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5305-01-600-0147
Panel Screw Assembly
5305016000147 016000147 CA2290-4-23-20
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 5305-01-600-0147
5305-01-600-0147 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. 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 5305-01-600-0147
- US Air Force (FLL5)
- Effective Date:
- 1 Nov 2011
Approved Sources 5305-01-600-0147
- Part Number
- Manufacturer
- Status
- CA2290-4-23-20
- Manufacturer
- 92215 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 5305-01-600-0147
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- End Item Identification [AGAV]
- F-22 Raptor Aircraft
Management Data 5305-01-600-0147
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Freight Information 5305-01-600-0147
5305-01-600-0147 has freight characteristics.. 5305-01-600-0147 has a variance between NMFC and UFC when transported by rail and the description should be consulted.