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9540-01-486-6271
Structural Beam
9540014866271 014866271 LS4725
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
January 2023
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Related Documents 9540-01-486-6271 1+ Documents (More...)
/fsg-95/fsc-9540/us 9540-01-486-6271 /fsg-95/fsc-9540/us 9540-01-486-6271 /fsg-95/fsc-9540/us 9540-01
-486-6271 /fsg-95/fsc-9540/us 9540-01 -486-6271 /fsg-95/fsc-9540/us 9540-01 -486-6271 /fsg-95/fsc-9540
Restrictions 9540-01-486-6271
9540-01-486-6271 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. This item does not contain a precious metal.
End Users 9540-01-486-6271
- New Zealand (ZE01)
- Effective Date:
- 1 Jul 2001
Approved Sources 9540-01-486-6271
- Part Number
- Manufacturer
- Status
- LS4725
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-486-6271
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- T Shape
- Fabrication Method [AARN]
- Any Acceptable
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.031 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.031 Inches Nominal
- First Tip Style [CMZY]
- Square End
- End Item Identification [AGAV]
- C-130 Aircraft
- Material [MATT]
- Aluminum Alloy
- Part Name Assigned By Controlling Agency [CXCY]
- Extrusion, Aluminum
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.781 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.125 Inches Nominal
- Leg Thickness [AJJP]
- 0.094 Inches Nominal
- Length [ABRY]
- 1.750 Inches Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 0.781 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.125 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.600 Inches Nominal
- Special Features [FEAT]
- Material 7075-T6
- Top Flange Width [BQJG]
- 1.750 Inches Nominal
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Freight Information 9540-01-486-6271
9540-01-486-6271 has freight characteristics managed by New Zealand.. 9540-01-486-6271 has a variance between NMFC and UFC when transported by rail and the description should be consulted.