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5320-01-468-3429
Solid Rivet
5320014683429 014683429 AF1090O1E8C14 3D0282E8-14 ARM4038E8-14 3D0282
A headed fastening device having a smooth solid shank designed to have the shank end upset after insertion. View more Solid Rivet
Managed by United States
NSN Created on 6 Oct 1999
Data Last Changed
January 2023
January 2023
NATO Update Count
3
3
NATO Data Quality
Marketplace 5320-01-468-3429
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Related Documents 5320-01-468-3429 5+ Documents (More...)
A 29 Sep 1999 5320-01-468-3868 Solid Rivet ARM4038E5-7RNCC: 5 | RNVC: 9 | DAC: A 7 Oct 1999 5320-01-468-3429
Account Upgrade 5320-01-468-2898Solid Rivet5320014682898 014682898 AF1090O1E5C6 3D0282E5-6 ARM4038E5-6 3D0282
E ARM4038E5-6 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
E ARM4038E5-6 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
Account Upgrade 5320-01-468-1703Solid Rivet5320014681703 014681703 AF1090O1E6C3 3D0282E6-3 ARM4038E6-3 3D0282
E ARM4038E6-3 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
E ARM4038E6-3 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
Account Upgrade 5320-01-468-1684Solid Rivet5320014681684 014681684 AF1090O1E6C8 3D0282E6-8 ARM4038E6-8 3D0282
E ARM4038E6-8 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
E ARM4038E6-8 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
Account Upgrade 5320-01-468-3438Solid Rivet5320014683438 014683438 AF1090O1E5C9 3D0282E5-9 ARM4038E5-9 3D0282
E ARM4038E5-9 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
E ARM4038E5-9 64728 - Aerospace Rivet Mfrs Corp (Obsolete) Canceled/Obsolete RNCC 5 RNVC 9 DAC A 3D0282
Restrictions 5320-01-468-3429
5320-01-468-3429 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 5320-01-468-3429
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5320-01-468-3429
- US Air Force (FBB5)
- Effective Date:
- 1 Aug 2000
- Former MOE Rule:
- FEKZ
Approved Sources 5320-01-468-3429
- Part Number
- Manufacturer
- Status
- AF1090O1E8C14
- Manufacturer
- 53551 - Allfast Fastening Systems, Llc (Active)
- Primary Buy
- Primary Buy
- 3D0282E8-14
- 88277 - The Boeing Company (Active)
- Secondary Buy
- Secondary Buy
- ARM4038E8-14
- 64728 - Aerospace Rivet Mfrs Corp (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- 3D0282
- 88277 - The Boeing Company (Active)
- Informational Drawing
- Informational Drawing
Datasheet 5320-01-468-3429
- Characteristic
- Specifications
- FIIG
- Specifications
- A040A0
- End Item Identification [AGAV]
- C-17 Aircraft
- Countersink Angle [CRSQ]
- 99.0 Degrees Minimum And 101.0 Degrees Maximum
- Fastener Length [AASB]
- 0.875 Inches Nominal
- Head Major Diameter [AAZG]
- 0.359 Inches Minimum And 0.365 Inches Maximum
- Head Style [AASK]
- Oval Countersunk
- Material Document And Classification [MDCL]
- Qq-A-430 Fed Spec Single Material Response Overall
- Material [MATT]
- Aluminum Alloy 7050 Overall
- Shank Diameter [AAZE]
- 0.249 Inches Minimum And 0.250 Inches Maximum
- Shank Style [AAZF]
- Straight W/Radius Chamfered Tip
- Part Name Assigned By Controlling Agency [CXCY]
- Rivet,Solid-100 Degree Flush Crown Shear Head
- Special Features [FEAT]
- Deburr And Break All Edges .005-.015;.001 Shank Diameter Increase Permissable Within 100 Of Base Of Head;Head Cocking Angle Of Rivet Head Relative To Axis Of Rivet 1/2In Max;Approximate Material For Full Upset Of Head;Closed Die Configuration Required;No Sharp Edges Or Burrs On Rivet;Dimentions Apply After Coating
- Surface Treatment Document And Classification [STDC]
- Mil-A-8625,Type1,Class1 Mil Spec Single Treatment Response Overall
- Surface Treatment [SFTT]
- Anodize Overall And Aluminum Overall
Management Data 5320-01-468-3429
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Aug 2005
- 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 “L” or “F”, 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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Freight Information 5320-01-468-3429
5320-01-468-3429 has freight characteristics.. 5320-01-468-3429 has a variance between NMFC and UFC when transported by rail and the description should be consulted.