Avex

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TBM 960

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TBM 960

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.
  • Pilot access door.
  • 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.
  • Carbon fiber engine cowling and winglets.
  • Electrically heated pitot tubes.
  • Electrically deiced stall warning sensor.
  • Electrically heated propeller blades & pitot tubes.
  • Environment and pressurization control system.
  • Flight data recorder.
  • 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 : Homesafe Autoland
  • 1 : GARMIN GWX 8000 StormOptix weather radar.
  • 1 : GARMIN GWX 8000 StormOptix doppler weather radar.
  • 1 : GARMIN GTX 330 transponder.
  • 1 : GARMIN GRA 55 Radar Altimeter displayed on PFDs.
  • 1 : GARMIN GMU 44 triaxial magnetometer.
  • 1 : GARMIN GMC 710 autopilot mode controller located in upper central panel.
  • 1 : GARMIN GIA 63W Nav/Com/ILS/WAAS GPS.
  • 1 : GARMIN GEA71B Engine and airframe interface unit.
  • 1 : GARMIN GDU 1250W 12 WUXGA high resolution Primary Flight Displays (PFDs).
  • 1 : GARMIN Flight Stream FS 510 Bluetooth/Wi-Fi allowing Tablet to Avionics exchange secured information.
  • 1 : FADEC w/ Autothrotle
  • 1 : Aural warnings
  • 1 : Angle of Attack (AOA) sensor + Electronic Stability Protection (ESP) + Under Speed Protection (USP), computer and PFD visualization
  • 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 : MD302 Back up Attitude, Airspeed, Altitude and heading digital display, 2 screens instrument with MD32 remote magnetometer.
  • 1 : RVSM data package.
  • 1 : TAWS-B, class B TAWS worldwide database.
  • 1 : Yaw Damper.

    • ADDITIONAL EQUIPMENT

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

    • CONTROLS

  • Fuel selector control - Auto slelect.
  • 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
  • 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 electrically heated seats with adjustable backrests and folding armrests in replacement for fabric.
  • Side beam seat polished aluminum finish.
  • 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
  • 28 V port + 2 USB port on copilot side + 2 USB port in passenger cabin.
  • Tri-band ELT with GPS connection
  • Electrical power control center
  • Starter generator 28V-300 Amp
  • Lead acid battery 24V-42 A.h
  • Ground clearance energy saver
  • Ground power plug receptacle
  • Taxiing and landing 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.
    LED interior lighting
    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.
  • 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..
  • Environment and pressurization control system.
  • 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- Enviro Systems Inc.
  • Pulse light anti-collision system.
  • Hour meter airborne.
  • Map reading tablet.

    • PROPELLER

    WARRANTY & MAINTENANCE

  • New hartzell propeller Warranty extension to 6 years or 4,000 hours.
  • System Warranty extension to 5 years or 1,000 hours for selected components.
  • Avionics System Warranty extension to 5 years for Garmin equipment only.

    • 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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