P2008JC MkII
TECNAM P2008 · Checklist
Overview
The document provides specifications and descriptions for the Tecnam P2008JC MkII aircraft, which is equipped with the Rotax 912 S2 engine. It covers the aircraft's design, performance, and equipment, aimed at aiding in the evaluation of its capabilities for flight training and recreational use.
- The P2008JC MkII is designed for both flight training and recreational flying.
- It features a carbon fiber fuselage and metal wings for improved efficiency and comfort.
- The aircraft includes advanced avionics with a GARMIn G3X Touch display.
- It has a maximum takeoff weight of 650 kg and an empty weight of 400 kg.
- The aircraft offers a maximum cruise speed of 120 KTAS and a range of 703 nautical miles.
- The cabin is designed for comfort with adjustable seats and ample baggage space.
- The P2008JC MkII complies with EASA CS-VLA certification requirements.
- It is available with various avionics and interior options.
Document
Source
Originally published by tecnamair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- File size ·
- 525 KB
- Publisher ·
- tecnamair.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 nmi ·
- 703
- Landing run (ft) ·
- 568
- Takeoff run (ft) ·
- 679
- Stall speed kcas ·
- 44
- Max cruise speed (kt) ·
- 120
- Practical ceiling (ft) ·
- 14000
V-speeds
- VS_KIAS ·
- 44
Weight & balance
- Useful load kg ·
- 250
- Empty weight kg ·
- 400
- Baggage allowance kg ·
- 20
- Max takeoff weight kg ·
- 650
What is the P2008JC MkII?
The P2008JC MkII is a checklist for the TECNAM P2008.
Where does the P2008JC MkII come from?
This copy of the P2008JC MkII was originally published by tecnamair.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 MkII is recognized for its versatility and comfort, making it a preferred choice for flight training and recreational flying.
Construction
The aircraft features a combination of carbon fiber and metal for enhanced strength, reliability, and aerodynamic efficiency.
Powerplant
Powered by the ROTAX 912 S2 engine, the P2008JC MkII has a higher fuel capacity and is designed for safety in crash scenarios.
Performance
Performance data includes a maximum cruise speed of 120 KTAS, a practical ceiling of 14,000 feet, and a takeoff distance of 1,404 feet.
Dimensions
The aircraft has an overall length of 22.87 ft and a wingspan of 29.5 ft, with a cabin height of 3 ft.
Standard Equipment
The P2008JC MkII comes equipped with dual displays, hydraulic toe brakes, and a range of safety and comfort features.
Safety notes
- Ensure compliance with EASA CS-VLA certification requirements.
- Use caution when operating in noise-restricted airfields.
- Verify fuel levels and system functionality before flight.
- Maintain awareness of weight limits and loading specifications.
Full document text
P2008JC MkII SPECIFICATION AND DESCRIPTION P2008JC MkII 2 Introduction All information here applies to the Tecnam model P2008JC MkII equipped with the Rotax 912 S2 engine. P2008JC MkII SPECIFICATION AND DESCRIPTION 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. http://www.tecnam.com/aircraft/p2008-jc/ 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 info@tecnam.com Innovation is in the air P2008JC MkII 3 Introduction All information here applies to the Tecnam model P2008JC MkII 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 MkII 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 MkII 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 P2008 MkII features a number of significant enhancements including new design of the dashboard and glare shied for the introduction of the GARMIn’s innovative G3X Touch with two large 10.6-inch displays that significantly improves the level of comfort for passengers and pilots alike. ouch display provides pilots with an intuitive split-screen mode with the option to view PFD, MFD, and engine information on a single display. Innovation is in the air Synthetic vision (SVX™) is a standard feature on G3X Touch, which provides a rich, three- dimensional depiction of terrain, obstacles, water features, the runway environment, and more. The P2008JC is available as VFR Day and VFR night. This version has a new improved lighting system featuring both ambient light and dimmer switches and MD302 backup attitude instrument. Customers can also choose the propeller available as 2 or 3 blades, for those pilots flying on noise- restricted airfields. Construction The P2008JC MkII 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 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 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 MkII is delivered in full compliance with the requirements of EASA CS-VLA. P2008JC MkII P2008JC MkII 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 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 the cabin P2008JC MkII 5 Views EXTERIOR MkII P2008JC MkII 6 Powerplant 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 MkII kg lb Maximum Take Off Weight 650 1,433 Empty Weight, Standard 400 882 Useful Load 250 551 Baggage allowance 20 44 P2008JC MkII 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 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
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DIMENSIONS DESIGN WEIGHT AND LOADING LOT Academy P2008JC MkII 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 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. AVIONIC OPTIONS AVIONIC OPTIONS AVIONICS OPTIONS P2008JC MkII P2008JC MkII 9 Standard STANDARD EQUIPMENT DuAL DISPLAy GDu 460 SySTeM WITh eIS Two GDU 460 Display Two GSU25 ADAHRS GEA 24 Unit Only GMU 22, Unit only GTP59 G3X Installation Kit Two GSU 25 Inst & Conn. Kit GEA 24 Conn. Kit GMU 22 Connector and install rack kit GAP 26 unheated FLIGhT CONTROLS Hydraulic Toe Brakes Parking Brake Electrical Flaps, preselect Dual Flight Controls Castering nose Wheel Stabilator Trim (Electric actuated from stick) OTheR INSTRuMeNTS / INDICATORS / WARNINGS Fuel Indicator RH and LH Warning Light: - Low Oil pressure - Low Fuel pressure - Alt. Out - Fuel Pump On eNGINe CONTROLS _ Central Quadrant With Single Throttle Lever _ Throttle _ Choke Flight Trim Controls _ Stabilator with Indicator Fuel Control Selector AnDAIR Panel Switches: _ Split Starter _ Avionic Starter Key ACS eLeCTRICAL SySTeM 12 VOLT 18A AMP. Battery 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 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 345 Audio Panel GnC 255A Com/nav GTX 335 Transponder ADS-B OUT 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 P2008JC MkII 10 Avionics Options Export certification requirements may require additional equipment and charges. Options also pictured. STANDARD AVIONICS VFR DAy Empty Weight 415 kg 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 P2008JC MkII 11 Avionics Options Export certification requirements may require additional equipment and charges. Options also pictured. GARMIN G3X 10’’ MkII VFR NIGHT PACkAGE Includes the following equipment: Trim Indicator Chronometer Heated Pitot GILL 25A Battery Instrument Light Emergency Light Map Light Dimmers Landing/Taxi Light LED nav. Light LED Compass Lighted Alternate Static Source Day & night Switch MD302 - Standby Attitude Module Digital Analogue Indicators: - RPM - Oil Temp - Head Temp - Volt Warning Light: - Pitot Heat - High Oil Press Empty Weight 421 kg VFR NIGHT P2008JC MkII 12 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 MkII 13 NEW PAINT Paint P2008JC MkII 14 Optional Extras P2008JC OPTION LIST AUDIO, RADIO & NAVIGATION EQUIPMENT cod kg GARMIN-COM/NAV/GPS 201 1,04 GARMIn GTR225A 10W COM 8.33 KHz WITH AnTEnnA AnD InST. 202 1,38 GARMIN GTR225B 16W COM 8.33 Khz with Antenna and Inst. 203 1,57 MD200 VOR Indicator Only for GnC255A 204 3 GTn 650 Com/nav/Gps with Antennas, Triplex and inst. With GI106A Ind. 205 3 GTN 650 Com/Nav/Gps with Antennas, Triplex. & inst. With GI106A Ind.(Exch. for Std. GNC255A) GARMIN-TRASPONDER 206 1,45 GTX 345 TRANSPONDER MODE S ADS-B IN/OUT PANEl MOUNTED WITh GPS, ANTENNA TDX AND INST. (EXCh FOR STD GTX335) BENDIX KING 207 1,27 KR 87 ADF with KI227 Indicator 208 1,27 DME Kn63 14 with KDI 572 Indicator OTHERS 209 0,29 Power Flarm TRX1500- AT-1 212 Coolant Operating Cabin heating System (Exch. Std. heating System) INTERIOR/EXTERIOR 213 CS-VLA Special Paint 214 P2008 Premium Edition 215 P2008 ABS interiors painted matt grey 2 tones -included in Premium Edition 216 Metallic Paint Upgrade - Requires Special Paint ENGINE and PROPELLER EQUIPMENT 215 MT ground adjustable 3 bladed propeller (exchange for Std FIX Prop.) for Noise Reduction OTHERS & ACCESSORIES 219 Clear-Com Headset, two 220 BOSE A20 Headset, two 221 Fuselage Cover 222 Controls Locker 223 Towing Bar J C - pack P2008JC Disassembling and Packing P2008JC MkII 15 NOTES SEVENAIR Portuguese Academy fleet Costruzioni Aeronautiche Tecnam SpA 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/ 20020414 Pascale Museum at Tecnam Headquarters, Capua 1 9 4 8 - 2 0 1 8 70 Y E A R S