Tecnam P92

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P-92 Eaglet

The Tecnam P92 Echo and Tecnam P92 Eaglet are high-winged, light aircraft built by the Tecnam aircraft company, which is based in Naples, Italy.^[1]

Variants

Tecnam P92 Taildragger

P92 JS: An upgraded version of the P92-J with 100 hp Rotax 912S. Changes include shortened wings, metal flaps, redesigned engine cowling and fairings.
P92 LY: As P92 JS but with Lycoming YO-233-B2A engine instead of Rotax
P92 Echo: Available with 80 hp or 100 hp Rotax 912 engine.

Tecnam P92 SEASKY

P92 SEASKY: Amphibian version (conventional floats with retractable wheels) of the P92 Echo.
P92 S Echo: Redesigned wings, engine cowling, windshield and fairing to reduce drag. Available with 81 hp Rotax 912U or 100 hp Rotax 912S.
P92 Echo Super: With 100 hp Rotax 912ULS.
P92 J: An upgraded version of the Echo. Available with 81 hp Rotax 912U.

P92 2000RG: Fuselage redesigned, shorter wingspan, retractable landing gear. With 100 hp Rotax 912S engine.
P92 Eaglet: 100 hp Rotax 912 engine, adds winglets to improve aerodynamic efficiency
P92 Eaglet G5: As P92 Eaglet but with free-castering nosewheel instead of steerable
P92 Eaglet LY: As P92 Eaglet G5 but with Lycoming YO-233-B2A engine instead of Rotax
P92 TD: A conventional geared (Taildragger) compliant with American Light Sport rules.^[2]

Operators

Civil

The P92 is popular with flight training schools and is also operated by private individuals and companies.

Military

Cambodian Air Force

Specifications (P92 Echo Super)

Data from http://www.tecnam.com/ing/echosuper.cfm

General characteristics

Crew: one, pilot
Capacity: one passenger
Length: 6.40 m (20 ft 11 in)
Wingspan: 8.70 m (28 ft 6 in)
Height: 2.50 m (8 ft 3 in)
Wing area: 12 m2 (129 ft2)
Empty weight: 670 lbs (304 kg)
Useful load: 650 lbs (295 kg)
Max. takeoff weight: 1,212 lbs (550 kg)
Powerplant: 1 × Rotax 912ULS, 100 hp (73.5 kW)

Performance

Never exceed speed: 270 km/h (168 mph)
Maximum speed: 235 km/h at sea-level (124 kts)
Cruise speed: 215 km/h (105 kts)
Stall speed: 63 km/h (33 kts)
Range: 800 km (500 mi)
Service ceiling: 4500 m (14,760 ft)
Rate of climb: 354 m/min (1,161 ft/min)
Take off run: 100 m (328 ft)
Landing distance: 100 m (328 ft)
Complies with JAR-VLA airworthiness regulations

References

↑ Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 80. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
↑ "Tecnam to Produce P92 Tail Dragger". Retrieved 6 August 2012.

External links

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