5307-21-845-0284
Plain Stud
5307218450284 218450284 62620 9860 5307-5310
A headless fastener not exceeding 12 inches (304.8 mm) in length, threaded externally on both ends with threads of the same nominal diameter. The maximum diameter of the unthreaded portion must not be greater than the nominal thread diameter plus 0.020 inches (0.508 mm). The unthreaded portion must be without locking or wrenching provisions. It may be thread relieved. See also ROD, THREADED END and ROD, CONTINUOUS THREAD. View more Plain Stud
Managed by Canada
NSN Created on 6 Oct 1968
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 5307-21-845-0284 5+ Documents (More...)
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Corp The.Who is CAGE Code 62620?
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Upgrade your Account Upgrade 4920-01-080-0226Anti-Icing Fixture Tooling Ball4920010800226 010800226 62620
enable JavaScript in your web browser . 1560-99-661-9427Aircraft Door1560996619427 996619427 S6120-62620
S6120-62620-19 An item which is a component of the structure of an aircraft. -3 S6120-62620-3 DOOR,ACCESS
enable JavaScript in your web browser . 1560-99-661-9427Aircraft Door1560996619427 996619427 S6120-62620
S6120-62620-19 An item which is a component of the structure of an aircraft. -3 S6120-62620-3 DOOR,ACCESS
enable JavaScript in your web browser . 1560-99-661-9427Aircraft Door1560996619427 996619427 S6120-62620
S6120-62620-19 An item which is a component of the structure of an aircraft.
-3 S6120-62620-3 DOOR,ACCESS,AIRCRAFT 6 EA NS Request Quotation S6120626203 DOOR,ACCESS,AIRCRAFT https
S6120-62620-19 An item which is a component of the structure of an aircraft.
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Restrictions 5307-21-845-0284
End Users 5307-21-845-0284
- Canada (ZC)
Approved Sources 5307-21-845-0284
- Part Number
- Manufacturer
- Status
- 62620
- Manufacturer
- 35086 - Slater Industries Incslacan Div (Active)
- Primary Buy
- Primary Buy
- 9860
- 35086 - Slater Industries Incslacan Div (Active)
- Secondary Buy
- Secondary Buy
- 5307-5310
- 35925 - Transport Canadamateriel And (Active)
- NATO Reference
- NATO Reference
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