SAE ARP982C

Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products.

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Standard:
  • ARP982
  • Revision: C
Reaffirmed:
  • 2002-12-19
Revised:
  • 1997-03-01
Revision:
  • Historical. Access the latest revision: ARP982D
Issuing:
  • Ams G Titanium And Refractory Metals Committee
Scope:

Primarily to provide recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products.

The detailed recommendations are based on laboratory experience and reflect those design practices and fabrication procedures which should obviate in-service stress-corrosion cracking of wrought titanium alloy products.

It must be emphasized that while stress-corrosion cracking in service has been observed, the chemical environmental conditions have, in all instances, been unusual and, although it is possible to produce stress-corrosion cracking of titanium alloys under more common conditions as discussed in these recommendations, there have been few, if any, failures in such environments.

History:
StandardPublishedRevisionStatus
ARP982D2007-12-12LatestReaffirmed
ARP982C1997-03-01HistoricalReaffirmed
ARP982B1984-04-01HistoricalRevised
ARP982A1971-11-01HistoricalRevised
ARP9821967-11-01HistoricalIssued
AKA:
  • SAE ARP 982
Sector:
  • Aerospace
Topic:
  • Metallurgy
  • Beryllium alloys
  • Titanium alloys
  • Aluminum
  • Titanium
  • Materials properties
  • Refractory materials
  • Beryllium

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