This standard specifies the technical and quality assurance requirements for externally threaded fasteners in
material NI-PH2601 (Inconel 718) of tensile strength class 1 275 MPa at room temperature, maximum test
temperature of material 650 °The externally threaded fasteners specified herein may be manufactured by machining from bar or by forging
at the manufacturer's option, if forged there is no requirement for control of grainflow.
BS EN 3388:2009 Referenced Document
EN 9100 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
ISO 2859-1 Sampling procedures for inspection by attributes - Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-lot inspection; Technical Corrigendum 1
ISO 3452 Non-destructive testing; Penetrant inspection; General principles
ISO 4288 Geometrical Product Specifications (GPS) - Surface texture: Profile method - Rules and procedures for the assessment of surface texture; Technical Corrigendum 1
ISO 6508-1 Metallic materials — Rockwell hardness test — Part 1: Test method*, 2023-12-13 Update
ISO 7961 Aerospace - Bolts - Test methods*, 2020-12-31 Update
ISO 9000 Quality management systems - Fundamentals and vocabulary [French version]*, 2015-09-15 Update
BS EN 3388:2009 history
2010BS EN 3388:2010 Aerospace series. Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification 1275 MPa/650C. Manufacturing method optional. Technical specification
2010BS EN 3388:2009 Aerospace series - Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification 1275 MPa/650 °C - Manufacturing method optional - Technical specification