The Nord Noratlas is a dedicated military transport aircraft, developed and manufactured by French aircraft manufacturer Nord Aviation. Development commenced during the late 1940s with the aim of producing a suitable aircraft to replace the numerous older types that were in service with the Armée de l'Air (French Air Force) which dated back to the Second World War. In response to a competition organised by the Direction Technique Industrielle (DTI), Nord produced their Nord 2500 proposal, which was selected as the most promising. Experiences with the first prototype, powered by Gnome-Rhône 14R engines, did not impress, thus the design was revised as the Nord 2501, powered by the SNECMA-built Bristol Hercules 738/9 engines instead, which was found acceptable. Accordingly, the Noratlas was introduced to service by the Armée de l'Air on 6 December 1953. Following its adoption by the Armée de l'Air, a number of other operators in both Europe and Africa chose to procure the Noratlas for their own military air services. Having found itself in a similar situation to France, the German Air Force of West Germany chose to adopt the same solution, procuring the type for their own purposes. The Israeli Air Force, the Hellenic Air Force, and the Portuguese Air Force all deployed the Noratlas under combat conditions. Furthermore, operators often found a wide variety of uses for the type, extensively adapting aircraft to suit secondary roles in some cases. The Noratlas was also adopted by a number of civil operators, although most aircraft were flown by military customers. As such, several hundred aircraft were produced during the Noratlas' production run, which lasted over a decade.
Development Following the end of the Second World War, the French Armée de l'Air was left with two primary transport aircraft: the German Junkers Ju 52, which was produced for some time in France after the end of the conflict, and the American Douglas C-47, (that was derived from the 1930s Douglas DC-3 civil airliner), which had been received from US surplus. While both of these types were typically known for their good service levels, they were by no means modern or particularly large in comparison with newer contemporaries. Both aircraft had suffered from a common set of flaws, such as the traditional tailwheel landing gear configuration, which gave them a nose-up attitude when at rest that complicated the loading and unloading of cargo, relatively restrictive side-loading doors and a limited payload capacity. In light of these apparent shortcomings, during 1947, the Direction Technique Industrielle (DTI) organised a design competition that sought a medium-weight cargo aircraft which would offer very high operational flexibility. In response to the competition, the Société Nationale de Construction Aéronautique du Nord (SNCAN) produced a response in the form of the proposed Nord 2500. Several other competing French aviation firms, such as Breguet and Sud-Ouest, offered their own designs, the BR-891R Mars and SO-30C, respectively. The Nord 2500, which was designed with rear-opening clamshell doors to allow for easy cargo handling, was considered to be the most promising of the submissions received; according, on 27 April 1948, DTI placed an order for a pair of prototypes to be constructed for evaluation. On 10 September 1949, the first prototype conducted its maiden flight. It was powered by a pair of Gnome-Rhône 14R engines, each capable of generating 1,600 hp (1,200 kW), which drove three-bladed variable-pitch propellers. However, flight testing soon determined that the first prototype was simply too slow to be useful for most applications. As such, on the second prototype, the 14Rs were replaced by a pair of SNECMA-built Bristol Hercules 738/9 engines, capable of producing 2,040 hp (1,520 kW), along with a new four-bladed Rotol propeller arrangement. The revised model was rechristened as the Nord 2501. Having been suitably impressed by its performance following the improvements, DTI decided to order three more pre-production aircraft to the Nord 2501 standard. These pre-production aircraft underwent extensive flight testing, which included a series of fly-offs against the similar American Fairchild C-82 Packet. From these, the N2501 was found to be superior, leading to an initial production order for a batch of 34 aircraft on 10 July 1951. Tragedy struck the development effort during 1952 when the first Nord 2501 prototype was lost in an accident during a test flight. On 9 January 1953, the Nord 2501 was baptised as the Noratlas by the widow of the pilot killed in the first prototype's crash. Despite the setback of the first prototype's loss, Nord continued the programme to schedule, fulfilling its initial contract for 34 aircraft by 25 June 1953, and the Armée de l'Air went on to order another 174 Noratlases, for a total of 228 aircraft in French service. Several different models were developed and were proposed, but ultimately were never built. Of those built, perhaps the most distinct was the civil-orientated 2502, which featured additional engines in the form of a pair of wing-tip mounted Turbomeca Marboré turbojets, giving it improved takeoff performance. The proposed 2506 was to have further built upon the 2502, having been intended to possess airbrakes, along with re-designed flaps and height-adjustable landing gear. Following an eventual production run of some 425 planes, the final Noratlas was constructed during 1961. It was succeeded and eventually replaced by the multinational Transall C-160.
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