Don't have a credit card? Never mind we support BANK TRANSFER .

Log inSign up
LANGUAGE en
Menu
STOREHelp centerContactsDelivery chargesABOUT US News
SEARCH
0
Total price
0 EUR
PRICES include / exclude VAT
>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.20 Aluminium>BS L 160:1976 Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)
immediate downloadReleased: 1976-05-28
BS L 160:1976 Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)

BS L 160:1976

Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)

Format
Availability
Price and currency
English Secure PDF
Immediate download
Printable - You are authorized to print 1 copy
150.08 EUR
English Hardcopy
In stock
150.08 EUR
Standard number:BS L 160:1976
Pages:8
Released:1976-05-28
ISBN:0 580 08979 7
Status:Standard
DESCRIPTION

BS L 160:1976


This standard BS L 160:1976 Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) is classified in these ICS categories:
  • 49.025.20 Aluminium

Print
Customers who bought this item also bought
BS 5L 100:2011+A1:2013
Procedure for inspection, testing and acceptance of wrought aluminium and aluminium alloys
Released: 2013-12-31
English Secure PDF
Immediate download
Printable - You are authorized to print 1 copy
369.60 EUR
English Hardcopy
In stock
369.60 EUR