The Lioré et Olivier LeO 8, Lioré et Olivier LeO 8-Cau 2 or Lioré et Olivier LeO 8 CAN 2 was a French two seat, parasol wing monoplane night fighter and reconnaissance aircraft, built in 1923. Design and development In April 1919 the Direction de l'Aéronautique () initiated an aircraft design programme to replace the World War I machines serving with the Aéronautique Militaire. Several different types were sought, including a two-seat reconnaissance aircraft and night fighter. The Leo 8 was designed to meet this specification. In the early 1920s French aircraft designers were beginning to appreciate the aerodynamic advantages of thick section wings on monoplanes, particularly their wide speed range even at high wing loadings. The Dewoitine D.1 was the first, followed by the LeO 8. The latter was a metal framed aircraft with a wing of almost rectangular plan and with constant profile, a form that simplified production as all its ribs were identical. The wing tips were slightly blunted and there was a rounded cut-out in its trailing edge for the pilot's head where he sat with the wing at eye level. The wing spars were rectangular duralumin tubes and the ribs were also duralumin. The wings were fabric covered and their outer trailing edges carried narrow chord unbalanced ailerons over half the span. Wing and fuselage were joined by two parallel pairs of streamlined struts on each side, the members of each pair attached to the forward and rear spars. The innermost pair connected the wing at about one-third span to the upper fuselage longeron and the outer pair ran from about two-thirds span to an undercarriage extension. Each pair was wire braced and the each outer pair also braced from their midpoints to the upper ends of the inner pair. The fuselage of the LeO 8 was also built from duralumin, with four rectangularly braced longerons, assisted by internal wire bracing, forming a simple flat sided structure with forward aluminium panels at the front and fabric covering aft. The aluminium covered section included the nose mounted, , twelve-cylinder Renault 12F engine and the underwing region in front of the pilot's open cockpit. The nose was rounded in plan but not profile. The engine was liquid cooled by finned, cylindrical Lamblin radiators hung separately below it and had a tall, single, central exhaust above. Fabric covering began at front of the pilot's cockpit; the gunner's cockpit