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5310-01-432-9777
Hexagon Single Ball Seat Self-Locking Nut
5310014329777 014329777 3D0006-7 VN376A070W
A nut having one convex, spherical bearing surface and 6 flat sides. Items may have a removable collar. An integral feature is incorporated for locking on the threads of a mating member. See also NUT (1), SELF-LOCKING, CONE SEAT, HEXAGON. View more Hexagon Single Ball Seat Self-Locking Nut
January 2023
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Restrictions 5310-01-432-9777
5310-01-432-9777 is a Hexagon Single Ball Seat 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 5310-01-432-9777
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5310-01-432-9777
- US Air Force (FBB5)
- Effective Date:
- 1 May 2000
- Former MOE Rule:
- FEKZ
Approved Sources 5310-01-432-9777
- Part Number
- Manufacturer
- Status
- 3D0006-7
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
- VN376A070W
- 92215 - Howmet Global Fastening Systems Inc (Active)
- Secondary Buy
- Secondary Buy
Datasheet 5310-01-432-9777
- Characteristic
- Specifications
- FIIG
- Specifications
- A021A0
- Ball Seat Radius [ACTC]
- 0.496 Inches Minimum And 0.506 Inches Maximum
- Hardness Rating [CQFM]
- 45.0 Rockwell C Maximum
- Material Document And Classification [MDCL]
- Mil-S-6049 Mil Spec 1St Material Response Overall Or Mil-S-5000 Mil Spec 1St Material Response Overall Or Ams6322 Assn Std 2Nd Material Response Overall
- Material [MATT]
- Steel Comp 8740 Overall Or Steel Comp 4340 Overall
- Nominal Thread Size [CQJX]
- 0.438 Inches
- Nut Height [ADEA]
- 0.382 Inches Minimum And 0.392 Inches Maximum
- Nut Style [ACTA]
- Single Ball Seat, Hexagon
- Locking Feature [AAUM]
- Prevailing Torque All Metal Design
- Lubrication [ABAJ]
- Dry Film Lubricant
- Special Features [FEAT]
- Self-Aligning Waher Included
- Thread Series [BZRR]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 20
- Width Across Flats [ASDB]
- 0.492 Inches Minimum And 0.502 Inches Maximum
- Surface Treatment Document And Classification [STDC]
- Qq-P-416 Fed Spec Single Treatment Response Overall
- Surface Treatment [SFTT]
- Cadmium Overall And Chromate Overall
- Temp Rating [AZKQ]
- 450.0 Deg Fahrenheit Maximum
- Thread Class [AAJD]
- 3B
- Thread Direction [AAJF]
- Right-Hand
Management Data 5310-01-432-9777
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Aug 2005
- Department of the Air Force (DF)
- EA
- Subscribe
- EA
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BA
- C-17 PROGRAM
- Price Validation Code:
- N
- The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of āLā or āFā, then it must be evaluated locally where purchased or fabricated.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
NATO Stock Numbers Related to 5310-01-432-9777
Freight Information 5310-01-432-9777
5310-01-432-9777 has freight characteristics.. 5310-01-432-9777 has a variance between NMFC and UFC when transported by rail and the description should be consulted.