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9540-01-478-9730
Structural Beam
9540014789730 014789730 HS1006DD61-0708
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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Restrictions 9540-01-478-9730
9540-01-478-9730 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 9540-01-478-9730
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 9540-01-478-9730
- United Kingdom (ZK01)
- Effective Date:
- 1 Oct 2000
Approved Sources 9540-01-478-9730
- Part Number
- Manufacturer
- Status
- HS1006DD61-0708
- Manufacturer
- 8V613 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-478-9730
- 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]
- 0.062 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.062 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- T-4 Solution Heat Treated Or T-3511 Solution Heat Treated
- End Item Identification [AGAV]
- Apache Helicopter
- Material Document And Classification [MDCL]
- Qq-A-200/3 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 2024
- Part Name Assigned By Controlling Agency [CXCY]
- Extrusion, Tee, Aluminum Alloy
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.000 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.050 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.050 Inches Nominal
- Length [ABRY]
- 7.250 Inches Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.000 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.050 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.180 Inches Nominal
- Top Flange Width [BQJG]
- 2.000 Inches Nominal
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
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Freight Information 9540-01-478-9730
9540-01-478-9730 has freight characteristics managed by the Bureau of Engraving and Printing.. 9540-01-478-9730 has a variance between NMFC and UFC when transported by rail and the description should be consulted.