P92 Classic De Luxe

Timeless Light.

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.

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Quick facts

0NM

Max Range

Fuel Capacity
45 x2 lt – 11,9 x2 US Gal

118 kts

Max Cruise Speed

219 km/h

0

Seating

Two seats side by side

17 l/h

Fuel Consumption

Only 4.5 US Gal  per hour,
AVGAS and MOGAS Automotive Fuel

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 instruments and indicators

• Magnetic Compass
• Airspeed Ind.
• Altimeter Dual Mode (In/Mb)
• Vertical Speed
• Bank Indicator
• Pitot System
• Static System
• Stabilator Trim Position Indicator

Flight controls

• Hydraulic Brakes
• Parking Brake
• Electrical Flaps
• Dual Flight Controls
• Steerable Nose Wheel
• Stabilator Trim (Electric Actuated From Stick)
• Engine Controls:

– Two Throttles
– Choke
• Flight Trim Controls:
– Stabilator With Indicator
• Fuel Control Selector With On/Off

Engine Instruments

Dynon D10 includes:

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

 

Panel switches

• Split Starter
• Avionics Master
• Starter Key Acs

 

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 95Lt\25Usgal Total Capacity
• Engine Driven Fuel Pump
• Fuel Tank Quick Drain , Two

 

Interior

• Pilot And Copilot Seats:
– Adjustable Fore And Aft
• Seat Belts & Shoulder Harness, All Seats • Wall To Wall Carpeting
• Map and Storage Pockets
• Luggage Compartments

Exterior

• Epoxy Corrosion Proofing, All Structure
• Lh/Rh Front Door Pilot/Copilot, Lock And Key
• Rear Window
• All Lateral And Rear Windows Tinted Brown
• Main Wheels, 5,00 X 5
• Nose Wheel, 5,00 X 5
• Wheel Fairing

Exteriors lights

Taxi Light LED

Cabin comfort system

Ventilator Adjustable, 2 Place

 

Powerplant and Propeller

• Engines P 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 P Sensenich, 2 Blade Fix
• Propeller Spinner
• Air Filter
• Oil Filter
• Oil And Water Coolers

 

Product Support/Documents

• Manufacturers Full Two Year Limited Warranty
• Pilots Operation Handbook
• Maintenance Manual
• Parts Catalog

Category Upgrades

C-1002 Advanced

Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:
– Fire Wall Inox
– Radio Garmin GTR 200 Com Installed
– GTX 335 Transponder With GPS Installed
– ELT Kannad 406 Mhz With Antenna & Remote Mounted Switch
– Fire Sleve On Fuel And Oil Tube
– Paracachute 600 Kg

C-1003 US-LSA

Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:

– Fire Wall Inox
– Airspeed Ind., Kts • Panel Switches:
_ Split Starter
_ Avionic
– Starter Key ACS
– Tie Down Rings
– Fire Sleeve On Fuel and Oil Tubes • Thermostatic Valve Oil
– Baggage Compartment Net
– Gull Wing Engine Cowling
– External Power Supply

– Circuit Breakers Panel
– Center Console
– Taxi Light LED
– Wing Strut Larger Size
– Wing Light Green/Red, White and Strobe AVEO Non TSO
– Auxiliary Fuel Pumps, Electric
– Lh Front Door Pilot, Lock and Key
– Windshield Defroster
– Heating System
– Cabin Ceiling, ABS
– Strut Firing
– Trim On The Stick
– Panel Protection Underneath The Seats
• Cloche Protection

Engine Upgrades

C-EUP 01 ROTAX 912 ULS2

912is-d127fb6b
Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:

ENGINE ROTAX 912 ULS2 100HP

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.

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