautiful AGUSTA A109 SP has single pilot dual controls IFR Avions and is configured for VIP Passengers in mind with Air conditioning ECS (environment control system), Primer-finished cabin walls, all seats that are crash-resistant and covered with leather or fabric/leather.

Type:
Aircraft (Turbine Helicopter)
Manufacturer:
Agusta
Model:
A109SP Grand New
Year:
2011
Serial Number:
Please enquire
Reg. Number:
Please enquire
Total Time:
Please enquire
Seats:
8
Price:
Price upon request

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Price:
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Aircraft Type:
Aircraft Model & Manufacturer:
Year:
2011
Total Time:
Not Listed
Registration Number:
Not Listed
Serial Number:
Not Listed
Seats:
8
Aircraft Location:
Contact Name:
Stephen Green
  MESSAGE SELLER

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Description

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 AWARENESS 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)
REVERSIONARY CONTROL PANEL (RCP)
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 CHELTONINTERFACED 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 CONTROLS

ADDITIONAL EQUIPMENT (INCLUDING CUSTOMER FITTED EQUIPMENT)
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
CENTREPILLAR, JUST ABOVE THE EMERGENCY DOOR
HANDLE RELEASE
HIGH INTENSITY STROBE LIGHTS ON HORIZONTAL STABILIZER

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

    COCKPIT EQUIPMENT:

INTERSEATCONSOLE TRAY WITH 12V POWER SUPPLY
MULTIPURPOSE HOLDER (WITH SPACE PROVISION FOR
FIRE EXTINGUISHER)
RIGHT DOOR POCKET
HEADSET HOOKS (X2)
CYCLIC AND COLLECTIVE LEATHER GATORS
CURTAINS IN COCKPIT ON UPPER WINDOWS

    EXTERIOR:

CUSTOMISED METALLIC PAINT SCHEME WITH WHITE BODY,
DARK BLUE UNDERCARRIAGE, STRIPING DETAIL AND COWLING

    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)

AIRFRAME
ALUMINIUM ALLOY / COMPOSITE MATERIAL AND BONDED PANEL FUSELAGE
SEMI-MONOCOQUEALUMINIUM ALLOY TAIL BOOM
THREE-WHEELED RETRACTABLE LANDING GEAR
TWO HINGED JETTISONABLECREW DOORS (LH AND RH)
TWO SLIDING PASSENGER DOORS (LH AND RH), 1.40 M OPENING, WITH JETTISONABLEWINDOWS
ACRYLIC WINDSHIELD AND SIDE WINDOWS
ACRYLIC 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
CO-PILOT BRAKE CONTROLS (IN ADDITION TO THE PILOT STANDARD ONES)

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 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 DETECTORTRANSMISSION COOLING AND
LUBRICATION SYSTEMTRANSMISSION 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)

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)