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9540-00-610-6902
Structural Beam
9540006106902 006106902 AMS-QQA200-13 1M5507-11396 QQA200-13
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
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Restrictions 9540-00-610-6902
9540-00-610-6902 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 9540-00-610-6902
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-610-6902
- Part Number
- Manufacturer
- Status
- AMS-QQA200-13
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 1M5507-11396
- 76301 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- QQA200-13
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQA200-13
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-610-6902
- 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 Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- O-Annealed
- Material Document And Classification [MDCL]
- Qq-A-200/13 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7178
- Nondefinitive Spec/Std Data [ZZZT]
- 0 Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.650 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]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.650 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]
- 1.700 Inches Nominal
- Top Flange Width [BQJG]
- 3.300 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.360 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
NATO Stock Numbers Related to 9540-00-610-6902
Freight Information 9540-00-610-6902
9540-00-610-6902 has freight characteristics managed by the Southwestern Power Administration.. 9540-00-610-6902 has a variance between NMFC and UFC when transported by rail and the description should be consulted.