NSN 5305-01-462-2742 · NIIN 014622742 · FSC 5305
NO DASHES 5305014622742
In Stock
SCREW,CLOSE TOLERANCE
Screws
Application: STRUCTURAL COMPENENTS; F18 AIRCRAFT
Technical characteristics
23 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 |
| AASA | THREAD LENGTH | INCHES NOMINAL 0.692 |
| AASB | FASTENER LENGTH | INCHES MINIMUM 2.1135 AND INCHES MAXIMUM 2.1605 |
| AASK | HEAD STYLE | |
| AASL | HEAD DIAMETER | INCHES MINIMUM 0.692 |
| AASU | HEAD HEIGHT | INCHES MINIMUM 0.1147 AND INCHES MAXIMUM 0.1167 |
| AAUR | GRIP DIAMETER | INCHES MINIMUM 0.3740 AND INCHES MAXIMUM 0.3745 |
| ABQZ | INTERNAL DRIVE STYLE | |
| AGAV | END ITEM IDENTIFICATION | STRUCTURAL COMPENENTS; F18 AIRCRAFT |
| AHYM | NOMINAL THREAD DIAMETER | INCHES 0.3750 |
| ANEE | GRIP LENGTH | INCHES MINIMUM 1.4275 AND INCHES MAXIMUM 1.4475 |
| CBBL | FEATURES PROVIDED | O RING AND CETYL ALCOHOL LUBRICANT |
| CMLP | THREAD QUANTITY PER INCH | 24 |
| CRSQ | COUNTERSINK ANGLE | DEGREES MINIMUM 99.0 AND DEGREES MAXIMUM 101.0 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SCREW, CLOSE TOLERANCE-ASSEMBLY, 100 DEGREE COUNTERSUNK SEALING HEAD, DOVETAIL SLOT, CRES |
| FEAT | SPECIAL FEATURES | O-RING MATERIAL - FLOUROSILICONE RUBBER PER MIL-R-25988, TYPE I, CLASS 1, GRADE 70 |
| MATT | MATERIAL | OVERALL STEEL COMP XM-13 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL ASSN STD SINGLE MATERIAL RESPONSE A-S5629, H13-8-O |
| SFTT | SURFACE TREATMENT | OVERALL PASSIVATE |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | OVERALL ASSN STD SINGLE TREATMENT RESPONSE A-S-QQ--35 |
| THSD | THREAD SERIES DESIGNATOR | UNIFIED NATIONAL JOINT FINE (UNJF) |