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9540-01-436-1422
Structural Angle
9540014361422 014361422 3326619-3
A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet. View more Structural Angle
January 2023
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Restrictions 9540-01-436-1422
9540-01-436-1422 is a Structural Angle 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 9540-01-436-1422
- United Kingdom (ZK01)
- Effective Date:
- 1 Sep 1996
Approved Sources 9540-01-436-1422
- Part Number
- Manufacturer
- Status
- 3326619-3
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-436-1422
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.144 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- First Tip Style [CMZY]
- Square End
- End Item Identification [AGAV]
- C130-J Hercules
- Material [MATT]
- Aluminum Alloy
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.144 Inches Nominal
- Length [ABRY]
- 4.500 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.250 Inches Nominal
- Overall Width [ABMK]
- 3.250 Inches Nominal
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Freight Information 9540-01-436-1422
9540-01-436-1422 has freight characteristics managed by the Bureau of Accounts.. 9540-01-436-1422 has a variance between NMFC and UFC when transported by rail and the description should be consulted.