DMS 1962 - 6Al-6V-2Sn Titanium Alloy Extrusions (Boeing/Douglas, Annealed)
DMS 1962 is the Boeing / McDonnell Douglas Material Specification for 6Al-6V-2Sn Titanium Alloy extrusions in the annealed condition. Titanium extrusions allow complex cross-section structural shapes — I-beams, Z-sections, channels, and custom profiles — to be produced in the high-strength 6Al-6V-2Sn alloy system, enabling efficient structural designs that reduce part count and fastener holes compared to built-up fabrications.
Extrusions per DMS 1962 are used in Boeing and Douglas aircraft stringer-frame structures, wing box members, and longitudinal structural elements where the combination of 6Al-6V-2Sn strength and extrusion cross-section efficiency provides the lightest structural solution.
6Al-6V-2Sn titanium alloy offers higher strength than 6Al-4V in the solution treated and aged condition, making it the preferred choice for the most highly stressed aerospace structural applications where standard 6Al-4V STA cannot meet design requirements.
Applications of DMS 1962 6Al-6V-2Sn Titanium
- Boeing and Douglas Structural Stringers and Frames
- Wing Box Structural Members
- Airframe Extrusion Sections
- Military Aircraft Structural Extrusions
AMS Titanium Specifications
SAE AMS material specifications for 6Al-6V-2Sn titanium alloy covering bars, billets, forgings, sheet, and strip for aerospace structural and engine applications.
Boeing / McDonnell Douglas Material Specifications
Boeing and McDonnell Douglas DMS and MMS material specifications for 6Al-6V-2Sn titanium alloy for Boeing, Douglas, and St. Louis aerospace programs.
Gulfstream Material Specifications
Gulfstream Material Specifications (GMS) for 6Al-6V-2Sn titanium alloy for Gulfstream business jet aerospace structural programs.
Certified Material for Critical Service
Materials supplied in 6Al-6V-2Sn titanium must meet strict aerospace certification and traceability requirements. Fighter Jet Metals supports sourcing across a wide range of AMS, MIL, and OEM specifications, ensuring compliance with industry standards.
All material is supplied with full mill certifications, complete heat-lot traceability, and detailed documentation. This ensures reliability and suitability for safety-critical aerospace, defense, and high-performance engineering applications.