If i remeber right most of the "new" European crop of aircraft are built to
CS-VLA 1 - basically
This airworthiness code is applicable to
aeroplanes with a single engine (spark- or
compression-ignition) having not more than two
seats, with a Maximum Certificated Take-off
Weight of not more than 750 kg and a stalling
speed in the landing configuration of not more
than 83 km/h (45 knots)(CAS), to be approved
for day-VFR only. (See AMC VLA 1).
CS-VLA 3 Aeroplane categories
This CS-VLA applies to aeroplanes intended
for non-aerobatic operation only. Non-aerobatic
operation includes -
(a) Any manoeuvre incident to normal
flying;
(b) Stalls (except whip stalls); and
(c) Lazy eights, chandelles, and steep turns,
in which the angle of bank is not more than 60°.
Try one of these DA20-C1.
If you are not sure about composite airframes talk to Tim Dews down at Airbourne Composites, He'll fill in the blanks.