ADV ULTRALIGHT
P92 Eaglet
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
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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 metal torsion box.
The airfoil is a Gottinga 398 modified for better low speed handling characteristics with a modified STOL wing-tip.
The leading edges of the wings are easily detachable for repairs.
The fuel tanks hold 11,2 GAL (45 lt) in each wing and are located in the wings separated from the fuselage for safety.
A rear window completes the extraordinary visibility allowing 360° of vision in the cockpit.
The stabilator 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 speed lower than 38 Kts.
The Eaglet has 38 degrees of flaps making steep approach landings easier.
 
Interior And Outdoor
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Seats are adjustable in flight and increase in height as they are moved forward.
The luggage area allowing for 44 pounds 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 widest cabin yet at 46 inches.
The interior is spacious, ergonomic and comfortable.
Dual throttles allow the pilot to fly either left or right handed.
Heat and defrost are standard.
The fresh air vents are conveniently located in the doors.
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.
 
Landing Gear
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The main landing gear is spring steel 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).
A hand actuated hydraulic brake is available as an option with toe brakes standard.
A parking brake is between the seats and is actuated by use of a single twist.
 
Engine And Propeller
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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 steel firewall is soundproofed.
The power plant is a Rotax 912 series 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 propeller comes standard with several ground adjustable propellers available as options.
The quick drain gascolator is installed in the engine compartment with easy access.
The engine installation allows for the addition of a 40 Ah external alternator.
Circuit breakers are standard.
The battery is located in the rear of the fuselage with easy access through a hinged door.
 
Standard Equipment
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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
 
Photo Gallery Details
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Photo Gallery Flights
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