ARP1795A Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials

Canceled

10/01/1990

Scope
Content
This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.
Meta TagsDetails
DOI
https://doi.org/10.4271/ARP1795A
Pages
6
Citation
SAE International Recommended Practice, Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials, SAE Standard ARP1795A, Cancelled October 1990, Issued April 1982, https://doi.org/10.4271/ARP1795A.
Additional Details
Publisher
Published
Oct 1, 1990
Product Code
ARP1795A
Content Type
Recommended Practice
Status
Canceled
Language
English

Revisions