NSN 5305-00-269-3235
Part Details | HEXAGON HEAD CAP SCREW
5305-00-269-3235 An externally threaded fastener designed for insertion into holes in assembled parts, for mating with a preformed internal thread and for tightening or releasing by torquing the head. The threaded and unthreaded portions are both of the same nominal diameter of 0.190 inch (5 mm) or larger. Head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. The thread length being the controlled dimension, the grip length is not specified. A locking feature may be incorporated in the design of the head or threads. The head is not designed to be held or driven with an inserted driver or by the thumb and fingers. Excludes BOLT,MACHINE; BOLT,EXTERNALLY RELIEVED BODY; BOLT,INTERNAL WRENCHING; and SCREW,CAP,SOCKET HEAD.
Alternate Parts: S210NA38FAK16354BNCG1, B1821BH038F088N, ASME B18.2.1, AES01F375875AW9A91, 18C614, 5305002693235, FFS85, FF-S-85, 14722, 14722, MS9072759, MS90727-59, 22399R1, 22399R1, T703, 5305-00-269-3235, 00-269-3235, 5305002693235, 002693235
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-269-3235 | 18257 ( SCREW, CAP, HEXAGON HEAD ) |
REFERENCE DRAWINGS & PICTURES
HEXAGON
Cross Reference | NSN 5305-00-269-3235
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| S210NA38FAK16354BNCG1 | 80204 | AMERICAN NATIONAL STANDARDSINSTITUTE, INCORPORATED |
| B1821BH038F088N | 80204 | AMERICAN NATIONAL STANDARDSINSTITUTE, INCORPORATED |
| ASME B18.2.1 | 05047 | AMERICAN SOCIETY OF MECHANICALENGINEERS, THE |
| AES01F375875AW9A91 | 05047 | AMERICAN SOCIETY OF MECHANICALENGINEERS, THE |
| 18C614 | 12603 | CLARK EQUIPMENT CO |
| 5305002693235 | SCY13 | E.C.A ETABLISSEMENTCENTRALD'APPROVISIONNEMENT DES |
| FF-S-85 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| 14722 | 04627 | HYSTER-YALE GROUP, INC. |
| 14722 | 30076 | HYSTER-YALE GROUP, INC. |
| MS90727-59 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 22399R1 | 66195 | SOLAR TURBINES INCORPORATED |
| 22399R1 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| T703 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5305-00-269-3235
| Characteristic | Specifications |
|---|---|
| THREAD SERIES DESIGNATOR | UNF |
| THREAD LENGTH | 0.875 INCHES MAXIMUM |
| FASTENER LENGTH | 0.875 INCHES NOMINAL |
| HEAD STYLE | HEXAGON |
| THREAD DIRECTION | RIGHT-HAND |
| NOMINAL THREAD DIAMETER | 0.375 INCHES |
| THREAD QUANTITY PER INCH | 24 |
| THREAD CLASS | 2A |
| MINIMUM TENSILE STRENGTH | 150000 POUNDS PER SQUARE INCH |
| MINIMUM YIELD STRENGTH | 120000 POUNDS PER SQUARE INCH |
| HEAD HEIGHT | 0.226 INCHES MINIMUM AND 0.243 INCHES MAXIMUM |
| WIDTH BETWEEN FLATS | 0.551 INCHES MINIMUM AND 0.562 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | W/S: SUPPORT EQUIPMENT, B-1 AIRCRAFT; CLOSE IN WEAPON SYSTEM (CIWS-PHALANX); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); AIRCRAFT, T-39; AIRCRAFT, C-2A (REPROCURED); SHIPBOARD MATERIAL HANDLING EQUIPMENT (MHE); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); VEHICLE, AIRCRAFT REFUELER R-14 |