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5320-00-825-0754

Solid Rivet

5320008250754 008250754 MS20470D6-40

A headed fastening device having a smooth solid shank designed to have the shank end upset after insertion. View more Solid Rivet

5320-00-825-0754 RIVET,SOLID 5320008250754 008250754

Managed by United States
NSN Created on 1 Jan 1962
Data Last Changed
January 2023
NATO Update Count
10
NATO Data Quality
AASK Style C28 for 5320-00-825-0754 1/2
NSN 5320-00-825-0754 (Identification) 1/2
AAZF Style D9 for 5320-00-825-0754 2/2
NSN 5320-00-825-0754 (Identification) 2/2

5320-00-825-0754 Stock and Availability Marketplace 5320-00-825-0754

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5320-00-825-0754 Related Documents Related Documents 5320-00-825-0754 2+ Documents (More...)

(Identification) 1/2 NSN 5320-00-825-0754 (Identification) 2/2 - - 1.
United States (US) 4. 5320-00-825-0754 Marketplace Restrictions Approved Sources Datasheet Management
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Active) Primary Buy RNCC 3 RNVC 2 DAC E MS20470D6 https//www.nsnlookup.com /fsg-53/fsc-5320/us 5320-00-825-0754
Solid Rivet 5320008250754 008250754 Upgrade for $1 a day Upgrade your Account Upgrade 5320-00-825
-0754Solid Rivet5320008250754 008250754 MS20470D6 NumberManufacturerStatusMS20470D6-40 80205 - National

5320-00-825-0754 Demil Restrictions 5320-00-825-0754

DEMIL: A | DEMILI: 1 | CRITICALITY: N | HMIC: N | PMIC: U | EDC: | ADPEC:

5320-00-825-0754 is a Solid Rivet 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. The precious metals content of this item is unknown.

5320-00-825-0754 HTS and ScheduleB Import and Export 5320-00-825-0754

5320-00-825-0754 End Users End Users 5320-00-825-0754

US Air Force (FBB5)
Effective Date:
1 Jan 2005
Former MOE Rule:
FXKZ
Greece (ZU01)
Effective Date:
1 Apr 1991

5320-00-825-0754 Manufacturers Approved Sources 5320-00-825-0754

5320-00-825-0754 Technical Data Datasheet 5320-00-825-0754

Characteristic
Specifications
FIIG
A040A0
Fastener Length [AASB]
2.490 Inches Minimum And 2.510 Inches Maximum
Grip Length [ANEE]
2.209 Inches Minimum And 2.229 Inches Maximum
Head Height [AASU]
0.080 Inches Minimum And 0.090 Inches Maximum
Head Major Diameter [AAZG]
0.356 Inches Minimum And 0.394 Inches Maximum
Head Style [AASK]
Universal
Material Document And Classification [MDCL]
Qq-A-430 Fed Spec Single Material Response Overall
Material [MATT]
Aluminum Alloy 2017 Overall
Shank Diameter [AAZE]
0.186 Inches Minimum And 0.191 Inches Maximum
Shank Style [AAZF]
Straight
Shear Strength [CQSX]
33000 Single Pounds Per Square Inch
Surface Treatment Document And Classification [STDC]
Mil-A-8625 Mil Spec 1St Treatment Response Overall Or Mil-C-5541 Mil Spec 2Nd Treatment Response Overall
Surface Treatment [SFTT]
Anodize Overall Or Oxide Film Overall

5320-00-825-0754 Management Data Management Data 5320-00-825-0754

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jan 2005
Department of the Air Force (DF)
EA
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5320-00-825-0754 Freight Data Freight Information 5320-00-825-0754

5320-00-825-0754 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. 5320-00-825-0754 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. 5320-00-825-0754 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. 5320-00-825-0754 is not classified as a special type of cargo when transported by water. 5320-00-825-0754 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.