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TECNAM P2008JCSpecification & Description

INDRODUCTION

This 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

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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

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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. 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. 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. 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.

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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 - 14.5x2 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.

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ͻ CertificationThe Tecnam P2008JC is delivered in full compliance with the requirements of EASA CS-VLA

ͻ Engine & Propeller Allowed engine power: 100 hp Manufacturer: ROTAX Models: 912ULS2 Propeller diameter: 1.73

Number of blades: 2 Approved manufacturers: GT Propeller Approved prop. types: Fixed

ͻ� Dimensions Overall Height: Overall Length:

8.76ft 22.87ft

2.67mt 6.97mt

ͻ� Wing Span (overall):

29.5ft

9.00mt Area: Dihedral: Aspect Ratio

131ft2

1° 6.7

12.2mt2

ͻ Cabin Height (seat to cover):

3ft

0.91mt Width (trim to trim): 3.9ft 1.2mt

ͻ�Baggage Compartment Width:

2.95ft

0.90mt Length: Height: Volume: Max. permissible load:

1.64ft 1.64ft 8cu.ft44lb

0.50mt 0.5mt 225lt20kg

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ͻ��ĞƐŝŐŶ�ǁĞŝŐŚƚ�ĂŶĚ��ĐĂƉĂĐŝƚŝĞƐ 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

ͻ�Performance (600kg\1320lbs-912 ULS-^ĞŶƐĞŶŝĐŚ propeller) Service Ceiling: Takeoff Distance S.L. (Ground Roll): Takeoff Distance S.L. (To Clear 50ft. Obstacle): Max Climb Rate S.L:Max Speed S.L: Max Range: Cruise Speed (75% pwr at 6.500ft): Vne (never exceed this speed) Landing Distance (Ground Roll): Landing Distance (To Clear 50 ft Obstacle): Stall Speed, flap UP Stall Speed, flap DW

13.000ft 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

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P2008JC Standard equipment list The following list of equipment is included on the standard aircraft Avionics Package and does not reflect optional equipment.

&ůŝŐŚƚ�ŝŶƐƚƌƵŵĞŶƚƐ�ĂŶĚ�ŶĂǀŝŐĂƚŝŽŶ • G3X DUAL SCREEN includes:

o AIRSPEED INDICATOR o ALTITUDE INDICATOR o ATTITUDE INDICATOR o GROUND SPEED o HDG TURNRATE o SEL. ALTITUDE o TAS o HDG BUG o HSI o GPS

Analog instruments • AIRSPEED and ALTIMETER BACKUP TSO • CHT • FUEL INDICATOR RH and LH • BANK INDICATOR • TRIM INDICATOR • CHRONOMETER • OAT • WARNING LIGHT

o LOW OIL PRESSURE o LOW FUEL PRESSURE o ALT. OUT o FUEL PUMP ON

&ůŝŐŚƚ�ĐŽŶƚƌŽůƐ • HYDRAULIC TOE BRAKES • PARKING BRAKE • ELECTRICAL FLAPS, PRESELECT • DUAL FLIGHT CONTROLS • CASTORING NOSE WHEEL • STABILATOR TRIM (Electric actuated from Stick) • ENGINE CONTROLS:

o CENTRAL QUADRANT with SINGLE TROTTLE LEVEL o CHOKE

• FLIGHT TRIM CONTROLS: o STABILATOR TRIM with INDICATOR

• FUEL CONTROL SELECTOR ANDAIR WĂŶĞů��ƐǁŝƚĐŚĞƐ • SPLIT STARTER • AVIONICS MASTER • STARTER KEY ACS • FUEL PUMP

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Electrical system • 12V 18 AMP. FIAM64 BATTERY • 14V ALTERNATORS-20 AMP.• ROCKER SWITCHES INTERNALLY LIGHTED

o Avionic master o Landing light o Nav light o Strobe light o Fuel press

• CIRCUIT BREAKER PANEL • 12 VOLT SOCKET • EXTERNAL POWER SUPPLY • AUXILIARY ALTERNATOR 40A

Fuel system • TWO INTEGRAL FUEL TANKS WITH 120lt\32USgal 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

o Eco leatherette o Adjustable 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, 5.00 X 5 - NOSE 5,00 X 5 • STALL WARNING

Exteriors ůŝŐŚƚƐ • WING TIP STROBE AND POSITION LIGHT LED • LANDING/TAXI LIGHT LED

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Cabin comfort system • WINDSHIELD DEFROSTER • VENTILATOR ADJUSTABLE• HEATING SYSTEM

Standard 'ĂƌŵŝŶ��ǀŝŽŶŝĐƐ Package • GMA 340 AUDIO PANEL • GNC 255A COM/NAV• GTX 328 TDX • ELT 406 Mhz • ANTENNAS:

o TRASPONDER o VHF o ELT o MARKER BACON

• SPEAKERS • MICROPHONE • STICK PUSH-TO-TALK SWITCH pilot/copilot • MIC & PHONE JACKS pilot/copilot

Powerplant and Propeller • ENGINE - 1 ROTAX 912ULS2 100 HP, 4

CYLINDERS o Liquid/air cooled o Integrated 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 �ǀŝŽŶŝĐ�ƉĂĐŬĂŐĞ

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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:

o ATTITUDE ELECTRIC o RPM o OIL TEMP o VOLT

• WARNING LIGHT: o PITOT HEAT o HIGH OIL PRESS

Export certificate requirements may require additional equipment or a different equipment list

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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 8.33 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 indicator

122A 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. 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)

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TECNAM COLORS Standard color, for more information please visit www.tecnam.com

Special paint #1

White = RAL 9016 Red = Mazda A/27 Vivid Blue = Adhesive Vinyl Avery 528 Silver = Adhesive Vinyl Avery 546

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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 9016Brilliant Orange = RAL Vivid Blue = Adhesive Vinyl Avery 528 Silver = Adhesive Vinyl Avery 546