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National Stock Number:
5306-01-174-8202
Federal Supply Class:
5306
National Item Identification Number:
011748202
Description:
BOLT,SHOULDER
Detail:
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.
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Manufacturer Information:
| L1700125-005 | 10000 | MANEY AIRCRAFT, INC. | | L1700125-005 | 43999 | THE BOEING COMPANY |
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Techincal Specification:
| DISTANCE FROM HEAD LARGEST BEARING SURFACE TO SHANK HOLE CENTER | 1.014 INCHES NOMINAL FIRST HOLE | | FASTENER LENGTH | 1.186 INCHES NOMINAL | | HEAD HEIGHT | 0.188 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | ST0160LB0013 FSCM 43999 MFR REF SINGLE MATERIAL RESPONSE OVERALL | | MATERIAL | STEEL COMP XM-13 OVERALL | | NOMINAL THREAD DIAMETER | 0.312 INCHES | | SHANK UNTHREADED HOLE DIAMETER | 0.076 INCHES NOMINAL FIRST HOLE | | SHOULDER DIAMETER | 0.4360 INCHES MINIMUM AND 0.4367 INCHES MAXIMUM FIRST SHOULDER | | SHOULDER DIAMETER | 0.5605 INCHES MAXIMUM AND 0.5615 INCHES MAXIMUM SECOND SHOULDER | | SHOULDER LENGTH | 0.130 INCHES MINIMUM AND 0.140 INCHES MAXIMUM SECOND SHOULDER | | SHOULDER SHAPE | ROUND ALL SHOULDERS | | SHOULDER LENGTH | 0.505 INCHES NOMINAL FIRST SHOULDER | | SPECIAL FEATURES | ECCENTRIC SHOULDERS | | THREAD DIRECTION | RIGHT-HAND | | THREAD CLASS | 3A | | THREAD LENGTH | 0.322 INCHES NOMINAL | | THREAD SERIES DESIGNATOR | UNJF | | THREAD QUANTITY PER INCH | 24 |
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