Premium Information is available for this item - Upgrade for $1 a day
5320-01-525-7589
Pin-Rivet
5320015257589 015257589 ELS420NC8-13
A metallic or nonmetallic item, headed at one end, with a cylindrically shaped shank which may be tapered, grooved, or threaded. A locking collar or sleeve may be provided to perform the same holding action as the clinching portion of a conventional rivet. The shank may include an external wrenching facility which breaks off at a predetermined applied torque. View more Pin-Rivet
May 2023
3
Marketplace 5320-01-525-7589
Request a Quotation from participating marketplace vendors
Restrictions 5320-01-525-7589
5320-01-525-7589 is a Pin-Rivet 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.
Import and Export 5320-01-525-7589
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5320-01-525-7589
- US Air Force (FMM5)
- Effective Date:
- 1 Nov 2004
Approved Sources 5320-01-525-7589
- Part Number
- Manufacturer
- Status
- ELS420NC8-13
- Manufacturer
- 06950 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
- ELS420NC8-13
- 1RC86 - Howmet Global Fastening Systems Inc. (Active)
- Secondary Buy
- Secondary Buy
Datasheet 5320-01-525-7589
- Characteristic
- Specifications
- FIIG
- Specifications
- A528U0
- End Item Identification [AGAV]
- Rq-4A
- Fastener Length [AASB]
- 1.151 Inches Minimum And 1.171 Inches Maximum
- Grip Length [ANEE]
- 0.807 Inches Minimum And 0.817 Inches Maximum
- Head Height [AASU]
- 0.080 Inches Minimum And 0.090 Inches Maximum
- Head Major Diameter [AAZG]
- 0.415 Inches Minimum And 0.440 Inches Maximum
- Head Style [AASK]
- Err-090
- Material [MATT]
- Titanium Alloy Uns R56400 Overall
- Nominal Thread Size [CQJX]
- 0.250 Inches
- Lubrication [ABAJ]
- Cetyl Alcohol
- Material Document And Classification [MDCL]
- Ams4928 Assn Std Single Material Response Overall Or Ams4967 Assn Std Single Material Response Overall
- Shank Diameter [AAZE]
- 0.2490 Inches Minimum And 0.2495 Inches Maximum
- Shank Style [AAZF]
- Pin-Rivet, Straight, Threaded
- Shear Strength [CQSX]
- 9300 Double Pounds Per Square Inch
- Part Name Assigned By Controlling Agency [CXCY]
- Pin,Protruding,Eddie
- Special Features [FEAT]
- Spline-Lok Recess
- Thread Series Designator [THSD]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 28
- Width Between Flats [AATB]
- 0.160 Inches Nominal
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
DLA Procurement Analysis 5320-01-525-7589
Management Data 5320-01-525-7589
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- DN
- RQ-4A
- 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 5320-01-525-7589
Freight Information 5320-01-525-7589
5320-01-525-7589 has freight characteristics.. 5320-01-525-7589 has a variance between NMFC and UFC when transported by rail and the description should be consulted.