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9520-01-562-3816
Structural Angle
9520015623816 015623816 70201-22101-117
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
November 2023
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Related Documents 9520-01-562-3816 5+ Documents (More...)
7616 https//www.nsnlookup.com /fsg-95/fsc-9520 Structural Shapes from United States (US) 2008 9520-01-562-3816
Structural Angle 9520015623816 015623816 https//www.nsnlookup.com /nato/nato-stock-numbers/inc
Restrictions 9520-01-562-3816
9520-01-562-3816 is a Structural Angle that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 9520-01-562-3816
- Australia (ZA01)
- Effective Date:
- 1 Apr 2008
Approved Sources 9520-01-562-3816
- Part Number
- Manufacturer
- Status
- 70201-22101-117
- Manufacturer
- 78286 - Sikorsky Aircraft Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 9520-01-562-3816
- Characteristic
- Specifications
- Material Document And Classification [MDCL]
- Specifications
- Qq-A-250/11 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 6061
- Special Features [FEAT]
- Used On The Upper Fuselage Frame
NATO Stock Numbers Related to 9520-01-562-3816
Freight Information 9520-01-562-3816
9520-01-562-3816 has freight characteristics managed by Australia.. 9520-01-562-3816 has a variance between NMFC and UFC when transported by rail and the description should be consulted.