Tecnam.com - P92 Eaglet 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 Eaglet US/LSA

GENERAL VIEW

BROCHURE

Technical Info

Photo Gallery Details

Photo Gallery Flights


	Tecnam designed the P92 Eaglet after re-examining the ultra light aircraft market and determined a significant need existed for a robust trainer for all levels of flight – Sport Pilot through Commercial training. The result is the Eaglet. Using the proven P92 as the base platform and paying particular anention to the needs of the new American LSA category, Tecnam has delivered the best high wing training and cross country aircraft to date in the light general aviation category. The Eaglet combines the best of the features of their existing high wing aircraft line merged into a single platform. The Eaglet features increased side visibility, smooth aerodynamic lines, a low profile modular panel able to accommodate a wide range of avionics, while still maintaining excellent visibility over the nose, a trait of all TECNAM aircrafts. The doors are fined with automotive type door seals, seats that give full support with excellent leg room, side map pockets as well as pockets in the back of the seats, and even a cup holder, make the Eaglet a luxury aircraft. All this makes the Eaglet the natural choice for discriminating buyers of all ages and levels of flight experience. But the real beauty of this fine bird is in the flying – uncompromised and unparalleled in feel and response.

Construction

This 5th generation P92 Eaglet 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.’’ The high efficiency wing is based on the well known NACA63A airfoil while the single-slot flaps, extending along much of the wing span, allow low stall speeds with great take off and landing performance.
The all movable type (stabilator) horizontal tail,traditional on all Tecnam aeroplanes, allows excellent controllability and “hands off” longitudinal stability.
The instrument panel size is increased due to the wider cabin and its modular design can accommodate the most complete instrumentation, be it analogue or digital.
The P92 Eaglet fuselage has modified in its forward section, thus allowing for an increase in the cabin width, larger doors for easier access and a wider baggage compartment, as well as the addition of a new vain provided with an external door which is useful for on-board equipment storage.

Landing Gear

The main spring leaf landing gear, including wheels, tyres and fairings are the same as on all of the other non-retractable Tecnam aeroplane models.
The nose gear is free castering and consists of a tubular steel leg, connected to the lower engine mount attachments and is braced by a oleo-pneumatic shock absorber which is dimensioned for unprepared surfaces and for nose landings, frequent in flight school activities.
All of the landing gear is faired to minimize drag. Ground steering is by differential braking.

Engine And Propeller

The Textron Lycoming YO-233-B2A, with a 2400 hrs TBO, provides 115 hp @2800 rpm. Coupled to a fixed pitch propeller, whose geometric and aerodynamic characteristics are carefully chosen, allowing it to reach top class performance. The engine is well isolated from vibrations through dyna-focal attachments, its easy and compact installation is readily accessible and fuel consumption at 5.3 gal/h in economy cruise, allows autonomies of automotive level. At the same time, the higher power available magnifies climb and ceiling performance.
Traditional starter’s and alternator’s characteristic drives and the new Electronic Ignition complete the efficiency and versatility of this new Textron Lycoming YO-233-B2A engine.

Standard Equipment

FLIGHT INSTRUMENTS and INDICATORS MAGNETIC COMPASS AIRSPEED IND. ALTIMETER DUAL MODE (IN/Mb) VERTICAL SPEED BANK INDICATOR FLAP INDICATOR PITOT SYSTEM STATIC SYSTEM STABILATOR TRIM POSITION INDICATOR	ENGINE INSTRUMENTS TACHOMETER OIL PRESS OIL TEMP. FUEL PRESS. VOLTMETER LH + RH FUEL QTY TRIM INDICATOR FLAP INDICATOR ROTAX DYNON D10 include: HOUR RECORDER HEAD TEMP. LYCOMING DYNON D120 include: CHT AMP EGT 4 CARB. AIR TEMP HOUR METER	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 (ONLY LYCOMING) - CENTRAL THROTTLE QUADRANT (ONLY LYCOMING) - CHOKE FLIGHT TRIM CONTROLS - STABILATOR with INDICATOR FUEL CONTROL SELECTOR WITH ON/OFF PANEL SWITCHES: - AVIONIC MASTER

ELECTRICAL SYSTEM 12 VOLT 18A AMP. BATTERY 12 VOLT ALTERNATORS-20 AMP. SWITCHES - Landing Light - Strobe Light 12 VOLT socket CIRCUIT BREAKER PANEL	FUEL SYSTEM TWO INTEGRAL FUEL TANKS WITH 92 LITRES, TOTAL CAPACITY ENGINE DRIVEN FUEL PUMP ELECTRICAL FUEL PUMPS FUEL QUICK DRAIN	INTERIOR PILOT and COPILOT SEATS - Adjustable Fore and Aft - Arm rest SEAT BELTS & Shoulder Harness, All Seats WALL TO WALL CARPETING MAP E STORAGE POCKETS LUGGAGE COMPARTMENTS

EXTERIOR EPOXY CORROSION PROOFING, All structure LH/RH FRONT DOOR Pilot/Copilot, Lock and Key REAR WINDOW ALL LATERAL AND REAR WINDOWS TINTED BROWN MAIN WHEELS, 5,00 X 5 NOSE WHEEL, 5,00 X 5	EXTERIOR LIGHTS WING LIGHT GREEN/RED, WHITE AND STROBE AVEO NON TSO TAXI LIGHT	CABIN CONFORT SYSTEM WINDSHIELD DEFROSTER VENTILATOR ADJUSTABLE, 2 place HEATING SYSTEM with DEFROST

POWERPLANT AND PROPELLER Opion I ROTAX FIRE WALL INOX 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 SPINNER AIR FILTER OIL FILTER OIL AND WATER COOLERS FIRE SLEEVE ON FUEL and OIL TUBES Opion II ROTAX IS FIRE WALL INOX ENGINES - 1 ROTAX UL IS 100 HP, 4 Cylinders Fuel Injected 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 FIRE SLEEVE ON FUEL and OIL TUBES Option III LYCOMING FIRE WALL INOX ENGINE - 1 LYCOMING YO-233-B2A 115 HP, 4 Cylinders Direct drive DUAL IGNITION SYSTEM THROTTLE CONTROL TUBULAR STEEL ENGINE MOUNT PROPELLER - GT 2 Blade fix PROPELLER SPINNER AIR FILTER OIL FILTER OIL COOLER CARBURETOR HEAT with Manual Control THERMOSTAT VALVE FIRE SLEEVE ON FUEL and OIL TUBES	PRODUCT SUPPORT/DOCUMENTS MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY PILOTS OPERATION HANDBOOK MAINTENANCE MANUAL PARTS CATALOG AIRCRAFT LOG BOOK ENGINE LOG BOOK	LSA include: INOX FIREALL AIRSPEED IND., Kts HYDRAULIC TOE BRAKES CASTERING Nose Wheel (Only for Lycoming code 1004) PANEL SWITCHES: - SPLIT STARTER - AVIONIC STARTER KEY ACS FIRE SLEEVE ON FUEL and OIL TUBES TIE DOWN RINGS THERMOSTATIC VALVE OIL BAGGAGE COMPARTMENT NET