Premium Information is available for this item - Upgrade for $1 a day
9540-01-110-8928
Structural Beam
9540011108928 011108928 1M5798
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
May 2023
9
Marketplace 9540-01-110-8928
Request a Quotation from participating marketplace vendors
Related Documents 9540-01-110-8928 1+ Documents (More...)
-01-110-8928 /fsg-95/fsc-9540/us 9540 RQST Updated Every Day 9540-01-110 - 8928 Restrictions 9540-01
- 110 -8928 Restrictions 9540-01-110-8928 Restrictions 9540-01-110-8928 Restrictions 9540-01-110-8928
Restrictions 9540-01-110-8928
9540-01-110-8928 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 9540-01-110-8928
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-01-110-8928
- Part Number
- Manufacturer
- Status
- 1M5798
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-110-8928
- 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]
- 0.090 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.090 Inches Nominal
- First Tip Inner Radius [CNBD]
- 0.010 Inches Nominal
- First Tip Outer Radius [CNBJ]
- 0.010 Inches Nominal
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- Material Document And Classification [MDCL]
- Qq-A-200/3 Fed Spec 1St Material Response And Qq-A-200/13 Fed Spec 2Nd Material Response
- Material [MATT]
- Aluminum Alloy 2024 And Aluminum Alloy 7178
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.845 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
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 0.845 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.060 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 0.810 Inches Nominal
- Top Flange Width [BQJG]
- 1.750 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.024 Pounds Per Piece
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
Similar Supply Items to 9540-01-110-8928
Freight Information 9540-01-110-8928
9540-01-110-8928 has freight characteristics managed by Germany.. 9540-01-110-8928 has a variance between NMFC and UFC when transported by rail and the description should be consulted.