NSN 5306-00-150-9105
Part Details | MACHINE BOLT
5306-00-150-9105 An externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. The threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. The head is not designed to be held or driven with an inserted driver or by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. Head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. For items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, BOLT, SHEAR. See also SCREW, CAP, HEXAGON HEAD and SCREW, MACHINE.
Alternate Parts: AN44A, AN4-4A, S13210044, S132100-4-4, S13210044, S132100-4-4, 6026403532, 6026-4035-32, AN44A, AN4-4A, 5306001509105, 2010233, 2010233, 2010233, 6628936P8, 6628864P8, 6628706P8, TK44A, TK4-4A, 5306PL0887407, AN44A, AN4-4A, 717124442300, 401 335, 401 307, 6026403532, 6026-4035-32, 7376018, TK44A, TK4-4A, 5306-00-150-9105, 00-150-9105, 5306001509105, 001509105
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1961 | 00-150-9105 | 01847 ( BOLT, MACHINE ) |
REFERENCE DRAWINGS & PICTURES
HEXAGON
Cross Reference | NSN 5306-00-150-9105
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AN4-4A | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| S132100-4-4 | 88277 | BOEING COMPANY, THEDBA BOEING |
| S132100-4-4 | 18355 | BOEING COMPANY, THEDBA BOEING |
| 6026-4035-32 | 20551 | CAE-LINK CORP |
| AN4-4A | 0NFB8 | DIALOGIC CORP.DBA DIALOGIC FASTENERS |
| 5306001509105 | SCY13 | E.C.A ETABLISSEMENTCENTRALD'APPROVISIONNEMENT DES |
| 2010233 | FB459 | EMBRAER AVIATION INTERNATIONAL |
| 2010233 | S4956 | EMBRAER EMPRESA BRASILEIRA DEAERONAUTICA SA |
| 2010233 | 001JK | EMBRAER S.A.DBA EMBRAER |
| 6628936P8 | 24446 | GENERAL ELECTRIC COMPANY |
| 6628864P8 | 24446 | GENERAL ELECTRIC COMPANY |
| 6628706P8 | 24446 | GENERAL ELECTRIC COMPANY |
| TK4-4A | 97928 | HUCK INTL INC |
| 5306PL0887407 | 9009H | INSPEKTORAT WSPARCIA SIL ZBROJNYCH |
| AN4-4A | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| 717124442300 | 0000V | NCB HUNGARY HONVEDSEGI EGYSEGESTERMEKKOD |
| 401 335 | 77294 | PIPER AIRCRAFT INC. |
| 401 307 | 77294 | PIPER AIRCRAFT INC. |
| 6026-4035-32 | 36378 | RAYTHEON TECHNICAL SERVICES COMPANY |
| 7376018 | 19207 | U S ARMY TANK AUTOMOTIVE COMMANDAMSTA-IM-MM |
| TK4-4A | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5306-00-150-9105
| Characteristic | Specifications |
|---|---|
| HEAD STYLE | HEXAGON |
| THREAD SERIES DESIGNATOR | UNF |
| NOMINAL THREAD DIAMETER | 0.250 INCHES |
| THREAD QUANTITY PER INCH | 28 |
| THREAD CLASS | 3A |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD LENGTH | 0.438 INCHES MINIMUM AND 0.516 INCHES MAXIMUM |
| FASTENER LENGTH | 0.516 INCHES MINIMUM AND 0.562 INCHES MAXIMUM |
| MINIMUM TENSILE STRENGTH | 125000 POUNDS PER SQUARE INCH |
| HEAD HEIGHT | 0.140 INCHES MINIMUM AND 0.172 INCHES MAXIMUM |
| WIDTH BETWEEN FLATS | 0.428 INCHES MINIMUM AND 0.440 INCHES MAXIMUM |
| GRIP LENGTH | 0.046 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
| FEATURES PROVIDED | FINISHED HEAD |
| END ITEM IDENTIFICATION | B-1 SUPPORT EQUIPMENT;SOF AIRCRAFT;TF-33 ENGINE;PHOENIX MISSILE;HARPOON MISSILE;TF-56 ENGINE;AIRCRAFT, C-2A (REPROCURED);ENGINE, AIRCRAFT, TF-33-P-7 |