Tecnam.com - P2002JR 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

P2002JR CS/VLA

GENERAL VIEW

BROCHURE

Technical Info

Photo Gallery Details

Photo Gallery Flights


	The P2002-JR is a two-seater side by side, low wing aircraft with retractable landing gear. The P2002-JR features superlative performance and flying qualities, now confirmed by hundreds of P2002’s and P2002 RG’s flying all over the world. The ease of piloting and maintenance make this aircraft an excellent solution for training with flight schools but also an ideal platform for surveillance and patrolling territory as well as, of course, for pure recreational tourism. The option to use AVGAS 100LL or unleaded MOGAS ASTM D4814-EN/228 SUPER make the P2002 JR even more flexible and economical. The P2002-JR represents the latest development of the Tecnam aircraft as result of the aircraft’s continued improvement, the use of advanced software for design with structural and fluidynamic analysis. Thanks to the tapered wing, the laminar airfoils, the sloned flaps and the streamline fuselage together with the retractable gear, the P2002-JR is an outstanding aircraft, with the perfect mix of aerodynamic and structural efficiency.

Construction

The Tecnam line employs a monocoque tail cone section with sheet aluminium over steel tubing for the forward section.
The aluminium tapered wing has a conventional structure with a forward load bearing spar and a conventional rear spar. The wing halves are attached to the fuselage by a very strong carry-through made of 2024-T3 grade aluminium fixed to the cabin truss.
The fuel tanks hold 13.2 gal/50l each, located in the wing leading edges separated from the fuselage for safety.
The sliding canopy allows 360° of vision in the cockpit. This canopy can be fully opened in flight below 70 knots.
The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column.
The excellent flying characteristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height.
The ailerons are effective in allowing for a quick roll rate without being overly sensitive.
All control surfaces are made out of aluminium.
The wide slotted flaps, electrically activated, allow stall speed lower than 73 km/h (40 Kts).
The canopy has full rollover protection.

Interior And Outdoor

Seats are adjustable and increase in height as they are moved forward.
The luggage area allowing for 44 pounds/20 kg of weight, located behind the seats with ample room for several travel bags.
All Tecnam aircraft have dual control sticks with a curve at the base for ease of ingress and egress.
The dual controls come standard with PTT and electric stabilator trim on both sticks with a trim indicator on the panel.
The fresh air vents are conveniently located on each side of the panel.
Heat and defrost are standard.
The aircraft comes with dual rudder pedals, connected to a steerable nose wheel.
The interior is spacious, ergonomic and comfortable.
Cabin is a roomy 44 in/112 cm wide.
The wide conventional type instrument panel allows placement of a broad range of equipment, in addition to standard VFR training.
Four point harness system is standard.

Landing Gear

The main landing gear is aluminium alloy with a rubber shock absorber system that is robust enough for rough strips. Retraction is by three hydraulic cylinders.
The trailing link nose gear uses an oleo-pneumatic shock absorber that provides excellent ground load absorption. The same system is used on the certified P2006.
A hydraulic Parker pump pressurises the system. In case of failure of the electro/hydraulic system, there is an emergency circuit with an independent tank which is constantly monitored. Should there be a total failure, the landing gear will drop under gravity.
The main landing gear wheels and brakes are conventional aircraft size (5.00x5).
The brake lever control and the parking brake are located forward between the seats.

Engine And Propeller

The top and bottom engine cowls are quickly and easily removable making any maintenance easier to accomplish. The top cowl has 2 large hinged openings for easy access to the engine compartment, without the need for tools to allow effective pre-flight inspections.
The engine’s mount is steel-tubing with shock mounts It also supports the nose wheel, while the retraction cylinder is anchored to the main fuselage structure.
The power plant is a Rotax 912 S2 series certified to FAR 33 four-cylinder, four-stroke engine.
The engine employs liquid and air cooling with an integrated 1:2.4286 reduction gear.
A constant speed wood and composite Hoffmann propeller certified to FAR 33 comes as standard.
The quick drain gascolator is installed in the engine compartment with easy outside access.
Drain taps are fitted to the underside of the wings to purge the tanks.
Circuit breakers are standard.
The battery is located in the rear of the fuselage with easy access through a hinged door.
There is also an external power socket.

Standard Equipment

FLIGHT INSTRUMENTS and INDICATORS MAGNETIC COMPASS AIRSPEED IND., Kts ALTIMETER (IN) VERTICAL SPEED ATTITUDE ELECTRIC DIRECTIONAL ELECTRIC TURN AND BANK INDICATOR FLAPS INDICATOR PITOT SYSTEM STATIC SYSTEM STABILATOR TRIM POSITION INDICATOR	ENGINE INSTRUMENTS RPM INDICATOR HOUR RECORDER OIL PRESS OIL TEMP. HEAD TEMP. FUEL PRESS. VOLTMETER AMMETER MANIFOLD PRESSURE LH + RH FUEL QTY	OTHER INSTRUMENTS / WARNING CHRONOMETER O.A.T. INDICATOR GENERATOR WARNING LIGHT

FLIGHT CONTROLS HYDRAULIC BRAKES PARKING BRAKE ELECTRICAL FLAPS DUAL FLIGHT CONTROLS STEERABLE NOSE WHEEL STABILATOR TRIM (Electric actuated from Stick) ENGINE CONTROLS - THROTTLE, TWO - CARBURETOR HEAT - CHOKE LANDING GEAR, RETRACTABLE ELECTROHYDRAULIC LANDING GEAR SELECTOR SWITCH LANDING GEAR WARNING HORN LANDING GEAR EMERGENCY EXTENSION FLIGHT TRIM CONTROLS - STABILATOR with INDICATOR FUEL CONTROL SELECTOR WITH ON/OFF PANEL SWITCHES: - STARTER - FUEL PUMP - ENGINE LH and RH IGNITION SWITCHES	ELECTRICAL SYSTEM 12 VOLT 18A AMP. BATTERY 12 VOLT ALTERNATORS-20 AMP. SWITCHES Nav. Lights - Landing Light - Strobe Light EXTERNAL POWER SUPPLY RECEPTABLE CIRCUIT BREAKER PANEL	FUEL SYSTEM TWO INTEGRAL FUEL TANKS WITH 100 LITRES TOTAL CAPACITY ENGINE DRIVEN FUEL PUMP AUXILIARY FUEL PUMPS, ELECTRIC FUEL QUICK DRAIN

INTERIOR PILOT and COPILOT SEATS Adjustable Fore and Aft SEAT BELTS & Shoulder Harness, All Seats WALL TO WALL CARPETING LUGGAGE COMPARTMENTS FIRE EXTINGUISHER RADIO CALL PLATE SOUNDPROOFING FIRST AID KIT	EXTERIOR EPOXY CORROSION PROOFING, All structure SLIDING CANOPY with lock and key REAR WINDOW TIE DOWN RINGS MAIN WHEELS, 5,00 X 5 CLEVELAND NOSE WHEEL, 4,00 X 4	EXTERIOR LIGHTS NAV. LIGHTS LED with strobe ORION 600 FULL LED TAXI LIGHT LED

CABIN CONFORT SYSTEM WINDSHIELD DEFROSTER VENTILATOR ADJUSTABLE, 2 place HEATING SYSTEM	POWERPLANT AND PROPELLER ENGINES - 1 ROTAX 912S3 100 HP, 4 Cylinders liquid/air cooled, integrated reduction gear AUXILIARY ALTERNATOR DUAL IGNITION SYSTEM THROTTLE CONTROL LH/RH TUBULAR STEEL ENGINE MOUNT PROPELLER - Hoffmann, 2 Blade Variable Pitch PROPELLER SPINNER AIR FILTER OIL FILTER OIL AND WATER COOLERS CARBURETOR HEAT with Manual Control THERMOSTAT VALVE	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 225A COM/NAV GTX 328 TDX ELT 406 Mhz Antennas: - Transponder - VHF - ELT Speakers Microphone Stick Push-To-Talk Switch-Pilot/Copilot Mic& Phone Jacks-Pilot/Copilot