PRICES include / exclude VAT
Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.20 Aluminium>BS L 170:1989 Specification for extruded bars and sections of aluminium-zinc-copper-chromium alloy (solution treated, controlled stretched and artificially aged) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.23) (7075)
Sponsored link
immediate downloadReleased: 1990-02-28
BS L 170:1989 Specification for extruded bars and sections of aluminium-zinc-copper-chromium alloy (solution treated, controlled stretched and artificially aged) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.23) (7075)

BS L 170:1989

Specification for extruded bars and sections of aluminium-zinc-copper-chromium alloy (solution treated, controlled stretched and artificially aged) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.23) (7075)

Format
Availability
Price and currency
English Secure PDF
Immediate download
162.14 EUR
You can read the standard for 1 hour. More information in the category: E-reading
Reading the standard
for 1 hour
16.21 EUR
You can read the standard for 24 hours. More information in the category: E-reading
Reading the standard
for 24 hours
48.64 EUR
English Hardcopy
In stock
162.14 EUR
Standard number:BS L 170:1989
Pages:8
Released:1990-02-28
ISBN:0 580 17954 0
Status:Standard
DESCRIPTION

BS L 170:1989


This standard BS L 170:1989 Specification for extruded bars and sections of aluminium-zinc-copper-chromium alloy (solution treated, controlled stretched and artificially aged) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.23) (7075) is classified in these ICS categories:
  • 49.025.20 Aluminium

This British Standard specifies the chemical composition, heat treatment, mechanical properties and the inspection and testing procedures applicable to extruded bars of aluminium-zinc-magnesium-copper-chromium alloy supplied in the solution treated, controlled stretched, and artificially aged condition, for use in that condition.


Chemical composition, heat treatment, mechanical properties and inspection and test procedures for bars supplied in the solution treated, controlled stretched and artificially aged condition, for use in that condition.