
The new EUROFOX...

as Tricycle...

or in taildragger configuration.

Also available with floats and hydraulic gear actuator!
THE EUROFOX
GENERAL
The EUROFOX is a classic tube-and-fabric
aircraft made from 4130 steel tubes with modern features and constructe
d
with the finest workmanship. It can be registered as well in the mircrolight
as in the normal aircraft classification. It is designed as a high-wing monoplane supported
by struts. A two-spar wing is provided with Junkers flaperons. The fuselage is a
lattice-work of steel tubes (4130) with folding wings for easy street
transprortation. The landing gear of the 3K version is a tricycle type
undercarriage with a controllable nose wheel. The 2K version has a
conventional tail wheel. The cockpit is accessible through big upwards opening
doors with two side by side upholstered seats of fiberglass.
CONTROLS
The
aeroplane is equipped by dual sticks. Elevator and ailerons are controlled by a
system of rods. The rudder is cable controlled. The wing flaps are controlled by
the lever and rod and through the countershaft is threaded into
aileron-flapperon circuit. Trim control is mounted as a standard. All engine
controls are placed on the instrument board.
PANEL 
The instrument panel is equipped with basic flight and engine instruments as: air speed indicator, vario, altimeter up to 3000m, bank indicator, compass and FLYDAT - digital engine monitoring system. All other equipment optional.
ENGINE 
The EUROFOX is powered by the 80 HP ROTAX 912 engine (four-stroke, four-cylinder liquid cooled, dual carburetor engine, electronic dual ignition, gearbox, electric starter, air and oil filter, liquid and oil cooler, special airbox design with carburetor heat system). The 100 HP Rotax 912 S is available as an option. A composite fixed pitch 3-blade propeller is fitted to the engine and a CS propeller optional
The fuel system has a total capacity of 56 / 85 l in two wing tanks. Fuel level indicators are part of each tank, a minimim fuel warning light is standard.
|
Aircraft Details |
UL (Ultralight) |
LSA (Standard) |
|
| Empty Weight | 280 kg | 280 kg | |
| MTOW | 450 kg | 560 kg | |
| Wing Span | 9,12 m | 9,12 m | |
| Length | 5,73 m | 5,73 m | |
| Hight | 1,72 m | 1,72 m | |
| Wing Area | 11,40 qm | 11,40 qm | |
| Stall Speed (Vmin) | 65 km/h | 65 km/h | |
| Normal Speed (Vo) | 110-160 km/h | 110-160 km/h | |
| Optimum Speed (Vopt) | 140 km/h | 140 km/h | |
| Economic Speed (Vek) | 120 km/h | 120 km/h | |
| Max. Speed (Vmax) | 185 km/h | 185 km/h |
|
First posted: December 1993 Last Revision: December 2005 |
|
Copyright © 2003 AirConsult Turkey Ltd. - All rights reserved |