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5320-01-391-4346

Threaded Pin-Rivet

5320013914346 013914346 VS3422DC-18-35 HST528DL-18-35 HK0099-18-35 WC199-18-35 3D0099-18-35

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

5320-01-391-4346 PIN-RIVET,THREADED 5320013914346 013914346

Managed by United States
NSN Created on 10 Jun 1994
Data Last Changed
January 2023
NATO Update Count
5
NATO Data Quality
AAZF Style B31 for 5320-01-391-4346 1/1
NSN 5320-01-391-4346 (Identification) 1/1

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5320-01-391-4346 Demil Restrictions 5320-01-391-4346

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

5320-01-391-4346 is a Threaded 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.

5320-01-391-4346 HTS and ScheduleB Import and Export 5320-01-391-4346

5320-01-391-4346 End Users End Users 5320-01-391-4346

US Air Force (FBB5)
Effective Date:
1 May 2000
United States of America (ZZ)

5320-01-391-4346 Manufacturers Approved Sources 5320-01-391-4346

5320-01-391-4346 Technical Data Datasheet 5320-01-391-4346

Characteristic
Specifications
FIIG
A528U0
End Item Identification [AGAV]
C-17
Fastener Length [AASB]
2.9475 Inches Minimum And 2.9675 Inches Maximum
Grip Length [ANEE]
2.1825 Inches Minimum And 2.1925 Inches Maximum
Head Height [AASU]
0.200 Inches Minimum And 0.210 Inches Maximum
Head Style [AASK]
Err-090
Head Major Diameter [AAZG]
0.842 Inches Minimum And 0.877 Inches Maximum
Material [MATT]
Titanium Alloy Uns R56400 Overall
Minimum Tensile Strength [CQBC]
160000 Pounds Per Square Inch
Nominal Thread Size [CQJX]
0.5625 Inches
Lubrication [ABAJ]
Solid Film And Cetyl Alcohol
Material Document And Classification [MDCL]
Ams 4967 Assn Std Single Material Response Overall Or Ams 4928 Assn Std Single Material Response Overall
Shank Diameter [AAZE]
0.5610 Inches Minimum And 0.5615 Inches Maximum
Shear Strength [CQSX]
47200 Double Pounds Per Square Inch
Shank Style [AAZF]
Pin-Rivet, Straight, Threaded
Part Name Assigned By Controlling Agency [CXCY]
Pin-Rivet,Threaded
Thread Series Designator [THSD]
Unjf
Width Between Flats [AATB]
0.306 Inches Minimum And 0.326 Inches Maximum
Thread Direction [AAJF]
Right-Hand
Thread Class [AAJD]
3A
Thread Quantity Per Inch [CMLP]
18

5320-01-391-4346 Management Data Management Data 5320-01-391-4346

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2010
Department of the Air Force (DF)
EA
Subscribe
1

Air Force 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 ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5320-01-391-4346 Freight Data Freight Information 5320-01-391-4346

5320-01-391-4346 has freight characteristics.. 5320-01-391-4346 has a variance between NMFC and UFC when transported by rail and the description should be consulted.