NSN 5305-00-255-5509 · NIIN 002555509 · FSC 5305
NO DASHES 5305002555509
In Stock
SCREW,CAP,SOCKET HEAD
Screws
Application: M1A2SYSTEM ENHANCEMENT PROG; AH-64D LONGBOW; TANK, COMBAT, FT, 120MM GUN (M1A1); AIRCRAFT, OSPREY V-22A, AIR FORCE; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); ENGINE, AIRCRAFT F-100-PW-229 (F15E, F16C/D); M1A2 ABRAMS TANK; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); AIRCRAFT, OSPREY V-22A, MARINE CORPS
Technical characteristics
21 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 |
|---|---|---|
| AASU | HEAD HEIGHT | INCHES MINIMUM 0.070 AND INCHES MAXIMUM 0.080 |
| AASL | HEAD DIAMETER | INCHES MINIMUM 0.205 AND INCHES MAXIMUM 0.219 |
| AASK | HEAD STYLE | |
| AASB | FASTENER LENGTH | INCHES MINIMUM 0.219 AND INCHES MAXIMUM 0.250 |
| AASA | THREAD LENGTH | INCHES MINIMUM 0.169 AND INCHES MAXIMUM 0.250 |
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| CSYM | SURFACE FINISH | BEARING SURFACE OF HEAD MICROINCHES 32.0 |
| CSYM | SURFACE FINISH | THREADS MICROINCHES 32.0 |
| MATT | MATERIAL | OVERALL STEEL COMP 4140 OR STEEL COMP E4340 OR STEEL COMP 6150 OR STEEL COMP 8735 OR STEEL COMP 8740 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL MIL SPEC 1ST MATERIAL RESPONSE -IL-S-5626 OR MIL SPEC 2ND MATERIAL RESPONSE -IL-S-5000 OR MIL SPEC 3RD MATERIAL RESPONSE -IL-S-8503 OR MIL SPEC 4TH MATERIAL RESPONSE -IL-S-6098 OR MIL SPEC 5TH MATERIAL RESPONSE -IL-S-6049 |
| SFTT | SURFACE TREATMENT | OVERALL CADMIUM AND CHROMATE |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | OVERALL FED SPEC SINGLE TREATMENT RESPONSE QQ--416,TY 2 CL 2 |
| THSD | THREAD SERIES DESIGNATOR | UNJC |
| ZZZK | SPECIFICATION/STANDARD DATA | PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD 80205-NAS1190 |
| ABQZ | INTERNAL DRIVE STYLE | |
| AGAV | END ITEM IDENTIFICATION | M1A2SYSTEM ENHANCEMENT PROG; AH-64D LONGBOW; TANK, COMBAT, FT, 120MM GUN (M1A1); AIRCRAFT, OSPREY V-22A, AIR FORCE; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); ENGINE, AIRCRAFT F-100-PW-229 (F15E, F16C/D); M1A2 ABRAMS TANK; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); AIRCRAFT, OSPREY V-22A, MARINE CORPS |
| AHYM | NOMINAL THREAD DIAMETER | INCHES 0.112 |
| CMLP | THREAD QUANTITY PER INCH | 40 |
| CQBC | MINIMUM TENSILE STRENGTH | POUNDS PER SQUARE INCH 160000 |
| CQFM | HARDNESS RATING | OVERALL ROCKWELL C MINIMUM 36.0 AND ROCKWELL C MAXIMUM 40.0 |
Cross-references
20 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| LK1190-04P4 | 26304 |
| NAS1190-04P4 | 30902 |
| NAS1190-04P4 | 50568 |
| NAS1190-04P4 | 53606 |
| NAS1190-04P4 | 56357 |
| NAS1190-04P4 | 56878 |
| NAS1190-04P4 | 58998 |
| NAS1190-04P4 | 73197 |
| NAS1190-04P4 | 80205 |
| NAS1190-04P4 | 80539 |
| NAS1190-04P4 | 92215 |
| NAS1190-04P4 | 97928 |
| NAS1190-04P4 | C4293 |
| NAS1190-04P4 | L4528 |
| NAS1190-04P4 | 04348 |
| NAS1190-04P4 | 07679 |
| NAS1190-04P4 | 08938 |
| NAS1190-04P4 | 07851 |
| NAS1190-04P4 | 16941 |
| NAS1190-04P4 | 17446 |
Supersedes
This item replaces cancelled NIINs 001450968 · 010067186. An older drawing citing one of those numbers resolves here.