General
Year: 2011
Manufacturer: AGUSTA
Model: AW109SP GRANDNEW
Condition: Used
Description: SINGLE PILOT DUAL CONTROLS IFR AVIONIC PACKAGE, FRESH ANNUAL, VIP PASSENGER
Airframe
Airframe Notes: 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)
Engine 1
Engine 1 Notes: 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
Avionics
Avionics/Radios: 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)
Exterior
Exterior Notes: FINISHING IN ACCORDANCE WITH MANUFACTURER SPECIFICATION (NTA 893 A)
PRIMER EXTERIOR PAINTING)
Interior
Interior Notes: 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
USD $3,250,000