
It is a great pleasure and a privilege to introduce this first guest article to 'American Aircraft for the RAF'. David Muir, the author of the superlative 'Southern Cross Mustangs', describes the quality control, testing and acceptance framework and methodologies used in the preparation and painting of aircraft manufactured in the USA for the RAF.
CONTRACTS and COLOURS
Before the RAF expansion programmes of the late 1930s the British and American military aircraft industries had significantly different approaches to the philosophy and management of their contracts with the client services. American manufacturers were largely responsible for quality control of their own output and warranted their products to the users on the basis that any faulty or defective product would be replaced at the manufacturer’s cost. Any involvement of the clients in quality matters tended to occur toward the end of the process as the aircraft were delivered and they were generally accepted on the signature of the firm’s Chief Inspector.
In contrast the Air Ministry (AM) – the main British procurement agency - had highly developed design requirements and regulations that controlled and monitored manufacturing throughout the process from basic materials through to the acceptance of the aircraft into service. The Ministry’s aim was partly to minimise defects during manufacture but more importantly in the field where manufacturing defects directly affected operations. In the UK the entire process was conducted by teams of Aeronautical Inspection Directorate (AID) staff who were located with a Resident Technical Officer (RTO) appointed by the Directorate of Technical Development (DTD) and a Test Pilot at each contractor’s factory and/or shared between a number of sub-contractors.
Central to the Ministry’s philosophy were the concepts of interchangeability and traceability. The AID Inspectors used gauges, special fittings and other measuring tools to check parts, components and assemblies to ensure that they conformed to the contract requirements and correctly mated with the counterparts to which they were to be fitted. An AID inspector’s approval (in the form of his unique symbol rubber stamped in ink on or steel stamped into) each item before it could be used in any subsequent stage of the production line. Each step between the original material and the finished and test flown aircraft was thus checked and the results documented to form a continuous record that allowed any defect to be traced back to its source.
In June 1938 when the British Air Mission placed the first orders (with Lockheed for Hudsons and North American Aviation for Harvards) it used contracts that closely followed AM requirements and practices. By July 12 two AID staff, a DTD RTO and a Test Pilot had arrived in Los Angeles to monitor the lines at Burbank and Inglewood. Despite the differences between the two engineering cultures – eg at first parts of the Harvard were not interchangeable between airframes – NAA recognised the advantages of the AID system and quickly adapted and incorporated changes to its tooling and methods.
With only one AID examiner at each factory, the LA based inspection process was largely delegated to the contractor’s staff with the examiners directly involved at only a few key points in the process. Nonetheless the British procedures largely prevailed with the documentation for each aircraft ultimately being signed off on AID Form 827 by the contractor’s Chief Inspector before being countersigned by the AID Inspector in Charge. These so called Inspection Reports stayed with the aircraft after being accepted by the RAF and were shipped to the UK for storage.
The same system continued after the BAM became the British Supply Board (BSB) within the British Purchasing Commission (BPC, November 1939) and later the British Air Commission (BAC, July 1940). BAC’s AID staff would prepare Critical Reports on new aircraft and modifications which passed to the RTO (A) and through him to the contracting firm (known as the Design Authority) for remedial action. The role is neatly summarised in the following extract from BAC correspondence with its staff in the factories:
…it is well that we should bear in mind the Order, the Drawing, and the Component. It is our function to see that the BAC get what it wants and the Contractual Requirement, the Technical Requirement and the Article supplied are the three elements of inspection.
NAA wholeheartedly embraced the underlying philosophy of the AM process. Thanks to the relationships established during the Harvard contract NAA’s design team were able to discuss AM design requirements and practices with the BPC staff during the early concept stages of the NA-50B design. Thus British principles of interchangeability and quality control were incorporated from the outset in the resulting NA-73 design purchased by the RAF as the Mustang.
Following the establishment of the Lend Lease programme all new aircraft manufacturing contracts were placed by the American Army and Navy and from August 1940 were coordinated by the Army-Navy-BPC Joint Committee which later became the Joint Aircraft Committee or JAC. In early 1942 this responsibility passed over to the Munitions Agreement Committee (Air) (MAC (Air)) which was part of the Committees of Combined Munitions Agreement Board.
The new arrangements under Lend Lease meant that the AID inspectors had no contractual role as such. However, on behalf of the Air Ministry they remained responsible for monitoring the effectiveness of the contractor’s inspection system and its staff, the documentation delivered with the aircraft, the allocation of RAF serials as well as the quality and contract conformity of the delivered products allocated to Britain and the Commonwealth. Their expertise was also sought to help solve construction quality problems in some largely or exclusively American programmes such as the B-24 and B-29, both of which initially had serious interchangeability difficulties.
NAA continued to manufacture Mustangs under lend Lease using the same quality control procedures established on the Harvard and early Mustang production. Damaged or defective parts or assemblies were still identified and a decision made by an Inspector as to the acceptance, reworking or scrapping of that item. Any significant deviation from the order/requirement/drawing/specification needed a formal Air Ministry Concession and was recorded in each aircraft’s documentation.
As with any other component Air Ministry Orders and DTD Technical Circulars set out the customer requirements for camouflage, markings and stencils and NAA specifications, drawings and diagrams describing them in detail were included in the contract between the parties. For example AMO A.664/42, DTD 83, DTD 360 and Air Diagrams 1160 and 2001 established the camouflage and insignia requirements for the RAF’s single seat fighters.
Their contents were incorporated into the NAA contracts in diagrams such as Diagram 99-20-23A (used as 956a (US) and 956b (RAF) of NAA Manual NA 5724) for the B/C/Mk III Mustangs and NAA Diagram 109-00-286/Figure 468 and drawings 102-00010 and 106-00010 for the later D/K/Mk IV/IVA variants. Careful reading of these documents reveals that changes were made, documented and implemented to the camouflage colours in the period when the RAF Mk 1s and Mk IIIs. For example Dark Olive Drab replaced Dark green on the early Mk IIIs.
For the Air Ministry and the RAF camouflage and marking of the aircraft was an important element of operational readiness. Just how important is demonstrated by the Air Ministry’s willingness to expend the time, resources, manpower and money needed to repaint earlier deliveries when the role of the Mustang was reclassified from army cooperation to fighter, thereby changing its camouflage requirements from the Temperate Land Scheme’s (TLS) green and brown to the Day Fighter Scheme’s (DFS) green and grey.
Given NAA’s well established inspection process and culture it is difficult to see the company or its staff even attempting to make unauthorised changes to the camouflage colours used on the RAF Mustangs. In order to be approved any such variation in the colour would have to have been small – i.e. essentially indistinguishable from the approved paint samples held by the AID team.
Any unauthorised larger variations (eg replacing RAF Sky with US Light Gray) would inevitably have been picked up down the line and risked having the aircraft rejected and/or sent back for reworking during the final acceptance process. Similarly it is likely that any request for an Air Ministry Concession to cover a variation that meant parts had to be repainted before they were used on another airframe would not have been approved by the AID team as it directly reduced interchangeability and would have necessitated unnecessary work by the RAF in the field.
In this context the hypothesis that American manufacturers were largely free to make whatever changes and substitutions they deemed necessary without regard to their contractual obligations or their British customer’s needs is clearly not credible. The idea that NAA unilaterally substituted an unidentified and noticeably different gray for the specified and contracted Sky Type S undersides on the RAF Mk IIIs is easily refuted by NAA’s own documentation. As late as the beginning of November 1943 NAA’s publications called for Sky Type S – not gray – on the B/C/Mk IIIs…just as it had contracted for, documented and used on all the Mustangs it had built up to that date.
Shortly thereafter the entire scheme changed from the TLS to the DFS - but that is a story for another day…
David Muir
The following books provide excellent coverage of the Anglo American aircraft programmes during World War 2; both are highly recommended for anyone interested in reading further.
‘The British Air Commission and Lend Lease’ compiled by K. J. Meekcoms (Air-Britain, Tunbridge Wells, 2000 ISBN 0 85130 291 2) covers the inspection and contract administration in detail.
‘Air Arsenal North America, Aircraft for the Allies 1938-1945, Purchases and Lend-Lease’ by Phil Butler and Dan Hagedorn (Midland Publishing, Hinkley, 2004 ISBN 1 85780 163 6) covers the individual aircraft in slightly greater depth.











