NSN 5306-01-620-2534
Part Details | SHOULDER BOLT
5306-01-620-2534 An externally threaded fastener whose threaded portion is of one nominal diameter, No. 10 (0.190 IN.) (5 mm) or larger. It has a round unthreaded neck or shank all or part of which is of greater diameter than the threaded portion. The head is not designed to be held or driven with an inserted drivers. A locking feature may be incorporated in the design of the head or threads. For items with a thread diameter smaller than No. 10 (0.190 IN.) (5 mm) and those items with an inserted drive head, use SCREW, SHOULDER. For items which are No. 10 (0.190 IN.) (5 mm) or larger in size and are both shouldered and have an externally relieved body, use BOLT, EXTERNALLY RELIEVED BODY. Excludes THUMBSCREW.
Alternate Parts: NAS1160321D, NAS1160-3-21D, 5306-01-620-2534, 01-620-2534, 5306016202534, 016202534
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JUL 11, 2013 | 01-620-2534 | 04905 ( BOLT, SHOULDER ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5306-01-620-2534
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| NAS1160-3-21D | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
Technical Data | NSN 5306-01-620-2534
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNJF |
| THREAD QUANTITY PER INCH | 32 |
| MINIMUM TENSILE STRENGTH | 2350 POUNDS PER SQUARE INCH |
| HOLE TYPE | DRILLED |
| HOLE DIAMETER | 0.070 INCHES MINIMUM AND 0.080 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | F-35 AIRCRAFT |