1、 AEROSPACE STANDARD BOLT, MACHINE - HEXAGON HEAD, DRILLED, 1 HOLE, FULL SHANK, CRES (UNS S17400), .3125-24 UNJF-3A AS9796Copyright 2015 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, elec
2、tronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 19
3、99-08REAFFIRMED2005-05REVISED 2015-01THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.B FEDERAL SUPPLY CLASS 5306 AS9796 SHEET 1 OF 2 REV. B PROCUREMENT SPECIFICATION: AS7474SAE Technical Standards Board Rules provide that: “This report ispublished by SAE toadvance thestate of technicalandengineering scie
4、nces. Theuse ofthisreport is entirelyvoluntary, andits applicability and suitability forany particularuse,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay berevised,reaffirmed, stabi
5、lized, orcancelled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS9796B RATIONALE CORRECT DATUM REFERENCES IN FEATURE CONTROL FRAMES FOR RUNOUT, REDRAW FIGURE 1 TO SHOW A FULL S
6、HANK DIAMETER PART, AND RESTORE ORIGINAL REQUIREMENTS FOR THREAD END CHAMFER. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9796B, NOTICE 1. THIS SAE STANDARD MAY RETAIN THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT. ANY RE
7、QUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LISTS (QPL) MAY CONTINUE TO BE MANDATORY FOR DOD CONTRACTS. REQUIREMENTS RELATING TO QPLS HAVE NOT BEEN ADOPTED BY THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT. FIGURE 1 - BOLT AEROSPACE STANDARD AS9796 SHEET 2 OF 2 REV. B BOLT, MACHIN
8、E - HEXAGON HEAD, DRILLED, 1 HOLE, FULL SHANK, CRES (UNS S17400), .3125-24 UNJF-3A TABLE 1 - PART NUMBERS AND DIMENSIONS L, K, AND APPROX MASS PART NUMBER L K APPROXMASS LB/100 PART NUMBER L K APPROXMASS LB/100 MS9796-13 1.052 - 1.072 .128 - .188 3.32 MS9796-37 3.115 - 3.135 2.190 - 2.250 7.69 MS979
9、6-14 1.115 - 1.135 .190 - .250 3.46 MS9796-38 3.240 - 3.260 2.315 - 2.375 8.00 MS9796-15 1.178 - 1.198 .252 - .312 3.59 MS9796-39 3.365 - 3.385 2.440 - 2.500 8.26 MS9796-16 1.240 - 1.260 .315 - .375 3.73 MS9796-40 3.490 - 3.510 2.565 - 2.625 8.53 MS9796-17 1.302 - 1.322 .378 - .438 3.86 MS9796-41 3.
10、615 - 3.635 2.690 - 2.750 8.80 MS9796-18 1.365 - 1.385 .440 - .500 3.99 MS9796-42 3.740 - 3.760 2.815 - 2.875 9.06 MS9796-19 1.428 - 1.448 .502 - .562 4.12 MS9796-43 3.865 - 3.885 2.940 - 3.000 9.33 MS9796-20 1.490 - 1.510 .565 - .625 4.26 MS9796-44 3.990 - 4.010 3.065 - 3.125 9.59 MS9796-21 1.552 -
11、 1.572 .628 - .688 4.39 MS9796-45 4.115 - 4.135 3.190 - 3.250 9.86 MS9796-22 1.615 - 1.635 .690 - .750 4.53 MS9796-46 4.240 - 4.260 3.315 - 3.375 10.13 MS9796-23 1.678 - 1.698 .752 - .812 4.66 MS9796-47 4.365 - 4.385 3.440 - 3.500 10.39 MS9796-24 1.740 - 1.760 .815 - .875 4.79 MS9796-48 4.490 - 4.51
12、0 3.565 - 3.625 10.66 MS9796-25 1.802 - 1.822 .878 - .938 4.93 MS9796-49 4.615 - 4.635 3.690 - 3.750 10.92 MS9796-26 1.865 - 1.885 .940 - 1.000 5.06 MS9796-50 4.740 - 4.760 3.815 - 3.875 11.20 MS9796-27 1.928 - 1.948 1.002 - 1.062 5.19 MS9796-51 4.865 - 4.885 3.940 - 4.000 11.47 MS9796-28 1.990 - 2.
13、010 1.065 - 1.125 5.32 MS9796-52 4.990 - 5.010 4.065 - 4.125 11.73 MS9796-29 2.115 - 2.135 1.190 - 1.250 5.59 MS9796-53 5.115 - 5.135 4.190 - 4.250 12.00 MS9796-30 2.240 - 2.260 1.315 - 1.375 5.86 MS9796-54 5.240 - 5.260 4.315 - 4.375 12.27 MS9796-31 2.365 - 2.385 1.440 - 1.500 6.12 MS9796-55 5.365
14、- 5.385 4.440 - 4.500 12.53 MS9796-32 2.490 - 2.510 1.565 - 1.625 6.39 MS9796-56 5.490 - 5.510 4.565 - 4.625 12.80 MS9796-33 2.615 - 2.635 1.690 - 1.750 6.66 MS9796-57 5.615 - 5.635 4.690 - 4.750 13.06 MS9796-34 2.740 - 2.760 1.815 - 1.875 6.93 MS9796-58 5.740 - 5.760 4.815 - 4.875 13.33 MS9796-35 2
15、.865 - 2.885 1.940 - 2.000 7.20 MS9796-59 5.865 - 5.885 4.940 - 5.000 13.59 MS9796-36 2.990 - 3.010 2.065 - 2.125 7.46 MS9796-60 5.990 - 6.010 5.065 - 5.125 13.86 NOTES: /1/ FOR PART NUMBERS AS9796-13 THRU AS9796-19 DATUM Z SHALL REPLACE DATUM Y. 2. PROCUREMENT SPECIFICATION: AS7474. 3. MATERIAL: CO
16、RROSION RESISTANT STEEL AMS5643 (COMPOSITION SIMILAR TO UNS S17400). 4. HARDNESS: HRC32-38. 5. FLUORESCENT PENETRANT INSPECTION PER ASTM E1417/E1417M, TYPE 1, SENSITIVITY LEVEL 2 MIN. 6. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO B
17、E 125 MICROINCHES Ra EXCEPT UPSET HEAD. 7. BREAK SHARP EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. 8. DIMENSIONS IN INCHES. 9. DIMENSIONS AND TOLERANCING: ANSI Y14.5M-1982 (ASME PUBLICATION) 10. DO NOT USE UNASSIGNED PART NUMBERS. 11. A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENI
18、ENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO THE PREVIOUS ISSUE OF THIS DOCUMENT. AN (R) SYMBOL TO THE LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY. AS AND AMS ARE SAE INTERNATIONAL PUBLICATIONS. ASME IS AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION. ASTM IS AN ASTM INTERNATIONAL PUBLICATION.
