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5310-01-451-4413

Cap Self-Locking Nut

5310014514413 014514413 26CL02

A nut internally threaded from one end, and completely enclosed on the opposite end. The outer periphery parallel to the threaded axis may be square, cylindrical, hexagonal, octagonal, dodecagonal or the like and taper to a cone or dome shape on the closed end. An integral feature is incorporated for locking on the threads of a mating memeber. Excludes NUT (1), STAMPED. View more Cap Self-Locking Nut

5310-01-451-4413 NUT,SELF-LOCKING,CAP 5310014514413 014514413

Managed by United States
NSN Created on 16 Dec 1997
Data Last Changed
January 2023
NATO Update Count
9
NATO Data Quality
ACTA Style A10 for 5310-01-451-4413 1/1
NSN 5310-01-451-4413 (Identification) 1/1

5310-01-451-4413 Stock and Availability Marketplace 5310-01-451-4413

5310-01-451-4413 Related Documents Related Documents 5310-01-451-4413 3+ Documents (More...)

26CL02 A nut internally threaded from one end, and completely enclosed on the opposite end.
Quotation Updated Every Day 5310-01-451-4413 RQST NE Updated Every Day 5310-01-451-4413 RQST Updated
Every Day 5310-01-451-4413 RQST NE Related Documents 5310-01-451-4413 3+ Documents ( More... ) https
Request a Quotation from participating marketplace vendors Request Subscribe to View Vendor Details... 26CL02
NUT,SELF-LOCKING,CAP 114 EA NS Request Quotation Subscribe to View Vendor Details... 26CL02 NUT,SELF-LOCKING
,CAP 574 EA NS Request Quotation Subscribe to View Vendor Details... 26CL02 NUT,SELF-LOCKING,CAP 574
$1 a day Upgrade your Account Upgrade 5310-00-915-8077Cap Self-Locking Nut5310009158077 009158077 26CL02
Quotation Subscribe to View Vendor Details... 26CL02 NUT,SELF-LOCKING,CAP 48 EA NS Request Quotation
F22K1-02 NUT,SELF-LOCKING,CAP 85 EA NS Request Quotation 26CL02 NUT,SELF-LOCKING,CAP 20 EA NS Request

5310-01-451-4413 Demil Restrictions 5310-01-451-4413

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

5310-01-451-4413 is a Cap 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. This item does not contain a precious metal.

5310-01-451-4413 HTS and ScheduleB Import and Export 5310-01-451-4413

5310-01-451-4413 End Users End Users 5310-01-451-4413

Australia (ZA01)
Effective Date:
1 Oct 2001
Belgium (ZB01)
Effective Date:
1 Jan 2002
Canada (ZC01)
Effective Date:
1 Jun 2012
United Kingdom (ZK01)
Effective Date:
1 Dec 1997

5310-01-451-4413 Manufacturers Approved Sources 5310-01-451-4413

5310-01-451-4413 Technical Data Datasheet 5310-01-451-4413

Characteristic
Specifications
FIIG
A021A0
Bearing Surface Type [CRTM]
Chamfered
End Item Identification [AGAV]
Used On C130-J Hercules Aircraft
Material [MATT]
Steel Overall
Nominal Thread Size [CQJX]
0.190 Inches
Nut Height [ADEA]
0.375 Inches Nominal
Nut Style [ACTA]
Cap
Locking Feature [AAUM]
Prevailing Torque With Nonmetallic Insert
Thread Series [BZRR]
Unc
Thread Quantity Per Inch [CMLP]
32
Width Across Flats [ASDB]
0.390 Inches Maximum
Surface Treatment Document And Classification [STDC]
Qq-F-416 Ty 2 Cl 3 Fed Spec Single Treatment Response Overall
Surface Treatment [SFTT]
Cadmium Overall And Chromate Overall
Temp Rating [AZKQ]
450.0 Deg Fahrenheit Nominal
Thread Class [AAJD]
3B
Thread Direction [AAJF]
Right-Hand

5310-01-451-4413 Related Items NATO Stock Numbers Related to 5310-01-451-4413

5310-01-451-4413 Freight Data Freight Information 5310-01-451-4413

5310-01-451-4413 has freight characteristics managed by the Bureau of Accounts.. 5310-01-451-4413 has a variance between NMFC and UFC when transported by rail and the description should be consulted.