P92 Echo Light

Light, only in weight. The Tecnam P92 Light is a high wing, two place, single engine light airplane equipped with tricycle landing gear. But is not only that. The P92 Light is the plane that gave wings to thousands of pilots.
Categories: Advanced Ultralight

The History began here

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.

Interiors Details

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!

Standard Equipment

Flight Controls

Hydraulic Brakes Hand Lever
Parking Brake
Electrical Flaps
Dual Flight Controls
Steerable Nose Wheel
Stabilator Trim (Between The Seats)
Engine Controls
– Throttle, Two
– Choke
Flight Trim Controls
– Stabilator With Indicator
Fuel Control Selector With On/Off
Panel Switches:
– Starter
– Engine Lh And Rh Ignition Switches

Flight instruments and indicators

Magnetic Compass
Airspeed Ind., Kts
Altimeter (In)
Vertical Speed
Bank Indicator
Flaps Indicator
Pitot System
Static System
Stabilator Trim Position Indicator


Engine Instruments

Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Qty Indicator

Electrical system

12 Volt 18A Amp. Battery Light 1 Kg
12 Volt Alternators-20 Amp.
12 Volt Socket
Circuit Fuses Panel

Fuel system

One Integral Fuel Tank With 45 Litres Total Capacity
Fuel Quick Drain


Pilot And Copilot Carbon Fiber Seats With Cushion
Adjustable Fore And Aft
Seat Belts & Shoulder Harness, All Seats
Light Interiors With Carpet
Luggage Compartments


Powerplant and Propeller

Engines – 1 Rotax 912Ul 80 Hp, 4 Cylinders
Liquid/Air Cooled, Integrated Reduction Gear
Dual Ignition System
Throttle Control Lh/Rh
Tubular Steel Engine Mount
Propeller – Sensenich Propeller, 2 Blade Fix
Propeller Spinner
Air Filter
Oil Filter
Oil And Water Coolers


Rear Window
Tie Down Rings
Main Wheels, 4,00 X 4
Nose Wheel, 4,00 X 4
Cabin Confort System
Ventilator Adjustable, 2 Place


Product Support/Documents

Manufacturers Full Two Year Limited Warranty
Pilots Operation Handbook
Maintenance Manual


Aircraft Dimensions

Fuselage Height 2.5 mt – 8.2 ft
Fuselage Length 6,3 m 21 ft
Wingspan 8.70 mt – 28.5 ft
Cabin Height (seat to cover) 0.91 mt – 3 ft
Cabin Width 1,06 mt – 3,5 ft
Max Seating capacity 2
Fuel tank capacity 45 lt – 11,9 US GAL


Engine Manufacturer Rotax 912 UL
Engine Power 80 hp
Time Before Overhaul 2000 hrs
Propeller Two-Bladed Fixed Pitch
Fuel Consumption  
Fuel Type Mogas and Avgas

Design Weight & Loading

Baggage allowance 20 kg – 44 lb
Design Weight 500 kg – 1100 lb



Max Cruise Speed (KTAS) 190 km/h –  103 kts
Stall Speed (Flaps Down Power Off) KCAS 63 km/h – 34 kts
Practical ceiling 3660 mt – 12000 ft
Take off run 100 mt – 328 ft
Take off distance 230 mt – 755 ft
Landing Run 100 mt – 328 ft
Landing Distance 250 mt – 820 ft
Rate of climb 885 ft/min – 4,5 m/sec
Range 270 NM – 500 km