NSN 5305-01-477-5835 · NIIN 014775835 · FSC 5305
NO DASHES 5305014775835
In Stock
SCREW,CLOSE TOLERANCE
Screws
Application: STRUCTURAL COMPONENTS; 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 0.531 |
| AASB | FASTENER LENGTH | INCHES MINIMUM 1.7025 AND INCHES MAXIMUM 1.7495 |
| AASK | HEAD STYLE | |
| AASL | HEAD DIAMETER | INCHES NOMINAL 0.575 |
| AASU | HEAD HEIGHT | INCHES MINIMUM 0.0878 AND INCHES MAXIMUM 0.0898 |
| AAUR | GRIP DIAMETER | INCHES MINIMUM 0.3115 AND INCHES MAXIMUM 0.3120 |
| ABQZ | INTERNAL DRIVE STYLE | |
| AGAV | END ITEM IDENTIFICATION | STRUCTURAL COMPONENTS; F18 AIRCRAFT |
| AHYM | NOMINAL THREAD DIAMETER | INCHES 0.3125 |
| ANEE | GRIP LENGTH | INCHES MINIMUM 1.1775 AND INCHES MAXIMUM 1.1975 |
| 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 DEG COUNTERSUNK HEAD, DOVETAIL SLOT,CRES |
| FEAT | SPECIAL FEATURES | O-RING PER ST7M251, NO FINISH, NO LUBRICANT; MINIMUM 40 PERCENT OF NON-BEARING HEAD SURFACE COAT WITH WHITE PAINT, COLOR 37875 PER FED-STD-595, REMOVABLE WITH SOLVENT |
| MATT | MATERIAL | FASTENER STEEL COMP XM-13 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FASTENER ASSN STD SINGLE MATERIAL RESPONSE A-S5629, H13-8-O |
| SFTT | SURFACE TREATMENT | FASTENER PASSIVATE |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | FASTENER ASSN STD SINGLE TREATMENT RESPONSE A-S-QQ--35 |
| THSD | THREAD SERIES DESIGNATOR | UNIFIED NATIONAL JOINT FINE (UNJF) |