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P92JS CS/VLA
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The P92-JS is a two-seater side by side, single strut braced, high wing aircraft. The aircraft's outstanding performance...

P2002 JF CS/VLA
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The P2002-JF is a two-seater side by side, low wing aircraft. The JF P2002 features superlative performance...

P2002 JR CS/VLA
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The P2002-JR is a two-seater side by side, low wing aircraft with retractable landing gear. The P2002-JR features...

P2008 JC CS/VLA
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Carbon fiber meets metal with innovation, style, and advanced technology to create a new aircraft line by Tecnam...

P2010 Ptwenty Ten CS/23
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The Tecnam P Twenty-Ten brings together an advanced technology all carbon fibre fuselage with a metal wing to deliver...

Certified Single Engine

Technical Specification

ENGINE P92JS DELUX P92JS LY
Manufacturer Rotax Lycoming
Model 912 S2 0-233-B2A
Power 98 hp 115 hp
Number of Cylinders 4 4
PROPELLER
Manufacturer Hoffmann GT PROPELLER
Model H017GHM GT 2
Number of Blades 2 2
Type FIX PITCH-WOOD FIX PITCH-WOOD
DESIGN WEIGHT & LOADING
MTOW 600 kg 1320 lb 630 kg 1388 lb
Standard Equip. Empty Weight 360 kg 795 lb 390 kg 860 lb
Standard Equip. Useful Weight 245 kg 540 lb 240 kg 530 lb
Baggage Allowance 20 kg 44 lb 20 kg 44 lb
Limit Loads +3,8 /-1,9G
Ultimate Loads +5,7 /-2,85G
DIMENSION
Fuselage Height 2,5 m 8,2 ft
Fuselage Length 6,4 m 21 ft
Wing Span 8,7 m 28,5 ft
Cabin Width 1,11 m 3,6 ft
Cabin Height SEAT TO COVER 0,91 m 3 ft
Fuel Tank Capacity 45 X2 lt 11,2 X2 GAL
PERFORMANCE 15°C SEA LEVEL 600KG / 1320LB 15°C SEA LEVEL 630KG / 1388LB
VMAX 222 Km/h 120 KTS 240 Km/h 130 KTS
Cruise Speed 75% 200 Km/h 108 KTS 220 Km/h 118 KTS
VNE 261 Km/h 141 KTS 261 Km/h 141 KTS
Stall Speed FLAPS DOWN POWER OFF 76 Km/h 41 KTS 78 Km/h 42 KTS
Practical Ceiling 4572 m 15000 ft 4400 m 14500 ft
Takeoff Run 120 m 394 ft 190 m 625 ft
Takeoff Distance 250 m 820 ft 295 m 970 ft
Landing Run 120 m 394 ft 170 m 560 ft
Landing Distance 302 m 991 ft 350 m 1150 ft
Rate of Climb 5,6 m/sec 1100 ft/min 6,1 m/sec 1200 ft/min
Range 493 N.M

The P92-JS is a two-seater side by side, single strut braced, high wing aircraft. The aircraft's outstanding performance and flying qualities together with low operating costs, easy piloting and maintenance, make this aircraft an excellent choice for flying schools and training activities and also for many other missions such as touring, territory surveillance, patrol, etc.

The option to use AVGAS 100LL or unleaded MOGAS ASTM D4814-EN/228 SUPER make the P92 JS even more flexible and economical. The P92-JS has been type certified in December 2001 in compliance with CS-VLA. The engine and propeller are certified to FAR 33.

Several well known research institutes have chosen the JS as a platform for research into automated systems for conducting flight and environmental research and are very satisfied with it.


Certified Single Engine

Technical Specification

ENGINE
Manufacturer Rotax
Model 912 S2
Power 100 hp
Number of Cylinders 4
PROPELLER
Manufacturer Hoffmann
Model H017GHM
Number of Blades 2
Type FIX
DESIGN WEIGHT & LOADING
MTOW 600 kg 1320 lb
Standard Equipped Weight 360 kg 790 lb
Standard Useful Load 240 kg 530 lb
Ultimate Loads +5.7 / -2.9G
Baggage Allowance 20 kg 44 lb
DIMENSION WING
Fuselage Length 6,63 m 21,7 ft
Fuselage Height 2,4 m 7,9 ft
Wing Span 8,6 m 28,2 ft
Wing Area 11,5 m² 124 sqft
Fuel Tank Capacity 50 X2 lt 13,2 X2 GAL
PERFORMANCE MTOW 450KG/990LB SPEED
Maximum at Sea Level, Gross Weight 222 km/h 120 kts
Cruise, 75% power 210 km/h 113 kts
VNE 256 km/h 138 kts
STALL SPEED
Flaps up, power off 83 km/h 45 kts
Flaps Down, power off 72 km/h 39 kts
Service Ceiling 4500 m 14,800 fts
Rate of Climb at Sea level 1100 ft/m
TAKEOFF PERFORMANCE
Ground roll 140 m 460 ft
Total over 50 fr obstacle 310 m 1017 ft
LANDING PERFORMANCE
Ground roll 140 m 460 ft
Total over 50 fr obstacle 326 m 1070 ft

The P2002-JF is a two-seater side by side, low wing aircraft. The JF P2002 features superlative performance and flying qualities, now confirmed by hundreds of P2002 ultralights sold throughout the world. The ease of piloting and maintenance make this aircraft an excellent solution for training in flight schools but also an ideal platform for surveillance and patrolling territory as well as, of course, for pure recreational use. The option to use AVGAS 100LL or unleaded MOGAS ASTM D4814-EN/228 SUPER make this airplane even more flexible and economical.

The P2002-JF represents the latest development of the Tecnam aircraft as result of the aircraft continuous improvement, the use of advanced software for design, the structural and fluidynamics analysis. Thanks to the tapered laminar flow airfoil and the sloned flaps the P2002 an outstanding aircraft, with the perfect mix of aerodynamic and structural efficiency.


Certified Single Engine

Technical Specification

ENGINE
Manufacturer Rotax
Model 912 S2
Power 98 hp
Numbers of cylinders 4
PROPELLER
Manufacturer Hoffmann
Model H0V352
Number of Blades 2
Type Variable Pitch
Design Weight & Loading
MTOW 620 Kg 1367 lb
Standard Equip. Empty Weight 390 Kg 860 lb
Standard Equip. Useful Weight 230 Kg 507 lb
Baggage Allowance 20 Kg 44 lb
Limit Loads +3,8/-1,9 G
Ultimate Loads +5,7/-2,85 G
Dimension
Fuselage Height 2,35 m 7,7 ft
Fuselage Length 6,61 m 21,7 ft
Wing Span 8,6 m 28,2 ft
Cabin Weight 1,11 m 3,6 ft
Cabin Height SEAT TO COVER 0,91 m 3 ft
Fuel Tank Capacity 50 X2 lt 13,2 X2 Gal
Performance 15°C Sea level 620 Kg / 1367 lb
VMAX 250 Km/h 135 KTS
Cruise Speed 75% 226 Km/h 122 KTS
VNE 267 Km/h 144 KTS
Stall Speed FLAPS DOWN POWER OFF 72 Km/h 39 KTS
Rate Of Climb 5,6 m/sec 1100 ft/min
Practical Ceiling 4572 m 15000 ft
Take Off Run 150 m 492 ft
Take Off Distance 350 m 1148 ft
Landing Run 142 m 466 ft
Landing Distance 326 m 1070 ft
Range 636 N.M.

The P2002-JR is a two-seater side by side, low wing aircraft with retractable landing gear. The P2002-JR features superlative performance and flying qualities, now confirmed by hundreds of P2002's and P2002 RG's flying all over the world. The ease of piloting and maintenance make this aircraft an excellent solution for training with flight schools but also an ideal platform for surveillance and patrolling territory as well as, of course, for pure recreational tourism.

The option to use AVGAS 100LL or unleaded MOGAS ASTM D4814-EN/228 SUPER make the P2002 JR even more flexible and economical. The P2002-JR represents the latest development of the Tecnam aircraft as result of the aircraft's continued improvement, the use of advanced software for design with structural and fluidynamic analysis.

Thanks to the tapered wing, the laminar airfoils, the sloned flaps and the streamline fuselage together with the retractable gear, the P2002-JR is an outstanding aircraft, with the perfect mix of aerodynamic and structural efficiency.


Certified Single Engine

Technical Specification

ENGINE
Manufacturer Rotax
Model 912 S2
Power 98 hp
Numbers of cylinders 4
PROPELLER
Manufacturer Gt Propeller
Model GT-2 / 173 / VRR-F
Number of Blades 2
Type FIXPIT H-WOODC
Design Weight & Loading
MTOW 620 Kg 1367 lb
Standard Equip. Empty Weight 370 Kg 816 lb
Standard Equip. Useful Weight 250 Kg 551 lb
Baggage Allowance 20 Kg 44 lb
Limit Loads +4/-2 G
Ultimate Loads +6/-3 G
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 Weight 1,2 m 3,9 ft
Cabin Height SEAT TO COVER 0,91 m 3 ft
Fuel Tank Capacity 55 X2 lt 14,5 X2 Gal
Performance 15°C Sea level 620 Kg / 1367 lb
VMAX 225 Km/h 122 KTS
Cruise Speed 75% 216 Km/h 117 KTS
VNE 263 Km/h 142 KTS
Stall Speed FLAPS DOWN POWER OFF 68 Km/h 37 KTS
Practical Ceiling 4572 m 15000 ft
Take Off Run 140 m 459 ft
Take Off Distance 300 m 984 ft
Landing Run 135 m 443 ft
Landing Distance 320 m 1050 ft
Range 628 N.M.

Carbon fiber meets metal with innovation, style, and advanced technology to create a new aircraft line by Tecnam. The latest addition to the Tecnam line is the P2008 CS-VLA. The Tecnam lineage is apparent the P2008JC CS-VLA which includes several exciting additions.

The P2008JC CS-LSA has metal wings and a metal stabilator. Tecnam chose to keep the metal wing and stabilator structures for strength, reliability, and ability to flex in flight providing a more comfortable ride. To produce the desired increase in cabin width and greater aerodynamic efficiency, Tecnam chose carbon fiber.

The decision to utilize both materials was for the optimization of aerodynamic qualities, flight characteristics, and reliability. The powerplant and associated cowlings are similar to all of the existing Tecnam line with few modifications. The P2008 CS-VLA has higher capacity than the existing line (55x2 lt - 14,5x2 GAL) and fuel tanks are installed in the wing box, behind the main spar. This is to preserve their integrity in case of a crash landing and to minimize fire potential. The instrument panel size is increased from other Tecnam models due to the increase in cabin width. It is modular in design and can accommodate the most complete instrumentation, analogical or digital type.


Certified Single Engine

Technical Specification

Design Weight & Loading
Takeoff Weight 1,160 Kg 2,557 lb
Landing Weight 1,157 Kg 2,550 lb
Standard Empty Weight 710 Kg 1,565 lb
Maximum Useful Load 450 Kg 992 lb
Baggage Allowance 88,3 ft³ 2,5 m³
Fuel Capacity 210 L 55.5 Gal
Performance
Service Ceiling 15.000 ft L
Max Climb Rate S.L 1050 fpm
Max Speed S.L 140 kts
Max Range 660 nm
Cruise Speed (75% pwr at 6.500 ft) 133 kts
Cruise Range and Endurance (75% pwr at
6.500 ft)
545 nm
Landing Distance (To Clear 50 ft Obstacle) 140 kts
Landing Distance (Ground Roll) 1027 ft 313 m
Takeoff Distance S.L. (Ground Roll) 804 ft 245 m
Takeoff Distance S.L. (To Clear 50ft. Obstacle) 1260 ft 384 m

The Tecnam P Twenty-Ten brings together an advanced technology all carbon fibre fuselage with a metal wing to deliver a superlative single engined, 4 seat aeroplane, designed by Italy's most innovative Aerospace design 'guru' Professor Luigi Pascale.

Powered by the well proven and reliable Lycoming IO-360-M1a ('Lycoming Light') engine, providing 180HP and 2700RPM. The Tecnam P Twenty-Ten has a high fuel capacity (240 litres). The fuel tanks are installed in the wing box, behind the main spar, to preserve their integrity in case of an accident. Of course carbon fibre equals a lighter and therefore more fuel efficient aeroplane.

Tecnam has always put the comfort for both pilots and passengers first. The Tecnam P Twenty-Ten with its spacious interior and its generous luggage compartment of 300 litres has been designed to be both a very enjoyable aeroplane to fly cross country as well as a robust trainer. The cabin width also allows for a large instrument panel, with its modular design specifically tailored to allow customers to fit either an analogue or digital instrumentation package.

The 12th of April has made its Maiden Flight which was extremely successful.