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SPECIFICATION & DESCRIPTION Pag. | TECNAM …

SPECIFICATION & DESCRIPTION Pag. | 1 TECNAMP2008 JCSpecification & DESCRIPTION INDRODUCTIONThis document is published for the purpose of providing general information for the evaluation of design, performance and equipment of the TECNAM model P2008JC. Should more information be required, please contact: This document describes only the TECNAM model P2008JC, its powerplant and equipment. INTRODUCTION Pag. | 2 SPECIFICATION & DESCRIPTION Table of Contents General DESCRIPTION .. 3 Construction .. 3 Landing Gear .. 3 Powerplant and propeller .. 4 Three views .. 7 P2008JC Standard equipment list .. 8 OPTION 1 P2008JC VFR NIGHT .. 11 OPTIONALS .. 12 TECNAM COLORS .. 13 SPECIFICATION & DESCRIPTION Pag. | 3 General DESCRIPTION All information here in applies to the TECNAM model P2008JC equipped with the engine Rotax 912 S2. The sleek and beautiful lines of the single-engine TECNAM P2008JC incorporate a level of comfort, quality and efficiency that have made it the ideal touring aircraft.

SPECIFICATION & DESCRIPTION Pag. | 3 www.tecnam.com General description All information here in applies to the Tecnam model P2008JC equipped with the engine

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Transcription of SPECIFICATION & DESCRIPTION Pag. | TECNAM …

1 SPECIFICATION & DESCRIPTION Pag. | 1 TECNAMP2008 JCSpecification & DESCRIPTION INDRODUCTIONThis document is published for the purpose of providing general information for the evaluation of design, performance and equipment of the TECNAM model P2008JC. Should more information be required, please contact: This document describes only the TECNAM model P2008JC, its powerplant and equipment. INTRODUCTION Pag. | 2 SPECIFICATION & DESCRIPTION Table of Contents General DESCRIPTION .. 3 Construction .. 3 Landing Gear .. 3 Powerplant and propeller .. 4 Three views .. 7 P2008JC Standard equipment list .. 8 OPTION 1 P2008JC VFR NIGHT .. 11 OPTIONALS .. 12 TECNAM COLORS .. 13 SPECIFICATION & DESCRIPTION Pag. | 3 General DESCRIPTION All information here in applies to the TECNAM model P2008JC equipped with the engine Rotax 912 S2. The sleek and beautiful lines of the single-engine TECNAM P2008JC incorporate a level of comfort, quality and efficiency that have made it the ideal touring aircraft.

2 With its carbon-fiber fuselage, metals wings and stabilator, the TECNAM P2008JC has a vast number of advantages over traditional aircraft. This combination of both composite material and metal has resulted in a more fuel efficient and much quieter aircraft. Pilots appreciate the quality and security built into this popular TECNAM design. In service with many Flight Schools around the globe the P2008JC is recognised as a state-of-the-art flight trainer and the most cost effective and environmentally friendly aircraft. The single-engine TECNAM P2008JC's versatility and ease of use has established it as both the aircraft of choice for Flight Training Organizations worldwide as well as recreational flyers. Construction The P2008JC has metal Wings and a metal stabilator. TECNAM chose metal wings and stabilator structures for strength, reliability, and ability to flex in flight providing a more comfortable ride.

3 To produce the desired increase in cabin width and greater aerodynamic efficiency, TECNAM chose carbon fiber. The decision to utilize both materials was for the optimization of aerodynamic qualities, flight characteristics, and reliability. This addition allows TECNAM to make decisions to be based on design and structural integrity rather than purely the cost of production. The wing is based on the well-known NACA63A airfoil, and through partial tapering, it is brought close to the optimal lift distribution (elliptical). The Single-slot flaps extend along much of the wing span. The Frise type aileron along with the taper design provides a high rate of roll. The all movable type (stabilator) horizontal tail, traditional on TECNAM aircraft, allows excellent controllability and excellent hands off longitudinal stability. Landing GearThe main springleaf landing gear, including wheels, tires and fairings, are the same as all of the other non-retractable TECNAM models.

4 This design has withstood the test of time and extensive use in flight training environments. The newly designed nose gear is free castoring and consists of a tubular steel leg, connected to the lower engine mount attachments and is braced by an oleo pneumatic shock absorber that provides excellent ground load absorption. All of the landing gear is faired to minimize drag, ground steering is by differential braking. Pag. | 4 SPECIFICATION & DESCRIPTION Powerplant and propeller The powerplant and associated cowlings are similar to all of the existing TECNAM line with few modifications. The P2008JC has higher fuel capacity than the existing line (55x2 lt - 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.

5 SPECIFICATION & DESCRIPTION Pag. | 5 CertificationThe Te c n a m P2008JC is delivered in full compliance with the requirements of EASA CS-VLA Engine & Propeller Allowed engine power: 100 hp Manufacturer: ROTAX Models: 912 ULS2 Propeller diameter: Number of blades: 2 Approved manufacturers: GT Propeller Approved prop. types: Fixed Dimensions Overall Height: Overall Length: Wing Span (overall): Area: Dihedral: Aspect Ratio 131ft2 1 Cabin Height (seat to cover): 3ft Width (trim to trim): Baggage Compartment Width: Length: Height: Volume: Max. permissible load: 225lt20kg Pag. | 6 SPECIFICATION & DESCRIPTION Standard empty weight Max Take-off Weight: Landing Weight: Maximum Useful Load: Fuel Capacity: 816lb 1388lb 1388lb 573lb 32US Gal 370kg 630kg 630kg 260kg 120lt Performance (600kg\1320lbs-912 ULS-^ propeller) Service Ceiling: Ta k e o f f Distance (Ground Roll): Ta k e o f f Distance (To Clear 50ft.)

6 Obstacle): Max Climb Rate :Max Speed : Max Range: Cruise Speed (75% pwr at ): Vne (never exceed this speed) Landing Distance (Ground Roll): Landing Distance (To Clear 50 ft Obstacle): Stall Speed, flap UP Stall Speed, flap DW 700ft 1180ft 900ft/min 120kt 633nm 118kt 145kt 500ft 915ft 48kt 40kt 3962mt 214mt 360mt 4,6mt/sec222km/h 219km/h268km/h 153mt 280mt 89km/h 74km/h SPECIFICATION & DESCRIPTION Pag. | 7 d Pag. | 8 SPECIFICATION & DESCRIPTION P2008JC Standard equipment list The following list of equipment is included on the standard aircraft Avionics Package and does not reflect optional equipment. & G3X DUAL SCREEN includes: oAIRSPEED INDICATOR oALTITUDE INDICATOR oATTITUDE INDICATOR oGROUND SPEED oHDG TURNRATE oSEL. ALTITUDE oTAS oHDG BUG oHSI oGPS Analog instruments AIRSPEED and ALTIMETER BACKUP TSO CHT FUEL INDICATOR RH and LH BANK INDICATOR TRIM INDICATOR CHRONOMETER OAT WARNING LIGHT oLOW OIL PRESSURE oLOW FUEL PRESSURE oALT.

7 OUT oFUEL PUMP ON & HYDRAULIC TOE BRAKES PARKING BRAKE ELECTRICAL FLAPS, PRESELECT DUAL FLIGHT CONTROLS CASTORING NOSE WHEEL STABILATOR TRIM (Electric actuated from Stick) ENGINE CONTROLS: oCENTRAL QUADRANT with SINGLE TROTTLE LEVEL oCHOKE FLIGHT TRIM CONTROLS: oSTABILATOR TRIM with INDICATOR FUEL CONTROL SELECTOR ANDAIR W SPLIT STARTER AVIONICS MASTER STARTER KEY ACS FUEL PUMP SPECIFICATION & DESCRIPTION Pag. | 9 Electrical system 12V 18 AMP. FIAM64 BATTERY 14V ALTERNATORS-20 AMP. ROCKER SWITCHES INTERNALLY LIGHTED oAvionic master oLanding light oNav light oStrobe light oFuel press CIRCUIT BREAKER PANEL 12 VOLT SOCKET EXTERNAL POWER SUPPLY AUXILIARY ALTERNATOR 40A Fuel system TWO INTEGRAL FUEL TANKS WITH 120lt\32 USgal total capacity ENGINE DRIVEN FUEL PUMP AUXILIARY FUEL PUMP, ELECTRIC FUEL TANK QUICK DRAIN , TWO 1 X SHUT OFF VALVE Interiors PILOT and CO-PILOT SEATS oEco leatherette oAdjustable fore and aft SEAT BELTS 3 POINTS ALL SEATS WALL TO WALL CARPETING MAP & STORAGE POCKETS RADIO CALL PLATE SOUNDPROOFING LUGGAGE COMPARTMENTS FIRE EXTINGUISHER FIRST AID KIT Exterior EPOXY CORROSION PROOFING, All structure DOORS, LOCK AND KEY ALL LATERAL WINDOWS TINTED TIE DOWN RINGS MAIN WHEELS, X 5 - NOSE 5,00 X 5 STALL WARNING Exteriors WING TIP STROBE AND POSITION LIGHT LED LANDING/TAXI LIGHT LED Pag.

8 | 10 SPECIFICATION & DESCRIPTION Cabin comfort system WINDSHIELD DEFROSTER VENTILATOR ADJUSTABLE HEATING SYSTEM Standard ' Package GMA 340 AUDIO PANEL GNC 255A COM/NAV GTX 328 TDX ELT 406 Mhz ANTENNAS: oTRASPONDER oVHF oELT oMARKER BACON SPEAKERS MICROPHONE STICK PUSH-TO-TALK SWITCH pilot/copilot MIC & PHONE JACKS pilot/copilot Powerplant and Propeller ENGINE - 1 ROTAX 912 ULS2 100 HP, 4 CYLINDERS oLiquid/air cooled oIntegrated reduction gear DUAL IGNITION SYSTEM THROTTLE CONTROL TUBULAR STEEL ENGINE MOUNT PROPELLER GT PROPELLER, 2 Blade fix PROPELLER SPINNER AIR FILTER OIL FILTER OIL AND WATER COOLERS CARBURETOR HEAT with manual control THERMOSTATIC WATER AND OIL VALVE AUXILIARY ALTERNATOR Product support/documents MANUFACTURER S FULL TWO YEAR LIMITED WARRANTY PILOT S OPERATION HANDBOOK MAINTENANCE MANUAL PARTS CATALOG AIRCRAFT LOG BOOK ENGINE LOG BOOK Standard Garmin G3X SPECIFICATION & DESCRIPTION Pag.

9 | 11 OPTION 1 P2008JC VFR NIGHT Non additive, replaces standard equipment and Avionics HEATED PITOT GILL 25A BATTERY INSTRUMENTS LIGHT EMERGENCY LIGHT MAP LIGHT DIMMER COMPASS LIGHTED ALTERNATE STATIC SOURCE DAY & NIGHT SWITCH ANALOGUE INDICATORS: oATTITUDE ELECTRIC oRPM oOIL TEMP oVOLT WARNING LIGHT: oPITOT HEAT oHIGH OIL PRESS Export certificate requirements may require additional equipment or a different equipment list ^ E s&Z ' ' y Pag. | 12 SPECIFICATION & DESCRIPTION OPTIONALS Code DESCRIPTION GARMIN 117/A GMA 35 Audio panel with antenna and installation ONLY for GTN750 Exchange for standard GMA340 119 MD200 VOR Indicator ONLY for GNC255A 120/A GARMIN GTR225 Com with antenna & Installation 120/B GARMIN GTR225A Com Mhz with antenna & Installation (From Nov. 2013 mandatory for EU) 121 GTN 650 Com/Nav/Gps with antennas, triplex and installation with GI106A indicator 121A GTN 650 Com/Nav/Gps with antennas, triplex and installation with GI106A indicator exch for std GNC255A 122 GTN 750 Com/Nav/Gps with antennas, triplex and installation with GI106A indicator122A GTN 750 Com/Nav/Gps with antennas, triplex and installation with GI106A indicator exch for std GNC255A 125A GTX 330 transponder mode S with antenna and installation exchange for std.

10 GTX328 126B GTX 33 transponder mode S remote mounted with ant. and install. exch for std. GTX328 (require opt. 122) BEKER 133/A RA3502 ADF with AN3500 indicator BENDIX KING 137 KR 87 ADF with KI227 Indicator 139 DME KN63-14 OTHERS 157 Two head sets 157/A BOSE A 20 Two head sets AIRCRAFT EQUIPMENTS 182 Fuselage cover 184/B Eco leatherette Interiors (see note #9) 184/E Spinner polished aluminum look 201 Special paint two colors #9 Eco Leatherette Interiors P2008 Two colours seats with TECNAM logochoice of colours combination:Choice # 1 Ivory and TobaccoChoice # 2 Gray and Navy BlueDoors PocketLateral Pocket (Rear luggage compartment) SPECIFICATION & DESCRIPTION Pag. | 13 TECNAM COLORS Standard color, for more information please visit Special paint #1 White = RAL 9016 Red = Mazda A/27 Vivid Blue = Adhesive Vinyl Avery 528 Silver = Adhesive Vinyl Avery 546 Pag. | 14 SPECIFICATION & DESCRIPTION Special paint #2 Special paint #3 Special paint #4 White = RAL 9016 Blue Marine = RAL 5002 Vivid Blue = Adhesive Vinyl Avery 528 Gold = Adhesive Vinyl Avery 547 White = RAL 9016 Brilliant Aluminum = RAL 9016 Black = Adhesive Vinyl Avery 502 Gold = Adhesive Vinyl Avery 547 White = RAL 9016 Brilliant Orange = RAL Vivid Blue = Adhesive Vinyl Avery 528 Silver = Adhesive Vinyl Avery 546


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