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>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.20 Aluminium>BS 2L 95:1971 Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)
immediate downloadReleased: 1971-08-31
BS 2L 95:1971 Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)

BS 2L 95:1971

Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)

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Standard number:BS 2L 95:1971
Pages:8
Released:1971-08-31
ISBN:0 580 06505 7
Status:Standard
DESCRIPTION

BS 2L 95:1971


This standard BS 2L 95:1971 Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15) is classified in these ICS categories:
  • 49.025.20 Aluminium

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