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>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.20 Aluminium>BS L 115:1971 Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)
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immediate downloadReleased: 1971-09-30
BS L 115:1971 Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)

BS L 115:1971

Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)

CURRENCY
74.4 EUR
Standard number:BS L 115:1971
Pages:6
Released:1971-09-30
ISBN:0 580 06805 6
Status:Standard
DESCRIPTION

BS L 115:1971


This standard BS L 115:1971 Specification for plate of aluminium-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (not exceeding 25 mm thickness) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7) is classified in these ICS categories:
  • 49.025.20 Aluminium

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