P92 Light
P92 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.
Contacteaza-ne acum la 021-22.22.55.4!
Cere o oferta de pret!
Max Range
Fuel Capacity 45 x1 lt - 11,9 x1 US Gal (Opt. 2nd 45lt tank)
Max Speed
190 km/h
Seating
Two seats side by side.
Fuel Consumption
Only 4.5 US Gal per hour, AVGAS and MOGAS Automotive Fuel
Exteriors
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
Tachometer
Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Qty Indicator
Fuel system
One Integral Fuel Tank With 45 Litres Total Capacity
Fuel Quick Drain
Interiors
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 – Gt Propeller, 2 Blade Fix
Propeller Spinner
Air Filter
Oil Filter
Oil And Water Coolers
Exterior
Rear Window
Tie Down Rings
Main Wheels, 4,00 X 4
Nose Wheel, 4,00 X 4
Exteriors lights
Cabin comfort system
Ventilator Adjustable, 2 Place
Product Support/Documents
Manufacturers Full Two Year Limited Warranty
Pilots Operation Handbook
Maintenance Manual
Specification
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 |
Powerplant
| 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
| Maximum Take Off Weight | Design Weight: 500 kg – 1100 lb |
| Std. Empty Weight | |
| Useful Load | |
| Baggage allowance | 20 kg – 44 lb |
Performance
| Vmax | 190km/h – 103 kts |
| Cruise Speed 75% | 170 km/h – 92 kts |
| Stall Speed (Flaps Down Power Off) | 63 km/h – 34 kts |
| Pratical ceiling | 3660 mt – 12000 ft |
| Take off run | 100 mt – 328 ft |
| Take off distance | 260 mt – 852 ft |
| Landing Run | 100 mt – 328 ft |
| Landing Distance | 260 mt – 852 ft |
| Rate of climb | 4,5 m/sec – 885 ft/min |
| Range | 270 NM |
| Flight Rule |