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5310-01-532-6900

Plate Self-Locking Nut

5310015326900 015326900 CB9023AA3CRP 3D0242-3-2P

A nut with a flanged base of varied shapes which may be plain or mounted by rivets, bolts, welding or integral prongs. An integral feature is incorporated for locking on the threads of a mating member. View more Plate Self-Locking Nut

5310-01-532-6900 NUT,SELF-LOCKING,PLATE 5310015326900 015326900

Managed by United States
NSN Created on 16 Aug 2005
Data Last Changed
January 2023
NATO Update Count
6
NATO Data Quality
ACTA Style A123 for 5310-01-532-6900 1/1
NSN 5310-01-532-6900 (Identification) 1/1

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5310-01-532-6900 Related Documents Related Documents 5310-01-532-6900 1+ Documents (More...)

2007 5310-01-552-4398 Plate Self-Locking Nut CB2203CR5-7RNCC: 3 | RNVC: 2 | DAC: 5 13 Jun 2007 5310-01-532-6900

5310-01-532-6900 Demil Restrictions 5310-01-532-6900

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

5310-01-532-6900 is a Plate 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.

5310-01-532-6900 HTS and ScheduleB Import and Export 5310-01-532-6900

5310-01-532-6900 End Users End Users 5310-01-532-6900

US Air Force (FBB5)
Effective Date:
1 Aug 2005
Canada (ZC01)
Effective Date:
1 Mar 2011
NATO Maintenance and Supply Agency (ZX01)
Effective Date:
1 Jan 2014

5310-01-532-6900 Manufacturers Approved Sources 5310-01-532-6900

5310-01-532-6900 Technical Data Datasheet 5310-01-532-6900

Characteristic
Specifications
FIIG
A021A0
End Item Identification [AGAV]
C-17A Aircraft
Counterbore Diameter [AAWY]
0.312 Inches Minimum First End
Material Document And Classification [MDCL]
Qq-A-250 Fed Spec Single Material Response Base
Material [MATT]
Aluminum Alloy 2024 Base
Material [MATT]
Iron Alloy 660 Nut
Material [MATT]
Steel Comp 302 Clip
Nominal Thread Size [CQJX]
0.190 Inches
Nut Counterbore Depth [ADFK]
0.125 Inches Minimum First End
Nut Length [ACVN]
0.948 Inches Maximum
Nut Height [ADEA]
0.299 Inches Maximum
Nut Style [ACTA]
Plate (Floating)
Locking Feature [AAUM]
Prevailing Torque All Metal Design
Lubrication [ABAJ]
Dry Film Lubricant
Material Document And Classification [MDCL]
Ams 5525 Assn Std Single Material Response Nut Or Ams 5731 Assn Std Single Material Response Nut Or Ams 5734 Assn Std Single Material Response Nut Or Ams 5737 Assn Std Single Material Response Nut
Material Document And Classification [MDCL]
Ams 5688 Assn Std Single Material Response Clip Or Ams 5866 Assn Std Single Material Response Clip
Plate Width [ADEC]
0.590 Inches Maximum
Plate Thickness [ADEB]
0.040 Inches Nominal
Special Features [FEAT]
Base Plate Primer-Epoxy Primer Per Mil-L-46010, Type I
Thread Series [BZRR]
Unjf
Thread Quantity Per Inch [CMLP]
32
Surface Treatment Document And Classification [STDC]
Ams-Qq-P-35 Assn Std Single Treatment Response Nut
Surface Treatment Document And Classification [STDC]
Mil-A-8625, Type I Mil Spec Single Treatment Response Base
Surface Treatment [SFTT]
Anodize Base
Surface Treatment [SFTT]
Passivate Nut
Thread Class [AAJD]
3B
Thread Direction [AAJF]
Right-Hand

5310-01-532-6900 Management Data Management Data 5310-01-532-6900

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2018
Department of the Air Force (DF)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
F
7
Substitute For 5310-01-411-5011
AAA
Department of the Air Force (DF)
I
7
Substitute For 5310-01-411-5011
AAA
Department of the Air Force (DF)
F
Dod I&S Family Master Nsn - - -
ABA
Department of the Air Force (DF)
I
Dod I&S Family Master Nsn - - -
ABA

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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5310-01-532-6900 Freight Data Freight Information 5310-01-532-6900

5310-01-532-6900 has freight characteristics.. 5310-01-532-6900 has a variance between NMFC and UFC when transported by rail and the description should be consulted.