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5325-00-543-3769
Turnlock Fastener Stud Assembly
5325005433769 005433769 2600-11S GS521A11S FON20-7524-11 9167787
A STUD, TURNLOCK FASTENER over which may be assembled an EYELET, TURNLOCK FASTENER. Stud(s) without cam slots or cam lead threads are provided with a crosspin or eared nut for locking with the mating RECEPTACLE, TURNLOCK FASTENER. May be spring loaded. For like items having a threaded fastener, see SCREW ASSEMBLY, PANEL or SCREW, PANEL FASTENER. View more Turnlock Fastener Stud Assembly
June 2023
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14-441-7185Turnlock Fastener Stud Assembly5325144417185 144417185NSA55132-0112600-11S J820 DAC 5 2600-11S
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005433769 2600-11S GS521A11S FON20-7524-11 GS521A11S 26512 - Northrop Grumman Systems Corporation (Active
STUD ASSEMBLY,TURNLOCK FASTENER RQST NS Request Quotation Subscribe to View Vendor Details... 2600-11S
Restrictions 5325-00-716-8971 DEMIL: A | DEMILI https//www.nsnlookup.com /fsg-53/fsc-5325/us 5325-00-543-3769
Restrictions 5325-00-543-3769
5325-00-543-3769 is a Turnlock Fastener Stud 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. The precious metals content of this item is unknown.
Import and Export 5325-00-543-3769
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5325-00-543-3769
- Brazil (YA01)
- Effective Date:
- 1 Jul 2010
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Singapore (YJ01)
- Effective Date:
- 1 Dec 2007
- Australia (ZA01)
- Effective Date:
- 1 Apr 1991
- France (ZF01)
- Effective Date:
- 1 Apr 1991
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
- Netherlands (ZN01)
- Effective Date:
- 1 Jul 2010
- Denmark (ZS01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Aug 1995
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
- NATO Maintenance and Supply Agency (ZX01)
- Effective Date:
- 1 Apr 2011
Approved Sources 5325-00-543-3769
- Part Number
- Manufacturer
- Status
- 2600-11S
- Manufacturer
- 71286 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
- 2600-11S
- D0680 - Fairchild Fasteners Europe - Camloc (Active)
- Secondary Buy
- Secondary Buy
- GS521A11S
- 26512 - Northrop Grumman Systems Corporation (Active)
- Secondary Buy
- Secondary Buy
- FON20-7524-11
- H1822 - Gkn Fokker Aerospace B.V. (Active)
- Secondary Buy
- Secondary Buy
- 9167787
- 18876 - Us Army Aviation And Missile Command (Active)
- Secondary Buy
- Secondary Buy
Datasheet 5325-00-543-3769
- Characteristic
- Specifications
- FIIG
- Specifications
- A05400
- Distance From Engaging Member To Largest Bearing Surface Of Head [AGRF]
- 0.842 Inches Minimum And 0.857 Inches Maximum
- Drive Type [AKCV]
- Slotted
- Diameter [ABMZ]
- 0.298 Inches Minimum And 0.308 Inches Maximum
- Eyelet Length [AGRK]
- 0.244 Inches Minimum And 0.250 Inches Maximum
- Eyelet Outside Diameter [AGRH]
- 0.244 Inches Minimum And 0.250 Inches Maximum
- Material [MATT]
- Steel Overall
- Material Accommodated Thickness [AGSM]
- 0.330 Inches Minimum And 0.359 Inches Maximum
- Securing Device Type [ADQB]
- Spring
- Turnlock Stud Head Style [AGRD]
- Flat Fillister
- Stud Head Height [CQYY]
- 0.088 Inches Minimum And 0.098 Inches Maximum
- Stud Assembly Style [AGRE]
- Stud Assembly
- Surface Treatment [SFTT]
- Passivate Overall
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Freight Information 5325-00-543-3769
5325-00-543-3769 has freight characteristics.. 5325-00-543-3769 has a variance between NMFC and UFC when transported by rail and the description should be consulted.