N700CZ - 2004 DAHER TBM 700C2


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    Aircraft Summary


    General

    Year
    2004
    Manufacturer
    DAHER
    Model
    TBM 700C2
    Serial Number
    301
    Condition
    Used
    Registration #
    N700CZ
    Description
    Compliant seats and cabin luggage restraint including 4 points harnesses on front seats and 3 points safety belts on other seats All seats with folding armrests and headrests Heavy duty main wheels and tires Ice protection: Pneumatically deiced wing and tail unit, with ice light Heated engine air intake lip Pilot controlled engine inertial separator Electrically heated propeller blades Electrically heated pitot tubes Electrically deiced stall warning sensor Left-hand and right hand electrically heated windshields Fuel Equipment: One Structural Fuel Tank per Wing Engine driven fuel pump Stand-by Electrical Fuel Pump Fuel Tank Selector with Automatic Sequencer Unit Capacitance Gauging with Low-Level Warning Miscellaneous: Parking protection kid Cabin cover Options: RVSM equipped Right hand map reading tablet Custom Painting and Decoration Miscellaneous: Ni-Cad battery (replacement of lead battery) Thommen needle chronometer (replacement of digital chronometer) Pulse light anticollision system 4 Bose X headsets connected and hardwired to battery Engine time hourmeter (replacement of flight time hourmeter) CD player kabinet with 4 Bose X headsets One Owner and Pilot Since New, Replaced w/ CJ3, RVSM Equipped.

    Airframe

    Total Time
    770.0
    Airframe Notes
    Metal Structure and Skin Paneling Anti-Corrosion Protection Treatment Pitch control through elevators with trim Yaw control through rudder with trim Electrical Flaps with Integrated Track and Dissymmetry Detektor and sensor Bank Control through Ailerons and Spoilers with trim on left aileron Retractable Gear with Electro Hydraulic actuation Hydraulic Disc Brakes Pressurized 6 seats cabin and baggage compartment Large Access Door with Retractable Stairway Front storage Compartment (not Pressurized) with External access Door Rear baggage Compartment (not Pressurized) with External access Door Emergency Exit Rear Fuselage Servicing Door Tie-Down Attachments Jacking Points Airframe pneumatic de-icing equipment Easy Maintenance Access Doors

    Engine Program

    Engine Program Notes
    PT6 A64 Pratt and Whitney Canada turboprop engine developing 1583 Shp thermodynamic, rated at 700 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 Servicing doors in cowlings

    Avionics

    Avionics/Radios
    Left hand and center panels: GMA 340 stereo audio panel with music input and marker beacon 1 Bose X pilot headset, stereo with noise attenuator EHSI/EADI EFIS 40 2 tubes with symbol generator, KVG 350, KCS 305 with heading comparator alarm, turn and bank indication GNS 530 VHF (FM immune) COM (25 kHz and 8,33 kHz spacing) /VOR-ILS/GPS GNS 530 VHF (FM immune) COM (25 kHz and 8,33 kHz spacing) /VOR-ILS/GPS with GI 106 A VOR/ILS indicator KMD 850 Multi-Function Display KMH 880 Traffic Alert System (TAS) and Terrain Awareness Warning System (TAWS) displayed on MFD WX 500 Stormscope displayed on MFD KMD 850 KNI 582 RMI Indicator Connected to Heading No. 2 KN 63 DME with Output to the EHSI and KDI 574 KEA 346 Encoding Drum Altimeter Connected to Transponder Nr. 1 Tri-band ELT with aircraft identification KFC 325 3 Axis Digital Auto Pilot with Pre-Select Altitude and Yaw Damper Stand-by Vacuum Artificial Horizon Right hand panel: KRA 405 B Radar Altimeter connected to EHSI KR 87 SC+ADF KDI 574 DME Indicator RDR 2000 Radar. Connected to MFD KMD 850 GTX 330 Mode S Transponder (Nr. 1) UI 35 000 ft Encoding Altimeter connected to Transpoter Nr. 2 GTX 327 Mode C Transpoter (Nr. 2) Electrical Artificial Horizon Vertical Speed Indicator Airspeed Indicator KCS 55 A heading n and KI 525 A HSI indicator, Connected to NAV 2 2nd Bose X stereo headset, with noise attenuator

    Additional Equipment

    Additional Equipment
    Electrical Equipment: Lead Acid Battery 24V-40A/h Starter Generator 28V -200Amp (rated at 180 Amp) Standby generator 28 V-70 Amp (rated at 57 Amp) Electrical power center for regulation and switching Circuit Breakers Anti-Collision Strobe Lights Navigation Lights Taxiing and Landing Lights Ice Detector Light Ground Power Plug Ground Clearance Energy Saving system Left-hand and right-hand map light Left-hand and right-hand electrical heated windshields Instruments: Integral Instrument Panel with Spare Locations for Options Airspeed Indicator Vertical Speed Indicator Magnetic Compass Torque Indicator Propeller Tachometer Turbine Temperature Indicator (ITT) OAT Indicator Airframe De-Icing Control Panel Inertial separator control Parking brake control Flaps Position Indicator Trim Position Indicator (Elevator, Rudder and Ailerons) Voltmeter and Ammeter Electric Generator Control and Monitoring on Overhead Panel Advisory Panel with Master Caution, Master Warning and Aural Warnings Fuel management panel Cabin temperature gauge Cabin altitude and differential pressure indicator Climb rate of climb indicator Heated stall warning system Flight time hourmeter Instrument panel lighting

    Interior

    Interior Notes
    Pressurized Cabin (p =6.2 PSI) Carpeting floor and Alcantara Upholstery Sound-Proofing and Thermal Insulation Air Conditioning (R 134) Cabin ventilation Individual Vents and Lightings Sun Visors and Curtains Fully Adjustable Pilots Seats (Height, Depth and backrest) All Seats with Adjustable Backrests Ashtrays Front and rear 24 V outputs Storable working table Air Way Charts Cabinet Refreshment Cabinet Gaseous Oxygen System Baggage Compartment with Straps and Net Coat-Rack Halon cabin extinguisher


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