The Potez 39 was a dedicated aerial reconnaissance aircraft that featured all-metal construction, which included the coverings of both the fuselage and wings. The aircraft had an oval-section fuselage that was formed out of two areas, the fuselage proper and the engine support. These spars comprised a duralumin web and four steel corrugated angles for stiffening, the latter being relatively easy to uniformly construct, as well as being relatively resistant to
rusting and vibrations alike. Both weight and construction time were minimised via the minimisation of both joints and riveting. The Potez 39 had a
parasol wing, the basic form of which was of an elongated rectangle with well-rounded tips, a feature which reportedly obtained the maximum achievable efficiency without resorting to a more complex wing design that incorporated multiple decreasing profiles. The wing was equipped with sizable
ailerons. It was operated by a crew of two, a pilot and observer, that sat in tandem in open cockpits. The aircraft was powered by a single
Hispano 12H, which produced 579 hp at 2,000
rpm. The fuel dumping mechanical was relatively simple, being stylised on that of a
firearm. The aircraft was equipped with a
conventional undercarriage. The tail unit of Potez 39 was directly attached to the sternpost, which was in turn carried by the aftermost frame of the fuselage frame; the rear of this sternpost supported the hinges of the unbalanced
rudder while the front received the
fin. The rear of the
stabiliser was attached to a movable support that permitted mid-flight adjustments with relatively little force via an arrangement of flexible joints and
ball bearings. The
elevator, which was positioned in front of the rudder, was unbalanced, slightly tapered, and had well-rounded tips; its structure was akin to that of the wing as well as covered by duralumin. ==Operational history==