Tecnam.com - P2006T

"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)

TWIN

P2006T

GENERAL VIEW

BROCHURE

Technical Info

Photo Gallery Details

Photo Gallery Flights


	The Tecnam P2006T Next-Generation twin is in a class of its own, bringing affordable multi-engine flying to aero-clubs, flying schools, syndicates and private aircraft owners. In addition, the P2006T has sparked significant interest on a larger scale for charter/air-taxi usage as well as a platform for surveillance and observation for government usage. The P2006T offers unbeatable value, coupled with low operating and ownership costs, innovative design and Italian styling. The Rotax '912S' engine (plus the option of a Garmin glass cockpit) allows the Tecnam P2006T to lead with respect to the environment too. With both a remarkable fuel saving offering and much lower noise emissions, it is redefining both the flight training and aircraft ownership experience in one step. Tecnam will delivery the P2006T s/n during AERO 2012, Friedrichshafen.

Construction

Tecnam P2006T is a twin-engine four-seat aircraft with fully retracting landing gear. The superior high-wing configuration offers stability, superior cabin visibility and easy access for passengers and luggage. Tecnam has used its extensive experience with aluminum airframes to create in the Tecnam P2006T a robust yet very light airframe, resulting in an outstanding payload-to-total-weight ratio.

Wings are of traditional construction, essentially mono spar configuration. Integral fuel tanks are located outboard of the engines holding 100 liters each for a total of 200 liters. A laminar NACA 63A airfoil of moderate thickness has been selected for the semi-tapered wing platform. This offers low drag and good high altitude behavior.

Wide slot aluminum flaps, electrically controlled, allow stall speeds lower than 48 kts. These flaps offer potential for very steep approaches and short landings. Fraise ailerons allow aggressive roll rates with minimal adverse yaw. Aileron control is via internal cabin cable linked to push-rods in the wing leading edges.

Particular attention was paid to the cabin's structural design in order to ensure the required crashworthiness prescribed in recent amendments to the FAA-FAR23 and EASA-CS23 codes. Fuselage structure, seats and seatbelts combine to protect occupants in case of a hard landing. The Tecnam P2006T's conformity to such safety requirements has been proven during dynamic tests (reaching forward load factors up to 26g) carried out by a certified laboratory.

The horizontal tail is an all-moving type, designed for remarkable longitudinal control-free stability and excellent control authority. A wide trim-tab, part of the stabilator trailing edge, doubles as an antitab device. The cable-type pitch trim is controlled by a wheel located between the pilots' seats and is fitted with a position indicator. As with most of the aircraft body, the horizontal stabilator and the vertical fins are metallic. The rudder features an electronically controlled trim-tab with a position indicator situated on the instrument panel

Interior And Outdoor

The generous interior dimensions of the Tecnam P2006T allow maximum space for pilots and passengers alike. With its two doors, its upholstered seats complete with headrests and vertical adjustment, the cabin provides great flexibility for pilots of varying physical stature to optimize their comfort.

Each seat is provided with three-point seat belts with inertia reel and the two Pilots' seats are equipped with a central armrest. Specific care has been given to cabin interiors and acoustic comfort.

The ventilation system features one vent outlet for each occupant. The heating system uniformly warms the cabin and a defrost manifold prevents the windshield from fogging even while taxiing. Wide and appropriate windows, together with the high wings, provide excellent visibility for a very pleasant flight, as well as for safe ground operations.

The cabin has a spacious luggage compartment of 350 liters, which is easily accessible from an external door.

Landing Gear

The retractable landing gear mechanism of the Tecnam P2006T is of an electro-hydraulic type, powered by a reversible pump, which is electrically controlled. The main landing gear is of a trailing link type, completely constructed from high strength aluminum alloys and 15CDV6 high strength steel, and is directly attached to the fuselage main bulkheads. An oleo-pneumatic shock absorber provides excellent ground load absorption. The main landing gear retraction is very simple through a 90° inboard rotation. The gear strut and the wheel are contained in the retracted position by the fuselage centre section baggand a side pod. The main gear of the Tecnam P2006T is held in position by an aluminum side brace, which also serves as the retraction mechanism operated by a hydraulic ram.

The main landing gear is equipped with Cleveland wheels (6.00-6) and rudder pedal activated brakes. The nose landing gear features a 5.00-5 wheel and telescopic strut with an oleo-pneumatic shock absorber. It is linked to the cabin's first bulkhead through a steel truss.

The gear extension of the Tecnam P2006T is speed-wise for higher safety and is operated by a hydraulic ram through the drag brace, which in turn locks it into the down position. When extended, the steering control on the nose gear is actuated by push-rods linked to the rudder pedals.

A system of lights and warning horn informs the pilot of the status of the landing gear's extended/retracted position. A back-up extension system, ensures landing gear extension even in the event of main system failure.

Engine And Propeller

The Tecnam P2006T is equipped with two four-cylinder four-stroke Rotax 912S engines of 100hp (73kW) each. These are liquid cooled with an integrated reduction gear (1:2.4286) driving constant speed propellers with pitch feathering devices.

Engine mounts are made of high strength Cr-Mo Steel tubes with engine vibration isolators. Very easy and convenient access to the engine compartment allows for fast daily inspections. From an operational point of view, the following benefits of the Tecnam P2006T should be stressed:

The option to use either automotive fuel or AVGAS allows operators to dramatically reduce the direct costs, making it possible to fly to locations where AVGAS is difficult to obtain or prohibitively expensive.
The twin-engine configuration of the Tecnam P2006T is extremely dependable, enabling the aircraft to travel long over water distances or over rough terrain.
The fuel system features two fuel tanks integral with the wings box for a total capacity of 200 liters.
Each engine is equipped with a mechanically driven fuel pump and an electric backup pump.
Tank selection and cross feeding are controlled by two valves positioned overhead

Standard Equipment

FLIGHT INSTRUMENTS and INDICATORS MAGNETIC COMPASS AIRSPEED IND., Kts ALTIMETER DUAL MODE (IN/Mb) VERTICAL SPEED DIRECTIONAL ELECTRIC ATTITUDE HORIZON ELECTRIC TURN AND BANK INDICATOR O.A.T. PITOT SYSTEM HEATED STATIC SYSTEM ALTERNATE STATIC SOURCE STALL WARNING AUDIBLE LANDING GEAR POSITION LIGHT, THREE LANDING GEAR-in-TRANSIT/NOT LOCKED LIGHT STABILATOR TRIM POSITION INDICATOR RUDDER TRIM POSITION INDICATOR	ENGINE INSTRUMENTS TACHOMETER + HOUR RECORDER, TWO MANIFOLD, DUAL OIL PRESS, TWO OIL TEMP., TWO HEAD TEMP., TWO FUEL PRESS., TWO AMMETER VOLTMETER LH + RH FUEL QTY ANNUNCIATOR PANEL LIGHTED PUSH TO TEST: - LH LOW FUEL - RH LOW FUEL - LH LOW OIL PRESS - RH LOW OIL PRESS - LH LOW VOLTAGE - RH LOW VOLTAGE - PILOT DOOR OPEN	FLIGHT CONTROLS HYDRAULIC BRAKES PARKING BRAKE ELECTRICAL FLAPS DUAL FLIGHT CONTROLS STEERABLE NOSE WHEEL AILERON AND ELEVATOR LOCK STABILATOR TRIM (MANUAL) ENGINE CONTROLS - THROTTLE, TWO - PROPELLERS, TWO - CARBURETTOR HEAT, TWO - CHOKE, TWO FLIGHT TRIM CONTROLS - RUDDER with INDICATOR - STABILATOR with INDICATOR LANDING GEAR, RETRACTABLE ELECTRO-HYDRAULIC LANDING GEAR SELECTOR SWITCH LANDING GEAR WARNING HORN LANDING GEAR EMERGENCY EXTENSION FUEL CONTROL SELECTOR WITH ON/OFF CROSSFEED OVERHEAD PANEL SWITCHES: - STARTER LH and RH - FUEL PUMP LH and RH - LEFT ENGINE LH and RH IGNITION SWITCHES - RIGHT ENGINE LH and RH IGNITION SWITCHES

ELECTRICAL SYSTEM 12 VOLT 35 Ah GILL 35A 12 VOLT ALTERNATORS-40 AMP., TWO ROCKER SWITCHES INTERNALLY LIGHTED - Master Switch - Landing Light - Taxi Light - Navigation Lights - Strobe Light - Pitot Heat - Map Light EXTERNAL POWER SUPPLY RECEPTABLE CIRCUIT BREAKER PANEL STATIC DISCHARGE WICKS LANDING/TAXI LIGHT	FUEL SYSTEM TWO INTEGRAL FUEL TANKS WITH 200 LITRES TOTAL CAPACITY ENGINE DRIVEN FUEL PUMPS, TWO AUXILIARY FUEL PUMPS, ELECTRIC, TWO FUEL TANK QUICK DRAIN, TWO 2 X SHUT OFF VALVES WITH CROSS FEED	INTERIOR PILOT and CO-PILOT SEA TS Simulated leather - Adjustable Fore and Aft - Vertical Adjustment TWO REAR PASSENGER SEATS SEAT BELTS & Shoulder Harness, All Seats WALL TO WALL CARPETING FIRE EXTINGUISHER MAP & STORAGE POCKETS RADIO CALL PLATE TOW BAR SOUNDPROOFING LUGGAGE COMP ARTMENTS OVERHEAD COCKPIT SPEAKER FOUR POSITION INTERCOM SYSTEM FIRST AID KIT

INTERIOR LIGHTING AVIONICS INSTRUMENTS internally lighted AVIONICS RADIOS internally lighted ENGINE INSTRUMENTS internally lighted FLIGHT INSTRUMENTS internally lighted COMPASS internally lighted MAP LIGHT	EXTERIOR EPOXY CORROSION PROOFING, All structure LH FRONT DOOR Pilot/Co-pilot, Lock and Key RH REAR DOOR Passenger REAR WINDOW ALL WINDOWS TINTED RETRACTABLE LANDING GEAR TIE DOWN RINGS MAIN WHEELS, 6.00 X 6 - NOSE 5,00 X 5	EXTERIOR LIGHTS NAVIGATION LH/RH wing tip and vertical tail VERTICAL TAIL STROBE LANDING / TAXI LIGHT

CABIN CONFORT SYSTEM WINDSHIELD DEFROSTER VENTILATOR ADJUSTABLE, 4 place HEATING SYSTEM	POWERPLANT AND PROPELLER ENGINES - 2 ROTAX 912S3 100 HP, 4 Cylinders liquid/air cooled, integrated reduction gear DUAL IGNITION SYSTEM THROTTLE CONTROL LH/RH TUBULAR STEEL ENGINE MOUNT PROPELLERS - 2 MT, 2 Blade, Constant Speed PROPELLER SPINNER, TWO PROPELLER CONTROL LH/RH AIR FILTER, TWO OIL FILTER, TWO OIL AND WATER COOLERS, TWO CARBURETOR HEAT with Manual Control	PRODUCT SUPPORT/DOCUMENTS MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY PILOT'S OPERATION HANDBOOK MAINTENANCE MANUAL PARTS CATALOG AIRCRAFT LOG BOOK ENGINE LOG BOOK

STANDARD GARMIN AVIONICS PACKAGE GTN 560 COMM/NAV/GPS Multifunction Display with GI-106A VOR/LOC/GS/GPS INDICATOR GTX 328 TRANSPONDER GMA 340 AUDIO PANEL MICROPHONE TELEX 100T PILOT and CO-PILOT PTT ELT 406 ARTEX