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

1990-10-01
CURRENT
ARP1795A
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.
Standard

Paint Stripping of Commercial Aircraft - Evaluation of Materials and Process

2021-01-12
WIP
MA4872B
This document details the technical requirements to be used in the evaluation of materials and processes developed for use in stripping organic finishes from fixed wing commercial aircraft. The requirements herein are intended to ensure that the materials and processes used are not detrimental to the commercial aircraft when used as specified. These requirements are not intended to judge performance of the stripping method.
Standard

POLISH, AIRCRAFT METAL

1992-10-01
HISTORICAL
AMS1650B
This specification covers a metal polish in the form of a liquid or paste.
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