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9540-01-353-5555
Structural Beam
9540013535555 013535555 60-685 AMS-QQ-A-200/3 4E117 QQ-A-200/3
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 9540-01-353-5555
9540-01-353-5555 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. This item does not contain a precious metal.
End Users 9540-01-353-5555
- Brazil (YA01)
- Effective Date:
- 1 Jul 2001
Approved Sources 9540-01-353-5555
- Part Number
- Manufacturer
- Status
- 60-685
- Manufacturer
- 29321 - Transtar Metals Corp (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-200/3
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 4E117
- 43999 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- QQ-A-200/3
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/3
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-353-5555
- 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 Radius [AJJB]
- 0.031 Inches Nominal
- First Tip Style [CMZY]
- Full Radius
- Heat Treatment [HEAT]
- T-8511 Solution Heat Treated
- Material Document And Classification [MDCL]
- Qq-A-200/3 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- T8511 Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.875 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.062 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.062 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 0.875 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.062 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.000 Inches Nominal
- Top Flange Width [BQJG]
- 1.750 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.203 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
NATO Stock Numbers Related to 9540-01-353-5555
Freight Information 9540-01-353-5555
9540-01-353-5555 has freight characteristics.. 9540-01-353-5555 has a variance between NMFC and UFC when transported by rail and the description should be consulted.