[2] The cockpit had numerous windows that were arranged so that the pilots were able to readily view multiple angles, including upwards and rearwards.

[4] These engines drove Ratier-built metal variable-pitch propellers and were fitted with lengthy exhaust pipes that functioned as silencers.

Both of the wing spars were braced so that stresses would be evenly conveyed between them, while the duralumin ribs were reinforced using rivetted stiffeners; sheet metal panels covered the exterior.

[5] The undercarriage, which was fitted with non-continuous elbow-type axles, had a structure that comprised a pair of independent flexible trihedrals.

[7] The compact axles connected with Messier-supplied oleo-pneumatic shock absorbers; the wheels were equipped with brakes in order to reduce the landing distance required.

While the main undercarriage was fitted with wheels, the tail element comprised a cast light alloy skid that was mounted directly underneath the sternpost.

[7] Data from European Transport Aircraft since 1910,[13] The Wibault 280 T.10 commercial airplane (French)[14]General characteristics Performance