P2008JC Specification and Description
TECNAM P2008 · Pilot's Operating Handbook
Overview
The document provides specifications and descriptions for the Tecnam P2008JC aircraft, which is equipped with the Rotax 912 S2 engine. It covers general information regarding design, powerplant, performance, and equipment, aimed at aiding evaluation for potential users.
- The P2008JC is designed for flight training and recreational flying.
- It features a carbon fiber fuselage and metal wings for improved efficiency.
- The aircraft includes full electronic flight display screens.
- It has a maximum takeoff weight of 650 kg.
- The practical ceiling is 14,000 feet.
- The aircraft is compliant with EASA CS-VLA certification.
- It offers a spacious cabin with adjustable seats and ample baggage space.
- The P2008JC is powered by a Rotax 912 S2 engine.
Document
Source
Originally published by tecnam.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- File size ·
- 940 KB
- Publisher ·
- tecnam.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Wing span (ft) ·
- 29.5
- Wing area sqft ·
- 131
- Overall height (ft) ·
- 8.76
- Overall length (ft) ·
- 22.87
- Baggage compartment max load (lb) ·
- 44
- Baggage compartment volume cuft ·
- 8
Performance
- Range (nm) ·
- 703
- Landing run (ft) ·
- 568
- Takeoff run (ft) ·
- 679
- Stall speed kcas ·
- 44
- Max cruise speed (kt) ·
- 120
- Practical ceiling (ft) ·
- 14000
Weight & balance
- Useful load kg ·
- 250
- Empty weight kg ·
- 400
- Baggage allowance kg ·
- 20
- Max takeoff weight kg ·
- 650
What is the P2008JC Specification and Description?
The P2008JC Specification and Description is a pilot's operating handbook for the TECNAM P2008.
Where does the P2008JC Specification and Description come from?
This copy of the P2008JC Specification and Description was originally published by tecnam.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the TECNAM P2008.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P2008manuals & documents
In this document
General Description
The Tecnam P2008JC is known for its versatility and comfort, making it suitable for both flight training and recreational use.
Construction
The aircraft combines metal wings and stabilator with a carbon fiber fuselage for enhanced aerodynamic efficiency and structural integrity.
Weight & Performance
The document outlines the aircraft's weight specifications, including maximum takeoff weight, empty weight, and useful load, along with performance metrics like cruise speed and range.
Powerplant & Accessories
The P2008JC is powered by a Rotax 912 S2 engine, featuring a dual ignition system and a gearbox reduction ratio of 2.43:1.
Standard Equipment
The aircraft comes equipped with a standard Garmin avionics package, including dual screens and various flight instruments.
Optional Extras
A variety of optional equipment and upgrades are available, including additional avionics and exterior options.
Full document text
P2008JC SPECIFICATION AND DESCRIPTION P2008JC 2 Introduction All information here applies to the Tecnam model P2008JC equipped with the Rotax 912 S2 engine. P2008JC SPECIFICATION AND DESCRIPTION This document applies only to the Tecnam P2008JC and is published for the purpose of providing general information for the evaluation of design, powerplant, performance and equipment. http://www.tecnam.com/aircraft/p2008-jc/ Should more information be required, please contact: Costruzioni Aeronautiche Tecnam srl Via Maiorise 81043 Capua CE - Italy Tel. +39 0823 622297 Fax. +39 0823 622899 www.tecnam.com info@tecnam.com Pascale Museum at Tecnam Headquarters, Capua Innovation is in the air P2008JC 3 Introduction All information here applies to the Tecnam model P2008JC equipped with the Rotax 912 S2 engine. GENERAL DESCRIPTION The single-engined Tecnam P2008’s versatility and ease of use has established it as both the aircraft of choice for Flight Training Organisations worldwide as well as recreational flyers alike. The Tecnam P2008JC is the best in its class, incorporates a level of comfort, quality and efficiency that have made it the ideal touring aircraft, assuring pilots and passengers alike of a very comfortable environment and the smoothest of flight experiences. With its carbon fibre fuselage, metal wings and stabilator, the Tecnam P2008JC has a vast number of advantages over traditional aircraft. The 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. The Tecnam P2008JC is equipped with full electronic flight display screens rather than the traditional knobs and dials seen on typical aircraft instrument panels. Innovation is in the air Construction The P2008JC has both metal wings and a metal stabilator. Tecnam chose to construct the P2008 with metal wings and stabilator structures for strength, reliability, and the ability to flex in flight, thereby ensuring a more comfortable ride. To produce the desired increase in cabin width and greater aerodynamic efficiency, Tecnam chose carbon fibre. The decision to use both materials was for the optimisation of aerodynamic qualities, flight characteristic, and reliability. This addition enables Tecnam to make construction decisions based on optimum 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. P2008JC Landing Gear The main springleaf landing gear, including wheels, tires and fairings, are the same as all of the other non-retractable Tecnam models. 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 minimise drag, ground steering is by differential braking. Certification The Tecnam P2008JC is delivered in full compliance with the requirements of EASA CS-VLA. P2008JC 4 Views CABIN 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 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 acccess 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 is designed to allow you and your passenger to experience the most outstanding style, comfort, and beauty of flight.. Enjoy the P2008JC the cabin P2008JC 5 Views EXTERIOR P2008JC 6 Weight & Performance PERFORMANCE All estimated performance data are based on airplane weights at MTOW; standard atmospheric conditions; level, hard surface, dry runways, no wind. P2008JC kg lb Maximum Take Off Weight 650 1,433 Empty Weight, Standard 400 882 Useful Load 250 551 Baggage allowance 20 44 P2008JC Fixed Propeller Max Cruise Speed KTAS 120 kts 222 km/h Stall Speed (Flaps Down Power Off) KCAS 44 kts 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 P2008JC RAF Flying Clubs Dimensions ft m Overall Height 8.76 2,67 Overall Length 22.87 6,97 Wing ft m Span (overall) 29.5 9 Area 131ft 2 12.2 sqm Dihedral 1° Aspect ratio 6.7 DIMENSIONS DESIGN WEIGHT AND LOADING P2008JC LOT Academy P2008JC 7 Powerplant POWERPLANT & ACCESSORIES • 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 ROTAX 912 S2 The P2008JC 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
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modifications. The P2008JC 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. P2008JC 8 Standard STANDARD EQUIPMENT FLIGHT INSTRUMENTS and INDICATORS G3X Dual Screen 2 X GDU370 LRU Kit Sensor Kit Installation Kit G3X Sensor kit Antenna GPS ENGINE INSTRUMENTS, GSU Configuration • Amps (Ammeter Shunt or Hall Effect) • Monitor CT • Aircraft bus voltages • Oil temperature • OAT • Oil pressure • Fuel pressure • RPM • Trim Indicator OTHER INSTRUMENTS / INDICATORS / WARNINGS Airspeed and Altimeter back up TSO CT Fuel Indicator RH and LH Bank Indicator Trim Indicator Chronometer Warning Light: - Low Oil pressure - Low Fuel pressure - Alt. Out - Fuel Pump ON FLIGHT CONTROLS Hydraulic Toe Brakes Parking Brake Electrical Flaps, preselect Dual Flight Controls Castering Nose Wheel Stabilator Trim (Electric actuated from stick) ENGINE CONTROLS _ Central Quadrant With Single Throttle Lever _ Throttle _ Choke Flight Trim Controls _ Stabilator with Indicator Fuel Control Selector Andair Panel Switches: _ Split Master/Alternator switch _ Avionic Starter Key ACS ELECTRICAL SYSTEM 12 VOLT 18A AMP. Battery FIAMM 64 12 VOLT Alternator 20 AMP. SWITCHES _Avionic Master _Fuel Press _Nav. Lights _Landing Light _Strobe Light 12 VOLT socket External Power Supply Receptical Auxiliary Alternator 40A Circuit Breaker Panel FUEL SYSTEM Two Integral Fuel Tanks With 120 Litres Total Capacity Engine Driven Fuel Pump Fuel Quick Drain Electrical Fuel Pump INTERIOR Pilot And Copilot Seats _ Adjustable Fore and Aft Seat Belts & Shoulder Harness, All Seats Wall To Wall Carpeting P2008JC 9 Standard Map and Storage Pockets Luggage Compartments Fire Extinguisher Radio Call Plate Soundproofing First Aid Kit EXTERIOR Epoxy Corrosion Proofing, All Structure Lh/Rh Front Door Pilot/Copilot, Lock And Key All Lateral Windows Tinted Main Wheels, 5,00 X 5 Nose Wheel, 5,00 X 5 Stall Warning EXTERIOR LIGHTS Nav. Lights LED with strobe AVEO full LED TSO Taxi Light LED CABIN COMFORT SYSTEM Windshield Defroster Ventilator Adjustable, 2 Place Heating System POWERPLANT AND PROPELLER ENGINE - 1 ROTAX 912S2 100 HP, 4 Cylinders liquid/air cooled, integrated reduction gear Dual Ignition System Throttle Control Tubular Steel Engine Mount Propeller - Hoffman, 2 Blade Fix Propeller Spinner Air Filter Oil Filter Oil And Water Coolers Carburetor Heat With Manual Control Thermostat Valve Water And Oil Auxiliary Alternator PRODUCT SUPPORT/DOCUMENTS Manufacturers Full Two Year Limited Warranty Pilots Operation Handbook Maintenance Manual Parts Catalog Aircraft Log Book Engine Log Book STANDARD GARMIN AVIONICS PACKAGE GMA 340 Audio Panel GNC 255A Com/Nav GTX 335 Transponder ADS-B OUT ELT 406 Mhz Antennas: - Transponder - VHF - ELT - Marker Beacon Speakers Microphone Stick Push-To-Talk Switch, Pilot/Copilot Mic & Phone Jacks, Pilot/Copilot AVIONIC OPTIONS AVIONIC OPTIONS AVIONICS OPTIONS P2008JC 11 Avionics Options Export certification requirements may require additional equipment and charges. Options also pictured. STANDARD GARMIN G3X AVIONICS PACKAGE • GMA 340 Audio Panel • GNC 255A Com/Nav • GTX 335 Transponder ADS-B OUT • ELT 406 Mhz • Antennas: - Transponder - VHF - ELT - Marker Beacon • Speakers • Microphone • Stick Push-To-Talk Switch, Pilot/Copilot • Mic & Phone Jacks, Pilot/Copilot STANDARD AVIONICS Empty Weight 415 kg P2008JC 12 Avionics Options Export certification requirements may require additional equipment and charges. Options also pictured. GARMIN G3X VFR NIGHT PACKAGE Includes the following equipment: • Heated Pitot • GILL 25A Battery • Instrument Light • Emergency Light • Map Light • Dimmer • Landing/Taxi Light LED • Nav. Light LED • Compass Lighted • Alternate Static Source • Day & Night Switch Analogue Indicators: • Attitude Electric • RPM • Oil Temp • Volt • Warning Light: • Pitot Heat • Oil High Press Empty Weight 421 kg AVIONICS OPTION 1 P2008JC 13 PAINT SCHEMES Paint Many colour options for your to choose: from base Standard livery to the Special Paint Two colours. More info on: colors.tecnam.com P2008JC 14 Optional Extras OPTIONS Code Description INSTRUMENTS 114/A Turn & Slip Indicator 2 1/4” RADIO & NAVIGATION EQUIPMENTS GARMIN-COM/NAV/GPS 120/A GTR225 COM 25 Mhz with Antenna and Installation 120/B GTR225A COM 8.33 Khz with Antenna and Installation 119 MD200 VOR Indicator Only for GNC255A 121 GTN 650 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Indicator 121/A GTN 650 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Ind.(Exchange for Std. GNC255A) 122 GTN 750 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Indicator 122/A GTN 750 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Ind.(Exchange for Std. GNC255A) GARMIN GPS 128 AERA 500 with Antenna, Panel Support and Installation 132 GARMIN 795 with Antenna, Panel Support and Installation BENDIX KING 137 KR 87 ADF with KI227 Indicator 139 DME KN63-14 with KDI 572 Indicator OTHERS 157 Head Sets, two 157/A BOSE A20 Head Sets, two P2008JC 15 Optional Extras Code Description AIRCRAFT EQUIPMENT 182 Fuselage Cover 185 Battery Gill G25 (Exchange for standard battery) 209 Control Lock 210 Towing Bar EXTERIOR 201 Special Paint Two Colours OPTIONS Costruzioni Aeronautiche Tecnam srl Via Maiorise 81043 Capua CE - Italy Tel. +39 0823 622297 Fax. +39 0823 622899 www.tecnam.com info@tecnam.com http://www.tecnam.com/aircraft/p2008-jc/ 17042714