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5320-01-458-1047
Pin-Rivet
5320014581047 014581047 VS3422VAP8-8 HST528AP-8-8 HK0099C8-8 WC199A-8-8 3D0099C8-8
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
January 2023
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Related Documents 5320-01-458-1047 3+ Documents (More...)
Pin-Rivet 5320014581047 014581047 Upgrade your Account Upgrade 5320-01-458-1047Pin-Rivet5320014581047
014581047 VS3422VAP8-8 HST528AP-8-8 HK0099C8-8 WC199A-8-8 3D0099C8-8 A metallic or nonmetallic item,
Pin-Rivet 5320014581047 014581047 Upgrade your Account Upgrade 5320-01-458-1047Pin-Rivet5320014581047
014581047 VS3422VAP8-8 HST528AP-8-8 HK0099C8-8 WC199A-8-8 3D0099C8-8 A metallic or nonmetallic item,
Pin-Rivet 5320014581047 014581047 Upgrade your Account Upgrade 5320-01-458-1047Pin-Rivet5320014581047
014581047 VS3422VAP8-8 HST528AP-8-8 HK0099C8-8 WC199A-8-8 3D0099C8-8 A metallic or nonmetallic item,
Restrictions 5320-01-458-1047
5320-01-458-1047 is a Pin-Rivet 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 5320-01-458-1047
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5320-01-458-1047
- US Air Force (FBB5)
- Effective Date:
- 1 May 2000
- Former MOE Rule:
- FEKZ
- Canada (ZC01)
- Effective Date:
- 1 Mar 2011
- NATO Maintenance and Supply Agency (ZX01)
- Effective Date:
- 1 Jan 2014
Approved Sources 5320-01-458-1047
- Part Number
- Manufacturer
- Status
- VS3422VAP8-8
- Manufacturer
- 06950 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
- HST528AP-8-8
- 06725 - Sps Technologies, Llc (Active)
- Primary Buy
- Primary Buy
- HK0099C8-8
- 17446 - Huck International, Inc. (Active)
- Primary Buy
- Primary Buy
- HST528AP-8-8
- 56878 - Sps Technologies, Llc (Active)
- Primary Buy
- Primary Buy
- WC199A-8-8
- 60516 - West Coast Aerospace, Inc. (Active)
- Primary Buy
- Primary Buy
- HST528AP-8-8
- 73197 - Hi-Shear Corporation (Active)
- Primary Buy
- Primary Buy
- HST528AP-8-8
- L4528 - Lisi Aerospace Canada Corp (Active)
- Primary Buy
- Primary Buy
- 3D0099C8-8
- 88277 - The Boeing Company (Active)
- Secondary Buy
- Secondary Buy
- HST528AP-8-8
- 0PTK6 - Sps Technologies Inc (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 5320-01-458-1047
- Characteristic
- Specifications
- FIIG
- Specifications
- A528U0
- Fastener Length [AASB]
- 0.885 Inches Minimum And 0.905 Inches Maximum
- Grip Length [ANEE]
- 0.495 Inches Minimum And 0.505 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
- Minimum Tensile Strength [CQBC]
- 5820 Pounds Per Square Inch
- Nominal Thread Size [CQJX]
- 0.250 Inches
- Lubrication [ABAJ]
- Cetyl Alcohol, Spec 305, Hi-Shear Corp
- Material Document And Classification [MDCL]
- Ams 4928 Assn Std Single Material Response Overall Or Ams 4967 Assn Std Single Material Response Overall
- Shank Diameter [AAZE]
- 0.2410 Inches Minimum And 0.2440 Inches Maximum
- Shank Style [AAZF]
- Pin-Rivet, Straight, Threaded
- Special Features [FEAT]
- Hi-Kote Aluminum Coating Per Hi-Shear Spec 294
- Thread Series Designator [THSD]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 28
- Width Between Flats [AATB]
- 0.0947 Inches Minimum And 0.0967 Inches Maximum
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
Management Data 5320-01-458-1047
- 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
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 5320-01-458-1047
Freight Information 5320-01-458-1047
5320-01-458-1047 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 106510. A Sub NMFC of X. It has a NMFC Description of RIVETS I/S PLAIN/GALVANIZED ETC. 5320-01-458-1047 is rated as class 50 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 54760 which rates the freight between FCL and LCL. 5320-01-458-1047 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 713 for ocean manifesting and military sealift. 5320-01-458-1047 is not classified as a special type of cargo when transported by water. 5320-01-458-1047 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.