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5310-01-445-9278

Double Hexagon Self-Locking Nut

5310014459278 014459278 AS3397-10

A nut having 12 drive points and 24 sides. The bearing surface may be washer faced. An integral locking feature is incorporated in the design of the head or in the threads. View more Double Hexagon Self-Locking Nut

5310-01-445-9278 NUT,SELF-LOCKING,DOUBLE HEXAGON 5310014459278 014459278

Managed by United States
NSN Created on 17 Jun 1997
Data Last Changed
January 2023
NATO Update Count
6
NATO Data Quality
ACTA Style A16 for 5310-01-445-9278 1/1
NSN 5310-01-445-9278 (Identification) 1/1

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5310-01-445-9278 Related Documents Related Documents 5310-01-445-9278 3+ Documents (More...)

AS3397-10 A nut having 12 drive points and 24 sides.
RQST NE Updated Every Day 5310-01-445-9278 RQST Updated Every Day 5310-01-445-9278 RQST NE Related Documents
5310-01-445-9278 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-53/fsc-5310/us 5310-01-445-9278
Hexagon Self-Locking Nut5310014638853 014638853 AS3477-10 NSN SPECIFIC V-22 AE1107C ENGINE AS3066-10 AS3397-10
Double Hexagon Self-Locking Nut 014459278 Upgrade your Account Upgrade 5310-01-445-9278Double Hexagon
Self-Locking Nut5310014459278 014459278 AS3397-10 www.nsnlookup.com /fsg-53/fsc-5310/us 5310-01-445-
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Self-Locking Nut5310014459278 014459278 AS3397 NumberManufacturerStatusAS3397-10 0U583 - Sae International

5310-01-445-9278 Demil Restrictions 5310-01-445-9278

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

5310-01-445-9278 is a Double Hexagon 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.

5310-01-445-9278 HTS and ScheduleB Import and Export 5310-01-445-9278

5310-01-445-9278 End Users End Users 5310-01-445-9278

US Air Force (FII5)
Effective Date:
1 Oct 2006
United Kingdom (ZK01)
Effective Date:
1 Jun 1997
Denmark (ZS01)
Effective Date:
1 Jul 2003

5310-01-445-9278 Manufacturers Approved Sources 5310-01-445-9278

5310-01-445-9278 Technical Data Datasheet 5310-01-445-9278

Characteristic
Specifications
FIIG
A021A0
Bearing Surface Type [CRTM]
Chamfered Or Washer Faced
Material [MATT]
Steel Overall
Nominal Thread Size [CQJX]
0.250 Inches
Nut Height [ADEA]
0.328 Inches Maximum
Nut Style [ACTA]
Double Hexagon
Thread Series [BZRR]
Unjf
Thread Quantity Per Inch [CMLP]
28
Width Across Flats [ASDB]
0.3125 Inches Nominal
Thread Class [AAJD]
3B
Thread Direction [AAJF]
Right-Hand

5310-01-445-9278 Management Data Management Data 5310-01-445-9278

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2006
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
RC
AE100D3/C-130J ENGINE
Price Validation Code:
P
The current standard price is the initial negotiated provisioned price.
This is the price paid by DoD for the item as the result of price negotiation of the Provisioned Item Order (PIO) or other initial negotiated price.
ZOP or Standard Price challenges are permissible but should be supported with adequate justification.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5310-01-445-9278 Freight Data Freight Information 5310-01-445-9278

5310-01-445-9278 has freight characteristics managed by the Bureau of Accounts.. 5310-01-445-9278 has a variance between NMFC and UFC when transported by rail and the description should be consulted.