AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
Part Number VLB240-6B11 described as Pin Rivet with NSN 5320-01-478-8492 with FSC 5320 Rivets by Manufacture Alcoa Global Fasteners Inc is available in stock. We provide comprehensive database of aerospace and aviation components, sub-assemblies, and completed assemblies allows us to respond to your RFQ within 15 minutes.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5320-01-478-8492 Item Description: Pin Rivet | 5320 | 014788492 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 111135-05b11 | 5 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ANEE | GRIP LENGTH | 0.688 INCHES NOMINAL |
| AAZE | SHANK DIAMETER | 0.189 INCHES MINIMUM AND 0.190 INCHES MAXIMUM |
| AASK | HEAD STYLE | FLUSH COUNTERSUNK |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT, HORNET F/A-18 |
| AAZF | SHANK STYLE | STUMP |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PIN-RIVET, GROOVED, 100 DEG CSUNK HEAD, SHEAR LOCKBOLT, STUMP TYPE, TITANIUM, 95 KSI FSU |
| AASB | FASTENER LENGTH | 0.936 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | NAS621 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| MATT | MATERIAL | TITANIUM ALLOY UNS R56400 OVERALL |
| ABAJ | LUBRICATION | SOLID FILM OR DRY FILM AND CETYL ALCOHOL |
| FEAT | SPECIAL FEATURES | 4 LOCKING GROOVES FOR 0.188 AND 0.250 DIAMETER;END MAY BE CUPPED OR FLAT;1,410 TO 2210 TENSION STRENGTH LBS MIN;COLLAR PART NUMBER NAS 1080-06 OR NAS1080AG06;PROCUREMENT SPEC NAS 621;HI-COTE 2 SOLID FILM LUBE OR DRY FILM LUBE PER AS5272 (KAL GARD FA ONLY) PLUS CETYL ALCOHAL;DIMENTIONS TO BE MET BEFORE LUBRICATION;LOCKING GROOVES MAY BE GROUND OR ROLLED AT THE MANUFACTURERS OPTION;CONCENTRICITY, CONICAL SURFACE OF HEAD TO SHANK WITHIN 0.003 TIR |
| AAZG | HEAD MAJOR DIAMETER | 0.293 INCHES MINIMUM AND 0.305 INCHES MAXIMUM |
| CRSQ | COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
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