Tecnam.com - P2002 Sierra De Luxe

"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)

ADV ULTRALIGHT

P2002 Sierra De Luxe

GENERAL VIEW

BROCHURE

Photo Gallery Details

Photo Gallery Flights


	To design the P2002 Sierra Tecnam has made use of the most advanced systems of 3D design, fluid dynamics and structural analysis, resulting in one of the best two-seater low wing aircraft in its category. Tapered laminar flow wing, sloned flaps, up turned wing tips and a streamlined fuselage give to the P2002 superlative performance, a complete harmony of controls and style. The resulting product is a symphony of aerodynamic and structure effectiveness with graceful, fluid flight. Designed with the pilot in mind, this aircraft will delight even the most discerning pilot while still keeping the inexperienced pilot safe and comfortable. The sliding canopy allows 360° of vision from the cockpit. This can be opened in flight up to 70 knots. The all moving Stabilator is fined with a trim tab controlled by bunons 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 canopy has full rollover protection.

Construction

The Tecnam line employs a monocoque construction style using sheet aluminium over steel tubing.
The wing is all aluminium and constructed in a conventional way with a single spar and metaeal torsion box.
The leading edges of the wings and are easily detachable for repairs.
The fuel tanks are each 13.2 gal/50 lt and are located in the leading edge separated from the fuselage for safety.
The sliding canopy allows 360° of vision in the cockpit.
The all-moving tailplane provides remarkable longitudinal hands-off stability along with minimum drag and weight penalty providing balanced, 2 finger, flight control.
The wide slotted flaps, electrically activated, allow stall speeds lower than 36 Kts.
The Sierra has 38 degrees of flaps making steep approach landings easier.
The all aluminium ailerons are effective in allowing for a quick roll rate without being overly sensitive.
All control surfaces are made out of aluminium.
The canopy has full rollover protection.

Interior And Outdoor

Seats are adjustable in flight and increase in height as they are moved forward.
The luggage area allowing for 44 pounds/20 kg of weight is 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 the stick with a trim indicator on the panel.
The interior is spacious, ergonomic and comfortable.
Dual throttles allow the pilot to fly either left or right handed.
Throttle quadrant with single throttle design.
The fresh air vents are conveniently located on the panel.
All Tecnam aircraft provide excellent forward visibility over the cowling.
The planes come with dual conventional rudder pedals with a steerable nose wheel.
The wide instrument panel is designed to accommodate a full variety of instrumentation, from a standard 6 pack to fully integrated EFIS installations.
The all new instrument panel is modular for ease of avionics installations.
Cabin is a roomy 44 in/112 cm wide.
Four point harness system is standard.

Landing Gear

The main landing gear is aluminium alloy that is robust enough for unimproved strips and requires no service.
The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment.
The main landing gear wheels and brakes are conventional aircraft size(5.00x5).
Toe brakes are available as an option.
The brake lever control is located forward between the seats.
A parking brake is between the seats and is actuated by use of a single twist.

Engine And Propeller

The top and bottom engine cowls are quickly and easily removed making any maintenance procedure faster to accomplish.
The top cowl has 2 large hinged openings for easy access to the engine compartment for effective pre-flight inspections.
The engine is mount is Cro-Moly steel-tubing with shock mounts.
The firewall is soundproofed.
The power plant is a Rotax 912 ULS2 series (100 Hp) four-cylinder, four-stroke engine.
The engine is a liquid and air cooled engine with an integrated 1:2.4286 reduction gear.
A fixed pitch wood and composite comes standard.
The quick drain gascolator is installed in the engine compartment with easy access. A back-up electrical pump engages if mechanical fuel pump is out.
The engine installation allows for the addition of a 40 Ah external alternator.

Standard Equipment

FLIGHT INSTRUMENTS and INDICATORS MAGNETIC COMPASS AIRSPEED IND., Kts ALTIMETER (IN) VERTICAL SPEED BANK INDICATOR FLAPS INDICATOR PITOT SYSTEM STATIC SYSTEM STABILATOR TRIM POSITION INDICATOR LANDING GEAR POSITION LIGHT THREE (only rg) LANDING GEAR-in-TRANSIT/NOT LOCKED LIGHT (only rg)	ENGINE INSTRUMENTS TACHOMETER HOUR RECORDER OIL PRESS OIL TEMP. HEAD TEMP. FUEL PRESS. VOLTMETER LH + RH FUEL QTY	FLIGHT CONTROLS HYDRAULIC TOE BRAKES PARKING BRAKE ELECTRICAL FLAPS DUAL FLIGHT CONTROLS STEERABLE NOSE WHEEL STABILATOR TRIM (Electric actuated from Stick) ENGINE CONTROLS - THROTTLE, TWO - CHOKE FLIGHT TRIM CONTROLS - STABILATOR with INDICATOR FUEL CONTROL SELECTOR WITH ON/OFF PANEL SWITCHES: - STARTER - FUEL PUMP - ENGINE LH and RH IGNITION SWITCHES LANDING GEAR, RETRACTABLE ELECTROHYDRAULIC (only rg) LANDING GEAR SELECTOR SWITCH (only rg) LANDING GEAR WARNING HORN (only rg) LANDING GEAR EMERGENCY EXTENSION (only rg)

ELECTRICAL SYSTEM 12 VOLT 18A AMP. BATTERY 12 VOLT ALTERNATORS-20 AMP. SWITCHES - Landing Light - Strobe Light CIRCUIT FUSES 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 CO-PILOT SEATS - Adjustable Fore and Aft SEAT BELTS & Shoulder Harness, All Seats WALL TO WALL CARPETING LUGGAGE COMPARTMENTS

EXTERIOR SLIDING CANOPY with lock and key REAR WINDOW TIE DOWN RINGS ALL WINDOWS TINTED MAIN WHEELS, 5.00 X 5 NOSE WHEEL, 4.00 X 6 RETRACTABLE LANDING GEAR MAIN WHEELS, 5,00 X 5 NOSE WHEEL, 4,00 X 6	EXTERIOR LIGHTS VERTICAL TAIL STROBE TAXI LIGHT	CABIN CONFORT SYSTEM VENTILATOR ADJUSTABLE, 2 place

POWERPLANT AND PROPELLER ENGINES - 1 ROTAX 912ULS2 100 HP, 4 Cylinders liquid/air cooled, integrated reduction gear DUAL IGNITION SYSTEM THROTTLE CONTROL LH/RH TUBULAR STEEL ENGINE MOUNT PROPELLER - GT Propeller, 2 Blade fix PROPELLER - GT Propeller, 2 Blade Variable Pitch (Only RG and TURBO) 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