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5320-01-132-4455
Pin-Rivet
5320011324455 011324455 HLT310TA-8-7 HLT310DL-8-7 HLT310TB-8-7 ST3M759V4-7 AIC-L-759V4-7 10111437
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
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November 2023
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Marketplace 5320-01-132-4455
Request a Quotation from participating marketplace vendors
Related Documents 5320-01-132-4455 1+ Documents (More...)
HLT310DL-8-7 PIN-RIVET 20 EA NS Request Quotation ST3M759V4-7 PIN-RIVET 23 EA NS Request Quotation Updated
Every Day 5320-01-132-4455 RQST NE Updated Every Day 5320-01-132-4455 RQST Updated Every Day 5320-01
Restrictions 5320-01-132-4455
5320-01-132-4455 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 5320-01-132-4455
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5320-01-132-4455
- US Air Force (FXGI)
- Effective Date:
- 1 Apr 2006
- Former MOE Rule:
- FXKZ
- US Navy (N9BZ)
- Effective Date:
- 1 Apr 2006
- Former MOE Rule:
- N9ZD
- Supplementary Collaborators:
- GTKE
- Finland (WF01)
- Effective Date:
- 1 Apr 2011
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Singapore (YJ01)
- Effective Date:
- 1 May 2012
- Malaysia (YW01)
- Effective Date:
- 1 Aug 1997
- Australia (ZA01)
- Effective Date:
- 1 Apr 1991
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 2008
Approved Sources 5320-01-132-4455
- Part Number
- Manufacturer
- Status
- HLT310DL-8-7
- Manufacturer
- L4528 - Lisi Aerospace Canada Corp (Active)
- Primary Buy
- Primary Buy
- HLT310DL-8-7
- 60516 - West Coast Aerospace, Inc. (Active)
- Primary Buy
- Primary Buy
- HLT310DL-8-7
- 56878 - Sps Technologies, Llc (Active)
- Primary Buy
- Primary Buy
- HLT310DL-8-7
- 73197 - Hi-Shear Corporation (Active)
- Primary Buy
- Primary Buy
- HLT310DL-8-7
- 06950 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
- HLT310DL-8-7
- 06725 - Sps Technologies, Llc (Active)
- Primary Buy
- Primary Buy
- HLT310DL-8-7
- 17446 - Huck International, Inc (Active)
- Primary Buy
- Primary Buy
- HLT310TB-8-7
- 17446 - Huck International, Inc (Active)
- Primary Buy
- Primary Buy
- ST3M759V4-7
- 60516 - West Coast Aerospace, Inc. (Active)
- Original Design
- Original Design
- HLT310TB-8-7
- 73197 - Hi-Shear Corporation (Active)
- Secondary Buy
- Secondary Buy
- HLT310TB-8-7
- 56878 - Sps Technologies, Llc (Active)
- Secondary Buy
- Secondary Buy
- HLT310DL-8-7
- K5673 - Sps Technologies Ltd, Tj Brooks (Active)
- Secondary Buy
- Secondary Buy
- HLT310TB-8-7
- 60516 - West Coast Aerospace, Inc. (Active)
- Secondary Buy
- Secondary Buy
- HLT310TB-8-7
- 06950 - Howmet Global Fastening Systems Inc (Active)
- Secondary Buy
- Secondary Buy
- HLT310TB-8-7
- 06725 - Sps Technologies, Llc (Active)
- Secondary Buy
- Secondary Buy
- HLT310TB-8-7
- K5673 - Sps Technologies Ltd, Tj Brooks (Active)
- Secondary Buy
- Secondary Buy
- HLT310TB-8-7
- L4528 - Lisi Aerospace Canada Corp (Active)
- Secondary Buy
- Secondary Buy
- ST3M759V4-7
- 92215 - Howmet Global Fastening Systems Inc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- HLT310TB-8-7
- 92215 - Howmet Global Fastening Systems Inc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- ST3M759V4-7
- 0ZC92 - Heartland Precision Fasteners Inc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- ST3M759V4-7
- 56878 - Sps Technologies, Llc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- ST3M759V4-7
- 73197 - Hi-Shear Corporation (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- HLT310DL-8-7
- 92215 - Howmet Global Fastening Systems Inc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- ST3M759V4-7
- 17446 - Huck International, Inc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- ST3M759V4-7
- 06725 - Sps Technologies, Llc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AIC-L-759V4-7
- 06725 - Sps Technologies, Llc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 10111437
- A486G - Nimikkeistokeskus Ncb Finland (Active)
- NATO Reference
- NATO Reference
- ST3M759V4-7
- 76301 - The Boeing Company (Active)
- Vendor Drawing
- Vendor Drawing
- HLT310TA-8-7
- 17446 - Huck International, Inc (Active)
- Advisory Reference
- Advisory Reference
- HLT310TA-8-7
- 92215 - Howmet Global Fastening Systems Inc (Active)
- Advisory Reference
- Advisory Reference
- HLT310TA-8-7
- 56878 - Sps Technologies, Llc (Active)
- Advisory Reference
- Advisory Reference
- HLT310TA-8-7
- 73197 - Hi-Shear Corporation (Active)
- Advisory Reference
- Advisory Reference
Datasheet 5320-01-132-4455
- Characteristic
- Specifications
- FIIG
- Specifications
- A528U0
- End Item Identification [AGAV]
- F/A-18E/F Hornet Aircraft;Aircraft, Eagle F-15;Aircraft, Hornet F/A-18
- Fastener Length [AASB]
- 0.823 Inches Minimum And 0.843 Inches Maximum
- Grip Length [ANEE]
- 0.443 Inches Maximum
- Head Height [AASU]
- 0.059 Inches Minimum And 0.069 Inches Maximum
- Head Major Diameter [AAZG]
- 0.387 Inches Minimum And 0.412 Inches Maximum
- Head Style [AASK]
- Straight Pan
- Material [MATT]
- Titanium Alloy Uns R56400 Overall
- Nominal Thread Size [CQJX]
- 0.250 Inches
- Lubrication [ABAJ]
- Solid Film And 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]
- 0.2490 Inches Minimum And 0.2495 Inches Maximum
- Shear Strength [CQSX]
- 95000 Single Pounds Per Square Inch
- Shank Style [AAZF]
- Pin-Rivet, Straight, Threaded
- Part Name Assigned By Controlling Agency [CXCY]
- (Inavy) Pin - Rivet, Threaded, Shear, Protruding Head, Hex Point Drive
- Width Between Flats [AATB]
- 0.0947 Inches Minimum And 0.0967 Inches Maximum
- Surface Treatment Document And Classification [STDC]
- Ti-Shield 3,Fscm 73197 Mfr Ref Single Treatment Response Overall
- Surface Treatment [SFTT]
- Anodize Overall
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Series Designator [THSD]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 28
Weapon Systems (WSDC) 5320-01-132-4455
DLA Procurement Analysis 5320-01-132-4455
- Last Stock Position:
- 1383 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 5320-01-132-4455
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 5320-01-132-4455
5320-01-132-4455 has freight characteristics managed by the Southwestern Power Administration.It has a National Motor Freight Classification (NMFC) of 136500. A Sub NMFC of Z. It has a NMFC Description of METAL NOI/METAL ALLOYS NOI. 5320-01-132-4455 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 68455 which rates the freight between FCL and LCL. 5320-01-132-4455 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. 5320-01-132-4455 is not classified as a special type of cargo when transported by water. 5320-01-132-4455 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.
Packaging Data 5320-01-132-4455
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- --
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- Plated/Coated Item
- 2lb or less, one dimension 2" or less, other dimensions less than 24"
- Above 110G
- No Requirement
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- --
- --
- --
- --
- Physical Protection
- Any Suitable Process
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- --
- --
- --
- PPP-B-566, PPP-B-676, or ASTM-D5118, Folding, Setup or Fiberboard Box
- No special marking
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement
Procurement History 5320-01-132-4455 1 Records
Contracting Technical Data File (CTDF) 5320-01-132-4455 April 2020
Criticality and Quality
- Critical Item Code:
- Flight Safety:
- Life Support:
- Certified Samples:
- Serialization:
- First Article Test (FAT):
- Certificate of Quality Compliance:
- Production Lot Testing:
- Special Testing:
- Qualified Products List (QPL):
Commercial Properties
- Government Furnished Material:
- Government Furnished Tooling:
- Government Furnished Property:
- Price Evaluation Code:
- Diminshing Manufacturing Sources:
- Warranty:
- Commerical Off The Shelf (COTS):
- End Item Application:
- Auctioning Candidate:
- Source of Procurement:
- Contract Option:
Restrictions
- Boeing Rights Guard:
- Export Controlled:
- Controlled Technical Data Package (TDP):
- Restricted Technical Data Package (TDP):
- Contains Classified Material
- Weapons System Indicator Code (WSIC):
- F
Packaging Requirements
- Packaging Determination Table:
- Packaging Review Code:
- N
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: