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5315-01-513-9355
Lock Pin
5315015139355 015139355 5013125
A fastening device formed from resilient wire stock into a shape resembling the letter "U", of which at least one of the prongs is straight for insertion into a hole; the other prong may have one or more curvatures along its length. It is designed to hold itself in place by its inherent spring action. See also CLIP, RETAINING and RING, RETAINING. View more Lock Pin
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January 2023
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Related Documents 5315-01-513-9355 2+ Documents (More...)
Every Day 5315-01-513-9355 RQST NE Related Documents 5315-01-513-9355 2+ Documents ( More... ) https
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Lock Pin 5315015139355 015139355,5013125 01-513-9355 DEMIL: A | DEMILI : 1 | CRITICALITY https/
www.nsnlookup.com /fsg-34/fsc-3439/us 3439-01-326- 1749 Welding Rod 3439013261749 013261749,25-50131 25-5013125
Restrictions 5315-01-513-9355
5315-01-513-9355 is a Lock Pin 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 5315-01-513-9355
- Denmark (ZS01)
- Effective Date:
- 1 Oct 2003
Approved Sources 5315-01-513-9355
- Part Number
- Manufacturer
- Status
- 5013125
- Manufacturer
- 0B9R9 - Meggitt Aircraft Braking Systems (Active)
- Primary Buy
- Primary Buy
Datasheet 5315-01-513-9355
- Characteristic
- Specifications
- FIIG
- Specifications
- A212A0
- End Item Identification [AGAV]
- F-16 Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Pin, Countersunk Head
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Freight Information 5315-01-513-9355
5315-01-513-9355 has freight characteristics.. 5315-01-513-9355 has a variance between NMFC and UFC when transported by rail and the description should be consulted.