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9540-00-973-7841
Structural Beam
9540009737841 009737841 LS4113
A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges. View more Structural Beam
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Restrictions 9540-00-973-7841
9540-00-973-7841 is a Structural Beam that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.
End Users 9540-00-973-7841
- Italy (ZR01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-973-7841
- Part Number
- Manufacturer
- Status
- LS4113
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-00-973-7841
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- T Shape
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.125 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.125 Inches Nominal
- First Tip Inner Radius [CNBD]
- 0.031 Inches Nominal
- First Tip Outer Radius [CNBJ]
- 0.031 Inches Nominal
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- Heat Treatment [HEAT]
- T-1 Solution Heat Treated And Artifically Aged
- Material [MATT]
- Aluminum Alloy,Qq-A-200/11,Alloy 7075
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.062 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.156 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.156 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.063 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.156 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 2.250 Inches Nominal
- Top Flange Width [BQJG]
- 2.125 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.790 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
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Freight Information 9540-00-973-7841
9540-00-973-7841 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 013220. A Sub NMFC of X. It has a NMFC Description of ALUM BEAMS. 9540-00-973-7841 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. 9540-00-973-7841 is rated as class 60 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 05420 which rates the freight between FCL and LCL. 9540-00-973-7841 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 576 for ocean manifesting and military sealift. 9540-00-973-7841 is not classified as a special type of cargo when transported by water. 9540-00-973-7841 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.