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5310-01-522-2868

Hexagon Single Ball Seat Self-Locking Nut

5310015222868 015222868 KFN619N10

A nut having one convex, spherical bearing surface and 6 flat sides. Items may have a removable collar. An integral feature is incorporated for locking on the threads of a mating member. See also NUT (1), SELF-LOCKING, CONE SEAT, HEXAGON. View more Hexagon Single Ball Seat Self-Locking Nut

5310-01-522-2868 NUT,SELF-LOCKING,SINGLE BALL SEAT,HEXAGON 5310015222868 015222868

Managed by United States
NSN Created on 26 Jul 2004
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
ACTA Style A8B for 5310-01-522-2868 1/1
NSN 5310-01-522-2868 (Identification) 1/1

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5310-01-522-2868 Related Documents Related Documents 5310-01-522-2868 2+ Documents (More...)

Assigned By Controlling Agency [CXCY]Washer, Self Aligning, ConcaveSpecial Features [FEAT]Used With P/N Kfn619n10
Single Ball Seat Self-Locking Nut 3D0006-7RNCC: 3 | RNVC: 2 | MEDALS: Y | DAC: A 19 Jun 1996 5310-01-522-2868

5310-01-522-2868 Demil Restrictions 5310-01-522-2868

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

5310-01-522-2868 is a Hexagon Single Ball Seat 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.

5310-01-522-2868 HTS and ScheduleB Import and Export 5310-01-522-2868

5310-01-522-2868 End Users End Users 5310-01-522-2868

United Kingdom (ZK01)
Effective Date:
1 Jul 2004

5310-01-522-2868 Manufacturers Approved Sources 5310-01-522-2868

5310-01-522-2868 Technical Data Datasheet 5310-01-522-2868

Characteristic
Specifications
FIIG
A021A0
End Item Identification [AGAV]
C-130J Hercules Aircraft
Ball Seat Radius [ACTC]
0.313 Inches Minimum And 0.318 Inches Maximum
Material [MATT]
Aluminum Alloy 7075 Overall
Nominal Thread Size [CQJX]
0.3125 Inches
Nut Height [ADEA]
0.372 Inches Maximum
Nut Style [ACTA]
Single Ball Seat, Hexagon
Locking Feature [AAUM]
Prevailing Torque All Metal Design
Material Document And Classification [MDCL]
Ams-Qq-A-225/9 Assn Std Single Material Response Overall
Part Name Assigned By Controlling Agency [CXCY]
Nut - 6 Point, Self Locking, Self Aligning
Special Features [FEAT]
Color Red; Cetyl Alcohol Lubricant; Three Cycle Reusablility; Upper Threaded Portion Formed Out Of Round To Provide Self Locking Action
Thread Series [BZRR]
Unjf
Thread Quantity Per Inch [CMLP]
24
Width Across Flats [ASDB]
0.357 Inches Minimum And 0.376 Inches Maximum
Surface Treatment [SFTT]
Passivate Overall
Thread Class [AAJD]
3B
Thread Direction [AAJF]
Right-Hand

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5310-01-522-2868 Freight Data Freight Information 5310-01-522-2868

5310-01-522-2868 has freight characteristics managed by the Bureau of Accounts.. 5310-01-522-2868 has a variance between NMFC and UFC when transported by rail and the description should be consulted.