|
|
National Stock Number: 5306-00-579-3077
Federal Supply Class: 5306
National Item Identification Number: 005793077
Description: BOLT,MACHINE
Detail: 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.
|
Manufacturer Information:
351406 | 00088 | ROYAL OAK GAGE INC | 351406 | 11449 | TURBO POWER & MARINE SYSTEM INC SUB OF UNITED TECHNOLOGIES CORP | 351406 | 4GP55 | ACUFAST AIRCRAFT PRODUCTS | 351406 | 77445 | RTX CORPORATION | 351406 | 80539 | SPS TECHNOLOGIES, LLC | 351406 | 92215 | HOWMET GLOBAL FASTENING SYSTEMS INC |
|
Techincal Specification:
THREAD DIRECTION | RIGHT-HAND | FASTENER LENGTH | 0.990 INCHES MINIMUM AND | | 1.010 INCHES MAXIMUM | MATERIAL | STEEL COMP 601 OVERALL | THREAD LENGTH | 0.688 INCHES MINIMUM | HEAD STYLE | HEXAGON | THREAD SERIES DESIGNATOR | UNF | NOMINAL THREAD DIAMETER | 0.312 INCHES | THREAD QUANTITY PER INCH | 24 | THREAD CLASS | 1A | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6304 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | SURFACE TREATMENT | NICKEL AND | | CADMIUM OVERALL | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS 2416 ASSN STD ALL TREATMENT RESPONSES OVERALL | HARDNESS RATING | 30.0 ROCKWELL C MINIMUM AND | | 38.0 ROCKWELL C MAXIMUM OVERALL | HEAD HEIGHT | 0.178 INCHES MINIMUM AND | | 0.198 INCHES MAXIMUM | WIDTH BETWEEN FLATS | 0.492 INCHES MINIMUM AND | | 0.502 INCHES MAXIMUM | GRIP LENGTH | 0.220 INCHES MINIMUM AND | | 0.240 INCHES MAXIMUM | FEATURES PROVIDED | FINISHED HEAD | SPECIAL FEATURES | FAILURE COULD CAUSE SERIOUS DAMAGE TO THE AIRCRAFT OR WEAPON SYSTEM OR AN UNCOMMANDED ENGINE SHUTDOWN THAT JEOPARDIZES SAFETY | CRITICALITY CODE JUSTIFICATION | FEAT |
|
|