The Potez 39 was a twin-seat single-engined parasol wing monoplane aerial reconnaissance and observation aircraft designed and produced by the French aircraft manufacturer Potez. It was the company's first all-metal aircraft.
It was developed in response to a specification released in 1928 for a new reconnaissance aircraft to succeed the Potez 25 and Breguet 19. The design team performed a detailed study of both mixed-construction and metal-centric aircraft prior to designing the all-metal Potez 39; numerous prototype and derivative aircraft were conceived of by Potez, including that of a floatplane, however, besides the French Air Force, only Peru would opt to order the type.
The new aircraft, which performed its maiden flight in January 1930, came as the runner up to the Breguet 27, but was still selected for production. While the Potez 39 was still in service with seven observation squadrons at the outbreak of the Second World War, the French Air Force elected to rapidly withdraw the type from frontline service and instead use it as a trainer aircraft up until the armistice of June 1940, after which point the remaining aircraft were scrapped.
Development
The Potez 39 was designed to a fulfil a requirement issued during 1928 for an aircraft to replace both the Potez 25 and Breguet 19 aircraft then in service with the French Air Force in the A2 (Artillerie Biplace - two seat observation aircraft) role. One key feature that was stipulated by the specification was the use of the Hispano-Suiza 12H engine, which was capable of producing up to 580bhp (430kW).[1][2]
In response, the company's design team produced a new aircraft along the same basic lines as the earlier Potez 25; however, unlike its predecessor, it featured all-metal construction instead the traditional mixed-construction practices that had been long used by the company.[3] Development of what would become the Potez 39 was heavily shaped by a period of methodical study conducted at Méaulte under the direction of the aeronautical engineer Louis Coroller; this was initially carried out on conventional monoplanes before progressing to metal aircraft that were adapted for quantity production.[4]
During January 1930, the prototype conducted its maiden flight. Although the Breguet 27 was selected as the winner of the competition, both it and the Potez, which was the runner-up, were chosen for production.[1] Compared to the Potez 25, of which over 2,000 were ordered, production of the Potez 39 series was on a smaller scale. A total of 100 Potez 390 aircraft were built for France while 12 Potez 391 aircraft, powered by a Lorraine-Dietrich 12H engine capable of generating up to 700bhp, were produced to the Peruvian Air Force. A number of prototype and development aircraft, including a floatplane, underwent flight testing, however, no further orders were received.
Design
The Potez 39 was a dedicated aerial reconnaissance aircraft that featured all-metal construction, which included the coverings of both the fuselage and wings.[3] The aircraft had an oval-section fuselage that was formed out of two areas, the fuselage proper and the engine support.[5] The latter, which was composed of duralumin sheeting, was attached to the fuselage proper via four spherical fittings that were bolted to the forward ends of the longerons. The former was supported via a trellis girder arrangement, comprising varying thicknesses of duralumin, the uprights and diagonals of which were joined via simple riveted gussets to the longerons.[5] Key attachment gussets were composed of high-resistance steel that greatly hindered the development of corrosion. The duralumin fuselage covering was directly secured to all primary structural members, providing great rigidity to the overall assembly; the fuselage was considered to be relatively strong for the era.[5]
The exterior of the aircraft was covered by sheets of duralumin were used of a typical thickness of .35 mm (0.014 in.); this covering was stiffened using corrugated sections at intervals of 85 mm (3.35 in.), which had a height of about 10 mm (0.4 in.). Extensive testing was performed by Potez to determine that these proportions provided sufficient rigidity without overly increasing friction.[6] The covering of the wing had numerous removable sections, both to permit inspection as well as to assist in repairs and maintenance, while the central section of the wing was attached via a rivets to the flanges of the spars, ribs, and cross pieces to constitute a rigid box girder that transmitted and shared stresses.[6] 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.[7]
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.[3] The flying performance of such a profile was thoroughly explored during comparative flight tests with both the Potez 31 and Potez 36. Lacking both dihedral or sweepback, the wing has an aspect ratio of 7.3.[3] It was attached to the fuselage via an inverted V-shaped cabane strut along with a pair of struts of which the threaded ends permitted adjustment; cross-bracing via means of struts made the aircraft incapable of becoming out of adjustment. The internal structure of the wing comprised two spars with diagonal bracing (using duralumin half-tubes) and widely spaced ribs.[8] The wing was equipped with sizable ailerons.[5]
It was operated by a crew of two, a pilot and observer, that sat in tandem in open cockpits.[5] The observer was armed with two Lewis guns on a ring mounting while the pilot was armed with a single synchronisedDarne machine gun. Additional armaments comprised light bombs, which could be carried internally in a compact bomb bay as well as on external racks. Reconnaissance apparatus included a fixed camera that operated through a hatch in the fuselage floor.[1][2]
The aircraft was powered by a single Hispano 12H, which produced 579 hp at 2,000 rpm.[9] Cooling was provided by both an water radiator and an oil radiator. Two pumps were used to deliver fuel to the engine from a suspended conical-shaped fuel tank, which permitted fuel dumping even in the event of deformation due to battle damage.[10] The fuel dumping mechanical was relatively simple, being stylised on that of a firearm.[11] The aircraft was equipped with a conventional undercarriage.[9] The main undercarriage, which had a track gauge of 3 m (9.84 ft.) and was furnished with wheel brakes, was of an axleless design that incorporated Potez's own elastic struts. The tail skid could be was easily inspected via a removable plate near the tail.[12]
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.[9] 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.[9]
Operational history
Deliveries to the French Air Force began in August 1933 and continued until April 1935.[13] The Potez 39 joined the French Air Force's Groupes d'Observation (GO), but from 1936, it was replaced in the GOs by more modern types, including the ANF Les Mureaux 117, Amiot 143 and Potez 540 aircraft, with the Potez 39s transferred to second-line Groupes Aériens Régionaux (GAR), which had the principal role of training reservists.[13][2] In 1938, the GARs were redesignated Groupes Aériens d'Observation (GAO).[14] In August 1938, during the Munich Crisis,General Joseph Vuillemin, Chief of Staff of the French Air Force, gave orders that, in the event of war breaking out, obsolescent observation aircraft such as the Potez 39 should never cross the front line.[15] At the outbreak of the Second World War, the Potez 39 was in service with seven GAOs, which despite their age and Vuillemin's 1938 instructions, were deployed on operational missions.[16][15] The Potez 39 proved to be vulnerable to German fighters, however,[16] and in October 1939, the units equipped with the Potez 39 and the equally outdated Breguet 27, were withdrawn from use at the front.[2][17] The Potez 39 continued to be used for liaison and casualty evacuation duties until the Battle of France concluded with the armistice of June 1940, at which point 41 aircraft reportedly remained in Metropolitan France.[18] These aircraft were deemed to be obsolete and thus were scrapped shortly thereafter.
Twelve Lorraine Pétrel-powered Potez 391s were purchased by Peru in 1933, during the Leticia War with Colombia, with the purchase being funded by popular subscription, but they only entered service early in 1935, after the war had ended.[19] The outbreak of the Second World War stopped deliveries of spare parts and technical assistance from France, and the type was phased out from active service.[20]
Variants
Potez 391 photo from L'Aerophile November 1934
Potez 37
Two seat reconnaissance aircraft developed in parallel with Potez 39, with narrow tail boom replacing conventional rear fuselage. Unsuccessful, with only three built, the ANF-Les Mureaux 110 being preferred.[2][21]
Potez 390 A2
Two-seat observation aircraft for French Air Force. Powered by a Hispano-Suiza 12Hb engine.
A single prototype powered by a 520kW (700hp)Hispano-Suiza 12YbrPotez 49 photo from L'Aerophile December 1932
Potez 49
Sesquiplane conversion of Potez 39. The lower wing was designed to be easily removable, so the aircraft could be configured either as a monoplane or a biplane, according to mission. One built.[21][22]
The Amiot 143 was a 1930s French 5-seat Multiplace de Combat (M.5) designed to meet 1928 specifications for a monoplane capable of day and night bombing, long-range reconnaissance and bomber escort.
The Blériot SPAD S.510 was a French single-seat, single-engined biplane fighter aircraft. First flying in 1933, 60 were built for the Armée de l'Air, entering service in 1936. The type remained in service as a fighter-trainer at the start of the Second World War. It was the last French biplane fighter to enter production.
The Potez 630 and its derivatives were a family of twin-engined, multirole aircraft developed for the French Air Force in the late 1930s. The design was a contemporary of the British Bristol Blenheim and the German Messerschmitt Bf 110.
The Breguet 19 was a sesquiplane bomber and reconnaissance aircraft which was also used for long-distance flights and was designed by the French Breguet company and produced from 1924.
The ANF Les Mureaux 110 and its derivatives were a family of all-metal military reconnaissance aircraft developed and produced by the French aircraft manufacturer ANF Les Mureaux.
The Letov Š-16 was a single-engined twin-seat biplane aircraft used in the bomber and aerial observation roles. It was designed by Alois Šmolík and produced by the Czechoslovak aircraft manufacturer Letov Kbely.
The Blériot 127 was a monoplane bomber aircraft developed and produced by the French aircraft manufacturer Blériot.
The Potez 540 was a French multi-role aircraft of the 1930s. Designed and built by Potez, it served with the French Air Force as a reconnaissance bomber, also serving with the Spanish Republican Air Force during the Spanish Civil War. Although obsolete as a bomber, it remained in service in support roles and in France's overseas colonies at the start of World War II.
The Bréguet 270 was a sesquiplane military reconnaissance aircraft designed and produced by the French aircraft manufacturer Breguet.
The SNCASE SE.100 was a French two-seat, twin-engined fighter that first flew in 1939. Mass production was planned to begin late in 1940 but the Fall of France prevented this.
The Potez 32 and its military version the Potez 33 was a single-engine monoplane transport design and built by the French aircraft manufacturer Potez. It was the first French-built medium-sized aircraft to see active use by both domestic and foreign airlines.
The SNCAC NC.150 was a prototype French high-altitude bomber aircraft designed and flown just prior to the start of the Second World War. It was a twin-engined monoplane, with a third engine driving a supercharger. Although testing was promising, and orders were planned for a modified version as a back-up for the Lioré et Olivier LeO 45 and Amiot 354 bombers, the surrender of France in June 1940 ended development with only the single example being built.
The SNCAO 200, sometimes written as CAO.200, was a French single-seat fighter aircraft prototype of the 1930s. It was a single-engined monoplane intended to compete with the Dewoitine D.520, but it was unsuccessful, and only one was built.
The Potez 37 was a two-seat, long range reconnaissance aircraft built to compete for a French government contract. It flew in mid-1930 but did not win the competition, so only two were completed.
The Bréguet 410 was an all-metal sesquiplane biplane bomber that was designed and produced by the French aircraft manufacturer Bréguet.
The Potez 220 was a prototype French twin-engined, three-seat reconnaissance and army cooperation aircraft. Two examples were built in 1939, but no production followed.
The Potez 230 was a French lightweight single-seat, single-engined fighter aircraft. One prototype was built and flew in 1940, but no production followed, with the prototype being captured and shipped to Germany for study.
The Blériot-SPAD S.91 was a light-weight fighter aircraft by the French aircraft manufacturer Blériot.
The Potez 31 was a prototype French two-seat night fighter, flown in about 1928, intended to fill the Cn.2 specification for the Armee de l'Air. Only one was built.
The Nieuport-Delage NiD 580 R.2 was a contender for a French government contract for a long range, two seat reconnaissance aircraft, issued in 1928. There were eight prototypes in the 1931-2 contest and the NiD 580 was not selected for production.
Breffort, Dominique; Jouineau, André (2004). French aircraft 1939-1942: Volume One: From Amiot to Curtiss. Paris, France: Histoire & Collections. ISBN2-915239-23-1.
Breffort, Dominique; Jouineau, André (2005a). French aircraft 1939-1942: Volume Two: From Dewoitine to Potez. Paris, France: Histoire & Collections. ISBN2-915239-49-5.
Breffort, Dominique; Jouineau, André (2005b). L'aviation française de 1939 à 1942: chasse, bombardement, reconnaissance et observation. Tome 2, De Dewoitine à Potez (in French). Paris: Histoire & collections. ISBN2-915239-48-7.
Coroller, Jean-Louis; Cortet, Pierre (March–April 2005). "Un "Classique" Français": Le Potez 39". Avions (in French). No.144. pp.20–37.
Coroller, Jean-Louis; Ledet, Michel (July–August 2005). "Un "Classique" Français": Le Potez 39 (3)". Avions (in French). No.146. pp.48–52.
Ledet, Jean-Louis; Coroller, Michel (May–June 2005). "Un "Classique" Français": Le Potez 39 (2)". Avions (in French). No.145. pp.26–38.
Passingham, Malcolm (July–August 1996). "Overtaken by Events: The Potez 39 Family". Air Enthusiast. No.64. Stamford, UK: Key Publishing. pp.42–47. ISSN0143-5450.
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