Tecnam.com - P2008 US/LSA

"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)

LSA

P2008 US/LSA

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. The Tecnam lineage is apparent the P2008 which includes several exciting additions. The P2008 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 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 E-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 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 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 E-LSA has higher capacity than the existing line (2x55 lt) 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
MAGNETIC COMPASS
AIRSPEED IND., Kts
ALTIMETER DUAL MODE (IN/Mb)
VERTICAL SPEED
BANK INDICATOR
PITOT SYSTEM
STATIC SYSTEM
STABILATOR TRIM POSITION INDICATOR

ENGINE INSTRUMENTS
TACHOMETER
HOUR RECORDER
OIL PRESS
OIL TEMP.
HEAD TEMP.
FUEL PRESS.
VOLTMETER
LH + RH FUEL QTY
TRIM INDICATOR
FLAP INDICATOR

FLIGHT CONTROLS
HYDRAULIC TOE BRAKES
PARKING BRAKE
ELECTRICAL FLAPS
DUAL FLIGHT CONTROLS
STEERABLE NOSE WHEEL
STABILATOR TRIM (Electric actuated from Stick)
ENGINE CONTROLS
- CENTRAL QUADRANT with SINGLE TROTTLE LEVEL
- THROTTLE, TWO
- CHOKE
FLIGHT TRIM CONTROLS
- STABILATOR with INDICATOR
FUEL CONTROL SELECTOR ANDAIR
PANEL SWITCHES:
- AVIONIC

ELECTRICAL SYSTEM
12 VOLT 18A AMP. BATTERY
12 VOLT ALTERNATORS-20 AMP.
SWITCHES
- Landing Light
- Strobe Light
- Nav Light
12 VOLT socket
CIRCUIT BREAKERS PANEL

FUEL SYSTEM
TWO INTEGRAL FUEL TANKS WITH 110 LITRES TOTAL CAPACITY
ENGINE DRIVEN FUEL PUMP
FUEL QUICK DRAIN

INTERIOR
PILOT and CO-PILOT SEATS
- Adjustable Fore and Aft
SEAT BELTS & Shoulder Harness, All Seats
WALL TO WALL CARPETING
MAP & STORAGE POCKETS
LUGGAGE COMPARTMENTS

EXTERIOR
EPOXY CORROSION PROOFING, All structure
LH/RH FRONT DOOR Pilot/Co-pilot, Lock and Key
REAR WINDOW
ALL WINDOWS TINTED
TIE DOWN RINGS
MAIN WHEELS, 5.00 X 5
NOSE WHEEL, 5.00 X 5

EXTERIOR LIGHTS
WING LIGHT GREEN/RED, WHITE AND STROBE AVEO NON TSO
TAIL LIGHT

CABIN CONFORT SYSTEM
WINDSHIELD DEFROSTER
VENTILATOR ADJUSTABLE, 2 place
HEATING SYSTEM

POWERPLANT AND PROPELLER
ENGINES - 1 ROTAX 912ULS2 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

PRODUCT SUPPORT/DOCUMENTS
MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
PILOT'S OPERATION HANDBOOK
MAINTENANCE MANUAL

LSA INCLUDING:
FIRE WALL INOX
AIRSPEED IND., Kts

FLIGHT INSTRUMENTS and INDICATORS MAGNETIC COMPASS AIRSPEED IND., Kts ALTIMETER DUAL MODE (IN/Mb) VERTICAL SPEED BANK INDICATOR FLAP INDICATOR PITOT SYSTEM STATIC SYSTEM STABILATOR TRIM POSITION INDICATOR	ENGINE INSTRUMENTS TACHOMETER HOUR RECORDER OIL PRESS OIL TEMP. HEAD TEMP. FUEL PRESS. VOLTMETER AMMETER LH + RH FUEL QTY O.A.T.	FLIGHT CONTROLS HYDRAULIC TOE BRAKES PARKING BRAKE ELECTRICAL FLAPS DUAL FLIGHT CONTROLS STEERABLE NOSE WHEEL STABILATOR TRIM (Electric actuated from Stick) ENGINE CONTROLS - CENTRAL QUADRANT with SINGLE TROTTLE LEVEL - 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 ALTERNATORS-20 AMP. SWITCHES - Landing Light - Strobe Light - Nav Light 12 VOLT socket CIRCUIT BREAKERS PANEL	FUEL SYSTEM TWO INTEGRAL FUEL TANKS WITH 110 LITRES TOTAL CAPACITY ENGINE DRIVEN FUEL PUMP FUEL QUICK DRAIN	INTERIOR PILOT and CO-PILOT SEATS - Adjustable Fore and Aft - Arm Rest SEAT BELTS & Shoulder Harness, All Seats WALL TO WALL CARPETING MAP & STORAGE POCKETS LUGGAGE COMPARTMENTS

EXTERIOR EPOXY CORROSION PROOFING, All structure LH/RH FRONT DOOR Pilot/Co-pilot, Lock and Key REAR WINDOW ALL WINDOWS TINTED TIE DOWN RINGS MAIN WHEELS, 5.00 X 5 NOSE WHEEL, 4.00 X 6	EXTERIOR LIGHTS VERTICAL TAIL STROBE TAXI LIGHT NAV. WING LIGHTS with STROBE TAIL LIGHT	CABIN CONFORT SYSTEM WINDSHIELD DEFROSTER VENTILATOR ADJUSTABLE, 2 place HEATING SYSTEM with DEFROST

POWERPLANT AND PROPELLER ENGINES - 1 ROTAX 912ULS2 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 FIRE SLEEVE ON FUEL and OIL TUBES AIR FILTER OIL FILTER OIL AND WATER COOLERS THERMOSTATIC VALVE OIL	PRODUCT SUPPORT/DOCUMENTS MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY PILOT'S OPERATION HANDBOOK MAINTENANCE MANUAL