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9540-00-027-9188
Structural Beam
9540000279188 000279188 LS6162
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 9540-00-027-9188
9540-00-027-9188 is a Structural Beam that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 9540-00-027-9188
- Italy (ZR01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-027-9188
- Part Number
- Manufacturer
- Status
- LS6162
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-00-027-9188
- 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]
- 0.094 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.094 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Material [MATT]
- Aluminum Alloy
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.500 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.060 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.060 Inches Nominal
- Length [ABRY]
- 0.089 Feet Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 0.500 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.060 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.060 Inches Nominal
- Top Flange Width [BQJG]
- 1.000 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.137 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
NATO Stock Numbers Related to 9540-00-027-9188
Freight Information 9540-00-027-9188
9540-00-027-9188 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. 9540-00-027-9188 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. 9540-00-027-9188 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. 9540-00-027-9188 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. 9540-00-027-9188 is not classified as a special type of cargo when transported by water. 9540-00-027-9188 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.