NSN 5320-01-389-4097 · NIIN 013894097 · FSC 5320
NO DASHES 5320013894097
In Stock
PIN-RIVET
Rivets
Application: F100 ENGINE; W/S: ENGINE, AIRCRAFT F100-PW-229 (F15E, F16C/D); GLOBAL HAWK HIGH-ALTITUDE-LONG ENDURANCE UNAMANNED AERIAL VEHICLE; AIRCRAFT, EAGLE F-15
Technical characteristics
17 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASB | FASTENER LENGTH | INCHES MINIMUM 0.552 AND INCHES MAXIMUM 0.572 |
| AASU | HEAD HEIGHT | INCHES MINIMUM 0.055 AND INCHES MAXIMUM 0.065 |
| AATB | WIDTH BETWEEN FLATS | INCHES MINIMUM 0.0635 AND INCHES MAXIMUM 0.0645 |
| AAZE | SHANK DIAMETER | INCHES MINIMUM 0.1630 AND INCHES MAXIMUM 0.1635 |
| AAZF | SHANK STYLE | |
| AAZG | HEAD MAJOR DIAMETER | INCHES MINIMUM 0.306 AND INCHES MAXIMUM 0.322 |
| ABAJ | LUBRICATION | CETYL ALCOHOL, SPEC 305, HI-SHEAR CORP |
| AGAV | END ITEM IDENTIFICATION | F100 ENGINE; W/S: ENGINE, AIRCRAFT F100-PW-229 (F15E, F16C/D); GLOBAL HAWK HIGH-ALTITUDE-LONG ENDURANCE UNAMANNED AERIAL VEHICLE; AIRCRAFT, EAGLE F-15 |
| ANEE | GRIP LENGTH | INCHES MINIMUM 0.245 AND INCHES MAXIMUM 0.255 |
| CQBC | MINIMUM TENSILE STRENGTH | POUNDS PER SQUARE INCH 160000 |
| CQJX | NOMINAL THREAD SIZE | INCHES 0.164 |
| CQSX | SHEAR STRENGTH | SINGLE POUNDS PER SQUARE INCH 95000 |
| MATT | MATERIAL | OVERALL TITANIUM ALLOY UNS R56400 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL ASSN STD SINGLE MATERIAL RESPONSE A-S4928 OR ASSN STD SINGLE MATERIAL RESPONSE A-S4967 |
| THSD | THREAD SERIES DESIGNATOR | UNJC |