Following Bréguet's success in the 1954 and 1956
World Gliding Championships with the
Type 901, Jean Cayla designed the Type 905 for the 1958 event. It is a Standard Class sailplane with a span. Like its predecessor, the 905 is a
cantilever mid-wing monoplane but its structure contains
glass reinforced plastic, more
plastic foam and less
fabric. It also has a
butterfly tail. It has a wing of straight tapered planform, terminated with small "salmon" fairings at the squared-off
wingtips. The major structural component is the main spar plus nose D-box unit, skinned with a plastic foam-filled ("Klegecel") sandwich with ply outer layers. Ribs,
ailerons and
Schempp-Hirth airbrakes are attached to this torsion box. The whole upper wing surface and outboard lower surface is ply, supported by an internal Klegecell lining, with fabric below, aft of the spar. Slotted ailerons occupy the outer 45% of the
trailing edge; there are no
flaps. Each complete wing weighs just . The Fauvettes's
fuselage is built in three parts. The nose section, with a moulded plastic foam shell over a steel frame contains the cockpit, which is covered by a high, one-piece
canopy over the upright seating position, giving the Fauvette a somewhat humpbacked look. The centre section also has a steel frame, covered by moulded polystyrene; wings, cockpit and twin fuselage side towing hooks are attached to this frame. Behind the cockpit the upper fuselage line is formed with a polystyrene
fairing which overlaps the conical rear fuselage, made of ply-foam sandwich. The V-tail is straight-tapered with sweep on both edges. The fixed surfaces are ply-foam sandwich structures, carrying fabric covered control surfaces. The Fauvette has a fixed,
monowheel undercarriage, assisted by a tailskid. ==Bréguet Bre 906 Choucas==