ADV ULTRALIGHT
P92 Echo Classic De Luxe
The P92 Echo Classic is a two-seat, single strut braced high wing aircraft.

The P92 Echo Classic was designed and manufactured according to the international airworthiness standards. This has been accomplished by one of the most renowned European Designers in the general aviation field, with the aid of modern planning instruments.

The P92’s performance and flying qualities are so superior that it compares to aircraft certified under FAR/CS 23.

The excellent flying characteristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height.

The large flaps are deployed electrically. The low stall speed and the general slow flying characteristics of the aircraft allow it to operate with ease on short runways.
Construction
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The Tecnam line employs a monocoque construction style using sheet aluminium over steel tubing.
The wing is all aluminium and constructed in a conventional way with a single spar and metal torsion box.
The airfoil is a Gottinga 398 modified for better low speed handling characteristics.
The fuel tanks hold 11.9 gal/45 lt in each wing and are located in the leading edge separated from the fuselage for safety.
A rear window completes the extraordinary visibility allowing 360° of vision in the cockpit.
The stabilator provides remarkable longitudinal hands-off stability along with minimum drag and weight penalty providing balanced, 2 finger, flight control.
The wide flaps, electrically activated, allow stall speed lower than 33 Kts.
The Echo Classic has 35 degrees of flaps making steep approach landings easier.
 
Interior And Outdoor
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Seats are adjustable in flight and increase in height as they are moved forward.
The luggage area allowing for 44 pounds/20 kg of weight is located behind the seats with ample room for several travel bags.
All Tecnam aircraft have dual control sticks with a curve at the base for ease of ingress and egress.
The dual controls come standard with PTT.
The interior is spacious, ergonomic and comfortable.
Dual throttles allow the pilot to fly either left or right handed.
The fresh air vents are conveniently located in the doors.
All Tecnam aircraft provide excellent forward visibility over the cowling.
The planes come with dual conventional rudder pedals with a steerable nose wheel.
The wide instrument panel is designed to accommodate a full variety of instrumentation.
 
Landing Gear
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The main landing gear is spring steel that is robust enough for unimproved strips and requires no service.
The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment.
The main landing gear wheels and brakes are conventional aircraft size (5.00x5).
The brake lever control is located forward between the seats.
A parking brake is between the seats and is actuated by use of a single twist.
 
Engine And Propeller
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The top and bottom engine cowls are quickly and easily removed making any maintenance procedure faster to accomplish.
The top cowl has a large opening for easy access to the engine compartment for effective pre-flight inspections.
The engine is mount is Cro-Moly steel-tubing with shock mounts.
The firewall is soundproofed.
Two power plant options are available: Rotax 912UL 80HP four-cylinder, four-stroke engine and Rotax 912 ULS 100HP four-cylinder, four-stroke engine.
The engine is a liquid and air cooled engine with an integrated 1:2.4286 reduction gear.
A fixed pitch wood and composite propeller comes standard.
The quick drain gascolator is installed in the engine compartment with easy access.
The battery is located in the rear of the fuselage with easy access through a hinged door.
 
Standard Equipment
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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 DYNON D10 include:
TACHOMETER
HOUR RECORDER
OIL PRESS
OIL TEMP.
HEAD TEMP.
FUEL PRESS.
VOLTMETER
LH + RH FUEL QTY
TRIM INDICATOR
FLAP INDICATOR
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
 
ELECTRICAL SYSTEM
12 VOLT 18A AMP. BATTERY
12 VOLT ALTERNATORS-20 AMP.
SWITCHES
- Landing Light
12 VOLT socket
CIRCUIT FUSES PANEL
FUEL SYSTEM
TWO INTEGRAL FUEL TANKS WITH 100 LITRES
ENGINE DRIVEN FUEL PUMP
FUEL QUICK DRAIN
INTERIOR
PILOT and CO-PILOT SEATS
- Adjustable Fore and Aft
- Arm Rest
SEAT BELTS & Shoulder Harness, All Seats
WALL TO WALL CARPETING
MAP E STORAGE POCKETS
LUGGAGE COMPARTMENTS
 
EXTERIOR
REAR WINDOW
ALL WINDOWS TINTED
TIE DOWN RINGS
MAIN WHEELS, 5,00 X 5
NOSE WHEEL, 4,00 X 6
WHEEL PANTS
EXTERIOR LIGHTS
TAXI LIGHT
CABIN CONFORT SYSTEM
VENTILATOR ADJUSTABLE, 2 place
 
POWERPLANT AND PROPELLER
ENGINES - 1 ROTAX 912UL 80/100 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
PRODUCT SUPPORT/DOCUMENTS
MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
PILOT'S OPERATION HANDBOOK
MAINTENANCE MANUAL
 
Photo Gallery Details
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Photo Gallery Flights
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