Part Details | SOCKET HEAD CAP SCREW
5305-00-935-7537 An externally threaded fastener whose threaded portion is of one nominal diameter. The head has an internal socket or multiple spline for use with an inserted driver. A locking feature may be incorporated in the design of the head or threads. Excludes items with bevel (conical) heads. See BOLT, INTERNAL WRENCHING. Excludes SCREW, SHOULDER; and SCREW, MACHINE.
Alternate Parts: NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, NAS119104T5, NAS1191-04T5, 5305-00-935-7537, 00-935-7537, 5305009357537, 009357537
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | APR 13, 2007 | 00-935-7537 | 16282 ( SCREW, CAP, SOCKET HEAD ) |
REFERENCE DRAWINGS & PICTURES
CROWNED HEXAGON
OFFSET CRUCIFORM (TORQUE SET)
Cross Reference | NSN 5305-00-935-7537
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| NAS1191-04T5 | 50568 | APCOM INC |
| NAS1191-04T5 | 58998 | FASTENER INNOVATION TECHNOLOGY, INC.DBA F I T |
| NAS1191-04T5 | 07679 | HARDWARE SPECIALTY CO. INC. |
| NAS1191-04T5 | 73197 | HI-SHEAR CORPORATION |
| NAS1191-04T5 | L4528 | LISI AEROSPACE CANADA CORPDIV HI SHEAR HOLDINGS INC |
| NAS1191-04T5 | 16941 | LONG-LOK FASTENERS CORPORATION |
| NAS1191-04T5 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| NAS1191-04T5 | 56357 | ND INDUSTRIES, INC.DIV EASTERN DIVISION |
| NAS1191-04T5 | 07851 | NOR-CAL SUPPLY CO.INC. |
| NAS1191-04T5 | 80539 | SPS TECHNOLOGIES, LLCDBA AEROSPACE FASTENERS GROUP |
Technical Data | NSN 5305-00-935-7537
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNC |
| NOMINAL THREAD DIAMETER | 0.112 INCHES |
| THREAD QUANTITY PER INCH | 40 |
| THREAD CLASS | 3A |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD LENGTH | 0.312 INCHES NOMINAL |
| FASTENER LENGTH | 0.312 INCHES NOMINAL |
| MINIMUM TENSILE STRENGTH | 160000 POUNDS PER SQUARE INCH |
| HEAD STYLE | 9 CROWNED HEXAGON |
| HEAD DIAMETER | 0.178 INCHES MINIMUM AND 0.183 INCHES MAXIMUM |
| HEAD HEIGHT | 0.059 INCHES MINIMUM AND 0.069 INCHES MAXIMUM |
| INTERNAL DRIVE STYLE | OFFSET CRUCIFORM (TORQUE SET) |
| SPECIFICATION/STANDARD DATA | 80205-NAS1191 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| END ITEM IDENTIFICATION | USED ON F-111 AIRCRAFT |