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Homepage>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.035 Components for aerospace construction>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)
immediate downloadReleased: 1975-05-30
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)

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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155.44 EUR
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Standard number:BS L 118:1975
Pages:10
Released:1975-05-30
ISBN:0 580 08942 8
Status:Standard
DESCRIPTION

BS L 118:1975


This standard 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) is classified in these ICS categories:
  • 49.035 Components for aerospace construction

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