1、 AEROSPACE STANDARD BOLT, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE,CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN,.3750-24 UNJF-3A AS9532Copyright 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 an
2、y means, electronic, 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.
3、org ISSUED 1998-08REAFFIRMED 2006-05REVISED 2015-07THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.B FEDERAL SUPPLY CLASS 5306AS9532 SHEET 1 OF 3 REV. B PROCUREMENT SPECIFICATION: AS7452, SEE NOTE 3SAE Technical Standards Board Rules provide that: “This report ispublished by SAE toadvance thestate of tec
4、hnicalandengineering sciences. 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 be
5、revised,reaffirmed, stabilized, orcancelled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS9532B RATIONALE FIGURE REDRAWN, GENERAL UPDATING OF NOTES WHERE REQUIRED. NOTICE THE I
6、NITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9532, AMENDMENT 1. THIS SAE STANDARD RETAINS THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT. ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LISTS (QPL) MAY CONTINUE TO BE MANDATORY FOR
7、DOD CONTRACTS. REQUIREMENTS RELATING TO QPLS HAVE NOT BEEN ADOPTED BY THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT. .623 MIN.564.553KL.00332250.343.35332CHAMFER 25 - 35 TO .552 - .572.3750 -24 UNJF-3APER AS8879 CHAMFER .037 - .057x 45APPROXTHREAD RUNOUTPER AS3062 SECTION THRUTHREA
8、D PROFILE32MARK PART NUMBERAND MANUFACTURERSIDENTIFICATION PERAS478 CLASS A.006.026.017R.025.015 .0025/1.006.020 U W .060 -.070 THRUCSK 85 - 95 TO ZZYYYW.144/1/ .090 - .110 BOTH ENDS250U.229.209250250HEX FLATSSHAPE IN THIS AREA OPTIONALVIEW A .522 MINBEARING SURFACE .572 MAX.017 YYAFIGURE 1 - BOLT A
9、EROSPACE STANDARD AS9532 SHEET 2 OF 3 REV. B BOLT, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN, .3750-24 UNJF-3A TABLE 1 - PART NUMBERS AND DIMENSIONS PART NO. L K APPROX. MASS LB/100 PART NO. L K APPROX. MASS LB/100 MS9532-04 MS9532-05 MS9532-06 MS9532-07 M
10、S9532-08 MS9532-09 MS9532-10 MS9532-11 MS9532-12 MS9532-13 MS9532-14 MS9532-15 MS9532-16 MS9532-17 MS9532-18 MS9532-19 MS9532-20 MS9532-21 MS9532-22 MS9532-23 MS9532-24 MS9532-25 MS9532-26 MS9532-27 MS9532-28 MS9532-29 MS9532-30 .615- .635 .678- .698 .740- .760 .802- .822 .865- .885 .928- .948 .990-
11、1.010 1.052-1.072 1.115-1.135 1.178-1.198 1.240-1.260 1.302-1.322 1.365-1.385 1.428-1.448 1.490-1.510 1.552-1.572 1.615-1.635 1.678-1.698 1.740-1.760 1.865-1.885 1.990-2.010 2.115-2.135 2.240-2.260 2.365-2.385 2.490-2.510 2.615-2.635 2.740-2.760 .088- .108 .088- .108 .088- .108 .088- .108 .088- .108
12、 .088- .108 .088- .108 .088- .108 .088- .125 .128- .188 .190- .250 .252- .312 .315- .375 .378- .438 .440- .500 .502- .562 .565- .625 .628- .688 .690- .750 .815- .875 .940-1.000 1.065-1.125 1.190-1.250 1.315-1.375 1.440-1.500 1.565-1.625 1.690-1.750 3.25 3.52 3.69 3.86 4.03 4.20 4.37 4.53 4.70 4.87 5
13、.04 5.21 5.37 5.54 5.71 5.88 6.05 6.21 6.38 6.72 7.05 7.39 7.73 8.06 8.40 8.73 9.07 MS9532-31 MS9532-32 MS9532-33 MS9532-34 MS9532-35 MS9532-36 MS9532-37 MS9532-38 MS9532-39 MS9532-40 MS9532-41 MS9532-42 MS9532-43 MS9532-44 MS9532-45 MS9532-46 MS9532-47 MS9532-48 MS9532-49 MS9532-50 MS9532-51 MS9532
14、-52 MS9532-53 MS9532-54 MS9532-55 MS9532-56 2.865-2.885 2.990-3.010 3.115-3.135 3.240-3.260 3.365-3.385 3.490-3.510 3.615-3.635 3.740-3.760 3.865-3.885 3.990-4.010 4.115-4.135 4.240-4.260 4.365-3.385 4.490-4.510 4.615-4.635 4.740-4.760 4.865-4.885 4.990-5.010 5.115-5.135 5.240-5.260 5.365-5.385 5.49
15、0-5.510 5.615-5.635 5.740-5.760 5.865-5.885 5.990-6.010 1.815-1.875 1.940-2.000 2.065-2.125 2.190-2.250 2.315-2.375 2.440-2.500 2.565-2.625 2.690-2.750 2.815-2.875 2.940-3.000 3.065-3.125 3.190-3.250 3.315-3.375 3.440-3.500 3.565-3.625 3.690-3.750 3.815-3.875 3.940-4.000 4.065-4.125 4.190-4.250 4.31
16、5-4.375 4.440-4.500 4.565-4.625 4.690-4.750 4.815-4.875 4.940-5.000 9.41 9.74 10.08 10.41 10.75 11.09 11.42 11.76 12.09 12.43 12.77 13.10 13.44 13.77 14.11 14.45 14.78 15.12 15.45 15.79 16.13 16.46 16.80 17.13 17.47 17.81 NOTES: NOTICE THIS DOCUMENT REFERENCES PARTS WHICH CONTAIN CADMIUM AS A PLATIN
17、G MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE ANY QUESTIONS CONCERNING CADMIUMS USE. 1. FOR PART NUMBERS MS9532-04 THRU MS9532-21 THE THREAD PD DATUM -Z- SHALL REPLACE DATUM -Y- . 2. MATERIAL: LOW ALLOY STEEL AMS6322 (UNS G87400). 3. PROCUREMENT SPECIFICATION: AS7452, EXCEPT HEAD SHALL BE UPSET. 4
18、. FINISH: CADMIUM PLATE PER AMS2400. DIMENSIONS ARE AFTER PLATING. 5. MAGNETIC PARTICLE INSPECTION PER ASTM E1444/E1444M AFTER PLATING 6. INCOMPLETE THREADS NOT TO ENTER FILLET. AEROSPACE STANDARD AS9532 SHEET 3 OF 3 REV. B BOLT, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE, CADMIUM PLATED, STEEL UNS G874
19、00, 125 KSI MIN, .3750-24 UNJF-3A 7. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra. 8. BREAK SHARP EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 9. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M-1982 (ASME PUBLIC
20、ATION). 10. DIMENSIONS IN INCHES. 11. DO NOT USE UNASSIGNED PART NUMBERS. 12. A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE 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
21、 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.
