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BS - British national standards
Page 2989
BS EN 4317:2025-TC (06/01/2026)
Tracked Changes. Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Consumable electrode remelted. Not heat treated. Forging stock. a or D ? 200 mm.
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BS EN 4318:2025 (22/12/2025)
Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Consumable electrode remelted. Solution treated and precipitation treated. Bars and sections. De <= 100 mm. Rm >= 960 MPa.
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BS EN 4318:2025-TC (06/01/2026)
Tracked Changes. Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Consumable electrode remelted. Solution treated and precipitation treated. Bars and sections. De <= 100 mm. Rm >= 960 MPa.
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BS EN 432:1994 (15/11/1994)
Resilient floor coverings. Determination of shear force.
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BS EN ISO 4320:1998 (15/03/1998)
Non-ionic surface active agents. Determination of cloud point index. Volumetric method.
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BS EN 4321:2004 (14/12/2004)
Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated. Classification. 1 550 Mpa (at ambient temperature)/650°C.
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BS 4322:1968 (25/07/1968)
Recommendations for buffering on hospital vehicles such as trolleys.
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BS EN 4322:2004 (15/12/2004)
Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature).
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BS 4323:1979 (28/02/1979)
Method for determination of dimensional change of fabrics induced by free steam.
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BS EN 4323:2004 (15/12/2004)
Aerospace series. Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated. Classification. 900 MPa (at ambient temperature) / 350°C.
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