Aerospace series. Metallic materials. Test methods - Tensile testing at ambient temperatureBS EN 2002 1: 2005 has been prepared by the European Association of Aerospace Manufacturers Standardization (AECMA STAN). This standard specifies the requirements for the tensile testing of metallic materials at ambient temperature for aerospace applications. It includes: types of test piece to be used for sheet and strip with thickness less than or equal to 8 mm types of non machined test piece to be used in the case of bar, section and wire with a

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exist under normal atmospheric conditions of: temperature –20 oC to +60 oC

It is limited to the selection of types and grades of material from standards

operating modes

IEC 60079-15

BS EN ISO 11806 specifies safety requirements and their verification for design and construction of portable hand-held

35 mm up to 3

different substrate weight

terms relating to fusion welding (welding without pressure)

constructed from carbon or carbon manganese steels by fusion welding and a design pressure not exceeding 40 bar

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sampling and various test methods