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5310-01-253-4150
Clinch Self-Locking Nut
5310012534150 012534150 512516-1
A nut having a sleeve portion on its under side, which can be crimped or clinched to hold the item in place when inserted in a hole. An integral feature is incorporated for locking. View more Clinch Self-Locking Nut
January 2023
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Clinch Self-Locking Nut 5310012534150 512516-1 A nut having a sleeve portion on its under side, which
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Restrictions 5310-01-253-4150
5310-01-253-4150 is a Clinch Self-Locking Nut 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 5310-01-253-4150
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5310-01-253-4150
- Belgium (ZB01)
- Effective Date:
- 1 Apr 1991
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
Approved Sources 5310-01-253-4150
- Part Number
- Manufacturer
- Status
- 512516-1
- Manufacturer
- 37695 - Raytheon Company (Active)
- Primary Buy
- Primary Buy
Datasheet 5310-01-253-4150
- Characteristic
- Specifications
- FIIG
- Specifications
- A021A0
- Thread Series [BZRR]
- Uns
- Nominal Thread Size [CQJX]
- 0.2500 Inches
- Thread Quantity Per Inch [CMLP]
- 40
- Thread Class [AAJD]
- 2B
- Thread Direction [AAJF]
- Right-Hand
- Material [MATT]
- Aluminum Alloy 6061 Overall
- Material Document And Classification [MDCL]
- Qq-A-225/8-T6 Fed Spec Single Material Response Overall
- Surface Treatment [SFTT]
- Anodize Overall
- Surface Treatment Document And Classification [STDC]
- Mil-A-8625 Ty2 Cl2 Mil Spec Single Treatment Response Overall
- Nut Style [ACTA]
- Clinch
- Pilot Diameter [AAVL]
- 0.323 Inches Nominal
- Pilot Length [AAVM]
- 0.094 Inches Nominal
- Nut Diameter [ACTD]
- 0.375 Inches Nominal
- Nut Height [ADEA]
- 0.460 Inches Nominal
- Locking Feature [AAUM]
- Prevailing Torque All Metal Design
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Freight Information 5310-01-253-4150
5310-01-253-4150 has freight characteristics managed by Canada.. 5310-01-253-4150 has a variance between NMFC and UFC when transported by rail and the description should be consulted.