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5305-01-516-1908
Panel Screw Assembly
5305015161908 015161908 CA2292-10-19-16
A headed, threaded fastening device over which may be assembled; (1) a stand-off; (2) a flanged bushing with washer(s) and/or a shouldered bushing without a flange, or it may have an internally threaded sleeve that is an integral part of the screw; a washer and an externally thread self-locking bushing that is driven by an inserted driver. Attached to panel by threaded bushing or by flaring end of stand-off, or bushing. Used in conjunction with a speed nut, nut plate, or driven into a threaded hole in the item that the panel is fastened to. May be spring loaded. View more Panel Screw Assembly
May 2023
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Restrictions 5305-01-516-1908
5305-01-516-1908 is a Panel Screw Assembly that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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 5305-01-516-1908
- US Air Force (FLL5)
- Effective Date:
- 1 Dec 2003
Approved Sources 5305-01-516-1908
- Part Number
- Manufacturer
- Status
- CA2292-10-19-16
- Manufacturer
- 29372 - Howmet Global Fastening Systems Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 5305-01-516-1908
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- End Item Identification [AGAV]
- F/A-22 Raptor
- Part Name Assigned By Controlling Agency [CXCY]
- Screw Assembly, Pane
Management Data 5305-01-516-1908
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Freight Information 5305-01-516-1908
5305-01-516-1908 has freight characteristics.. 5305-01-516-1908 has a variance between NMFC and UFC when transported by rail and the description should be consulted.