This specification establishes the engineering requirements for the heat treatment of titanium and titanium alloy parts. Heat treatment of raw material by raw material producers, forge shops, or foundries shall be in accordance with the material procurement specification AMS-H-81200.
Rationale
AMS2801D is a limited revision which revises the racking requirement for fasteners and small parts (see 3.3.2.2) and adds a new Table 7 to allow higher processing temperature for Beta alloys with related changes to Hydrogen Pick-Up (see 3.4.1) and Surface Contamination (see 3.4.2) provisions. Subsequent table numbers have been revised based on the addition of Table 7.
The committee of Titanium, Beryllium, and Refractory Materials, AMS Committee G, is responsible for preparation, revision, review and approval of documents related to aerospace application of these materials. Included are titanium, beryllium, and refractory metallic such as molybdenum, tantalum, and columbium. The committee provides a forum for interchange of experience and ideas among industry representatives, both suppliers and users, along with interested government agencies, to ensure the utility, proper technical content, and industry acceptance of published documents.
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AMS2801D
Heat Treatment of Titanium Alloy Parts
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Heat Treatment of Titanium Alloy Parts
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