Part Details | MACHINE SCREW
5305-00-984-4989 An externally threaded fastener whose threaded portion is of one nominal diameter, No 0 (0.060 in./1.5 mm) or larger, designed to be held or driven with either a wrench or an inserted driver or both (excluding internal socket or internal multiple spline types), in sizes below No. 10 (0.190 in./5 mm). No. 10 and larger sizes must have a head designed for any type inserted driver (excluding internal socket or internal multiple spline types), but may also be designed for external wrenching. A locking feature may be incorporated in the design of the head or threads. Excludes BOLT, CLEVIS; BOLT, EXTERNALLY RELIEVED BODY; SCREW, EXTERNALLY RELIEVED BODY; and SCREW, ASSEMBLED WASHER. See also, SCREW, INSTRUMENT; BOLT, MACHINE; BOLT, INTERNAL WRENCHING; and SCREW, CAP SOCKET HEAD.
Alternate Parts: AN51567, AN515-6-7, 911724, 91-172-4, 85806300, 858063-00, 5305009844989, 2035, 19045, FFS92TYPE3STYLE9C, 0714207, 65564493229, 655-644-93229, 6550159012, 655-015-9012, A88470391, A8847039-1, A88470391, A8847039-1, MS35206229, MS35206-229, MS2458426, MS24584-26, NASM35206, MS35206229, MS35206-229, 9461192607, 946119-2607, 124C941H13, 935.63.11.041, 415 146, 55836315, 558363-15, C103950307, C10395-0307, C103950307, C10395-0307, 471070, 471-070, MS3522529, MS35225-29, MS3520626, MS35206-26, 5305-00-984-4989, 00-984-4989, 5305009844989, 009844989
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1962 | 00-984-4989 | 06657 ( SCREW, MACHINE ) |
REFERENCE DRAWINGS & PICTURES
UNDERCUT HEXAGON
CROSS RECESS TYPE 1
Cross Reference | NSN 5305-00-984-4989
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AN515-6-7 | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| 91-172-4 | 04320 | CURTISS-WRIGHT CONTROLS INTEGRATEDSENSING, INC. |
| 858063-00 | 32345 | DEFENSE REDUCTION AGENCY |
| 5305009844989 | SCY13 | E.C.A ETABLISSEMENTCENTRALD'APPROVISIONNEMENT DES |
| 2035 | 73734 | FEDERAL SCREW PRODUCTS INC. |
| 19045 | 73734 | FEDERAL SCREW PRODUCTS INC. |
| FFS92TYPE3STYLE9C | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| 0714207 | S3002 | GENERAL DYNAMICS EUROPEAN,LAND-SYSTEMS-MOWAG GMBH |
| 655-644-93229 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 655-015-9012 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| A8847039-1 | 11447 | L3 TECHNOLOGIES, INC.DBA COMMUNICATION SYSTEMS - EAST |
| A8847039-1 | 49671 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| MS35206-229 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS24584-26 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| NASM35206 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| MS35206-229 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| 946119-2607 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| 124C941H13 | 97942 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS |
| 935.63.11.041 | S4080 | PILATUS AIRCRAFT LTD |
| 415 146 | 77294 | PIPER AIRCRAFT INC. |
| 558363-15 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
| C10395-0307 | 60678 | ROSEMOUNT AEROSPACE INC.DBA ROSEMOUNT AEROSPACE DIVISION |
| C10395-0307 | U8539 | ROSEMOUNT AEROSPACE LTD |
| 471-070 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| MS35225-29 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| MS35206-26 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5305-00-984-4989
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNC |
| NOMINAL THREAD DIAMETER | 0.138 INCHES |
| THREAD QUANTITY PER INCH | 32 |
| THREAD CLASS | 2A |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD LENGTH | 0.376 INCHES MINIMUM AND 0.438 INCHES MAXIMUM |
| FASTENER LENGTH | 0.438 INCHES NOMINAL |
| SCREW MATERIAL | 0$1$3 |
| SCREW MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD ALL MATERIAL RESPONSES |
| SCREW SURFACE TREATMENT | CADMIUM AND CHROMATE |
| SCREW SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE |
| MINIMUM TENSILE STRENGTH | 60000 POUNDS PER SQUARE INCH |
| HEAD STYLE | 3 UNDERCUT HEXAGON |
| HEAD DIAMETER | 0.256 INCHES MINIMUM AND 0.270 INCHES MAXIMUM |
| HEAD HEIGHT | 0.087 INCHES MINIMUM AND 0.097 INCHES MAXIMUM |
| INTERNAL DRIVE STYLE | CROSS RECESS TYPE 1 |
| SPECIAL FEATURES | FLIGHT SAFETY CRITICAL AIRCRAFT PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |