
AEROPRO EURO
FOX
FLIGHT MANUAL
- date - 1-3
1.4 Brief Description
1.4.1 Aircraft Type
EuroFOX is an ultralight designed as a high-wing monoplane supported
by struts. A two-spar wing is provided with flaperon. Fuselage is a lattice-
work of steel tubes. Tail unit is formed of a lattice-work tube frame.
Landing device is a type of trigear undercarriage with a controllable nose
wheel
1.4.2 Power Unit
The EUROFOX ultralight is powered by ROTAX 912 UL engine. It is a
four-cylinder, four-stroke, opposed-cylinder, centre-camshaft engine with
over-head valves. Engine cooling is of a combined type, cylinder heads
are water-cooled, while cylinders are air-cooled. Dry sump lubrication.
The ignition system is of a dual, distributorless and capacitor flywheel
magneto type. The engine is equipped with an electric starter, AC
generator and a mechanical fuel delivery pump. The propeller is
powered from an integrated reduction gear with mechanical damping.
WARNING This engine has not been certified as an aircraft one and its
failure may occur at any time! The aircraft pilot is fully
responsible for consequences of such failure.
1.4.3 Propellers
The propeller made by Woodcomp/FITI/DUC company is a three-
bladed, right-handed, tractor, composite.
1.4.4 Aircraft Dimensions
Wing span..................................................................................9,125 m
Length........................................................................................5,605 m
Height ........................................................................................2,25 m
Wing area with flap..................................................................11,4 m
2
Chord length without flap...........................................................1,12 m
with flap...........................................................1,3 m
Wing loading ..........................................................................39,47 kgm
-2
Aspect-ratio................................................................................7,3
Propeller clearance (in flight position).......................................0,22 m