P92 Echo Classic

advanced ultra light

De Luxe

p92 echo Classic

Specifications

DESIGN WEIGHT & LOADING
Designed MTOW Limit Loads Ultimate Loads Baggage Allowance

+4 / -2 g +6 / 3 g 20 44

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 P92s performance and flying qualities are so superior that it compares to aircraft certified under FAR/CS 23.

Dimension

Wing Span Lenght Over-All Height Over-All Width Cabin Wing Area Transv. Dihedral Tailplane Span Wheel Track Wheel Tyres
9,4 30,8 6,5 21,3 2,5 8,2 1,1 3,6 13,4 m 144 sqft 1,5 2,9 9,5 1,8 5,9 Air Trac 5.00-5 (main gear) rotax 100 HP rotax 80 HP 73.5 kW (98.5 hp) 59.6 kW (80 hp) 2,4286:1 2,273:1 GT Tonini Auto fuel: Min. RON 95 (AKI 91 Premium USA)/Avgas: 100LL 45 x 2 litres 11,8 x 2 gal 100 HP 230 Km/h 124 kts 205 Km/h 110 kts 260 Km/h 140 kts 6,2 m/sec 1220 ft/min 64 Km/h 34,5 kts 4500 m 15000 ft 750 Km 466 N.m. 100 m 328 ft 4000 Km/h 13000 ft 720 Km/h 447 N.m. 110 Km/h 360 ft 45x2 Lt 11,9x2 GAL 6 Km/h 1180 ft/miN 80 HP 219 Km/h 117 kts 190 Km/h 102 kts

Engine And Propeller

Power Max. @ 580M0 Rinpumte (Sm) Ax. 5 Reduction Propeller Fuel

Advantages

Superior performance and flight characteristics 205 km/h (100 kts) cruise speed Stable and responsive
Ideal for flight schools High level of comfort that makes it ideal for long routes Excellent visibility

Performance

Max Speed S/L Cruising Speed 75% 5250 Rpm Vne - Never Exceed Speed Rate Of Climb Stalling Speed (with Flap) Service Celling Max Range (without Reserve) 65% Take Off Run & Landing Run

Fuel Tank Capacity

Construction
The Tecnam line employs a monocoque tail cone section with the forward fuselage using sheet aluminium over steel tubing. The wing is an all aluminium conventional structure with a single strut. The fuel tanks hold 11.9 gal/45l each, located in the wing leading edge separated from the fuselage for safety. A wide rear window together with large side windows complete the extraordinary visibility allowing 360 of vision in the cockpit. The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column. 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.

Landing Gear

The main landing gear legs are made of spring steel, directly connected to the main structure. The landing gear is robust enough for rough strips and require no maintenance. The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment with easy and economical maintenance. The main landing gear wheels and brakes are conventional aircraft size (5.00x5) The brake lever control and the parking brake are located forward between the seats.

Engine and Propeller

Interior
Seats are adjustable 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 easy access in flight. All Tecnam aircraft have dual control sticks, throttles and rudder pedals. The trim tab and the flaps are electrically activated with a position indicator on the instrument panel. The fresh air vents are conveniently located in the doors. The aircraft has dual rudder pedals with a steerable nose wheel. The wide instrument panel is designed to accommodate a full variety of instrumentation.
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 engines mount is steel-tubing with shock mounts. It also supports the nosewheel that is not anchored directly to the cabins structure. Two power plant options are available: Rotax 912UL 80HP four-cylinder, four-stroke engine and Rotax 912 ULS 100HP four-cylinder, four-stroke engine. Both engines come with an integrated 1:2.4286 reduction gear. A fixed pitch wood and composite propeller comes as standard. The quick drain gascolator is installed in the engine compartment with easy outside access. The fuel system uses a mechanical engine driven pump along is with an electrical back-up pump. The battery is located in the rear of the fuselage with easy access through a hinged door.

standard equipment

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. Lh + Rh Fuel Qty 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 Exterior Rear Window Tie Down Rings Main Wheels, 5,00 X 5 Nose Wheel, 4,00 X 6 Wheel Pants Fuel System Two Integral Fuel Tanks With 90 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 & Storage Pockets Luggage Compartments Cabin Confort System Ventilator Adjustable, 2 Place Powerplant And Propeller Engines: 1 Rotax 912ULS2 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 Pilots Operation Handbook Maintenance Manual
COSTRUZIONI AERONAUTICHE TECNAM S.R.L.
Costruzioni Aeronautiche Tecnam operates in three facilities. The Casoria facility is located adjacent to the Napoli Capodichino Airport and covers an area of 10.8000 sq ft with 43.100 sq ft of enclosed facilities. The Capua facility is located adjacent to the Oreste Salomone Airport, covers an area of 12.9000 sq ft with 43.100 sq ft of enclosed facilities. Capua has already a new area of 38.7000 sq ft with 64.600 sq ft of enclosed facilities. This extension will double the production capacity of the Capua plant. Modern reinforced concrete buildings are used for manufacturing processes, design activities and office administration. And finally the TECNAM Spain facility located in Villanueva del Gallego, Zaragoza - Spain covers an area of 16.404 sq ft with 65.661 sq ft of enclosed facilities with a runway adjacent of 3.937 length/ft.

ECHO CLASSIC

A D VA N TA G E S
Great Value! Low Cost! Built to ASTM Standards Can be Configured as a Float Plane 620 Pound Useful Load
MAIN CHARACTERISTICS / PERFORMANCE

ENGINE

Manufacturer Model Power Number of Cylinders Rotax 912ULS/Shp 4

WEIGHTS

PROPELLER
Maximum Take-off weight Standard Equipped weight Standard Useful Load Limit Loads Ultimate Loads
1320 lbs. 700 lbs. 620 lbs. +4/-2g +6/-3g
Max. at Sea Level, Gross Weight 113 kts Cruise, 75% Power 108 kts Vne 138 kts

STALL SPEED

Manufacturer Model Number of Blades Type

Tonini GT 2 Fixed

DIMENSION
Flaps up, Power off Flaps down, Power off 29.5 ft. 129 sq. ft. 21 ft. 8.2 ft. 44 lbs. Rate of Climb at Sea Level Service Ceiling Takeoff run over 50 ft. Obstacle Landing run over 50 ft. Obstacle Demonstrated crosswind
36 kts 26 kts 1200 ft/m 14,800 ft. 820 ft. 853 ft. 20 kts
Wing Span Wing Area Fuselage Length Fuselage Height Baggage Allowance

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FLIGHT INSTRUMENTS and INDICATORS Magnetic Compass Airspeed Indicator - Kts Altimeter Dual Mode - IN/Mb Vertical Speed Bank Indicator Flap Indicator Pitot System Static System Stabilator Trim Positiion Indicator ENGINE INSTRUMENTS Tachometer Hour Recorder Oil Pressure Oil Temperature Cylinder Head Temperature Fuel Pressure Voltmeter LH + RH Fuel Quantity
INTERIOR Pilot and Copilot Seats Adjustable Fore and Aft Arm Rest Seat Belts and Shoulder Harness (all seats) Wall to Wall Carpeting Map and Storage Pockets Luggage Compartment EXTERIOR Epoxy Corrosion Proofing, all structure Lockable LH and RH Doors Rear Window All Windows Tinted Tie Down Rings Main Wheels, 5.00 x 5 Nose Wheel, 4.00 x 6 EXTERIOR LIGHTS Vertical Tail Strobe Taxi Light Nav. Wing Lights with Strobe Tail Light POWERPLANT and PROPELLER Engines - 1 ROTAX 912ULSHP, 4 Cylinders liquid/air cooled Integrated Reduction Gear Dual Ignition System Dual Throttle Control Tubular Steel Engine Mount Propeller - fixed pitch Propeller Spinner Fire Sleeve on Fuel and Oil Lines Air Filter Oil Filter Oil and Water Radiators Thermostatic Oil Valve PRODUCT SUPPORT / DOCUMENTS Manufacturers Full 2 Year Limited Warranty Pilot Operating Handbook Maintenance Manual
FLIGHT CONTROLS Hydraulic Toe Brakers Parking Brake Electric Flaps Dual Flight Controls Steerable Noise Wheel Stabilitor Trim (electricaly acutuated from stick) Engine Controls Dual Throttle Choke Flight Trim Controls Stabilator (electricaly acutuated from stick) Fuel Control Selector with on/off Panel Switches Split Master Switch Avionics Master Starter Key ELECTRICAL SYSTEM 18 Amp. Hour Battery 12 Volt Alternator - 20 Amp. Switches Landing Light Strobe Light Nav. Light 12 Volt Socket Circuit Breaker Panel FUEL SYSTEM 2 Integral Fuel Tanks (24 gal.) Total Capacity Engine Driven Fuel Pump Fuel Quick Drains Fuel Gascolator

NORTH AMERICA

TECNAM
11152 Air Park Road Ashland, VA 23005 [P] 888.359.4682
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