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5305-01-488-6868

Panel Screw Assembly

5305014886868 014886868 CA2290-06-5-10

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

5305-01-488-6868 SCREW ASSEMBLY,PANEL 5305014886868 014886868

Managed by United States
NSN Created on 30 Aug 2001
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
5305-01-488-6868 SCREW ASSEMBLY,PANEL 5305014886868 014886868 1/1
NSN 5305-01-488-6868 (Generic Image) 1/1

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5305-01-488-6868 Related Documents Related Documents 5305-01-488-6868 2+ Documents (More...)

CA2290-06-5-10 A headed, threaded fastening device over which may be assembled; (1) a stand-off; (2)
United States (US) 4. 5305-01-488-6868 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 5305-01-488-6868 RQST Updated Every Day 5305-01-488-6868 RQST NE Related Documents
3 RNVC 2 DAC 5 CA2290 https//www.nsnlookup.com https//www.nsnlookup.com /fsg-53/fsc-5305/us 5305-01-488-6868
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6868Panel Screw Assembly5305014886868 014886868 CA2290 www.nsnlookup.com /fsg-53/fsc-5305/us 5305-01-

5305-01-488-6868 Demil Restrictions 5305-01-488-6868

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

5305-01-488-6868 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.

5305-01-488-6868 End Users End Users 5305-01-488-6868

US Air Force (FLL5)
Effective Date:
1 Aug 2001

5305-01-488-6868 Manufacturers Approved Sources 5305-01-488-6868

5305-01-488-6868 Technical Data Datasheet 5305-01-488-6868

Characteristic
Specifications
FIIG
A003B0
End Item Identification [AGAV]
F/A-22 Raptor
Part Name Assigned By Controlling Agency [CXCY]
Captive Screw

5305-01-488-6868 Management Data Management Data 5305-01-488-6868

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2018
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
FR
F-22 AIRCRAFT
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5305-01-488-6868 Freight Data Freight Information 5305-01-488-6868

5305-01-488-6868 has freight characteristics.. 5305-01-488-6868 has a variance between NMFC and UFC when transported by rail and the description should be consulted.