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9540-01-444-6076
Structural Angle
9540014446076 014446076 389253-1
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 9540-01-444-6076
9540-01-444-6076 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 9540-01-444-6076
- United Kingdom (ZK01)
- Effective Date:
- 1 May 1997
Approved Sources 9540-01-444-6076
- Part Number
- Manufacturer
- Status
- 389253-1
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-444-6076
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- First Tip Style [CMZY]
- Left Taper Length
- First Tip Thickness [CNPS]
- 0.820 Inches Nominal
- Material [MATT]
- Aluminum Alloy
- End Item Identification [AGAV]
- Panel Support Angle Bl 42.0L, Fus Sta 245.0, C130-J Acft
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Lower Taper Length
- Second Tip Thickness [CNPT]
- 0.750 Inches Nominal
- Special Features [FEAT]
- 2 Holes 0.193/0.199 In. Dia
- Overall Height [ABKW]
- 2.000 Inches Nominal
- Overall Width [ABMK]
- 2.000 Inches Nominal
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Freight Information 9540-01-444-6076
9540-01-444-6076 has freight characteristics managed by the Bureau of Accounts.. 9540-01-444-6076 has a variance between NMFC and UFC when transported by rail and the description should be consulted.