Tecnam.com - P2008JC CS/VLA

"Ultimately operators have been demanding a next generation aeroplane that can deliver not only profits but reliability, efficiency and off course passenger comfort. The Tecnam design team have answered all these needs in developing the P2012 Traveller, one of the first new FAR23/CS23 aeroplanes in 25 years! The P2012 Traveller builds on our commitment to continue to develop outstanding, stylish, innovative and affordable aeroplanes. For the Tecnam team, designing and building aeroplanes isn’t just a job, it’s an extension of our passion for flying."

(Paolo Pascale, Tecnam Managing Director)

P2006T

Twin engine - High Wing - Retractable Gear
Analog or Glass cockpit (opt.)
Fully metal - 17 Lt/Hr per engine - Four seats
Superior performance and flight characteristics
Stable and responsive
High level of comfort that makes it ideal for long routes
Great visibility - Width cabin size
The best choice for Flight School
EASA CS-23 and FAA FAR-23 EASA CS-VLA (the certification is expected to be finished at the end of 2012 or beginning of 2013)

P2010 Ptwenty - Ten CS/23

Single engine - High Wing - Fixed Gear - Analog cockpit - Fully Metal - 17 Lt/Hr
Automobile Fuel(Mogas) and AVGAS
Superior performance and flight characteristics
Low stall speed
Stable and Responsive
Ideal for flight schools
High level of comfort that makes it deal for long routes
Excellent visibility
Comfortable 45 in/114 cm wide cabin
JAR-VLA certified

P92 Echo Classic De Luxe US/LSA

P92 Echo Light US/LSA

P92 Eaglet US/LSA

P92 Tail Dragger US/LSA

Single engine - High Wing - Fixed Gear - Analog cockpit and Glass
Fully Metal - 17 Lt/Hr
Automobile Fuel(Mogas) and AVGAS
Superior performance and flight characteristics
Low stall speed
Stable and responsive
The best for flight schools
High level of comfort that makes it ideal for long routes
Excellent visibility
This year is the 20th Anniversary of the first P92 built

P92 Echo Classic De Luxe

Single engine - High Wing - Fixed Gear - Analog cockpit and Glass
Fully Metal - 17 Lt/Hr
Automobile Fuel(Mogas) and AVGAS
Superior performance and flight characteristics
Low stall speed
Stable and responsive
The best for flight schools
High level of comfort that makes it ideal for long routes
Excellent visibility
This year is the 20th Anniversary of the first P92 built

TECNAM MMA

TECNAM MRI

The TECNAM MMA - an efficient multi-fuel twin engine aircraft is developed, certified and marketed by Airborne Technologies and gives a complete new perspective for Airborne Special Services (Law Enforcement, Peacekeeping & Environmental Monitoring)

CERTIFIED SINGLE ENGINE

P2008JC CS/VLA

BROCHURE

Technical Info

Photo Gallery Details

Photo Gallery Flights


	Carbon fiber meets metal with innovation, style, and advanced technology to create a new aircraft line by Tecnam. The latest addition to the Tecnam line is the P2008 CS-VLA. The Tecnam lineage is apparent the P2008JC CS-VLA which includes several exciting additions. The P2008JC CS-LSA has metal wings and a metal stabilator. Tecnam chose to keep the metal wing 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. The powerplant and associated cowlings are similar to all of the existing Tecnam line with few modifications. The P2008 CS-VLA has higher capacity than the existing line (55x2 lt - 14,5x2 GAL) and fuel 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 from other Tecnam models due to the increase in cabin width. It is modular in design and can accommodate the most complete instrumentation, analogical or digital type.

Construction

The P2008 CS-LSA has metal wings and a metal stabilator.
Tecnam chose to keep the metal wing 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.
Tecnam was able to utilize the expertise from its aquisition of Tecnam Spain.
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 singleslot 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 all 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 castering and consists of a tubular steel leg, connected to the lower engine mount attachments and is braced by a rubber shock absorber.
The steerable nose wheel is also available.
All of the landing gear is faired to minimize drag. Ground steering is by differential braking.

Engine And Propeller

The powerplant and associated cowlings are similar to all of the existing Tecnam line with few modifications.
The P2008 CS-LSA has higher capacity than the existing line (55x2 lt - 14,5x2 GAL) and fuel 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 from other Tecnam models due to the increase in cabin width.
It is modular in design and can accommodate the most complete instrumentation, analogical or digital type.

Standard Equipment

FLIGHT INSTRUMENTS and INDICATORS G3X DUAL SCREEN GDU370 GDU375 LRU Kit SENSOR Kit INSTALLATION Kit G3X Sensor kit Antenna GPS	ENGINE INSTRUMENTS, GSU Configuration Amps (Ammeter Shunt or Hall Effect) Monitor CHT Aircraft bus voltages OIL TEMP. OAT OIL PRESS FUEL PRESS. RPM FUEL QTY TRIM INDICATOR	OTHER INSTRUMENTS / WARNING CHRONOMETER GENERATOR WARNING LIGHT WARNING LIGHT: - LOW OIL PRESSURE - LOW FUEL PRESSURE

FLIGHT CONTROLS HYDRAULIC TOE BRAKES PARKING BRAKE ELECTRICAL FLAPS DUAL FLIGHT CONTROLS CASTERING NOSE WHEEL STABILATOR TRIM (Electric actuated from Stick) ENGINE CONTROLS - CENTRAL QUADRANT with SINGLE TROTTLE LEVEL - THROTTLE - CHOKE FLIGHT TRIM CONTROLS - STABILATOR with INDICATOR FUEL CONTROL SELECTOR WITH ANDAIR PANEL SWITCHES: - SPLIT STARTER - AVIONIC STARTER KEY ACS	ELECTRICAL SYSTEM 12 VOLT 18A AMP. BATTERY FIAMM 64 12 VOLT ALTERNATORS-20 AMP. SWITCHES Nav. Lights - Landing Light - Strobe Light 12 VOLT socket EXTERNAL POWER SUPPLY RECEPTABLE AUXILIARY ALTERNATOR 40A CIRCUIT BREAKER PANEL	FUEL SYSTEM TWO INTEGRAL FUEL TANKS WITH 110 LITRES, TOTAL CAPACITY ENGINE DRIVEN FUEL PUMP ELECTRICAL FUEL PUMPS FUEL QUICK DRAIN

INTERIOR PILOT and COPILOT SEATS - Adjustable Fore and Aft SEAT BELTS & Shoulder Harness, All Seats WALL TO WALL CARPETING MAP E 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 WINDOWS TINTED MAIN WHEELS, 5,00 X 5 Marc Ingegno NOSE WHEEL, 5,00 X 5 STALL WARNING	EXTERIOR LIGHTS NAV. LIGHTS WITH STROBE TAXI LIGHT TAIL LIGHT

CABIN CONFORT SYSTEM WINDSHIELD DEFROSTER VENTILATOR ADJUSTABLE, 2 place HEATING SYSTEM	POWERPLANT AND PROPELLER ENGINES - 1 ROTAX 912S2 100 HP, 4 Cylinders liquid/air cooled, 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 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 23 TDX remote mounted ELT 406 Mhz Antennas: - Transponder - VHF - ELT Speakers Microphone Stick Push-To-Talk Switch-Pilot/Copilot Mic& Phone Jacks-Pilot/Copilot