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5310-01-495-9102
Double Hexagon Single Ball Seat Self-Locking Nut
5310014959102 014959102 NAS1727C4ND
A nut having one convex, spherical bearing surface, with 12 drive points, 24 sides. Items may have a removable collar. An integral feature is incorporated for locking on the threads of a mating member. View more Double Hexagon Single Ball Seat Self-Locking Nut
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,NAS1727C4ND NAS1727C4ND A nut having one convex, spherical bearing surface, with 12 drive points, 24
Restrictions 5310-01-495-9102
5310-01-495-9102 is a Double 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 5310-01-495-9102
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5310-01-495-9102
- Federal Bureau of Investigation (FDD5)
- Effective Date:
- 1 Mar 2002
Approved Sources 5310-01-495-9102
- Part Number
- Manufacturer
- Status
- NAS1727C4ND
- Manufacturer
- 80205 - National Aerospace Standards (Active)
- Primary Buy
- Primary Buy
Datasheet 5310-01-495-9102
- Characteristic
- Specifications
- FIIG
- Specifications
- A021A0
- Ball Seat Radius [ACTC]
- 0.300 Inches Minimum And 0.310 Inches Maximum
- End Item Identification [AGAV]
- Used On F119 Engine
- Material [MATT]
- Iron Alloy 660 Overall
- Nominal Thread Size [CQJX]
- 0.250 Inches
- Nut Height [ADEA]
- 0.330 Inches Minimum And 0.340 Inches Maximum
- Nut Style [ACTA]
- Single Ball Seat, Double Hexagon
- Locking Feature [AAUM]
- Prevailing Torque All Metal Design
- Material Document And Classification [MDCL]
- Ams 5737, Heat Treat 160 Ksi Min Per Mil-H-6875 Assn Std Single Material Response Overall
- Special Features [FEAT]
- Used On F119 Engine
- Thread Series [BZRR]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 28
- Width Across Flats [ASDB]
- 0.305 Inches Minimum And 0.313 Inches Maximum
- Surface Treatment [SFTT]
- Passivate Overall
- Temp Rating [AZKQ]
- 800.0 Deg Fahrenheit Maximum
- Thread Class [AAJD]
- 3B
- Thread Direction [AAJF]
- Right-Hand
Management Data 5310-01-495-9102
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Jan 2014
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- RF
- F-119-PW-100 FOR ATF-ENGINE
- 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).
NATO Stock Numbers Related to 5310-01-495-9102
Freight Information 5310-01-495-9102
5310-01-495-9102 has freight characteristics.. 5310-01-495-9102 has a variance between NMFC and UFC when transported by rail and the description should be consulted.