Continental Steel & Tube offers a wide range of aluminum extrusions in a variety of alloy grades and tempers.
Aluminum Extrusion Part Numbers
- Army Navy: AND
- Boeing: BAC
- Federal: S-
- Grumman Aerospace: GS
- International: LN
- Lockheed Martin: LS
- McDonnell Douglas: S
- Tierney: 60-
Including:
- Agusta
- Airbus
- ATR
- BAE Systems
- Bell Helicopters
- Bombardier
- Canadair
- Cessna
- Deutsche
- Douglas
- Embraer
- General Dynamics
- Lear Jet
- Northrop Grumman
- Sikorsky
- TSPE
Continental Steel is a leading provider of a number of BAC Extrusions and AND Extrusions in many different aluminum alloys and tempers. All material is ISO/AS approved This list includes, but is not limited to:
- BAC Extrusions
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BAC1489, BAC1490, BAC1491, BAC1492, BAC1493, BAC1494, BAC1495, BAC1496, BAC1498, BAC1500, BAC1517, BAC1501, BAC1503, BAC1514, BAC1504, BAC1505, BAC1506, BAC1507, BAC1508, BAC1509, BAC1510, BAC1518, BAC1511, BAC1512, BAC1513, BAC1519, BAC1520, BAC1521, BAC1522, BAC1530, BAC1534
- AND Extrusions
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AND10133, AND10134, AND10135, AND10136, AND10137, AND10138, AND10139, AND10140, AND10141
- Available Alloys
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1100, 2014, 2024, 2219, 5052, 5083, 5086, 5454, 5456, 6061, 6063, 7050, 7075, 7150, 7175, 7178
- Available Tempers
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F, T0, T3, T3511, T4, T4511, T5, T6, T651, T6511, T73, T7351, T73511, T76, T76511, T77, T851, T8511
Aerospace Extrusion Shapes:
- “L” Angles
- “H” Beams
- “Z” Sections
- “T” Sections
- Channels
- Roll Form
- Seat Track
- Wide Flanges
- Equal & unequal thickness and legs
- Custom Designed Shapes
AMS Specifications for Aluminum
AMS specifications evaluate materials, devices, and components that are used in aerospace and aircraft applications. The AMS specifications for aluminum involve requirements for aluminum alloy bars, rods, shapes, structural shapes, wires, tubes, and extrusions. Specific requirements for each of these products in a particular alloy are covered by a separate, detailed specification.
For example, the AMS specifications for an aluminum alloy involve its chemical composition, broken down into the required percentages of each included material, and ranges for tensile strength, yield strength, and elongation. There are separate specifications for tensile properties that vary according to a component’s engineering requirements, section thickness, and orientation.