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5310-01-541-5624
Spline Self-Locking Nut
5310015415624 015415624 CB4022V3CR6P 3D0260-101P
A nut having an externally splined sleeve, which holds it in position when forced into a hole of slightly smaller diameter. An integral feature is incorporated for locking. View more Spline Self-Locking Nut
January 2023
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Related Documents 5310-01-541-5624 2+ Documents (More...)
5310-01-541-5624 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-53/fsc-5310/us 5310-01-541-5624
Sources Datasheet Management RQST NE Updated Every Day 5310-01-541-5624 RQST Updated Every Day 5310-
Spline Self-Locking Nut 5310015415624 Documents 5310-01-541-5624 1+ Documents ( More... ) https
the Air Force (DF)FEReplaced By 5310-01-541-5624Department of the Air Force (DF)IEReplaced By 5310-01-541-5624
Restrictions 5310-01-541-5624
5310-01-541-5624 is a Spline 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.
Import and Export 5310-01-541-5624
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5310-01-541-5624
- US Air Force (FBB5)
- Effective Date:
- 1 Jun 2006
Approved Sources 5310-01-541-5624
- Part Number
- Manufacturer
- Status
- CB4022V3CR6P
- Manufacturer
- 66530 - Click Bond Inc (Active)
- Primary Buy
- Primary Buy
- 3D0260-101P
- 88277 - The Boeing Company (Active)
- Secondary Buy
- Secondary Buy
Datasheet 5310-01-541-5624
- Characteristic
- Specifications
- FIIG
- Specifications
- A021A0
- Material [MATT]
- Iron Alloy 660 Nut
- Nominal Thread Size [CQJX]
- 0.190 Inches
- Nut Length [ACVN]
- 0.587 Inches Nominal
- Nut Height [ADEA]
- 0.305 Inches Minimum And 0.335 Inches Maximum
- Nut Style [ACTA]
- Spline (Floating)
- Locking Feature [AAUM]
- Prevailing Torque All Metal Design
- Material Document And Classification [MDCL]
- Ams5525 Assn Std Single Material Response Nut
- Pilot Diameter [AAVL]
- 0.270 Inches Nominal
- Pilot Length [AAVM]
- 0.120 Inches Minimum And 0.180 Inches Maximum
- Special Features [FEAT]
- Retainer Material A-286 And 304 Or 305 Cres, Spec Ams5525, Ams5639, Ams5514 Finish Passivate Spec Qq-P-35, Standard Base Plate-Material Glass/Thermoplastic, 350 Degrees F, Finish Abrasive Clean, Spline Nut Can Be Removed From Retainer And Replaced, Base Plate Angle Length Is 0.375, Install With Baseplate Epoxy Primer Mil-P-85582
- Thread Series [BZRR]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 32
- Width Across Flats [ASDB]
- 0.405 Inches Nominal
- Surface Treatment [SFTT]
- Passivate Nut
- Thread Class [AAJD]
- 3B
- Thread Direction [AAJF]
- Right-Hand
Weapon Systems (WSDC) 5310-01-541-5624
Management Data 5310-01-541-5624
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Nov 2018
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- F
- G
- Replaces 5310-01-507-4944
- AAA
- G
- 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 5310-01-507-4944
- AAA
- G
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Freight Information 5310-01-541-5624
5310-01-541-5624 has freight characteristics.. 5310-01-541-5624 has a variance between NMFC and UFC when transported by rail and the description should be consulted.