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P92 Echo Classic
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The P92 Echo Classic was designed and manufactured according to the international airworthiness standards.

P92 Eaglet
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The Eaglet combines the best of the features of their existing high wing aircraft line merged into a single..

P2002 Sierra
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Tecnam designed the P2002 Sierra using advanced computer design, structural and fluid dynamics modeling making it unquestionably the finest low wing 2 seat airplane in its class.

P2008
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TCarbon fiber meets metal with innovation, style, and advanced tecnology to create a new aircraft..

P92 Tail Dragger
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Tecnam P92 Tail Dragger is the first new aircraft this particular marketplace has seen in a very..

P92 Seasky
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Tecnam's reputation for developing aeroplanes for all aspects of General Aviation flying was further established today with the introduction of the Tecnam P92 Sea-Sky Hydroplane.

P92 Echo Light
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The italian ultralight market was young, and all the airplanes flying as microlight were dacron covered-two strokes engine with open cabin and low cruise speed.

Astore
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Astore is a technology concentrate and you can find this for each single configuration.

Snap
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The FR-01 is a single seat, low wing and fixed landing gear aircraft.

Adv Ultralight

Technical Specification

ENGINE
Manufacturer Rotax
Model 912 ULS
Power 98hp
Numbers of cylinders 4
PROPELLER
Manufacturer GT Propeller
Model GT-2/173/VRR-SRTC FW101
Number of Blades 2
Type Fix pitch - wood
Design Weight & Loading
MTOW 600 Kg 1320 lb
Baggage Allowance 20 Kg 44 lb
Limit Loads +4/-2 G
Ultimate Loads +6/-3 G
Dimension
Fuselage Height 2.5 m 8.2 ft
Fuselage Length 6.4 m 21 ft
Wing Span 9.3 m 30.5 ft
Cabin Weight 1.06 m 3.5 ft
Cabin Height 0.91 m 3 ft
Fuel Tank Capacity 45 X2 lt 11.2 X2 Gal
Performance 15°C Sealevel 450Kg/990lb
VMAX 222 Km/h 120 KTS
Cruise Speed 75% 204 Km/h 110 KTS
VNE 260 Km/h 141 KTS
Stall SpeedFLAPS DOWN POWER OFF 65 Km/h 35 KTS
Practical Ceiling 4572 m 15000 ft
Takeoff Run 100 m 328 ft
Takeoff Distance 200 m 656 ft
Landing Run 90 m 295 ft
Landing Distance 250 m 820 ft
Rate of Climb 6,1 m/sec 1200 ft/min
Range 503 N.M

The P92 Echo Classic was designed and manufactured according to the international airworthiness standards. This has been accomplished by one of the most known European Designers in the general aviation field, with the aid of modern planning instruments. The P92's performances and flying qualities are so superior that it compares to those planes certified under FAR 23

The P92 Echo Classic is a two- seater, single strut braced high wing aircraft. The main features of the design and construction are direct towards the aim of low weight and low cost.


Advantages

  • Superior performance and flight characteristics
  • Low stall speed
  • 100 knots cruise
  • Stable and Responsive
  • Uncompromising build quality
  • Excellent visibility
  • Roomy, quiet and ergonomic

Adv Ultralight

Technical Specification

DESIGN WEIGHT & LOADING
Designed MTOW 600 kg 1320 lb
Limit Loads +4/-2 G
Ultimate Loads +6/-3 G
Baggage Allowance 20 kg 44 lb
DIMENSION WING
Wing Span 8,7 m 28,5 ft
Wing Area 12,4 sqm 133 sqft
FUSELAGE
Length 6,5 m 21,3 ft
Height 2,5 m 8,2 ft
LH-RH CABIN DOOR
Height 0,83 m 33 in
Width 0,76 m 30 in
ENGINE
Manufacturer ROTAX
Model 912 ULS2
Power 98 hp
Number of Cylinders 4
PROPELLER
Manufacturer GT PROPELLER
Model GT
Number of Blades 2
Type Fix
PERFORMANCE SPEED 15°C Sealevel 450Kg/990lb
Maximum at Sea Level 235 Km/h 127 KTS
Cruise, 75% power 215 Km/h 116 KTS
VNE 270 Km/h 146 KTS
STALL SPEED
Flap Down, Power off 65 m 35 ft
Rate of Climb at Sea Level 5,6 m/sec 1100 ft/min
Service Ceiling 4500 m 14,800 ft
TAKE OF PERFORMANCE
Ground roll 110 m 360 ft
Total over 50 fr obstacle 350 m 673 ft
LANDING PERFORMANCE
Ground roll 160 m 360 ft
Total over 50 fr obstacle 260 m 850 ft
FUEL
Fuel Tank Capacity 45 X2 lt 11,9 X2 GAL

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 attention 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 fitted 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.


Adv Ultralight

Technical Specification

ENGINE P2002 SIERRA DELUXE P2002 SIERRA TURBO
Manufacturer ROTAX ROTAX
Model 912 ULS 914 UL
Power 98 hp 115 hp
Number of Cylinders 4 4
PROPELLER
Manufacturer GT PROPELLER GT PROPELLER
Model GT-2/173/VRR-SRTC FW101 GT
Number of Blades 2 2
Type FIX PITCH-WOOD FIX PITCH-WOOD
DESIGN WEIGHT & LOADING
MTOW 600 kg 1320 lb 600 kg 1320 lb
Baggage Allowance 20 kg 44 lb 20 kg 44 lb
Limit Loads +4 /-2G +4 /-2G
Ultimate Loads +6 /-3G +6 /-3G
DIMENSION
Fuselage Height 2, 43 m 8 ft 2, 43 m 8 ft
Fuselage Length 6, 65 m 21, 8 ft 6, 65 m 21, 8 ft
Wing SPan 8, 6m 28, 2ft 8, 6m 28, 2ft
Cab in Width 1, 11 m 3, 6 ft 1, 11 m 3,6 ft
Cab in Height 0, 91 m 3ft 0, 91 m 3ft
Fuel Tank Capacity 50 X2 lt 13, 2 X2 GAL 50 X2 lt 13, 2 X2 GAL
PERFORMANCE 15°C SEA LEVEL 450KG / 990LB
VMAX 244 Km/h 132 KTS 258 Km/h 139 KTS
Cruise Speed 75% 226 Km/h 122 KTS 258 Km/h 139 KTS
VNE 285 Km/h 154 KTS 290 Km/h 157 KTS
Stall SPeed 65 Km/h 35 KTS 65 Km/h 35 KTS
Practical Ceiling 4572 m 15000 ft 5486 m 18000 ft
Takeoff Run 105 m 344 ft 120 m 394 ft
Takeoff Distance 200 m 656 ft 220 m 722 ft
Landing Run 90 m 295 ft 120 m 394 ft
Landing Distance 200 m 656 ft 270 m 885 ft
Rate of Climb 6,1 m/sec 1200 ft/min 6,6 m/sec 1300 ft/min
Range 636 N.M 680 N.M

Tecnam designed the P2002 Sierra using advanced computer design, structural and fluid dynamics modeling making it unquestionably the finest low wing 2 seat airplane in its class. Tapered wing, laminar flow airfoils, slotted flaps, up turned wing tips and a streamlined fuselage give the P2002 to outstanding performance, complete control harmony and graceful style.

The resulting product is a symphony of aerodynamic and structure effectiveness with graceful, fluid flight responsiveness. Designed with the pilot in mind, this aircraft will delight even the most discriminating pilot while still keeping the inexperienced pilot safe and comfortable.


Advantages

  • Low stall speed
  • 122 knots cruise
  • Stable and Responsive
  • Uncompromising build quality
  • Excellent visibility
  • Sliding canopy can be opened in flight

Adv Ultralight

Technical Specification

ENGINE
Manufacturer ROTAX
Model 912 ULS
Power 98 hp
Number of Cylinders 4
PROPELLER
Manufacturer GT PROPELLER
Model GT-2/173/VRR-SRTCFW101
Number of Blades 2
Type FIX PITCH-WOOD
DESIGN WEIGHT &LODING
MTOW 600 kg 1320 lb
Baggage Allowance 20 kg 44 lb
Limit Loads +4 /-2G
Ultimate Loads +6 /-3G
DIMENSION
Fuselage Height 2,46 m 8,1 ft
Fuselage Length 6,93 m 22,7 ft
Wing Span 9 m 29,5 ft
Cabin Width 1,2 m 3,9 ft
Cabine Height SEAT TO COVER 0,91 m 3 ft
Fuel Tank Capacity 55 X2 lt 14,5 X2 GAL
PERFORMANCE 15°C Sealevel 450Kg/990LB
VMAX 235 km/h 127 KTS
Cruise Speed 75% 219 km/h 118 KTS
VNE 260 km/h 141 KTS
Stall Speed FLAPS DOWN POWER OFF 65 km/h 35 KTS
Practical Ceiling 4572 m 15000 ft
Takeoff Run 105 m 344 ft
Takeoff Distance 200 m 656 ft
Landing Run 90 m 295 ft
Landing Distance 200 m 656 ft
Rate of Climb 5,6 m/sec 1100 ft/min
Range 633 N.M
MAIN FEATURES
Fueselage COMPOSITE
High Wing METALLIC
Gear FIXED WITH FREE CASTERING OR STEERABLE NOSE WHEEL

Carbon fiber meets metal with innovation, style, and advanced tecnology to create a new aircraft line by Tecnam. The latest addition to the Tecnam line is the P2008 E-LSA.


Advantages

  • A carbon fiber fuselage and vertical stabilizer
  • Increased cabin size
  • Larger doors
  • A semi-tapered metal wing As with all of

Adv Ultralight

Technical Specification

ENGINE
Manufacturer ROTAX LYCOMING
Model 912 ULS YO-233-B2A
Power 98 hp 115 hp
Number of Cylinders 4
PROPELLER
Manufacturer GT PROPELLER
Model GT2
Number of Blades 2
Type FIX PITCH-WOOD
DESIGN WEIGHT & LOADING
MTOW 600 kg 1320 lb
Standard Equip.
Empty Weight
345 kg 760 lb 387 kg 850 lb
Standard Equip.
Useful Weight
255 kg 560 lb 213 kg 470 lb
Baggage Allowance 20 kg 44 lb
Limits Loads +6/-3G
DIMENSION
Fuselage Height 2,5 m 8,2 ft
Fuselage Length 6,4 m 21 ft
Wing Span 8,7 m 28,5 ft
Wing Area 12,4 sqm 133 sqft
Cabin WidthSEAT TO COVER 1,14 m 45 in
Cabin Height 0,91 m 3 ft
Fuel Tank Capacity 45 X2 lt 11,2 X2 GAL
PERFORMANCE 15°C Sealevel 450Kg/990lb
VMAX 220 km/h 120 KTS
Cruise Speed 75% 220 km/h 118 KTS
VNE 270 km/h 146 KTS
Stall SpeedFLAPS DOWN POWER OFF 76 km/h 41 KTS 78 km/h 42 KTS
Practical Ceilig 4572 m 15000 ft
Takeoff Run 93 m 305 ft 90 m 295 ft
Takeoff Distance 270 m 41 KTS 78 km/h 42 KTS
Landing Run 130 m 426 ft
Landing Distance 250 m 820 ft
Rate of Climb 5.6 m/sec 1100 ft/min 6.1 m/sec 1200 ft/min
Range 493 N.M 460 N.M

This Tail Dragger version of the Tecnam P92 is the first new aircraft this particular marketplace has seen in a very long time and promises its owners and pilots significantly improved flight characteristics.

Approval : France - United Kingdom - Germany - USA (Special LSA) - Australia


Adv Ultralight

Technical Specification

DESIGN WEIGHT &LODING
MTOW 650 kg 1430 lb 650 kg 1430 lb
Standard Equip. Empty Weight 430 kg 950 lb 410 kg 900 lb
Standard Equip. Useful Load 220 kg 485 lb 240 kg 520 lb
Limits Loads +4 /-2G +4 /-2G
Baggage Allowance 20 kg 44 lb 20 kg 44 lb
DIMENSION WING
Wing Span 8.7 m 28.5 ft 8.7 m 28.5 ft
Wing Area 12.4 sqm 133 sqft 12.4 sqm 133 sqft
FUSELAGE(including floats)
Fuselage Lenght 6.9 m 22.6 ft 6.9 m 22.6 ft
Fuselage Height 3.15 m 10.3 ft 3.15 m 10.3 ft
ENGINE
Manufacturer ROTAX ROTAX
Model 912 ULS2 912 ULS2
Power 98 hp 98 hp
Number of Cylinder 4 4
PROPELLER
Manufacturer GT PROPELLER GT PROPELLER
Model GT GT
Number of Blades 2 2
Type FIX FIX
PERFORMANCE SPEED
Maximum at Sea Level 180 Km/h 97 KTS 185 Km/h 100 KTS
Cruise 75% Power 168 km/h 91 KTS 171 km/h 92 KTS
VNE 240 km/h 130 KTS 240 km/h 130 KTS
STALL SPEED
Flaps Down, power off 76 Km/h 41 KTS 76 Km/h 41 KTS
Flaps Up, power off 83 km/h 45 KTS 83 km/h 45 KTS
Rate of Climb at Sea Level 4 m/sec 790 ft/min 4 m/sec 790 ft/min
Service Ceiling 3500 m 11,500 ft/min 3500 m 11,500 ft/min
Takeoff Performance
(run)-Water
<200 m/h <656 ft <200 m/h <656 ft
Takeoff Performance
(run)-RWY
150 m 492 ft 150 m 492 ft
Takeoff Performance
(over 50 obstacle)-RWY
290 m 950 ft 290 m 950 ft
Landing Performance-Water less than 80m 260 ft less than 80m 260 ft
Landing Performance
(run)-RWY
150 m 492 ft 150 m 492 ft
Total from 50 obstacle-RWY 260 m 850 ft 260 m 850 ft
Fuel Tank Capacity 45x2 lt 11.9x2 GAL 45x2 lt 11.9x2 GAL

Tecnam's reputation for developing aeroplanes for all aspects of General Aviation flying was further established today with the introduction of the Tecnam P92 Sea-Sky Hydroplane.

Requiring a take-off run of less than 200 metres, coupled with an impressive climb rate and a 100 hp engine, the Tecnam P92 Sea-Sky Hydroplane affords ease of operation, both on the water (be it lakes, rivers or sea) and in the air.

"Our Tecnam P92 Sea-Sky Hydroplane offers you the pleasure of enjoying both blue waters and blue skies'' by using our innovative 4 wheels retractable landing gear. Wherever you want to go today Tecnam has got the right aeroplane for you! Enjoy your time, meet land, sky and water!"


Adv Ultralight

Technical Specification

POWERPLANT
Engine Rotax 912 UL
Horsepower 80 hp
TBO 2000 hrs
Propeller Two Bladed Fixed Pitch
Design Weight & Loading
MTOW 500 Kg 1100 lb
Baggage Allowance 20 Kg 44 lb
Limit Loads +4/-2 G
Ultimate Loads +6/-3 G
Dimension
Fuselage Height 2.5 m 8.2 ft
Fuselage Length 6.3 m 21 ft
Wing Span 8.7 m 28.5 ft
Cabin Height SEAT TO COVER 0.91 m 3 ft
Cabin Weight 1.06 m 3.5 ft
Maximum Seating Capacity 2
Fuel Tank Capacity 45 lt 11.9 US Gal
Performance
VMAX 190 Km/h 103 KTS
Cruise Speed 75% 170 Km/h 92 KTS
Stall Speed FLAPS DOWN POWER OFF 65 Km/h 34 KTS
Practical Ceiling 3660 m 12000 ft
Takeoff Run 100 m 328 ft
Takeoff Distance 260 m 852 ft
Landing Run 100 m 328 ft
Landing Distance 260 m 852 ft
Rate of Climb 4.5 m/sec 852 ft/min
Range 270 N.M

The story of P92 airplane begins in early 90s...

The italian ultralight market was young, and all the airplanes flying as microlight were dacron covered-two strokes engine with open cabin and low cruise speed. In that period, TECNAM was young too as company as it was created on 1986 by the Partenavia's founders: the Pascale brothers Luigi and Giovanni.

TECNAM was in that period in charge to produce parts, assembly and test the ATR-42/72 horizontal tail, vertical tail and fuselage sections. On 1990 Paolo Pascale suggested his uncle to enter in the microlight business analyzing primarily what the market offered in those years...

The result was the development of a microlight with characteristics of a bigger General Aviation airplane: the result was the TECNAM P92: the first microlight with general aviation style.

Today, 20 years since the first flight, P92 is still one of best selling model of Tecnam production line: with 13 variants and versions, with over 500 customizations, P92 has been delivered almost 2000 units as ULM/LSA and VLA with more than 180.000 flown hours.

Tecnam decided to celebrate this model introducing the Taildragger 20th and betting, on September 2012, on "P92 Echo Classic Celebrating Program": the production of a special variant with a unique price for the end customer: anything not needed to fly fun has been removed or listed as optional, in order to have the possibility to purchase a real 270kg empty weight microlight with an unbeatable price for a Tecnam aeroplane.

Why purchase one trainer for your flight school, when you can have two!


Adv Ultralight

Technical Specification

POWERPLANT
Engine Rotax 912 ULS
Horsepower 98 hp
TBO 2000 hrs
Propeller Two Bladed Fixed Pitch
Design Weight & Loading
MTOW 600 Kg 1320 lb
Baggage Allowance 40 Kg 88 lb
Limit Loads +4/-2 G
Ultimate Loads +6/-3 G
Dimension
Fuselage Height 2.3 m 7.54 ft
Fuselage Length 7 m 23 ft
Wing Span 8.65 m 28.4 ft
Cabin Height SEAT TO COVER 0.98 m 3.2 ft
Cabin Weight 1.15 m 3.8 ft
Maximum Seating Capacity 2
Fuel Tank Capacity 55 X2 lt 14.5 X2 US Gal
Performance
VMAX 244 Km/h 132 KTS
Cruise Speed 75% 222 Km/h 120 KTS
Stall Speed FLAPS DOWN POWER OFF 65 Km/h 34 KTS
Practical Ceiling 4572 m 15000 ft
Takeoff Run 105 m 344 ft
Takeoff Distance 200 m 656 ft
Landing Run 90 m 295 ft
Landing Distance 200 m 656 ft
Rate of Climb 6.1 m/sec 1200 ft/min
Range 670 N.M

BEAUTY - because now you can find the typical luxury car style, both for exteriors and interiors, on your Astore, shaped lines and sharp edges, all 3D formed sheet metal gives you the pleasure to watch your plane for hours before stepping inside it!

TECHNOLOGY - Astore is a technology concentrate and you can find this for each single configuration. For the first time the Apple iPad Mini is part of the standard equipment for your flying and free time pleasure. Loudspeakers, Bose Headsets, and LEVIL AHRS equipment to make your iPad a funny EFIS are also available as optionals and so the possibility to lock the aircraft by remote controlThe P92 Echo Classic is a two- seater, single strut braced high wing aircraft. The main features of the design and construction are direct towards the aim of low weight and low cost.

INTEGRATION - this word means that you will be always able to have any equipment and any component under your control: hearing music uploaded on your iPad at home, answering your phone, using WiFi connection with LEVIL AHRS and pitot/static system in order to display on iPad the attitude and speed/altitude/GPS parameters, or simply compute the actual Weight and Balance, looking at procedures, checklists, POH with Tecnam Astore app (pre-installed on your iPad) is now possible!

ENTERTAINMENT - There is a wide selection of standard and optional equipments that will make your flight experience relaxing: watching a movie on the iPad, hearing your favourite music via bluetooth on your Bose headphones or Loudspeakers, allow your passenger to fly without control stick.... all this flying 15km/liter!

COMFORT - Seating inside the Astore is a singular experience: you will see yourself involved into a unique interiors design and soft materials, always with a great visibility and with all controls and switches that can be fastly reached. The 4-points safety belt is self regulating and in order to ensure your safety the ballistic parachute can be fitted on demand


Adv Ultralight

Technical Specification

POWERPLANT
Engine Rotax 912 ULS
Horsepower 98 hp
TBO 2000 hrs
Propeller Two Bladed Fixed Pitch
Design Weight & Loading
MTOW 420 Kg - Non ACRO 925 lb - Non ACRO
Baggage Allowance N/A N/A
Limit Loads +4/-2 G (420 kg) +6/-4 (395 kg)
Ultimate Loads +10/-9 G
Dimension
Fuselage Height 1.81 m 5.9 ft
Fuselage Length 6.35 m 21 ft
Wing Span 7.20 m 23.6 ft
Cabin Height SEAT TO COVER 0.68 m 2.23 ft
Cabin Weight 0.68 m 2.23 ft
Maximum Seating Capacity 1
Fuel Tank Capacity St 40/lt
Opt 20 + 25 lt
10.5 US Gal
6.6 + 6.6 US Gal
Performance
VMAX 290 Km/h 157 KTS
Cruise Speed 75% 260 Km/h 140 KTS
Stall Speed FLAPS DOWN POWER OFF 83 Km/h - no flap 45 KTS - no flap
Practical Ceiling 4572 m 15000 ft
Takeoff Run 100 m 330 ft
Takeoff Distance 140 m 460 ft
Landing Run 280 m 920 ft
Landing Distance 427 m 1400 ft
Rate of Climb 10.1 m/sec 1400 ft/min
Range 600 N.M

The FR-01 is a single seat, low wing and fixed landing gear aircraft. The main feature of the aircraft is the high power to weight ratio and the capability to perform aerobatics with a low operating costs.

The structure is metallic with 4130 steel fuselage truss and light alloy wing, stabilizer/elevator and fin. Rudder and aileron are made in composite carbon/glass/epoxy structure and so the fuselage cover and engine cowlings. The lower tailcone is covered by fabric while the main landing gear is a single 2024T3 bended and tapered beam. The adjustable rudder pedals allow the comfortable seating of people from 1,6 to 1,98mt.

The standard fuel tank is in front central position. The main unit is a 35litres tank while it is possible to install an acro (header) tank below the main tank that allows the aircraft to perform inverted flight if the electronic injection engine and inverted oil system are installed. The total amount of fuel is about 40litres in frontal main+acro tank plus 25+25litres in the optional wing tanks. Only the central tank feeds the engine and is equipped with an ANDAIR shut off valve. An in-flight fuel transfer system provides the fuel to go from the wing tank(s) to the main one. All the cabin 3/8'' fuel hoses are rigid with AN6 fittings.

The standard engine is the 98hp Rotax 912 but the ROTAX 912is can be installed as well. Finally it is possible to install a special ROTAX 912 derived engine with 23hp of extra power where allowed (ULM and EXPERIMENTAL categories only). The injected engines can be equipped with an inverted oil system. The exhaust system is made by a 4 in 1 with central muffler and optional smoke system. MT-Propeller constant speed 183cm diameter is finally available as an optional.