Tecnam.com - P92 Echo Classic De Luxe 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

P92 Echo Classic De Luxe US/LSA

GENERAL VIEW

BROCHURE

Technical Info

Photo Gallery Details

Photo Gallery Flights


	The P92 Echo Classic is a two-seat, single strut braced high wing aircraft. The P92 Echo Classic was designed and manufactured according to the international airworthiness standards. This has been accomplished by one of the most renowned European Designers in the general aviation field, with the aid of modern planning instruments. The P92’s performance and flying qualities are so superior that it compares to aircraft certified under FAR/CS 23. The excellent flying characteristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height. The large flaps are deployed electrically. The low stall speed and the general slow flying characteristics of the aircraft allow it to operate with ease on short runways.

Construction

The Tecnam line employs a monocoque tail cone section with the forward fuselage using sheet aluminium over steel tubing.
The wing is an all aluminium conventional structure with a single strut.
The fuel tanks hold 11.9 gal/45l each, located in the wing leading edge separated from the fuselage for safety.
A wide rear window together with large side windows complete the extraordinary visibility allowing 360° of vision in the cockpit.
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 large flaps are deployed electrically.
The low stall speed and the general slow flying characteristics of the aircraft allow it to operate with ease on short runways.

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 is located behind the seats with easy access in flight.
All Tecnam aircraft have dual control sticks, throttles and rudder pedals.
The trim tab and the flaps are electrically activated with a position indicator on the instrument panel.
The fresh air vents are conveniently located in the doors.
The aircraft has dual rudder pedals with a steerable nose wheel.
The wide instrument panel is designed to accommodate a full variety of instrumentation.

Landing Gear

The main landing gear legs are made of spring steel, directly connected to the main structure.
The landing gear is robust enough for rough strips and require no maintenance.
The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment with easy and economical maintenance.
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 removed making any maintenance procedure faster to accomplish. The top cowl has a large opening for easy access to the engine compartment for effective pre-flight inspections.
The engine's mount is steel-tubing with shock mounts. It also supports the nosewheel that is not anchored directly to the cabin's structure.
Two power plant options are available: Rotax 912UL 80HP four-cylinder, four-stroke engine and Rotax 912 ULS 100HP four-cylinder, four-stroke engine. Both engines come with an integrated 1:2.4286 reduction gear.
A fixed pitch wood and composite propeller comes as standard.
The quick drain gascolator is installed in the engine compartment with easy outside access.
The fuel system uses a mechanical engine driven pump along is with an electrical back-up pump.
The battery is located in the rear of the fuselage with easy access through a hinged door.

Standard Equipment

FLIGHT INSTRUMENTS and INDICATORS MAGNETIC COMPASS AIRSPEED IND., Kts ALTIMETER (IN) VERTICAL SPEED BANK INDICATOR PITOT SYSTEM STATIC SYSTEM STABILATOR TRIM POSITION INDICATOR	ENGINE INSTRUMENTS DYNON D10 include: TACHOMETER HOUR RECORDER OIL PRESS OIL TEMP. HEAD TEMP. FUEL PRESS. VOLTMETER LH + RH FUEL QTY TRIM INDICATOR FLAP INDICATOR	FLIGHT CONTROLS HYDRAULIC BRAKES PARKING BRAKE ELECTRICAL FLAPS DUAL FLIGHT CONTROLS STEERABLE NOSE WHEEL STABILATOR TRIM (Between the seats) ENGINE CONTROLS - THROTTLE, TWO - CHOKE FLIGHT TRIM CONTROLS - STABILATOR with INDICATOR FUEL CONTROL SELECTOR WITH ON/OFF PANEL SWITCHES: - STARTER - ENGINE LH and RH IGNITION SWITCHES

ELECTRICAL SYSTEM 12 VOLT 18A AMP. BATTERY 12 VOLT ALTERNATORS-20 AMP. SWITCHES - Landing Light 12 VOLT socket CIRCUIT FUSES PANEL	FUEL SYSTEM TWO INTEGRAL FUEL TANKS WITH 100 LITRES 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 E STORAGE POCKETS LUGGAGE COMPARTMENTS

EXTERIOR REAR WINDOW ALL WINDOWS TINTED TIE DOWN RINGS MAIN WHEELS, 5,00 X 5 NOSE WHEEL, 4,00 X 6 WHEEL PANTS	CABIN CONFORT SYSTEM VENTILATOR ADJUSTABLE, 2 place	POWERPLANT AND PROPELLER ENGINES - 1 ROTAX 912UL 80/100 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 SPINNER AIR FILTER OIL FILTER OIL AND WATER COOLERS

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