Tecnam P92

Tecnam

Industry	Aerospace
Founded	1986 (1986)
Founder	Luigi Pascale
Headquarters	Capua , Italy
Products	Light aircraft, including Tecnam P92 series

Tecnam P92

The Tecnam P92 series consists of two-seat, high-wing light aircraft engineered by Luigi Pascale and produced by Tecnam at their facility in Capua, Italy.

Introduced to the market in 1993, this ultralight aircraft was designed specifically for the ultralight aviation segment. Since its debut, it has become one of Tecnam's most extensively manufactured models, with over 2,500 units operational as of 2018.

The P92 has found widespread application in recreational flying and as a primary trainer across Europe, North America, and various other regions. Over the years, the model has undergone several iterations, including variants such as the Echo, Echo Super, JS, and Eaglet. The current production model, known as the P92 Echo MkII, was launched in 2016.

The P92 Echo MkII features a strut-supported high wing configuration with fixed tricycle landing gear and accommodates two occupants seated side-by-side. Its structure predominantly utilizes metal components combined with a carbon-fiber composite fuselage, whereas earlier versions were constructed entirely from metal. Power is supplied by the Rotax 912ULS engine series, delivering 100 horsepower. The aircraft boasts a stall speed near 39 knots (72 km/h) when fully flapped and requires a takeoff run of approximately 1,211 feet (369 meters).

Development

The P92 marked Tecnam's inaugural aircraft conceived and produced entirely in-house. Prior to the 1990s, Tecnam's operations were focused on manufacturing components for other aerospace firms, including Aeritalia and McDonnell Douglas. The enactment of Italian Law 106/1985, which authorized recreational flying with ultralight aircraft and opened fresh commercial prospects, inspired Tecnam to revisit a previous Luigi Pascale design. This effort resulted in the development of the Tecnam P92, a two-seat, high-wing, all-metal ultralight crafted for both private pilots and flight training purposes.

The prototype of the P92 took to the skies for its first flight on 14 March 1993 in Capua, shortly followed by its presentation at the Bassano del Grappa Air Show. Over time, the P92 was adopted by numerous flying clubs and pilot training centers. Throughout its evolution, Tecnam introduced several variants including the P92-J, P92 Echo Super, P92 Eaglet, and P92 MkII. Each iteration featured incremental improvements in avionics, aerodynamic design, materials—such as the integration of composite fuselages—and cockpit comfort enhancements. Aviation expert Dan Johnson noted that by 2018, global deliveries had surpassed 2,500 units, establishing the P92 as Tecnam’s most extensively produced model.

Design

The latest iteration of the P92 series is the Echo MkII, launched in 2016 and currently the sole version in production. While it retains the classic features such as a strut-supported high wing, side-by-side seating arrangement, and fixed tricycle landing gear, this version incorporates structural enhancements and ergonomic refinements compared to earlier models.

The Echo MkII’s fuselage employs carbon-fiber composite materials that reduce overall weight while enhancing structural integrity. Meanwhile, its wings and tail remain crafted from aluminum alloy. This combination provides durability suited for rigorous training use alongside the benefits of composite materials’ weight reduction and design flexibility. The landing gear is fixed and reinforced to withstand frequent takeoff and landing cycles typical of flight school operations.

The cockpit has been redesigned to enhance pilot visibility, noise insulation, and overall comfort. It supports both traditional analog instrumentation and modern glass cockpit avionics setups, including optional systems like the Garmin G3X Touch. Entry is facilitated by spacious side doors, with seating configured for two occupants seated side-by-side.

Powering the aircraft is a 100 hp Rotax 912ULS four-stroke engine arranged in a tractor configuration paired with a fixed-pitch propeller. Published performance data indicate a stall speed near 39 knots (72 km/h) when full flaps are deployed and a takeoff roll measuring approximately 1,211 feet (369 meters) under standard atmospheric conditions.

The P92 Echo MkII is offered in multiple configurations to meet regulatory requirements for European ultralight aircraft (maximum takeoff weight of 472.5 kg) as well as US light-sport aircraft (LSA) standards allowing up to 600 kg MTOW. It is listed among FAA-certified Special Light-Sport Aircraft (S-LSA) and holds certifications from various national civil aviation authorities.

Variants

File:TecnmamP92TD.jpg

Tecnam P92 Taildragger

P92-JS

This model is an enhanced variant of the P92-J, featuring a 100 hp (75 kW) Rotax 912S engine. Modifications include reduced wingspan, metal flap surfaces, and a redesigned engine cowling along with updated fairings.

P92-LY

Similar to the P92-JS but powered by a Lycoming IO-233-B2A engine instead of the Rotax.

P92 Echo

Offered with either an 80 hp (60 kW) Rotax 912UL or a 100 hp (75 kW) Rotax 912ULS powerplant.

File:P92-SEASKY.jpg

Tecnam P92 Sea-Sky

P92 Sea-Sky

An amphibious variant of the P92 Echo equipped with traditional floats that incorporate retractable wheels.

P92-S Echo

Features redesigned wings, engine cowling, windshield, and fairings aimed at reducing aerodynamic drag. Engine options include an 81 hp (60 kW) Rotax 912U or a 100 hp (75 kW) Rotax 912S.

P92 Echo Super

Powered by a 100 hp (75 kW) Rotax 912ULS engine.

P92-J

An advanced version of the Echo model, equipped with an 81 hp (60 kW) Rotax 912U engine.

P92 2000RG

Features a redesigned fuselage, shortened wingspan, and retractable landing gear. It is powered by a 100 hp (75 kW) Rotax 912S engine.

P92-JS

P92 Eaglet

Equipped with a 100 hp (75 kW) Rotax 912 engine and includes winglets to enhance aerodynamic efficiency.

P92 Eaglet G5

Similar to the P92 Eaglet but fitted with a free-castering nosewheel instead of a steerable one.

P92 Eaglet G5LY

Based on the P92 Eaglet G5 but powered by a Lycoming IO-233-B2A engine replacing the Rotax unit.

P92-TD

Taildragger model with conventional landing gear, designed to meet American Light Sport Aircraft regulations. It had its maiden flight on 22 December 2011 and was unveiled at Sun 'n Fun in 2012.

P92 Echo Light Classic

A version equipped with tricycle landing gear and a maximum gross weight of 500 kg (1,102 lb).

Civil

The P92 series enjoys widespread use among flight training organizations and is also operated by private owners and corporate entities.

Military

• Cambodian Air Force

Specifications (P92 Echo MkII)

{{Aircraft specs | ref = P92 latest infopage | prime units? = met | crew = 2 | length m = 6.4 | length note = | span m = 8.7 | span note = | height m = 2.5 | height note = | wing area sqm = | wing area note = | aspect ratio = | airfoil = | empty weight kg = 356 | empty weight note = | gross weight kg = | gross weight note = | max takeoff weight kg = 600 | max takeoff weight note = | fuel capacity = 90 L (24 US gal; 20 imp gal) total capacity with 80 L (18 imp gal; 21 US gal) usable fuel volume | eng1 number = 1 | eng1 name = Rotax 912ULS | eng1 type = Four-cylinder air-cooled horizontally opposed piston engine | eng1 kw = 73.5 | eng1 note = | prop blade number = 2 | prop name = Sensenich | prop dia m = | prop dia note = | max speed kmh = 213 | max speed note = Maximum true airspeed cruise | max speed mach = | cruise speed kmh = | cruise speed note = | stall speed kmh = 72 | stall speed note = With flaps deployed | never exceed speed kmh = | never exceed speed note = | range km = 1296 | range note = | combat range km = | combat range note = | ferry range km = | ferry range note = | endurance = | ceiling m = | ceiling note = | g limits = | roll rate = | glide ratio = | climb rate ms = 4.9 | climb rate note = | time to altitude = | wing loading kg/m2 = | wing loading note = | fuel consumption kg/km = | power/mass = | more performance =

• Take-off run: 214 m (702 ft)
• Landing run: 154 m (505 ft)
• Take-Off Distance: 369 m (1,211 ft)

|}

External links

• Official website