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5310-01-552-2422

Barrel Self-Locking Nut

5310015522422 015522422 CB2296CR4-2

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

5310-01-552-2422 NUT,SELF-LOCKING,BARREL 5310015522422 015522422

Managed by United States
NSN Created on 8 Jun 2007
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
5310-01-552-2422 NUT,SELF-LOCKING,BARREL 5310015522422 015522422 1/1
NSN 5310-01-552-2422 (Generic Image) 1/1

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5310-01-552-2422 Related Documents Related Documents 5310-01-552-2422 2+ Documents (More...)

5310-01-552-2422 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-53/fsc-5310/us 5310-01-552-2422
Barrel Self-Locking Nut 5310015522422 United States (US) 4. 5310-01-552-2422 Marketplace Restrictions
RQST NE Updated Every Day 5310-01-552-2422 RQST Updated Every Day 5310-01-552-2422 RQST NE Related
Every Day 5310-01-538-4651 RQST NE Restrictions https//www.nsnlookup.com /fsg-53/fsc-5310/us 5310-01-552-2422
Barrel Self-Locking Nut 5310015522422 Documents 5310-01-552-2422 1+ Documents ( More... ) https
the Air Force (DF)FEReplaced By 5310-01-552-2422Department of the Air Force (DF)IEReplaced By 5310-01-552-2422

5310-01-552-2422 Demil Restrictions 5310-01-552-2422

DEMIL: A | DEMILI: 7 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

5310-01-552-2422 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. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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.

5310-01-552-2422 HTS and ScheduleB Import and Export 5310-01-552-2422

5310-01-552-2422 End Users End Users 5310-01-552-2422

US Air Force (FLL5)
Effective Date:
1 Jun 2007

5310-01-552-2422 Manufacturers Approved Sources 5310-01-552-2422

5310-01-552-2422 Technical Data Datasheet 5310-01-552-2422

Characteristic
Specifications
FIIG
A021A0
End Item Identification [AGAV]
F-22 Raptor
Part Name Assigned By Controlling Agency [CXCY]
Nut, Self-Locking

5310-01-552-2422 Management Data Management Data 5310-01-552-2422

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Dec 2021
Department of the Air Force (DF)
EA
Subscribe
1
Sep 2020
Department of the Air Force (DF)
EA
Subscribe
1
Aug 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
G
Replaces 5310-01-538-4651
AAA
Department of the Air Force (DF)
F
Dod I&S Family Master Nsn - - -
AAB
Department of the Air Force (DF)
I
Dod I&S Family Master Nsn - - -
AAB
Department of the Air Force (DF)
I
G
Replaces 5310-01-538-4651
AAA

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
FR
F-22 AIRCRAFT
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).

5310-01-552-2422 Related Items NATO Stock Numbers Related to 5310-01-552-2422

5310-01-552-2422 Freight Data Freight Information 5310-01-552-2422

5310-01-552-2422 has freight characteristics.. 5310-01-552-2422 has a variance between NMFC and UFC when transported by rail and the description should be consulted.