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BS L 118:1975 | British Standards

Standards Shop | ICS 49 |  ICS 49.035

49.035 Components for aerospace construction

Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)

Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)

BS L 118:1975

Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)


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ISBN: 0580089428

Keywords:
Chromium-containing alloys, Non-destructive testing, Dimensions, Aluminium alloys, Silicon-containing alloys, Solution heat treatment, Mechanical properties of materials, Hydraulic tests, Pressure testing, Pressure pipes, Magnesium-containing alloys, Pipes, Thickness, Diameter, Chemical composition, Copper-containing alloys, Air transport engineering, Ageing (materials), Dimensional tolerances, He, PDF
Publication Date30 May 1975
Product SKU119768
ISBN0580089428
BSI CodeBS L 118:1975
No. of pages10
PublisherBritish Standards Institution




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