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

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.
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.

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STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials - ARP1795 - SAE International
Warrendale, PA, United States
STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials
ARP1795
STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials ARP1795
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.

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.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number ARP1795
Product Name STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials
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