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5310-01-424-2375

Hexagon Castellated Self-Locking Nut

5310014242375 014242375 E9925-16 3D0026-16

A nut having 6 flat sides, flat on the bottom and having a slotted cylindrical or dome shaped upper portion. An integral feature is incorporated for locking on the threads of a mating member. The slots when used in conjunction with a solid or split (cotter) pin, act as an extra "fail safe" feature in critical applications. Excludes NUT (1), SELF-LOCKING, SLOTTED, HEXAGON. View more Hexagon Castellated Self-Locking Nut

5310-01-424-2375 NUT,SELF-LOCKING,CASTELLATED,HEXAGON 5310014242375 014242375

Managed by United States
NSN Created on 24 Jan 1996
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
ACTA Style A1 for 5310-01-424-2375 1/1
NSN 5310-01-424-2375 (Identification) 1/1

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5310-01-424-2375 Related Documents Related Documents 5310-01-424-2375 1+ Documents (More...)

00-431-8844 Hexagon Castellated Self-Locking Nut 230647RNCC: 3 | RNVC: 2 | DAC: 5 28 Apr 1971 5310-01-424-2375

5310-01-424-2375 Demil Restrictions 5310-01-424-2375

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

5310-01-424-2375 is a Hexagon Castellated 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 contains Silver.

5310-01-424-2375 HTS and ScheduleB Import and Export 5310-01-424-2375

5310-01-424-2375 End Users End Users 5310-01-424-2375

US Air Force (FBB5)
Effective Date:
1 May 2000
Former MOE Rule:
FEKZ

5310-01-424-2375 Manufacturers Approved Sources 5310-01-424-2375

5310-01-424-2375 Technical Data Datasheet 5310-01-424-2375

Characteristic
Specifications
FIIG
A021A0
Bearing Surface Type [CRTM]
Chamfered
Hardness Rating [CQFM]
46.0 Rockwell C Maximum
Material [MATT]
Iron Alloy 660 Overall
Nominal Thread Size [CQJX]
1.000 Inches
Nut Style [ACTA]
Castellated, Hexagon
Nut Height [ADEA]
1.000 Inches Nominal
Locking Feature [AAUM]
Prevailing Torque All Metal Design
Material Document And Classification [MDCL]
Ams 5737 Assn Std Single Material Response Overall
Precious Material [PRMT]
Silver
Precious Material And Location [PMLC]
Overall Silver
Thread Series [BZRR]
Unjf
Thread Quantity Per Inch [CMLP]
12
Width Across Flats [ASDB]
1.110 Inches Minimum And 1.130 Inches Maximum
Surface Treatment Document And Classification [STDC]
Ams2410 Assn Std Single Treatment Response Overall And Ams2411 Assn Std Single Treatment Response Overall
Surface Treatment [SFTT]
Silver Overall
Thread Class [AAJD]
3B
Thread Direction [AAJF]
Right-Hand

5310-01-424-2375 Management Data Management Data 5310-01-424-2375

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Aug 2005
Department of the Air Force (DF)
EA
Subscribe

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5310-01-424-2375 Freight Data Freight Information 5310-01-424-2375

5310-01-424-2375 has freight characteristics.. 5310-01-424-2375 has a variance between NMFC and UFC when transported by rail and the description should be consulted.