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9540-01-323-9701
Structural Beam
9540013239701 013239701 LS043-1243 2024-T3511 60-19141 AMS-QQ-A-200/3 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 9540-01-323-9701
9540-01-323-9701 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 9540-01-323-9701
- Brazil (YA01)
- Effective Date:
- 1 Jul 2001
Approved Sources 9540-01-323-9701
- Part Number
- Manufacturer
- Status
- LS043-1243 2024-T3511
- Manufacturer
- 43999 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- 60-19141
- 29321 - Transtar Metals Corp (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-200/3
- 0U583 - Sae International (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 9540-01-323-9701
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Z Shape
- Bottom Flange Width [BQJH]
- 2.280 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.125 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- T-3511 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]
- T3511 Temper
- Left Side Top Flange Thickness [ADXR]
- 0.095 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Bottom Flange Thickness [BMPQ]
- 0.080 Inches Nominal
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 3.165 Inches Nominal
- Top Flange Width [BQJG]
- 2.100 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.825 Pounds Per Linear Foot
- Web Flange Thickness [BPXN]
- 0.100 Inches Nominal
NATO Stock Numbers Related to 9540-01-323-9701
Freight Information 9540-01-323-9701
9540-01-323-9701 has freight characteristics.. 9540-01-323-9701 has a variance between NMFC and UFC when transported by rail and the description should be consulted.