ARP1795 STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials

Revised

04/01/1982

Features
Issuing Committee
Scope
Content
This recommended practice 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.
Meta TagsDetails
DOI
https://doi.org/10.4271/ARP1795
Pages
6
Citation
SAE International Recommended Practice, STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials, SAE Standard ARP1795, Issued April 1982, https://doi.org/10.4271/ARP1795.
Additional Details
Publisher
Published
Apr 1, 1982
Product Code
ARP1795
Content Type
Recommended Practice
Status
Revised
Language
English

Revisions