NSN 5305-00-253-5607
Part Details | DRIVE SCREW
5305-00-253-5607 A hardened cylindrical fastener with multiple spiral flutes on its shank. It also has an end smaller in diameter than the outside diameter of the spiral flutes, which acts as a pilot when driven into a drilled hole.
Alternate Parts: MS213188, MS21318-8, 145984, 1459-84, 5305002535607, 0711044, MS213188, MS21318-8, MS213188, MS21318-8, 43S4944, 1770125, 177012-5, 10125084, 109371, 0467005, 0467-005, M3851011502BXX, M38510/11502BXX, AN53503, AN535-0-3, 17701252P, 177012-5-2P, 5305-00-253-5607, 00-253-5607, 5305002535607, 002535607
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-253-5607 | 15896 ( SCREW, DRIVE ) |
REFERENCE DRAWINGS & PICTURES
DISHED HEXAGON
NARROW FLUTE (TYPE E)
Cross Reference | NSN 5305-00-253-5607
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MS21318-8 | K0407 | BAE SYSTEMS GLOBAL COMBAT SYSTEMSLIMITED |
| 1459-84 | 72452 | BRAD FOOTE GEAR WORKS INC |
| 5305002535607 | A00AM | E.C.A ETABLISSEMENT CENTRALDESAPPROVISIONNEMENTS DES FORCES |
| 0711044 | S3002 | GENERAL DYNAMICS EUROPEAN,LAND-SYSTEMS-MOWAG GMBH |
| MS21318-8 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS21318-8 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| 43S4944 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 177012-5 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 10125084 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| 109371 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| 0467-005 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| M38510/11502BXX | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| AN535-0-3 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| 177012-5-2P | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5305-00-253-5607
| Characteristic | Specifications |
|---|---|
| NONMACHINE THREAD STYLE | 6 NARROW FLUTE (TYPE E) |
| NONMACHINE NOMINAL THREAD DIAMETER | 0.073 INCHES |
| FASTENER LENGTH | 0.188 INCHES NOMINAL |
| HEAD STYLE | 7 DISHED HEXAGON |
| HEAD DIAMETER | 0.118 INCHES MINIMUM AND 0.127 INCHES MAXIMUM |
| HEAD HEIGHT | 0.041 INCHES MINIMUM AND 0.049 INCHES MAXIMUM |
| PILOT DIAMETER | 0.060 INCHES MINIMUM AND 0.063 INCHES MAXIMUM |
| PILOT LENGTH | 0.047 INCHES NOMINAL |
| FEATURES PROVIDED | CASEHARDENED |
| END ITEM IDENTIFICATION | COMMUNICATIONS TERMINAL, SATELLITE AN/GSC-39(V)1; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); TRAINER, B-1B AIRCRAFT; SYSTEMS, JP-5 AVIATION FUELS; AIRBORNE MOBILE DIR AIR SPT CTL (2ID), 02M JUL83)(AN/UYQ-3A); CLOSE IN WEAPON SYSTEM (CIWS-PHALANX); ENGINE, AIRCRAFT TF33-PW-102 (C135E, EC-135H/K/P); AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130); SUPPORT EQUIPMENT, B-1 AIRCRAFT; GUN, 5-IN./54 CAL, MK-54; GUIDED MISSILE LAUNCHING SYS |