NSN 5320-01-468-0829 of Rivet Solid - Parts Details
| Alternative NSN: 5320014680829 |
| Item Name: Rivet Solid |
| FSG: 53 Hardware and Abrasives |
| Federal Supply Class (FSC): 5320 Rivets |
| NIIN: 014680829 |
| NCB Code: USA (01) |
| Manufacturers: West Coast Aerospace Inc , Allfast Fastening Systems Inc , Boeing Company |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers WC283E5-6, AF1091O1E5C6, 3D0283E5-6, 3D0283 under NSN 5320-01-468-0829 of Rivet Solid manufactured by West Coast Aerospace Inc, Allfast Fastening Systems Inc, Boeing Company.
Federal Supply Class of NSN 5320-01-468-0829 is FSC 5320 contains part details of Rivets. Quote for your desired part numbers.
Part Number's List for NSN 5320-01-468-0829, 5320014680829
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Part No Manufacturer Item Name QTY RFQ WC283E5-6 West Coast Aerospace Inc rivet solid Avl RFQ AF1091O1E5C6 Allfast Fastening Systems Inc rivet solid Avl RFQ 3D0283E5-6 Boeing Company rivet solid Avl RFQ 3D0283 Boeing Company rivet solid Avl RFQ
Characteristics Data of NSN 5320014680829MRC Criteria Characteristic AASB Fastener Length 0.375 INCHES NOMINAL AAZG Head Major Diameter 0.260 INCHES MINIMUM AND 0.264 INCHES MAXIMUM AAZE Shank Diameter 0.155 INCHES MINIMUM AND 0.159 INCHES MAXIMUM SFTT Surface Treatment ANODIZE OVERALL AND ALUMINUM OVERALL AGAV End Item Identification AIRCRAFT,AIRLIFTER C-17A MDCL Material Document And Classification QQ-A-430,T73 FED SPEC SINGLE MATERIAL RESPONSE OVERALL CXCY Part Name Assigned By Controlling Agency RIVET, SOLID, 100 DEGREE FLUSH CROWNRIVET HEAD AASK Head Style OVAL COUNTERSUNK MATT Material ALUMINUM ALLOY 7050 OVERALL AAZF Shank Style STRAIGHT W/RADIUS CHAMFERED TIP FEAT Special Features END ITEM C-17A AIRCRAFT;SURFACE TEXTURE 125 MICROINCHES RA MAX PER ANSI B46.1-78;DEBURR AND BREAK ALL EDGES .005-.015;HEAD COCKING ANGLE OF RIVET HEAD REALTIVE TO AXIS OF RIVET 1/2 MAXIMUM;CLOSED DIE CONFIGURATION REQUIRED;NO SHARP EDGES OR BURRS ON RIVET;RIVET SHALL DRIVE AS RECIEVED TO 1.6XDIAMETER OF RIVET WITHOUT CRACKING MRC Decoded Requirement Clear Text Reply STDC Surface Treatment Document And Classification MIL-A-8825,TYPE1,CLASS1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL CRSQ Countersink Angle 100.0 DEGREES NOMINAL
| MRC | Criteria | Characteristic |
|---|---|---|
| AASB | Fastener Length | 0.375 INCHES NOMINAL |
| AAZG | Head Major Diameter | 0.260 INCHES MINIMUM AND 0.264 INCHES MAXIMUM |
| AAZE | Shank Diameter | 0.155 INCHES MINIMUM AND 0.159 INCHES MAXIMUM |
| SFTT | Surface Treatment | ANODIZE OVERALL AND ALUMINUM OVERALL |
| AGAV | End Item Identification | AIRCRAFT,AIRLIFTER C-17A |
| MDCL | Material Document And Classification | QQ-A-430,T73 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| CXCY | Part Name Assigned By Controlling Agency | RIVET, SOLID, 100 DEGREE FLUSH CROWNRIVET HEAD |
| AASK | Head Style | OVAL COUNTERSUNK |
| MATT | Material | ALUMINUM ALLOY 7050 OVERALL |
| AAZF | Shank Style | STRAIGHT W/RADIUS CHAMFERED TIP |
| FEAT | Special Features | END ITEM C-17A AIRCRAFT;SURFACE TEXTURE 125 MICROINCHES RA MAX PER ANSI B46.1-78;DEBURR AND BREAK ALL EDGES .005-.015;HEAD COCKING ANGLE OF RIVET HEAD REALTIVE TO AXIS OF RIVET 1/2 MAXIMUM;CLOSED DIE CONFIGURATION REQUIRED;NO SHARP EDGES OR BURRS ON RIVET;RIVET SHALL DRIVE AS RECIEVED TO 1.6XDIAMETER OF RIVET WITHOUT CRACKING |
| MRC | Decoded Requirement | Clear Text Reply |
| STDC | Surface Treatment Document And Classification | MIL-A-8825,TYPE1,CLASS1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| CRSQ | Countersink Angle | 100.0 DEGREES NOMINAL |