The Eurofox are factory-built two-seat aircraft manufactured by Aeropro in Slovakia. Aeropro has been producing aircraft since 1990 with now over 700 aircraft now flying around the world. The Eurofox has modern designs with excellent performance and features — built with the finest workmanship and materials resulting in a completed aircraft of the highest quality.
The EuroFOX is a real aircraft in every respect. It is joy to fly and own, extremely comfortable with responsive, coordinated controls which immerse the pilot in the pleasure of flight. With class leading visibility, the EuroFOX provides true agility and tremendous satisfaction for the pilot and passenger.
Available with the world’s leading aero engine for all LSA aircraft, the Rotax 912 series. The aircraft is a high wing STOL aircraft with class leading handling, specification, payload and performance that cannot be matched by its direct competitors. Having the widest undercarriage in class, constructed in robust GRP, the aircraft is proven over decades with almost half a million landings. The EuroFOX is a real fun and engaging aircraft capable of operating from the shortest and roughest strips, whilst efficiently cruising at 100 knots.
Wingspan | 9,125 m |
Length | 5,605 m |
Height | 2,25 m |
Cockpit Width | 1,12 m |
Wing area with flap | 11.4 m² |
Chord length without flap | 1,12 m |
Chord length with flap | 1,3 m |
Wingloading | 39,47 kgm‑2 |
Aspect ratio | 7.3 |
Min. speed | 65 km/h |
Operating speed | 110–160 km/h |
Optimal speed Vopt | 140 km/h |
Economical speed Vek | 160 km/h |
Max. Flap Extension Speed | 150 km/h |
Max.speed | 208 km/h |
All up Empty Weight (Average A/C) | 289 kg |
Max. Take-off Weight-LSA category | 560 kg |
Baggage hold | 20kgs as standard |
Cross wind limit | 27.8 km/h |
Glide Ratio | 9:1 |
Range | 997 km (6Hrs) |
Take-off Ground Roll at MAUW | 139 m |
Landing Ground Roll at MAUW | 130 m |
Max Width | 2,4 m |
Max Height | 1,77 m |
Length | 6,4 m |
Main Gear Width | 2,3 m |
Eurofox 2K taildragger features a composite main landing gear and has wide-spaced main wheels to aid with cross-wind landings and takeoffs, as well as resulting in superior ground handling. EuroFOX 2K is a taildragger type with controlled tail wheel and are equipped by the Beringer dual toe brake system.
EuroFOX 3K a fixed tricycle undercarriage with a controllable nose wheel. Eurofox 3K has a composite main landing gear and chromoly metal tube front leg. Main gear are equipped by the hydraulic disk brakes operated from the left and right seat. A parking brake is optional.
EuroFOX is a strong performer, able to tow gliders up to 800 kgs and also performance gliders with a wing loading over 50 kg/m2. From a Nimbus 3DT to a JS1, all club two seaters and vintage in between…..
The aircraft is very economical to own and run, with proven capability and reliability, frugal annual maintenance costs with excellent tug performance.
The EuroFOX has been aerotowing in world for a decade, most sites being difficult grass airstrips. The EuroFOX can be specified as a tail dragger or nose wheel, and with the majority of EU gliding sites being unpaven grass strips, often boggy, sometimes short in length, only the EuroFOX tail dragger with tundra tyres will do.
The EuroFOX wingfold is a standard and central feature of the aircraft, there is no wear and tear, it is designed to have the wings folded on a daily basis if that is required. One person can open or fold the wings, single handedly in less than 10 minutes, no tricks, no heavy lifting or any extra hands needed.
Our wingfold was designed from the outset and an integral part of the aircraft, not an afterthought as so many other “wingfold” claims are. All the EuroFOX aircraft are always kept with wings folded, and they have been so for many years, no problems at all after many hundreds of daily “fold and unfolds”.
Wing of rectangular platform with its own aerofoil section is of frame structure with two spar tubes and the system of diagonal struts and system of ribs. Al-alloy tubes of 63 mm diemater are reinforced in the hinges regions by tubes of corresponding diameter. A system of ribs consists of 14 ribs and of 13 aux. ribs supporting the fabric skin in the front wing area. In the horizontal plane the wing is braced by a system of diagonal steel spar tube.
The wing is covered by synthetic fabric POLY FIBER, with applied stretching lacquer and sprayed by a first-rate exterior enamel. flaperons (Junkers flap) are attached through five hinges to the ribs under the wing trailing edge. The flapperon structure consists of Al-alloy tube and laminate sandwich (foam, epoxy resin, glass) formed in a negative mould. Both wings are attached to the fuselage in the upper part through the main tube hinges and in the bottoom part by the hinges of the “V” ‑shaped wing struts. The system of common rear wing hinge and tilt truss axes allows the wing to tilt along the fuselage rear part. This saves a lot of storage place and allows the road transport.
The fuselage is designed to provide maximum strength, pilot and passenger comfort, and ease of construction. The canopy frame, engine attach points is enveloped in a high-strength, 4130 Chromoly cage — the same steel used to manufacture rifle barrels — providing an additional layer of security and safety.
Fuel system has a total capacity of 86 l. It consists of two wing tanks (40 l each) and of an 5 l equalizing tank in the fuselage, connected through the pipes with the fuel cock and filter. Fuel level indicators are part of each tank, the minimim fuel warning light is mounted as standard.
The aeroplane is equipped by dual stick control. Elevator and ailerons are controlled by a system of rods whereas 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. Rudder control – pedals of foot control are situated on the floor in front part of cockpit. Moving of pedals is transmitted on the rudder through steel cable. Wing flaps – handle of wing flaps is situated in middle part of cockpit.
Electric system is formed single-wire system of cabling with ground connection negative pole. Network supplies alternator with rectifier with 250W power and accumulator 12V / 16Ah. Board network is switched by a switch key of switch box. Individual circuits of appliances are switched by separate switches and protected by a safety limit switch.
Wing of rectangular platform with its own aerofoil section is of frame structure with two spar tubes and the system of diagonal struts and system of ribs. Al-alloy tubes of 63 mm diemater are reinforced in the hinges regions by tubes of corresponding diameter. A system of ribs consists of 14 ribs and of 13 aux. ribs supporting the fabric skin in the front wing area. In the horizontal plane the wing is braced by a system of diagonal steel spar tube.
The 2×25,5 l fuel tanks are housed in the wing root part. Tanks are welded from Al-alloy sheet. The leading edge shape is guaranteed by a fiberglass part bonded in front of the spar tube. The trailing edge is fitted with an Al-alloy shaped batten.
The wing is covered by synthetic fabric POLY FIBER, with applied stretching lacquer and sprayed by a first-rate exterior enamel. flaperons (Junkers flap) are attached through five hinges to the ribs under the wing trailing edge. The flapperon structure consists of Al-alloy tube and laminate sandwich (foam, epoxy resin, glass) formed in a negative mould. Both wings are attached to the fuselage in the upper part through the main tube hinges and in the bottoom part by the hinges of the “V” ‑shaped wing struts. The system of common rear wing hinge and tilt truss axes allows the wing to tilt along the fuselage rear part. This saves a lot of storage place and allows the road transport.
CRAFTED IN EUROPEAN UNION