PRICES include / exclude VAT
Homepage>BS 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)
Sponsored link
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)

Format
Availability
Price and currency
English Secure PDF
Immediate download
151.20 EUR
You can read the standard for 1 hour. More information in the category: E-reading
Reading the standard
for 1 hour
15.12 EUR
You can read the standard for 24 hours. More information in the category: E-reading
Reading the standard
for 24 hours
45.36 EUR
English Hardcopy
In stock
151.20 EUR
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