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9540-01-616-5910
Structural Beam
9540016165910 016165910 S1243285T
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 9540-01-616-5910 1+ Documents (More...)
United States (US) 4. 9540-01-616-5910 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 9540-01-616-5910
9540-01-616-5910 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 a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.
End Users 9540-01-616-5910
- US Air Force (FBB5)
- Effective Date:
- 1 Feb 2013
Approved Sources 9540-01-616-5910
- Part Number
- Manufacturer
- Status
- S1243285T
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-616-5910
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- T Shape
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.064 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.064 Inches Nominal
- First Tip Style [CMZY]
- Square End
- End Item Identification [AGAV]
- C-17A Globemaster Iii
- Material [MATT]
- Aluminum Alloy
- Part Name Assigned By Controlling Agency [CXCY]
- Extrusion
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.625 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.064 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.064 Inches Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 0.625 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.064 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.00 Inches Nominal
- Top Flange Width [BQJG]
- 1.25 Inches Nominal
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
Management Data 9540-01-616-5910
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2013
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
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Freight Information 9540-01-616-5910
9540-01-616-5910 has freight characteristics.. 9540-01-616-5910 has a variance between NMFC and UFC when transported by rail and the description should be consulted.