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2010 Agusta A109S Grand

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Aircraft Information Reference #: JA052318A
  • Registration:  C-GTMI
  • Serial No:  22160
  • Location:  Ontario, Canada
Airframe
  • 535 TTSN
Left Engine:  Pratt & Whitney PW2O7C -960 SHP
  • 535 TTSN
  • 862 Cycles
  Right Engine:  Pratt & Whitney PW2O7C -960 SHP
  • 535 TTSN
  • 862 Cycles
Exterior
  • Navy Blue Metallic Paint with White Accents
  • Gold Accent Striping
Interior
  • VIP Interior
  • 3 Forward Facing and 3 Aft Facing Crash Resistant Seats in Blue Leather
  • Gold Platted Seat Belt Hardware, Door Handles and Cabin Vents & Lighting
  • Interior Reading Lights, Advisory Lights & Floor Courtesy Lights
  • 4 Point Shoulder Harnesses with Inertia Reels and Safety Belts
  • Blue Leather Lower Interior Panels with Wood Grain Accents
  • Blue Floor Carpet with Tan Interior Upper Panels
  • Cabin Double Layer Acrylic Windows
  • Cabin Silent Soundproofing
  • Cabin Loudspeakers
Avionics
  • Garmin GNS 530 VHF COM/NAV/GPS
  • Garmin GNS 430 VHF COM/NAV/GPS
  • Bendix/King KMD 550 Moving Map
  • Bendix/King KT-73 Transponder-Mode S
  • Bendix/King KR-87 ADF
  • Bendix/King KDM 706A DME
  • AEM AA31 Intercom System
  • Dual AEM AA95 Audio Panels
  • Bendix/King KMR 675 Marker Beacon
  • Honeywell AA 300 Radio Altimeter
  • Honeywell SP711 3-Axis Duplex AFCS
  • Radio Master Switch w/ Ground Function
 
  • Dual Pilot and Co-Pilot MFD
  • Dual Systems Display Panels
  • Artex C406-2HM ELT
  • EFIS Pilot/Copilot in Command Switch
  • Barometric Encoding Altimeter
  • LC Integrated Display System (IDS)
  • 8 Day Clock with Elapsed
  • Honeywell C14 Gyrocompass
  • Magnetic Compass Indicator
  • Instantaneous Vertical Speed Indicator
  • Pilot and Copilot Headsets
  • 6 Passenger Noise Reduction Headsets
  • TAS SKY 497 Displays on GNS 530
  • Honeywell FZ 702 Flight Director w/ Autotrim
  • Flightline System 46060-11 Vertical Gyro #1
  • JET Electronics VG-208 Vertical Gyro #2
  • AC Power Supply System (two inverters)
  • Pilot ICS - (Includes Pilot/Copilot Control Panel, Mode Controller, Audio Cabin Control)
  • Pilot Navigation Instruments (LCD EADI and EHSI, Stand-by ADI)
  • Copilot Flight/Navigation Instruments (LCD EAD1 and EHSI, Barometric Altimeter, Airspeed Indicator, VSI)
Equipment
  • Dual Controls
  • Air Conditioning ECU Garret
  • Pilot & Copilot Sliding Windows
  • Two Hinged Jettisonable Crew Doors
  • Crew Open Door Actuators
  • Anti Reflection Instrument Panel
  • Ventilation Ram Air Inlets
  • Three Wheel Retractable Landing Gears
  • Quick Disconnecting Chip Detectors
  • Engine Fire Detection System
  • Fuel Drain Electrical Valves
  • External Power Receptacle
  • Passive Vibration Absorber
  • Engine Compartment Fire Extinguishers
  • Pulsed Engine Oil Chip Detectors
  • Two DC Ammeters (on IDS display)
  • Two DC Voltmeters (on IDS display)
  • RH Refueling Point
  • Rotor Brake
 
  • Instrument Lights w/ Dimming Switch
  • Retractable/Rotating Landing Light
  • Two 250 W Landing Lights
  • Two 150 W Taxing Lights
  • Two Anti Collision Lights
  • Position Lights
  • Two Utility Lights
  • Baggage Compartment Light
  • Quick Opening Hinged Inspection Doors
  • Portable Fire Extinguisher
  • Air Intake/Exhaust Covers
  • Pitot Tubes Covers
  • All-Weather Covers
  • First Aid Kit
  • Tie-down Fittings Provisions
  • Locking Fuel Cap
  • Ground Fuel Drains
  • Airframe Hour Meter
  • Tail Boom Strake
  • Two Sliding Passenger Doors with Jettisonable Windows
  • Crash-Resistant Pilot Seats - Fore and Aft Adjustable with Lap Belts
  • Pilot and Copilot Shoulder Harness with Inertia Reel
  • Pilot and Copilot Windshield Wipers with Wiper Switch on Cyclic Grip
  • 24 volt DC 27 Ah Nckel Cadmium Battery with Temperature Probe
  • Extended Baggage Compartment w/ Hinged Door
Additional Information
  • Dual Separate-Redundant Hydraulic Systems
  • Two Independent Electronic Control Systems (FADEC)
  • Corrosion-Protected Titanium Main Rotor Hub
  • Interchangeable Composite M/R Blades w/ Swept Tips
  • Composite Tail Rotor Blades
  • Hydraulically Powered Anti-Torque T/R Control System
  • Swiveling Front Wheel with Tow Bar Attachment
  • Adjustable Friction Devices on Cyclic and Collective System
  • Force Trim and Artificial Feel System
  • Adjustable, Elongated T/R Control Pedals
  • Dynamic Main Rotor Blade Flapping Lock Mechanism
  • Engine-Mounted Fuel Management Unit (FMU)
  • Crash-Resistant Extended Range Fuel System (213 USG)
  • Jacking and Hoisting Points
  • Rotorcraft Flight Manual and Technical Publications
  • Ground Tools Kit (Includes Tow Bar, Lifting Tool, Wheel Chocks)
  • Structural Provision for Utility Equipment (Emergency Floats, Rescue Hoist, Cargo Hook, Weather Radar, Engine Fire Extinguisher, Flight Director, AFCS)
  • Maximum Takeoff Weight - 3,175 KG / Empty Weight - 2,200 KG
Asking Price:   $3,595,000 USD
  Reduced to $3,295,000 USD

Aircraft Subject To Availability & Verification Of Specifications


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