NSN 5305-00-150-9747
Part Details | MACHINE SCREW
5305-00-150-9747 An externally threaded fastener whose threaded portion is of one nominal diameter, No 0 (0.060 in./1.5 mm) or larger, designed to be held or driven with either a wrench or an inserted driver or both (excluding internal socket or internal multiple spline types), in sizes below No. 10 (0.190 in./5 mm). No. 10 and larger sizes must have a head designed for any type inserted driver (excluding internal socket or internal multiple spline types), but may also be designed for external wrenching. A locking feature may be incorporated in the design of the head or threads. Excludes BOLT, CLEVIS; BOLT, EXTERNALLY RELIEVED BODY; SCREW, EXTERNALLY RELIEVED BODY; and SCREW, ASSEMBLED WASHER. See also, SCREW, INSTRUMENT; BOLT, MACHINE; BOLT, INTERNAL WRENCHING; and SCREW, CAP SOCKET HEAD.
Alternate Parts: AN5071032R22, AN507-1032R22, 7S51022, 7S5-10-22, 10875101022, 1087510-10-22, 10875101022, 1087510-10-22, MS24693S279, MS24693S279, 5305-00-150-9747, 00-150-9747, 5305001509747, 001509747
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-150-9747 | 06657 ( SCREW, MACHINE ) |
REFERENCE DRAWINGS & PICTURES
DISHED HEXAGON
CROSS RECESS TYPE 1
Cross Reference | NSN 5305-00-150-9747
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AN507-1032R22 | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| 7S5-10-22 | 43999 | BOEING COMPANY, THEDBA BOEING |
| 1087510-10-22 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1087510-10-22 | 18355 | BOEING COMPANY, THEDBA BOEING |
| MS24693S279 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS24693S279 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
Technical Data | NSN 5305-00-150-9747
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNF |
| NOMINAL THREAD DIAMETER | 0.190 INCHES |
| THREAD QUANTITY PER INCH | 32 |
| THREAD CLASS | 2A |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD LENGTH | 1.313 INCHES MINIMUM AND 1.375 INCHES MAXIMUM |
| FASTENER LENGTH | 1.375 INCHES NOMINAL |
| SCREW MATERIAL | STEEL COMP 1010 |
| SCREW MATERIAL DOCUMENT AND CLASSIFICATION | AQQ-S-630$AQQ-S-631$AQQ-S-634 1ST MATERIAL RESPONSE |
| SCREW SURFACE TREATMENT | CADMIUM AND CHROMATE |
| SCREW SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TYPE 2,CLASS 3 FED SPEC ALL TREATMENT RESPONSES |
| MINIMUM TENSILE STRENGTH | 60000 POUNDS PER SQUARE INCH |
| HEAD STYLE | 9 DISHED HEXAGON |
| HEAD DIAMETER | 0.333 INCHES MINIMUM AND 0.385 INCHES MAXIMUM |
| COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
| INTERNAL DRIVE STYLE | CROSS RECESS TYPE 1 |
| END ITEM IDENTIFICATION | W/S: INTERMEDIATE FORWARD TEST EQUIP (IFTE) SYSTEM; SUPPORT EQUIPMENT, B-1 AIRCRAFT; AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, B-2 BOMBER (ATB); AIRCRAFT, F-111; AVIATION ENGINE TEST SYSTEM (AETS); AIRCRAFT, HAWKEYE E-2C; F4S AIRCRAFT |