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5320-01-526-3421
Pin-Rivet
5320015263421 015263421 ELS420HC8-5
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
1
Marketplace 5320-01-526-3421
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Restrictions 5320-01-526-3421
5320-01-526-3421 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 5320-01-526-3421
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5320-01-526-3421
- US Air Force (FMM5)
- Effective Date:
- 1 Dec 2004
Approved Sources 5320-01-526-3421
- Part Number
- Manufacturer
- Status
- ELS420HC8-5
- Manufacturer
- 06950 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
- ELS420HC8-5
- 1RC86 - Howmet Global Fastening Systems Inc. (Active)
- Secondary Buy
- Secondary Buy
Datasheet 5320-01-526-3421
- Characteristic
- Specifications
- FIIG
- Specifications
- A528U0
- End Item Identification [AGAV]
- Rq-4A
- Fastener Length [AASB]
- 0.637 Inches Minimum And 0.657 Inches Maximum
- Grip Length [ANEE]
- 0.307 Inches Minimum And 0.317 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]
- Straight Pan
- Material [MATT]
- Titanium Alloy Uns R56400 Overall
- Minimum Tensile Strength [CQBC]
- 5320 Pounds Per Square Inch
- Nominal Thread Size [CQJX]
- 0.2500 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]
- 0.2481 Inches Minimum And 0.2485 Inches Maximum
- Shank Style [AAZF]
- Pin-Rivet, Straight, Threaded
- Shear Strength [CQSX]
- 9380 Double Pounds Per Square Inch
- Thread Series Designator [THSD]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 28
- Width Between Flats [AATB]
- 0.160 Inches Nominal
- Surface Treatment Document And Classification [STDC]
- +5103 Mil Spec Single Treatment Response Overall
- Surface Treatment [SFTT]
- Aluminum Overall
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
Management Data 5320-01-526-3421
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- DN
- RQ-4A
- Price Validation Code:
- V
- The current standard price has been validated.
The item has been analyzed in conjunction with the Zero Overpricing Program and is in the accepted price range.
The item was procured under open competition and under the competitive arena the price is considered fair and reasonable.
ZOP or Standard price challenges are permissible but must be supported by adequate justification.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
NATO Stock Numbers Related to 5320-01-526-3421
Freight Information 5320-01-526-3421
5320-01-526-3421 has freight characteristics.. 5320-01-526-3421 has a variance between NMFC and UFC when transported by rail and the description should be consulted.