Aircraft Information |
Reference #: JA052318A |
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- Registration: C-GTMI
- Serial No: 22160
- Location: Ontario, Canada
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Airframe |
Left Engine: Pratt & Whitney PW2O7C -960 SHP
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Right Engine: Pratt & Whitney PW2O7C -960 SHP
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Exterior |
- Navy Blue Metallic Paint with White Accents
- Gold Accent Striping
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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
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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
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- 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
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- 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)
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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
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- 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
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- 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
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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
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Asking Price: |
Reduced to $3,295,000 USD SOLD! |
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