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family of two-seat, high-wing , light aircraft
Tecnam P92 is a family of two-seat, high-wing , light aircraft originating in Italy. It was built by Tecnam.
Two-seat ultralight monoplane
Italy
Tecnam
Luigi Pascale
In production
14 March 1993
2
6.4 m (21 ft 0 in)
8.7 m (28 ft 7 in)
2.5 m (8 ft 2 in)
356 kg (785 lb)
600 kg (1,323 lb)
90 L (24 US gal; 20 imp gal) total with 80 L (21 US gal; 18 imp gal) usable
1 × Rotax 912ULS 4-cylinder air-cooled horizontally-opposed piston engine, 73.5 kW (98.6 hp)
2-bladed Sensenich
213 km/h (132 mph, 115 kn) Max cruise speed TAS
72 km/h (45 mph, 39 kn) flaps down
1,296 km (805 mi, 700 nmi)
4.9 m/s (960 ft/min)
214 m (702 ft)
154 m (505 ft)
369 m (1,211 ft)
The Tecnam P92 is a family of two-seat, high-wing , light aircraft designed by Luigi Pascale and manufactured by Tecnam in Capua , Italy .
Today, the P92 Echo MkII, features a strut-braced high wing, fixed tricycle landing gear, and side-by-side seating. Its airframe is primarily metal, with a composite (carbon‑fibre) fuselage, while earlier versions had all‑metal construction. It is powered by Rotax 912ULS series engines with 100 hp. The P92 Echo MkII has a published stall speed of approximately 39 knots (72 km/h) with full flaps, and a take-off distance of 1211ft (369 metres).
The P92 prototype conducted its maiden flight on 14 March 1993 in Capua and shortly after debuted at the Bassano del Grappa Air Show. The P92 progressively entered service with a wide range of flying clubs and pilot training institutions. Throughout its development, Tecnam released multiple versions, such as the P92-J, P92 Echo Super, P92 Eaglet, and P92 MkII, each incorporating gradual upgrades in avionics, aerodynamics, construction materials (including the introduction of composite fuselages), and cockpit ergonomics. As reported by aviation journalist Dan Johnson, by 2018 more than 2,500 units had been delivered globally, making the P92 Tecnam’s most produced aircraft to date.
The aircraft is powered by a 100 hp Rotax 912ULS four-stroke engine in tractor configuration, and is equipped with a fixed-pitch propeller. According to published specifications, the Echo MkII has a stall speed of approximately 39 knots (72 km/h) with full flaps and a take-off distance of 1,211 ft (369 m) under standard atmospheric conditions.
The P92 Echo MkII is available in different configurations to comply with both European ultralight regulations (MTOW 472.5 kg) and US light-sport aircraft (LSA) standards (MTOW up to 600 kg). It is included in the list of FAA-accepted Special Light-Sport Aircraft (S-LSA) and is certified under various national civil aviation authorities.
An upgraded version of the P92-J with 100 hp (75 kW) Rotax 912S . Changes include shortened wings, metal flaps, redesigned engine cowling and fairings.
Available with 80 hp (60 kW) Rotax 912UL or 100 hp (75 kW) Rotax 912ULS engine.
Redesigned wings, engine cowling, windshield and fairing to reduce drag. Available with 81 hp (60 kW) Rotax 912U or 100 hp (75 kW) Rotax 912S .
With 100 hp (75 kW) Rotax 912ULS .
An upgraded version of the Echo. Available with 81 hp (60 kW) Rotax 912U .
Fuselage redesigned, shorter wingspan, retractable landing gear. With 100 hp (75 kW) Rotax 912S engine.
100 hp (75 kW) Rotax 912 engine, adds winglets to improve aerodynamic efficiency
Tricycle landing gear equipped version with a gross weight of 500 kg (1,102 lb)
Length: 6.4 m (21 ft 0 in)
Wingspan: 8.7 m (28 ft 7 in)
Height: 2.5 m (8 ft 2 in)
Empty weight: 356 kg (785 lb)
Max takeoff weight: 600 kg (1,323 lb)
Powerplant: 1 × Rotax 912ULS 4-cylinder air-cooled horizontally-opposed piston engine, 73.5 kW (98.6 hp)
Maximum speed: 213 km/h (132 mph, 115 kn) Max cruise speed TAS
Stall speed: 72 km/h (45 mph, 39 kn) flaps down
Range: 1,296 km (805 mi, 700 nmi)
Rate of climb: 4.9 m/s (960 ft/min)
Take-off run: 214 m (702 ft)
Landing run: 154 m (505 ft)
Take-Off Distance: 369 m (1,211 ft)
Reference text from Wikipedia contributors, used under CC BY-SA 4.0.
Tecnam P92 equipment records. Variants, orders and quantities are shown as reported in each inventory source; coverage is incomplete.
CambodiaAir Force exact named equipment holdings: P-92 Echo (pilot trg/recce). Active, operational-reserve and training units excluding equipment in store; November 2025 IISS assessment. Named service only; no parent-force or national total inferred. Source role: AIRCRAFT / Light. Original estimates, ranges, reporting names, reserve, lease and employment scopes retained; nested included counts are not added. Missile-system quantities mean launchers, not rounds. No readiness, crew, carried weapon, payload, factory-production or future order count inherited.