IR(A) SEP, IR(A) MEP(A), FI(A)COMPLEX PILOT TRAININGTECNAM P2010COMPLEX PILOT TRAININGIR(A) SEP, IR(A) MEP(A), FI(A)COMPLEX PILOT TRAININGPPL(A), CPL(A), ATP(A) LICENCEZERO TO ATPLZERO TO ATPLPPL(A), CPL(A), ATP(A) LICENCE

P92 Echo Light Classic

Tecnam P92 Echo Classic Light

 

DESCRIPTION

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.
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., 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

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

ELECTRICAL SYSTEM
12 VOLT 18A AMP.

BATTERY LIGHT 1 KG
12 VOLT ALTERNATORS-20 AMP.
SWITCHES
12 VOLT socket
CIRCUIT FUSES PANEL

FUEL SYSTEM
ONE INTEGRAL FUEL TANK WITH 45 LITRES
TOTAL CAPACITY
FUEL QUICK DRAIN

INTERIOR
PILOT and COPILOTCARBON FIBER SEATS with CUSHION
Adjustable Fore and Aft
SEAT BELTS & Shoulder Harness, All Seats
LIGHT INTERIORS WITH CARPET
LUGGAGE COMPARTMENT

EXTERIOR
REAR WINDOW
TIE DOWN RINGS
MAIN WHEELS, 4,00 X 4
NOSE WHEEL, 4,00 X 4

EXTERIOR LIGHTS
NAV. LIGHTS WITH STROBE
TAXI LIGHT

CABIN CONFORT SYSTEM
VENTILATOR ADJUSTABLE, 2 PLACE

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

 

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