The History began here

The Tecnam P92 Echo Classic Deluxe is an all metal, two seat , single strut braced high wing aeroplane. It is one of the most successful and popular aeroplanes produced by Tecnam.
With a choice of powerplants, either the 100 HP Rotax 912ULS or the80 HP Rotax 912UL, the P92 Echo Classic range will climb at 1200 ft/m and cruise on 75% power at 207km/h.
With its spacious interior, its generous 20 kgs of luggage space coupled with superb visibility is a very enjoyable aeroplane to fly cross country. It has also proved itself a robust trainer.

The P92’s excellent flying characteristics, with neutral handling makes it extremely stable and easy to fly for people of any weight/height. This features has established it as a popular choice for many Flight School aircraft fleets.
The large flaps are deployed electrically. Its low stall speed and general slow flying characteristics allow the P92 Classic to operate with ease on short runways.

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
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
Pitot System
Static System
Stabilator Trim Position Indicator

Engine Instruments

Tachometer
Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Press.
Voltmeter
Lh + Rh Fuel Qty
Trim Indicator
Flap Indicator

Electrical system

12 Volt 18A Amp. Battery
12 Volt Alternators-20 Amp.
Switches
_Landing Light
12 Volt Socket
Circuit Breakers Panel

Fuel system

Two Integral Fuel Tanks With 95 Litres
Total Capacity
Engine Driven Fuel Pump
Fuel Quick Drain

Interior

Pilot And Copilot Seats
_ Adjustable Fore And Aft
_Arm Rest
Seat Belts & Shoulder Harness, All Seats
Wall To Wall Carpeting
Map and Storage Pockets
Luggage Compartments

Powerplant and Propeller

Engine – 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, 2 Blades Fixed
Propeller Spinner
Air Filter
Oil Filter
Oil And Water Coolers

Exterior

Rear Window
All Lateral And Rear Windows Tinted Brown
Tie Down Rings
Main Wheels, 5,00 X 5
Nose Wheel, 5,00 X 5
Wheel Pants

Exteriors lights

Taxi Light

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	9,30 mt – 30.5 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	2 x 45 lt – 2 x 11,9 US GAL

Powerplant

Engine Manufacturer	Rotax 912 ULS
Engine Power	80 / 98 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	600 kg – 1323 lb

Performance

Max Cruise Speed (KTAS)	219 km/h – 118 kts
Stall Speed (Flaps Down Power Off) KCAS	65 km/h – 35 kts
Practical ceiling	4..267 mt – 14,000 ft
Take off run	140 mt – 459 ft
Take off distance	260 mt – 853 ft
Landing Run	110 mt – 360 ft
Landing Distance	250 mt – 820 ft
Rate of climb	6.1 m/sec – 1200 ft/min
Range	503 NM – 931 km

Specifications subject to change without notice. Always consult the Aircraft Flight Manual.

P92 Classic De Luxe