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5310-01-506-3646

Barrel Self-Locking Nut

5310015063646 015063646 SLN223-1612 3D0326-16 SLN233-1612

A nut of cylindrical or partly cylindrical cross-section with integral threads perpendicular to the axial centerline. Ends may be flat or flanged. An integral feature is incorporated for locking on the threads of a mating member. Excludes NUT (1), SELF-LOCKING, ROUND. View more Barrel Self-Locking Nut

5310-01-506-3646 NUT,SELF-LOCKING,BARREL 5310015063646 015063646

Managed by United States
NSN Created on 27 Mar 2003
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
ACTA Style A40 for 5310-01-506-3646 1/1
NSN 5310-01-506-3646 (Identification) 1/1

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SLN223-1612 3D0326-16 SLN233-1612 A nut of cylindrical or partly cylindrical cross-section with integral
RQST NE Updated Every Day 5310-01-506-3646 RQST Updated Every Day 5310-01-506-3646 RQST NE Related Documents
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5310-01-506-3646 Demil Restrictions 5310-01-506-3646

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

5310-01-506-3646 is a Barrel 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.

5310-01-506-3646 HTS and ScheduleB Import and Export 5310-01-506-3646

5310-01-506-3646 End Users End Users 5310-01-506-3646

US Air Force (FBB5)
Effective Date:
1 Mar 2003

5310-01-506-3646 Manufacturers Approved Sources 5310-01-506-3646

5310-01-506-3646 Technical Data Datasheet 5310-01-506-3646

Characteristic
Specifications
FIIG
A021A0
End Item Identification [AGAV]
C-17A Aircraft
Barrel Height [ADBA]
0.870 Inches Minimum And 0.880 Inches Maximum
Hardness Rating [CQFM]
50.0 Rockwell C Maximum
Material [MATT]
Nickel Alloy 718 Shell
Material [MATT]
Nickel Alloy 718 Nut
Nominal Thread Size [CQJX]
1.000 Inches
Nut Diameter [ACTD]
1.556 Inches Minimum And 1.559 Inches Maximum
Nut Length [ACVN]
1.878 Inches Minimum And 1.898 Inches Maximum
Nut Style [ACTA]
Floating Self-Locking Barrel
Nut Height [ADEA]
1.281 Inches Maximum
Locking Feature [AAUM]
Prevailing Torque All Metal Design
Material Document And Classification [MDCL]
Ams 5662 Assn Std Single Material Response Nut
Material Document And Classification [MDCL]
Ams 5662 Assn Std Single Material Response Shell
Special Features [FEAT]
Rollpin-Material Crs Per Aisi 420Or Aisi 302, Finnish Passivate Per Qq-P-35
Thread Series [BZRR]
Unjf
Thread Quantity Per Inch [CMLP]
12
Surface Treatment Document And Classification [STDC]
Ams 2411 Assn Std Single Treatment Response Nut
Surface Treatment Document And Classification [STDC]
Qq-P-35 Fed Spec Single Treatment Response Shell
Surface Treatment [SFTT]
Passivate Shell
Surface Treatment [SFTT]
Silver Nut
Thread Class [AAJD]
3B
Thread Direction [AAJF]
Right-Hand

5310-01-506-3646 Management Data Management Data 5310-01-506-3646

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Aug 2005
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5310-01-506-3646 Freight Data Freight Information 5310-01-506-3646

5310-01-506-3646 has freight characteristics.. 5310-01-506-3646 has a variance between NMFC and UFC when transported by rail and the description should be consulted.