AMC 25.621 Casting Factors

• ED Decision 2005/006/R found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

AMC 25.621 Casting Factors ED Decision 2005/006/R 1. Purpose. [CS 25.621](#_DxCrossRefBm1709821087) is an additional rule/requirement for structural substantiation of cast parts and components. It is used in combination with a number of other paragraphs, and does not replace or negate compliance with any other paragraph of CS-25. The intent of this AMC is to provide general guidance on the use and background of "Casting Factors" as required by [CS 25.621](#_DxCrossRefBm1709821087). 2. General Guidance For Use Of Casting Factors. 2.1 For the analysis or testing required by [CS 25.307](#_DxCrossRefBm1709820910), the ultimate load level must include limit load multiplied by the required factor required by [CS 25.619](#_DxCrossRefBm1709821085). The testing required in accordance with [CS 25.621](#_DxCrossRefBm1709821087) may be used in showing compliance with [CS 25.305](#_DxCrossRefBm1709820909) and [CS 25.307](#_DxCrossRefBm1709820910). These factors need not be considered in the fatigue and damage tolerance evaluations required by [CS 25.571](#_DxCrossRefBm1709820942). 2.2 The inspection methods prescribed by [CS 25.621(c) and (d)](#_DxCrossRefBm1709821087) for all production castings must be such that 100% of the castings are inspected by visual and liquid penetrant techniques, with total coverage of the surface of the casting. With regard to the required radiographic inspection, each production casting must be inspected by this technique or equivalent inspection methods; the inspection may be limited to the structurally significant internal areas and areas where defects are likely to occur. 2.3 With the establishment of consistent production, it is possible to reduce the inspection frequency of the non-visual inspections required by the rule for non-critical castings, with the acceptance of the Agency. This is usually accomplished by an accepted quality control procedure incorporating a sampling plan. (Refer to [CS 25.621(d)(5)](#_DxCrossRefBm1709821087).) 2.4 The static test specimen(s) should be selected on the basis of the foundry quality control inspections, in conjunction with those inspections prescribed in [CS 25.621(c) and (d)](#_DxCrossRefBm1709821087). An attempt should be made to select the worst casting(s) from the first batch produced to the production standard. 2.5 If applicable, the effects on material properties due to weld rework should be addressed. The extent and scope of weld rework should be detailed in the manufacturing specifications as well as on the design drawings. 3. Background. 3.1 Regulatory Background. [CS 25.621](#_DxCrossRefBm1709821087) (“Casting factors”) requires classification of structural castings as either “critical” or “non-critical.” Depending on classification, the requirement specifies the accomplishment of certain inspections and tests, and the application of special factors of safety for ultimate strength and deformation. 3.2 Application of Special Factors of Safety. The application of factors of safety applied to castings is based on the fact that the casting process can be inconsistent. Casting is a method of forming an object by pouring molten metal into a mould, allowing the material to solidify inside the mould, and removing it when solidification is complete. Castings are subject to variability in mechanical properties due to this casting process, which can result in imperfections, such as voids, within the cast part. Using certain inspection techniques, for example radiographic (X-ray), it is possible to detect such imperfections above a minimum detectable size, but accurate detection depends on the dimensions of the part, the inspection equipment used, and the skill of the inspector. 3.2.1 [CS 25.619](#_DxCrossRefBm1709821085) (“Special factors”) includes a requirement to apply a special factor to the factor of safety prescribed in [CS 25.303](#_DxCrossRefBm1709820908) for each part of the aeroplane structure whose strength is subject to appreciable variability because of uncertainties in the manufacturing processes or inspection methods. Since the mechanical properties of a casting depend on the casting design, the design values established under [CS 25.613](#_DxCrossRefBm1709821065) (“Material strength properties and material design values”) for one casting might not be applicable to another casting made to the same specification. Thus, casting factors have been necessary for castings produced by normal techniques and methodologies to ensure the structural integrity of castings in light of these uncertainties. 3.2.2 Another approach is to reduce the uncertainties in the casting manufacturing process by use of a “premium casting process” (discussed in [AMC 25.621(c)(1)](#_DxCrossRefBm1709821089)), which provides a means of using a casting factor of 1.0. [CS 25.621](#_DxCrossRefBm1709821087) (“Casting factors”) does permit the use of a casting factor of 1.0 for critical castings, provided that: — the manufacturer has established tight controls for the casting process, inspection, and testing; and — the material strength properties of the casting have no more variability than equivalent wrought alloys. [Amdt 25/1]