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1、 AEROSPACE STANDARD SCREW, MACHINE STEEL UNS G87400, CADMIUM PLATE, DRILLED, 1 HOLE, HEXAGON HEAD, .1640-36 UNJF-3A AS9528 Copyright 2007 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, el
2、ectronic, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 200
3、0-08 REAFFIRMED 2004-07 REVISED 2007-09 THIRD ANGLE PROJECTION CUSTODIAN: SAE E-25 REV. A FEDERAL SUPPLY CLASS 5305 AS9528 SHEET 1 OF 2 REV. A SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of thi
4、s report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or canc
5、elled. SAE invites your written comments and suggestions. RATIONALE STANDARD UPDATED, CADMIUM WARNING NOTE ADDED, THREAD SPECIFICATION REVISED TO AS8879, AND GEOMETRIC CONTROLS FOR SHORT LENGTH SCREWS CLARIFIED TO AGREE WITH AS1132. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIREC
6、TLY FROM U.S. MILITARY STANDARD MS9528. 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 DOD CONTRACTS. REQUIREMENTS RELATING TO QPLS HAVE NOT BEEN ADOPTED B
7、Y THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT. .003 Y THREAD RUNOUT PER A 3062S 250 250 32 K L CHAMFER 25 - 35 TO .302 - .322 OO .003/1 .006 Z - Y - .151 .141 SEE NOTE 1 .010 Y .010 Y R 32 CHAMFER .015- .035 X 45 APPROX O .1640-36 UNJF-3A PER AS8879 - Z - - W - - U - .020 .010 .1
8、39 .127 SHAPE IN THIS AREA OPTIONAL .272 MIN BEARING SURFACE .322 MAX VIEW A .313 .305 .339 MIN A .026 .006 MARK PART NUMBER AND MANUFACTURERS IDENTIFICATION PER CLASS AAS478 .042 - .052 THRU CSK 85 - 95 TO .060 - .080 BOTH ENDS OO .014 U W M .074 32 SECTION THRU THREAD PROFILE FIGURE 1 - SCREW Copy
9、right SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 20:57:47 MSTNo reproduction or networking permitted without license from IHS -,-,- AEROSPACE STANDARD SCREW, MACHINE STEEL UNS G87400, CADMIUM PLATE, DRILLED, 1 HOLE, HEXAG
10、ON HEAD, .1640-36 UNJF-3A AS9528 SHEET 2 OF 2 REV. A TABLE 1 - PART NUMBERS AND DIMENSIONS. .PART NUMBER L K APPROX MASS LB/100 PART NUMBER L K APPROX MASS LB/100 MS9528-03 MS9528-04 MS9528-05 MS9528-06 MS9528-07 MS9528-08 MS9528-09 MS9528-10 MS9528-11 MS9528-12 MS9528-13 MS9528-14 MS9528-15 .302 -
11、.322 .365 - .385 .428 - .448 .490 - .510 .552 - .572 .615 - .635 .678 - .698 .740 - .760 .802 - .822 .865 - .885 .928 - .948 .990 - 1.010 1.052 - 1.072 .062- .082 .062- .082 .062- .082 .062- .082 .062- .082 .062- .082 .062- .110 .112- .172 .174- .234 .237- .297 .300- .360 .362- .422 .424- .484 .43 .
12、46 .49 .53 .56 .59 .62 .65 .69 .72 .75 .78 .81 MS9528-16 MS9528-17 MS9528-18 MS9528-19 MS9528-20 MS9528-21 MS9528-22 MS9528-23 MS9528-24 MS9528-25 MS9528-26 MS9528-27 MS9528-28 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 - 1.6
13、35 1.678 - 1.698 1.740 - 1.760 1.865 - 1.885 1.990 - 2.010 .487 - .547 .550 - .610 .612 - .672 .674 - .734 .737 - .797 .800 - .860 .862 - .922 .924 - .984 .987 - 1.047 1.050 - 1.110 1.112 - 1.172 1.237 - 1.297 1.362 - 1.425 .84 .88 .91 .94 .97 1.00 1.04 1.07 1.10 1.13 1.16 1.23 1.29 NOTES: NOTICE TH
14、IS DOCUMENT REFERENCES PARTS WHICH CONTAIN CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE ANY QUESTIONS CONCERNING CADMIUMS USE 1. FOR PART NUMBERS MS9528-03 THRU MS9528-13 THE THREAD PD (DATUM “Z”) SHALL REPLACE DATUM “Y”. 2. MATERIAL: LOW ALLOY STEEL AMS 6322 (UNS G87400). 3. P
15、ROCUREMENT SPECIFICATION: AS7452, EXCEPT HEAD SHALL BE UPSET. 4. FINISH: CADMIUM PLATE PER AMS 2400. DIMENSIONS ARE AFTER PLATING. 5. MAGNETIC PARTICLE INSPECTION PER ASTM E 1444. 6. INCOMPLETE THREADS NOT TO ENTER FILLET. 7. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UN
16、LESS 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 PUBLICATION). 10. DIMENSIONS IN INCHES. 11. DO NOT USE UNASSIGNED PART NUMBERS. 12. THE CHANGE BAR ( l ) LOCATED IN T
17、HE 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 LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT. AS AND AMS ARE SAE INTERNATIONAL
18、 PUBLICATIONS. ASME IS AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION. ASTM IS AN ASTM INTERNATIONAL PUBLICATION. Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 20:57:47 MSTNo reproduction or networking permitted without license from IHS -,-,-