8720 - 2009 TECNAM P2006T


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    Aircraft Summary


    General

    Year
    2009
    Manufacturer
    TECNAM
    Model
    P2006T
    Serial Number
    011
    Registration #
    8720
    Condition
    Used
    FlightRules
    IFR
    Description
    Newly Certified, burning only 9-10 gallons per hour, the Tecnam P2006T is the perfect twin for flight schools and cross country travelers. It is a twin that makes sense! Place Your Deposit Today! This is a general listing for the new Tecnam P2006T twin engine aircraft. Quoted price includes ALL standard configuration equipment. Available in Analogue or Glass Cockpit (Garmin G950) Configuration for additional cost. ABOUT THE AIRPLANE: Dimension: Wing...37.4 ft Cabin width...49.2 inches Length, overall...28.5 feet Height, overall...9.3 feet Engines...Rotax 912S3, 4 cylinders, 98 HP per side...92 continuous. Tanks...2 tanks x 25.6 US gallons Propellers...MT propeller, constant speed, full-feathering...2 blades Design and weight loading Standard equipped weight....1723 ilbs. MTOW...2599 ilbs. Useful load....880 ilbs. Performance.... Max Speed sea level...148 knots Cruise speed (75% 7000 feet) 140 knots Cruise speed (65% 9000 feet) 135 knots Rate of climb...1,140 ft/min Rate of climb...single engine is 230 ft/min Stalling speed...with flaps is 49 knots Service ceiling...15,000 feet Service ceiling...single engine 7,500 feet Max. range at 65% power, 30 min reserve is 620 nm. Take off distance...1213 feet Take off run....898 feet Landing distance....1279 feet Landing run...656 feet VLO....91 knots VA...116 knots VNE 168 knots Fuel burn is 4.5 gallons on each side...

    Airframe

    Total Time
    1113.0

    Engine 1

    Engine 1 Time Since
    SNEW
    Engine 1 Notes
    - Manufacturer Bombardier-Rotax GmbH Model 912 S3 - Certification basis FAR 33 - Amendment 15 - Type Certificate EASA TCDS no. E.121 dated 1 April 2008 - Engine type 4 cylinders horizontally opposed with 1352 c.c. of overall displacement, liquid cooled cylinder heads, ram-air cooled cylinders, two carburetors, integrated reduction gear box with torsional shock absorber and overload clutch. - Maximum power (at declared rpm) 73.5 kW (98.6hp) @ 5800 rpm –5 minutes maximum. 69.0 kW (92.5hp) @ 5500 rpm (continuous)

    Props

    Prop Notes
    PROPELLERS: MANUFACTURER MT PROPELLER TYPE CONSTANT SPEED, FULL FEATHERING NUMBER OF BLADES 2 MODEL MTV-21-A-C-F/CF178-05

    Avionics

    Avionics/Radios
    IFR Equipped: Garmin GNS 530 GPS/WAAS COM/NAV Garmin GNS 430 GPS/WAAS COM/NAV Two Garmin GI106A VOR-Glide Slope Indicators Garmin GTX 328 Mode "S" Transponder King KN 63 DME S-Tec 55X Autopilot with electric pitch trim (NO Altitude Hold Function) Artex ME 406 ELT with panel mounted remote switch Pilot and copilot push to talk switch Digital Clock Full Co-Pilot instrument panel with folliwing instruments: Attitude Indicator Airspeed Indicator Altimeter

    Additional Equipment

    Additional Equipment
    TANKS: FUEL TANKS STANDARD (USABLE) 2 x 25.6 US GAL

    Exterior

    Year Painted
    2009
    Exterior Notes
    Like new White with white stripes

    Interior

    Year Interior
    2009
    Number of Seats
    4
    Interior Notes
    Like new Light beige leather

    Inspection Status

    Inspection Status
    - (ATA 05) Inspection A+B+C+D Performed - (ATA 05) MLG dampers replaced pn 26-8-1110-000 - (ATA 05) Rudder Trim Actuator pn-7T replaced - (ATA 05) Flush hydraulic fluid replaced - (ATA 05) Weight fire extinguisher performed - LG up down switch replaced. Pn MS24660-23D - Fuel assy televel (aforador) RH pn 26-1-5100-000 replaced - Hot air in cabin cable assy pn 29-9-0015-00 replaced - Replaced LH and RH Orings brake caliper MS 28775-224 - Replaced LH and RH linings brake pn 066-11200 and rivets RA 105-00200 - Replaced Taxi Landing GE 4509 and Lamp assy A555A-V-14V - Spark plugs LH and RH replaced pn DCPR8E - Oil filter LH and RH replaced pn 825706 - Sb080-CS performed - AD 2012-0043 performed iaw SB080CS - Sb102-CS performed - AD 2012-0146 performed iaw SB102CS


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