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9540-01-232-7036
Structural Beam
9540012327036 012327036 SS1512-4
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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Related Documents 9540-01-232-7036 1+ Documents (More...)
RQST Updated Every Day 9540-01-232 - 7036 Restrictions 9540-01 - 232 -7036 Restrictions 9540-01-232-7036
Restrictions 9540-01-232-7036 Restrictions 9540-01-232-7036 DEMIL: A | DEMILI : | CRITICALITY : X |
Restrictions 9540-01-232-7036
9540-01-232-7036 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 9540-01-232-7036
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-01-232-7036
- Part Number
- Manufacturer
- Status
- SS1512-4
- Manufacturer
- 78286 - Sikorsky Aircraft Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-232-7036
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Z Shape
- Bottom Flange Width [BQJH]
- 0.780 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.156 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.156 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Material Document And Classification [MDCL]
- Qq-A-250/13 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075 And Aluminum Alloy 7072
- Left Side Top Flange Thickness [ADXR]
- 0.063 Inches Nominal
- Right Side Bottom Flange Thickness [BMPQ]
- 0.063 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.060 Inches Nominal
- Top Flange Width [BQJG]
- 0.310 Inches Nominal
- Web Flange Thickness [BPXN]
- 0.063 Inches Nominal
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Freight Information 9540-01-232-7036
9540-01-232-7036 has freight characteristics managed by Germany.. 9540-01-232-7036 has a variance between NMFC and UFC when transported by rail and the description should be consulted.