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9540-01-035-8128
Structural Beam
9540010358128 010358128 AMS-QQ-A-200/11 AND10136-2406 QQ-A-200/11
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 9540-01-035-8128
9540-01-035-8128 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 9540-01-035-8128
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-01-035-8128
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AND10136-2406
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- QQ-A-200/11
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-035-8128
- 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]
- 0.125 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.125 Inches Nominal
- First Tip Radius [AJJB]
- 0.156 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- Heat Treatment [HEAT]
- T-6511 Solution Heat Treated And Stress Relieved By Stretching
- Material [MATT]
- Aluminum Alloy,Qq-A-200/11,Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- T6511 Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.250 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.156 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.156 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 212.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.250 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.156 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.625 Inches Nominal
- Top Flange Width [BQJG]
- 2.500 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.740 Pounds Per Linear Foot
- Third Tip Radius [CNBB]
- 0.078 Inches Nominal
- Third Tip Style [CNQM]
- Full Radius
- Third Tip Relationship To Preceding Tips [CNQL]
- Not Identical
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Freight Information 9540-01-035-8128
9540-01-035-8128 has freight characteristics.. 9540-01-035-8128 has a variance between NMFC and UFC when transported by rail and the description should be consulted.