|
|
National Stock Number: 5305-01-098-3640
Federal Supply Class: 5305
National Item Identification Number: 010983640
Description: SCREW,CAP,SOCKET HEAD
Detail: 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.
|
Manufacturer Information:
A01408-524 | 94697 | MOOG INC | A01408-524 | 9P5N5 | MOOG MILITARY AIRCRAFT LLC |
|
Techincal Specification:
THREAD SERIES DESIGNATOR | UNRF | NOMINAL THREAD DIAMETER | 0.250 INCHES | THREAD QUANTITY PER INCH | 28 | THREAD DIRECTION | RIGHT-HAND | THREAD LENGTH | 1.000 INCHES MINIMUM AND | | 1.500 INCHES MAXIMUM | FASTENER LENGTH | 1.500 INCHES NOMINAL | MATERIAL | STEEL OVERALL | MATERIAL DOCUMENT AND CLASSIFICATION | FF-S-86 FED SPEC SINGLE MATERIAL RESPONSE OVERALL | SURFACE TREATMENT | OXIDE OVERALL | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-13924,CLASS 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL | HARDNESS RATING | 38.0 ROCKWELL C MINIMUM AND | | 45.0 ROCKWELL C MAXIMUM OVERALL | MINIMUM TENSILE STRENGTH | 170000 POUNDS PER SQUARE INCH | HEAD STYLE | FLAT CHAMFER | HEAD DIAMETER | 0.365 INCHES MINIMUM AND | | 0.375 INCHES MAXIMUM | HEAD HEIGHT | 0.244 INCHES MINIMUM AND | | 0.250 INCHES MAXIMUM | INTERNAL DRIVE STYLE | HEXAGON | WIDTH ACROSS FLATS | 0.187 INCHES NOMINAL | HOLE CONFIGURATION STYLE | ROUND INTERNAL HEXAGON | HOLE TYPE | DRILLED | HOLE QUANTITY | 6 | HOLE DIAMETER | 0.047 INCHES NOMINAL | SPECIAL FEATURES | COLOR BLACK | PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVY SPECIAL PROJECT |
|
|