2006 TBM 850 S/N 386 N850AR Available 12/06 2006 TBM 850 S/N TBD NTBD Available 3/07 2006 TBM 850 S/N TBD NTBD Available 5/07	Socata TBM 700 / 850 320 KTAS, 1520 NM Range, Full fuel payload 849 lbs, Honeywell EFIS/Autopilot, Dual Garmin 530’s, Honeywell KMD 850 Multi Func. Display, ADF, DME, RMI, Full Co-Pilot Instruments, Bose Head Sets,  Metallic Paint, Leather Interior, Flight Training.
AIRFRAME Metal structure and skin panelling Anti-corrosion protection treatment Retractable gear with electrohyd raulic actuation Hydraulic disc brakes Pressurized 6 seats cabin (6.2 psi) and baggage compartment Sound proofing and thermal insulation Large access door with retractable stairway Emergency exit Front storage compartment (not pressurized) with external door Rear baggage compartment (not pressurized) with external door Rear fuselage servicing door Easy maintenance access doors Tie-down attachments Jacking points Standard painting and decoration   ENGINE PT6A-66D Pratt & Whitney Canada turboprop engine developing 1825 SHP     thermodynamic, flat rated at 850 SHP Electrically de-iced four bladed Hartzell constant speed propeller with overspeed limiter, full feathering and reverse Polished aluminum spinner cone Oil cooler Inertial separation anti-icing air inlet Dual exhaust Service access doors     INSTRUMENT PANEL Airspeed Indicator Vertical speed indicator Magnetic compass Torque indicator Propeller tachometer Turbine temperature indicator (ITT) Gaz generator tachometer Oil pressure and temperature indicator OAT Indicator Airframe de-icing control panel Inertial separator control Parking brake control Landing gear position monitoring panel Flaps position indicator Trim position indicator (elevator, rudder and ailerons) Voltmeter and ammeter Electric generation controls and monitoring on overhead panel Advisory panel with master caution, master warning and aural warning Fuel management panel Cabin temperature control Cabin altitude and differential pressure indicator Cabin rate of climb indicator Heated stall warning system Digital chronometer Flight time hourmeter Instrument panel lighting Tn-band ELT with aircraft identification KFC 3253 axis digital auto pilot with pre-select altitude and yaw damper   ELECTRICAL SYSTEM Lead Acid battery 24V-43 A.h Startergenerator28V-200Amp (rated at 180 Amp) Standby generator 28 V-b Amp (rated at 57 Amp) Electrical Power Center for regulation and switching Circuit breakers Anticollision strobe lights Navigation lights Taxiing and landing lights Ground Power Unit (GPU) plug Ground clearance energy saver   FUEL EQUIPMENT One structural fuel tank per wing Engine driven fuel pump Standby electrical fuel pump Fuel tank selector with automatic sequencer unit Capacitance gauging with low level warning   CONTROLS Dual flight controls Electrical pitch and rudder trims on LH control wheel Pitch control through elevators with trim Yaw control through rudder with trim Electrical flaps with integrated track, dissymety detectors and sensor Bank control through ailerons and spoilers with trim on left aileron Central console including:  - power control  - propeller pitch control  - condition lever  - manual control override  - electric flaps control  - fuel selector control  - manual pitch trim  - ailerons electric trim Adjustable rudder and nosewheel steering pedals Landing gear retraction and extension control Dual toe brakes Parking brake Landing gear emergency extension control Environment and pressurization control system Alternate static source control Alternate ram air source control MISCELLANEOUS Halon cabin extinguisher Parking protection kit Cabin cover