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TBM 850 G

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TBM 850 G

Total Time :

  • Registration #
  • FlightRules
    IFR
  • Serial Number
  • Based at
  • Condition
  • Total Landings:

Description

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AIRFRAME

  • Environment system w/ engine driven air-conditioning system (VCS).
  • Pneumatically deiced wing and tail unit.
  • Pilot electrically heated windshields.
  • Pilot & Co-pilot electrically heated windshields.
  • Parking brake control.
  • Landing gear control panel.
  • Ice detector light.
  • Heated stall warning system.
  • Cabin temperature control (dual zone, with override capability).
  • Airframe de-icing control panel.
  • Adjustable rudder pedals.
  • Large cabin and baggage compartment.
  • High-speed pneumatic de-icing equipment.
  • Jacking points.
  • Tie-down attachments.
  • Rear fuselage servicing door.
  • Emergency exit.
  • Front storage compartment (not pressurized) with external door.
  • Large access door with retractable stairway.
  • Retractable gear with electro hydraulic actuation.
  • Electrical pre-select flaps with integrated track and dissymmetry detector.
  • Metal structure and skin paneling.
  • Electric generation controls and monitoring on overhead panel.
  • Gaseous oxygen system for 6 seats and quick-donning masks for pilot and copilot.
  • Sound proofing and thermal insulation.
  • Pressurized 6 seats cabin (6.2psi) and baggage compartment.
  • Electric pitch and rudder trims on pilot & co-pilot control wheel.
  • Electrically heated pitot tubes.
  • Electrically deiced stall warning sensor.
  • Electrically heated propeller blades & pitot tubes.
  • Environment and pressurization control system.
  • Hydraulic disc breaks.
  • Bank control through ailerons and spoilers with aileron trim.
  • Anticorrosion protection treatment.

    • AVIONICS

  • 1 : Instrument panel lighting, CB dedicated switch lighting.
  • 1 : GARMIN Flight Stream FS 210 Bluetooth/Wi-Fi allowing Tablet to Avionics exchange secured information.
  • 1 : WX 500 Stormscope.
  • 1 : GARMIN GWX 68 Digital weather radar.
  • 1 : GARMIN GTX 330 transponder.
  • 1 : GARMIN GTS 820 Traffic Advisory System (TAS) displayed on MFD and PFD inset map.
  • 1 : GARMIN GTA 82 adapter for yaw auto trim device.
  • 1 : GARMIN GSA 81 brush less flight servos (yaw, pitch, trim and roll).
  • 1 : GARMIN GRS 77 Attitude and Heading Reference System (AHRS).
  • 1 : GARMIN GMU 44 triaxial magnetometer.
  • 1 : GARMIN GMC 710 autopilot mode controller located in upper central panel.
  • 1 : GARMIN GMA 1347D Dual digital audio controller with integrated marker beacon receiver, intercom and public address capability on outer side for pilot and co-pilot side.
  • 1 : GARMIN GIA 64W Nav/Com/ILS/WAAS/GPS.
  • 1 : GARMIN GEA 71 Engine and airframe interface unit.
  • 1 : GARMIN GDL 69A SXM datalink weather information and XM audio infotainment (US coverage only)
  • 1 : GARMIN GDC 74B Digital air-data computers with dual probe system.
  • 1 : GARMIN GCU 485 remote FMS control panel conveniently located on the central console.
  • 1 : Aural warnings
  • 1 : Advisory panel displayed on GDU 1500 Master Caution, alerts & Aural warnings.
  • 1 : KN 63 DME displayed on GDU 1050As.
  • 1 : Flight time hour meter.
  • 1 : Voice alert system.
  • 1 : Dedicated master warning and caution for Crew Alerting System message acknowledgement.
  • 1 : LPV, LNAV/VNAV (including Baro VNAV) approaches support and advisory vertical guidance for LP, LNAV and Visual approaches.
  • 1 : Digital chronometer displayed on GDU 1040s.
  • 1 : RVSM data package.
  • 1 : TAWS-B, class B TAWS worldwide database.
  • 1 : RA-4500 Freeflight radar altimeter.
  • 1 : Yaw Damper.
  • 1 : King KN 63 DME.

    • ADDITIONAL EQUIPMENT

  • Electrically deiced stall warning sensor.
  • Heated engine air intake lip.
  • Cabin Temperature Control.
  • Environment and pressurization control system.

    • CONTROLS

  • Power controls.
  • Fuel selector control - Auto slelect.
  • Central console including single lever power control with bleed inhibition in low idle condition, electric flap control, fuel selector, manual pitch trim, ailerons electric trim, manual override control.
  • Ailerons, rudder, and elevator electric trim.
  • Alternate ram air source control.
  • Alternate static source control.
  • Automatic environment and pressurization control system with max diff. mode
  • Landing gear emergency extension handle.
  • Electrical pre-select flaps with integrated asymmetry detection system.
  • Elevator, rudder and aileron electric trim.
  • Electric flaps control
  • Manual control override.
  • Propeller pitch control.
  • Adjustable rudder and nose wheel steering pedals.
  • Electrical pitch and rudder trim (LH and RH).
  • Dual flight controls.

    • CABIN FITTINGS

  • Fully adjustable pilots seats (height and depth).
  • Fully adjustable (3-axis) pilot and co-pilot seats and adjustable rudder pedals.
  • Front head rests with folding armrests and headrests.
  • Cup Holders.
  • Carpeting and upholstery.
  • Cabin halon fire extinguisher.
  • Baggage compartment
  • All seats with adjustable backrests.
  • 6x Genuine leather seats with adjustable backrests and folding armrests in replacement for fabric.
  • Ship-powered headset jacks behind each seat (Bose Lemo plugs).
  • Pilot and co-pilot sun visors.
  • Leather upper cabin side panels, leather covered lower cabin side panels, wool carpeting.
  • Pilot and Co-pilot Seats: 4 -point safety belts w/quick release.
  • Reel up 3 points safety belts at all Passenger seats.
  • Individual vents and lightings.
  • Sound-proofing and thermal insulation.
  • Pressurized cabin (6.2 PSI).

    • ELECTRICAL EQUIPMENT

  • Ice Detection light
  • Tri-band ELT with GPS connection
  • Electrical power control center
  • Standby generator 28 V- 100 Amp
  • Lead acid battery 24V-42 A.h
  • Ground clearance energy saver
  • Ground power plug receptacle
  • Taxiing and landing lights
  • Navigation lights
  • Anti-collision strobe lights
  • Circuit breakers
  • High safety electrical power system for regulation and switching
  • Auxiliary generator
  • Automatic starter generator transition during start

    • ENGINE NOTES

    EXTERIOR

    EXTERIOR COLOR

    FUEL EQUIPMENT

    INTERIOR

    Year Design :
    Number of seats : 6
    Interior Notes : Oxygen System: Gaseous
    Retractable working table.
    Metallic finishing
    High comfort leather seats.

    INTERIOR COLOR

    INTERIOR EQUIPMENT

  • Retractable working table.
  • Pneumatically deiced wing and tail unit.
  • Platinum Edition including ice protection.
  • Pilot controlled engine inertial separator.
  • Pilot & Co-pilot electrically heated windshields.
  • Oxygen System.
  • Ice detector light.
  • Heated engine air intake lip.
  • Electrically heated propeller blades.
  • Electrically heated pitot tubes.
  • Electrically deiced stall warning sensor.
  • High comfort leather seats.
  • Baggage compartment with straps.
  • Belts w/quick release.
  • Pilot & Co-Pilot Seats 4-point safety.

    • ICE PROTECTION

    INSTRUMENT PANEL

  • Electric generator control and monitoring on overhead panel - voltmeter and ammeter.
  • Alternate ram air source control.
  • Alternate static source control..
  • Stall warning system.
  • Airframe de-icing control panel.
  • Advisory panel with master caution, master warning and aural warnings.
  • Instrument panel lighting.
  • Trim position indicator (elevator, rudder and ailerons).
  • Flaps position indicator
  • Landing gear control and monitoring panel.
  • OAT Indicator*
  • Turbine temperature indicator (ITT)*
  • Torque indicator*
  • Oil pressure indicator*
  • Fuel management panel*
  • Propeller tachometer.
  • Gas generator tachometer*
  • Digital Chronometer*
  • Magnetic compass.
  • Vertical speed indicator*
  • Sensitive altimeter*
  • Airspeed Indicator*

    • MISCELLANEOUS

  • Air Conditioning-
  • Pulse light anti-collision system.
  • Hour meter airborne.
  • Map reading tablet.

    • PROPELLER

    WARRANTY & MAINTENANCE

    • BLACK CIRCLE
    • Maximum Ciruse Speed 326 KTS : ISA Condition -No Wind-FL 310 Minute Reserve
    • RED CIRCLE
    • Long Range Ciruse speed 252 KTS : ISA Condition-No Wind-FL 310 Minute Reserve


    • From

    • To

    • Distance

    • Duration

    • Empty Fuel Burn

    • Load Fuel Burn

    Disclaimer: Distances calculated may be approximative. Wind is not taken into consideration. No flight can be based on this application. Please consult the Aircraft Pilot Operating Handbook (POH) for flight planning purposes.

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