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5320-01-391-2196
Solid Rivet
5320013912196 013912196 MS14219E5-5
A headed fastening device having a smooth solid shank designed to have the shank end upset after insertion. View more Solid Rivet
November 2023
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Related Documents 5320-01-391-2196 1+ Documents (More...)
United States (US) 4. 5320-01-391-2196 Marketplace Restrictions Approved Sources Datasheet Management
BUY NE FedMall Updated Every Day 5320-01-391-2196 RQST NE Updated Every Day 5320-01-391-2196 RQST
Restrictions 5320-01-391-2196
5320-01-391-2196 is a Solid 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 5320-01-391-2196
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5320-01-391-2196
- US Air Force (FXGI)
- Effective Date:
- 1 Aug 2005
- Former MOE Rule:
- FXKZ
Approved Sources 5320-01-391-2196
- Part Number
- Manufacturer
- Status
- MS14219E5-5
- Manufacturer
- 96906 - Military Standards (Active)
- Definitive Standard
- Definitive Standard
Datasheet 5320-01-391-2196
- Characteristic
- Specifications
- FIIG
- Specifications
- A040A0
- Countersink Angle [CRSQ]
- 118.5 Degrees Minimum And 121.5 Degrees Maximum
- Fastener Length [AASB]
- 0.302 Inches Minimum And 0.322 Inches Maximum
- Head Style [AASK]
- Dished Countersunk
- Head Major Diameter [AAZG]
- 0.256 Inches Minimum And 0.258 Inches Maximum
- Material Document And Classification [MDCL]
- Qq-A-430 Fed Spec Single Material Response Overall
- Material [MATT]
- Aluminum Alloy 7075 Overall
- Minimum Tensile Strength [CQBC]
- 68000 Pounds Per Square Inch
- Minimum Yield Strength [CQHQ]
- 58000 Pounds Per Square Inch
- Shank Diameter [AAZE]
- 0.155 Inches Minimum And 0.158 Inches Maximum
- Shank Style [AAZF]
- Straight W/Chamfered Tip
- Shear Strength [CQSX]
- 46000 Single Pounds Per Square Inch
- Surface Treatment [SFTT]
- Anodize Overall
Weapon Systems (WSDC) 5320-01-391-2196
DLA Procurement Analysis 5320-01-391-2196
- Last Stock Position:
- 790 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 5320-01-391-2196
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Jul 2023
- Defense Logistics Agency (DS)
- EA
- Subscribe
- 1
- EA
- Oct 2022
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2021
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2020
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2019
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 5320-01-391-2196
5320-01-391-2196 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 096320. A Sub NMFC of X. It has a NMFC Description of RIVETS I/S NICKEL PLATED BUFFED. 5320-01-391-2196 is rated as class 77.5 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 50430 which rates the freight between FCL and LCL. 5320-01-391-2196 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. 5320-01-391-2196 is not classified as a special type of cargo when transported by water. 5320-01-391-2196 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 5320-01-391-2196
- 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
- 1
- --
- --
- --
- Physical Protection
- Any Suitable Process
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- --
- --
- --
- Bags made of material conforming to MIL-P-130, MIL-DTL-17667, MIL-PRF-121, or any material authorized by MIL-DTL-117. Closure may be by staples, tape, adhesive or heat seal
- No special marking
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- PPP-B-566, PPP-B-676, or ASTM-D5118, Folding, Setup or Fiberboard Box
Contracting Technical Data File (CTDF) 5320-01-391-2196 August 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: