2008 Socata TBM 850

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The SOCATA TBM 850 is a single-engine turboprop aircraft manufactured by DAHER. It is a high-performance aircraft that is capable of cruising at speeds of up to 330 knots (606 km/h) and has a range of 1,515 nautical miles (2,800 km). It is typically used for business and personal travel, and is known for its comfortable cabin and advanced avionics. The TBM 850 is equipped with a Pratt & Whitney PT6A-66D engine, which produces 850 horsepower. It can accommodate up to 6 passengers and is often used for missions requiring long distance travel.


  • Total Hours: 3,035.8
  • Total Landings: 2,100
  • Garmin G1000 NXi Avionics Suite with Synthetic Vision 2 x GDU 1050A
  • 10" PFD displays with three axis flight dynamics, air speed, altitude, vertical speed
  • HSI w/ perspective modes, turn, bank side slip
  • NAV/COM frequencies indication and AP annunciation
  • GDU 1550 15" multi-function display with engine (WI optimum TRQ setting display) pressurization, electrical, fuel, flaps and trim indication
  • Crew Alerting Systems (CAS)
  • Aircraft synoptics and large navigation mapping system
  • 2x GIA 63W Nav/Com/ILS GPS
  • 2x GMA 1347D audio panel & marker beacon system
  • 2x GEA 71 Engine and airframe interface unit
  • 2x GRS 77 Attitude and Heading Reference System (AHRS)
  • 2x GMU 44 triaxial magnetometer
  • 2x GDC 74B digital air-data computers w/ dual probe system
  • 2x Garmin GTX33ES Transponder ADS-B out
  • GCU 475 remote FMS control panel conveniently located on the central console
  • GMC 700 autopilot mode controller located in upper central panel
  • GTA 82 adapter for yaw auto trim device
  • GDL 69 XM weather and music
  • Dual flight controls
  • Electric pitch and rudder trim on pilot control wheel
  • Elevator, Rudder and Aileron electric trim
  • Electrical flaps with integrated track, dissymmetry 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
  • Adjustable rudder pedals with dual toe brakes
  • Landing gear emergency extension handle
  • Environment and pressurization control system
  • Alternate static source control
  • Alternate ram air source control
  • Pneumatically deiced wing and tail unit

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