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For Sale Price: USD $2,450,000

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Perfect condition - Low time and VAT paid TBM 850 G1000 - Great value to European private buyers!
Pre-owned maintenance and warranty program available
Metal structure and skin paneling
Anti-corrosion protection treatment
Electrical pre-select flaps with integrated track
and dissymmetry detector
Bank control through ailerons and spoilers with
trim on left aileron
Retractable gear with electro hydraulic control
Hydraulic disc brakes
Large cabin and baggage compartment Large
access door with retractable stairway
Front storage compartment (not pressurized) with
external door
Emergency exit
Rear fuselage servicing door
Tie-down attachments
Jacking points Painting and decoration
High-speed pneumatic de-icing equipment
Easy maintenance access doors
Electrical starter/generator
Oil cooler
Inertial separation anti-icing air inlet
Dual exhaust
Servicing doors in cowlings
Prop Specs
Hartzell 4-blade prop
G1000 Flight Deck includes:
• Airspeed Indicator displayed on GDU 1040s
• Vertical speed indicator displayed on GDU 1040s
• Magnetic compass
• Torque indicator displayed on GDU 1500
• Propeller tachometer displayed on GDU 1500
• Turbine temperature indicator (ITT) displayed on GDU 1500
• Gas generator tachometer displayed on GDU 1500
• Oil pressure and temperature indicator displayed on GDU 1500
• OAT Indicator displayed on GDU 1040s
• Airframe de-icing control panel
• Inertial separator control
• Parking brake control
• Landing gear position monitoring panel
• Flap position indicator displayed on GDU 1500
• Trim position indicator (elevator, rudder and ailerons) displayed on GDU 1500
• Voltmeter and ammeter displayed on GDU 1500
• Electric generation controls and monitoring on overhead panel
• Advisory panel with master caution, master also displayed on GDU 1500 warning and aural warning
• Fuel management panel displayed on GDU 1500
• Cabin temperature control
• Cabin altitude and differential pressure indicator displayed on GDU 1500
• Cabin rate of climb indicator displayed on GDU 1500
• Heated stall warning system
• Digital chronometer displayed on GDU 1040s
• Flight time hour meter
• Instrument panel lighting
• Backup instrumentation with pneumatic attitude,airspeed and altimeter indicators

Instrument Panel:
Integral instrument panel w/ spare locations for options
Airspeed Indicator
Sensitive altimeter
Vertical speed indicator
Electrical turn and bank indicator
Magnetic compass
Digital Chronometer
Gas generator tachometer
Propeller tachometer
Fuel management panel
Data Computer
Oil pressure indicator
Torque indicator
Turbine temperature indicator (ITT)
OAT Indicator
Landing gear control and monitoring panel
Flaps position indicator
Trim position indicator (elevator, rudder and ailerons)
Voltmeter and ammeter
Electric generator control and monitoring on overhead panel Instrument panel lighting
Advisory panel with master caution, master warning and aural warnings
Environment and pressurization control system
Airframe de-icing control panel
Stall warning system
Alternate static source
Additional Equipment
Electrical Equipment:
Lead Acid battery 24V-43A/h
Starter generator 28V
Auxiliary generator
High safety electrical power center for regulation and switching
Circuit breakers
Anti-collision strobe lights
Navigation lights
Taxiing and landing lights
Ice detector light
Ground power plug receptacle
Ground clearance energy saver

Cabin Fittings:
Pressurized cabin (6.2 PSI)
Carpeting and upholstery
Sound-proofing and thermal insulation
Air conditioning
Individual vents and lightings
Sun visors
Fully adjustable pilots seats (height and depth)
All seats with adjustable backrests
Front and head rests with folding armrests and headrests
Reel up 3 points safety belts at all
Passenger seats
Pilot & Co-Pilot Seats 4-point safety belts w/quick
Retractable working table
Airway charts cabinet
Supplementary Oxygen system
Baggage compartment with straps and net

Dual flight controls
Electrical pitch and rudder trim (LH and RH)
Adjustable rudder and nose wheel steering pedals
Central console including:
-Power control
-Propeller pitch control
-Condition lever
-Manual control override
-Electric flaps control
-Fuel selector control
-Ailerons electric trim
Dual toe brakes
Parking brake

Additional Equipment:
Emergency gear extension handle
Environment & pressurization control
Alternate static source control
Alternate ram air source control
Pneumatically deiced wing and tail
Heated engine air intake lip
Pilot controlled inertial separator
Electrically heated propeller blades & Pilot Tubes
Electrically deiced stall warning
Pilot heated windshields
Ice detector light

Map reading tablet
Refreshment cabinet LH
Hour meter airborne
Pulse light anti-collision system
Supplementary Gaseous Oxygen
Fuel Equipment:
One structural fuel tank per wing
Constantly operating mechanical fuel pump
Stand-by electrical fuel pump
Fuel tank selector with automatic sequencer unit
Capacitance gauging with low-level warning
Year Painted
White blue and light blue stripe
Year Interior
Light grey
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