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P2008JC Mkii P2008JC MkII SPECIFICATION AND DESCRIPTION P2008JC MkII Introduction SPECIFICATION AND DESCRIPTION P2008JC MkII Innovation is in the air This document applies only to the Tecnam P2008JC MkII and is published for the purpose of providing general information for the evaluation of design, powerplant, performance and equipment. Should more information be required, please contact: Costruzioni Aeronautiche Tecnam SpA Via Maiorise 81043 Capua CE - Italy Tel. +39 0823 622297 Fax. +39 0823 622899 www.tecnam.com [email protected] http://www.tecnam.com/aircraft/p2008-jc/ All information here applies to the Tecnam model P2008JC MkII equipped with the Rotax 912 S2 engine. 2 P2008JC MkII Introduction GENERAL DESCRIPTION P2008JC MkII Innovation is in the air The single-engined Tecnam P2008’s versatility Synthetic vision (SVX™) is a standard feature wing span. The Frise type aileron along with the and ease of use has established it as both the on G3X Touch, which provides a rich, three- taper design provides a high rate of roll. The all aircraft of choice for Flight Training Organisations dimensional depiction of terrain, obstacles, water movable type (stabilator) horizontal tail, traditional worldwide as well as recreational flyers alike. features, the runway environment, and more. on Tecnam aircraft, allows excellent controllability The Tecnam P2008JC MkII is the best in its The P2008JC is available as VFR Day and VFR and excellent “hands off” longitudinal stability. class, incorporates a level of comfort, quality Night. This version has a new improved lighting and efficiency that have made it the ideal touring system featuring both ambient light and dimmer Landing Gear aircraft, assuring pilots and passengers alike of a switches and MD302 backup attitude instrument. very comfortable environment and the smoothest Customers can also choose the propeller available The main springleaf landing gear, including wheels, of flight experiences. as 2 or 3 blades, for those pilots flying on noise- tires and fairings, are the same as all of the other With its carbon fibre fuselage, metal wings and restricted airfields. non-retractable Tecnam models. This design has stabilator, the Tecnam P2008JC MkII has a vast withstood the test of time and extensive use in number of advantages over traditional aircraft. Construction flight training environments. The combination of both composite material and The newly designed nose gear is free castoring metal has resulted in a more fuel efficient and The P2008JC MkII has both metal wings and a and consists of a tubular steel leg, connected much quieter aircraft. Pilots appreciate the quality metal stabilator. Tecnam chose to construct the to the lower engine mount attachments and is and security built into this popular Tecnam design. P2008 with metal wings and stabilator structures braced by an oleo pneumatic shock absorber that The P2008 MkII features a number of significant for strength, reliability, and the ability to flex in provides excellent ground load absorption. All of enhancements including new design of the flight, thereby ensuring a more comfortable ride. the landing gear is faired to minimise drag, ground dashboard and glare shied for the introduction To produce the desired increase in cabin width steering is by differential braking. of the GARMIN’s innovative G3X Touch with two and greater aerodynamic efficiency, Tecnam large 10.6-inch displays that significantly improves chose carbon fibre. Certification the level of comfort for passengers and pilots The wing is based on the well-known NACA63A alike. ouch display provides pilots with an intuitive airfoil, and through partial tapering, it is brought The Tecnam P2008JC MkII is delivered in split-screen mode with the option to view PFD, close to the optimal lift distribution (elliptical). full compliance with the requirements of MFD, and engine information on a single display. The single-slot flaps extend along much of the EASA CS-VLA. All information here applies to the Tecnam model P2008JC MkII equipped with the Rotax 912 S2 engine. 3 P2008JC MkII Views CABIN The cabin offers newly designed seats and seat rails which are easily operated and adjustable fore and aft via a single handle with a reinforced area between the rails to make cabin access even easier. A roomy baggage compartment with internal access accommodates voluminous items. A wide cockpit panel provides plenty of room for glass panel avionics. A comfortable armrest and USB charger round out the luxurious interior. Everything about the Tecnam P2008JC i MkII s designed to allow you and your passenger to experience the most outstanding style, comfort, and beauty of flight.. Demanding owners can also choose Premium interior, with a dark styling of the cabin and ceiling, new design of the doors, coupled with premium leather seats. Enjoy the P2008JC MkII Cabin ft m Height 3 0,91 Width 3.9 1,2 Baggage Compartment Width 2.95ft 0,90m Length 1.64ft 0,50m Height 1.64ft 0,50m Volume 8cu.ft 225lt Max. permissible load 44lb 20kg the cabin 4 P2008JC MkII Views EXTERIOR MkII 5 P2008JC MkII Weight & PerformancePowerplant DIMENSIONS Wing ft m Dimensions ft m Span Overall Height 8.76 2,67 29.5 9 (overall) Overall Length 22.87 6,97 Area 131ft2 12.2 sqm Dihedral 1° Aspect ratio 6.7 P2008JC MkII DESIGN WEIGHT AND LOADING kg lb Maximum Take Off Weight 650 1,433 Empty Weight, Standard 400 882 Useful Load 250 551 RAF Flying Clubs Baggage allowance 20 44 LOT Academy P2008JC MkII PERFORMANCE Fixed Propeller Max Cruise Speed KTAS 120 kt 222 km/h Stall Speed (Flaps Down Power Off) KCAS 44 kt 81 km/h Practical ceiling 14000 ft 4267 m Take off run 679 ft 207 m Take off distance 1404 ft 428 m Landing Run 568 ft 173 m Landing Distance 1253 ft 382 m Rate of climb 755 ft/min 3,8 m/sec Range 703 NM 1302 km All estimated performance data are based on airplane weights at MTOW; standard atmospheric conditions; level, hard surface, dry runways, no wind. 6 P2008JC MkII Powerplant POWERPLANT & ACCESSORIES The P2008JC MkII is powered by the Rotax 912 S2 engine. This powerplant and associated cowlings are similar to all of the existing Tecnam line models with few modifications. The P2008JC MkII has higher fuel capacity than the existing line (55x2 lt - 14.5x2 US Gal) and tanks are installed in the wing box, behind the main spar. This is to preserve their integrity in case of a crash landing and to minimize fire potential. The instrument panel size is increased to match the additional cabin width. It is modular in design and can accommodate the most complete instrumentation. ROTAX 912 S2 • 4-cylinders • 4-stroke liquid-/air-cooled engine with opposed cylinders • Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet • Mechanical fuel pump • Dual electronic ignition • Propeller speed reduction unit • Air intake system • Gearbox Reduction Ratio 2,43:1 7 P2008JC MkII AVIONICAVIONICAVIONICS OPTIONSOPTIONS OPTIONS P2008JC MkII Standard STANDARD EQUIPMENT DUAL DISPLAY GDU 460 SYSTEM WITH EIS _Avionic Master POWERPLANT AND PROPELLER Two GDU 460 Display _Fuel Press ENGINE - 1 ROTAX 912S2 100 HP, 4 Cylinders Two GSU25 ADAHRS _Nav. Lights liquid/air cooled, integrated reduction gear GEA 24 Unit Only _Landing Light Dual Ignition System GMU 22, Unit only _Strobe Light Throttle Control GTP59 12 VOLT socket Tubular Steel Engine Mount G3X Installation Kit External Power Supply Receptical Propeller - Hoffman, 2 Blade Fix Two GSU 25 Inst & Conn. Kit Auxiliary Alternator 40A Propeller Spinner GEA 24 Conn. Kit Circuit Breaker Panel Air Filter GMU 22 Connector and install rack kit Oil Filter GAP 26 unheated FUEL SYSTEM Oil And Water Coolers Two Integral Fuel Tanks With 120 Litres Total Capacity Carburetor Heat With Manual Control FLIGHT CONTROLS Engine Driven Fuel Pump Thermostat Valve Water And Oil Hydraulic Toe Brakes Fuel Quick Drain Auxiliary Alternator Parking Brake Electrical Fuel Pump Electrical Flaps, preselect PRODUCT SUPPORT/DOCUMENTS Dual Flight Controls INTERIOR Manufacturers Full Two Year Limited Warranty Castering Nose Wheel Pilot And Copilot Seats Pilots Operation Handbook Stabilator Trim (Electric actuated from stick) _ Adjustable Fore and Aft Maintenance Manual Seat Belts & Shoulder Harness, All Seats Parts Catalog OTHER INSTRUMENTS / INDICATORS / WARNINGS Wall To Wall Carpeting Aircraft Log Book Fuel Indicator RH and LH Map and Storage Pockets Engine Log Book Warning Light: Luggage Compartments - Low Oil pressure Fire Extinguisher STANDARD GARMIN AVIONICS PACKAGE - Low Fuel pressure Radio Call Plate GMA 345 Audio Panel - Alt. Out Soundproofing GNC 255A Com/Nav - Fuel Pump ON First Aid Kit GTX 335 Transponder ADS-B OUT ELT 406 Mhz ENGINE CONTROLS EXTERIOR Antennas: _ Central Quadrant With Single Throttle Lever Epoxy Corrosion Proofing, All Structure - 35 GPS/WAAS _ Throttle Lh/Rh Front Door Pilot/Copilot, Lock And Key - GA56 _ Choke All Lateral Windows Tinted - Transponder Flight Trim Controls Main Wheels, 5,00 X 5 - COM1 _ Stabilator with Indicator Nose Wheel, 5,00 X 5 - VOR Fuel Control Selector ANDAIR Stall Warning - ELT Panel Switches: - Marker Beacon _ Split Starter EXTERIOR LIGHTS Speakers _ Avionic Nav. Lights LED with strobe AVEO full LED TSO Microphone Starter Key ACS Taxi Light LED Stick Push-To-Talk Switch, Pilot/Copilot Mic & Phone Jacks, Pilot/Copilot ELECTRICAL SYSTEM CABIN COMFORT SYSTEM 12 VOLT 18A AMP. Battery Windshield Defroster 12 VOLT Alternator 20 AMP. Ventilator Adjustable, 2 Place Switches: Heating System 9 P2008JC MkII Avionics Options STANDARD AVIONICS VFR DAY GARMIN G3X 10’’ Mkii VFR DAY PACkAGE Includes the following equipment: GMA 345 Audio Panel GNC 255A Com/Nav GTX 335 Transponder ELT 406 Mhz Antennas: - 35 GPS/WAAS - GA56 - Transponder - COM1 - VOR - ELT - Marker Beacon Speakers Microphone Stick Push-To-Talk Switch-Pilot/Copilot Mic& Phone Jacks-Pilot/Copilot Empty Weight 415 kg 10 Export certification requirements may require additional equipment and charges.
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