SAE ARP1795 PDF
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STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials
Category: ARP
Tags: Alloys, Corrosion, Drying, Fabrication, Fastening, Heat treatment, Sodium, Test procedures, Titanium alloys
Description
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.
History
| ARP1795A | 1990-10-01 | Latest | Canceled |
| ARP1795 | 1982-04-01 | Historical | Revised |
| ISSUING COMMITTEE | AMS J Aircraft Maintenance Chemicals and Materials Committee |
|---|---|
| DATE | 1982-04-01 |
| DOI | |
| ISCURRENT | |
| PAGE | 6 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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