1、 AEROSPACE STANDARD BOLT, MACHINE HEXAGON HEAD, DRILLED, 6 HOLES, FULL SHANK, UNS S66286, 130 KSI MIN, .3125-24 UNJF-3A AS9585Copyright 2017 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,
2、 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.org ISSU
3、ED1999-08REAFFIRMED 2007-06REVISED2017-04THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.CFEDERAL SUPPLY CLASS 5306 AS9585 SHEET 1 OF 3 REV. C PROCUREMENT SPECIFICATION: AS7477 SAETechnicalStandardsBoard Rulesprovidethat:“Thisreportispublished bySAEto advance the state oftechnicaland engineering sciences
4、.The use ofthisreportisentirelyvoluntary,anditsapplicabilityandsuitabilityforanyparticularuse,includinganypatentinfringementarising therefrom,isthe sole responsibilityoftheuser.”SAEreviewseachtechnicalreportatleasteveryfiveyearsatwhich time itmaybe revised,reaffirmed,stabilized,orcancelled.SAEinvite
5、syourwritten commentsandsuggestions.SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AS9585C RATIONALE TO CORRECT HEAD HEIGHT FROM .260 -.271 TO .271 - .291. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILI
6、TARY STANDARD MS9585B, AMENDMENT 1. THIS SAE STANDARD MAY RETAIN THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT. ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LISTS (QPLS) 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. .015 Y.552 MIN.502.492MARK PART NUMBER ANDMANUFACTURERS IDENTIFICATIONPER AS478 CLASS A.026.006R .025.01532KL32.003THREAD RUNOUTPER AS3062250.3125-24 UNJF-3APER AS8879 .003/1.006.510 MAXVIEW A ENLARGED32SECTION THRUTHREAD PROFILE.312
8、.309/3/AUCHAMFER.037 - .057X 45 APPROXZZYCHAMFER 25 - 35TO .490 - .510.291.271250.201.105.085W.178.198.015BEARING SURFACE .460 MINYSHAPE IN THISAREA OPTIONALY6X 60ARRANGEMENT OPTIONAL6X .065 - .075 THRU.090 - .110 X 85 - 90 WYUM M .015250FIGURE 1 BOLT AEROSPACE STANDARD AS9585 SHEET 2 OF 3 REV. C BO
9、LT, MACHINE HEXAGON HEAD, DRILLED, 6 HOLES, FULL SHANK, UNS S66286, 130 KSI MIN, .3125-24 UNJF-3A TABLE 1 - PART NUMBERS AND DIMENSIONS PART NUMBER L K APPROX MASS LB/100 PART NUMBER L K APPROX MASS LB/100 MS9585-04 .490- .510 .088- .108 2.59 MS9585-32 2.740-2.760 1.815-1.875 7.47 MS9585-05 .552- .5
10、72 .088- .108 2.73 MS9585-33 2.865-2.885 1.940-2.000 7.74 MS9585-06 .615- .635 .088- .108 2.86 MS9585-34 2.990-3.010 2.065-2.125 8.01 MS9585-07 .678- .698 .088- .108 3.00 MS9585-35 3.115-3.135 2.190-2.250 8.28 MS9585-08 .740- .760 .088- .108 3.14 MS9585-36 3.240-3.260 2.315-2.375 8.55 MS9585-09 .802
11、- .822 .088- .108 3.27 MS9585-37 3.365-3.385 2.440-2.500 8.82 MS9585-10 .865- .885 .088- .108 3.41 MS9585-38 3.490-3.510 2.565-2.625 9.09 MS9585-11 .928- .948 .088- .108 3.54 MS9585-39 3.615-3.635 2.690-2.750 9.36 MS9585-12 .990-1.010 .125- .145 3.68 MS9585-40 3.740-3.760 2.815-2.875 9.63 MS9585-13
12、1.052-1.072 .128- .188 3.81 MS9585-41 3.865-3.885 2.940-3.000 9.90 MS9585-14 1.115-1.135 .190- .250 3.95 MS9585-42 3.990-4.010 3.065-3.125 10.17 MS9585-15 1.178-1.198 .252- .312 4.08 MS9585-43 4.115-4.135 3.190-3.250 10.44 MS9585-16 1.240-1.260 .315- .375 4.22 MS9585-44 4.240-4.260 3.315-3.375 10.71
13、 MS9585-17 1.302-1.322 .378- .438 4.35 MS9585-45 4.365-4.385 3.440-3.500 10.98 MS9585-18 1.365-1.385 .440- .500 4.49 MS9585-46 4.490-4.510 3.565-3.625 11.25 MS9585-19 1.428-1.448 .502- .562 4.62 MS9585-47 4.615-4.635 3.690-3.750 11.52 MS9585-20 1.490-1.510 .585- .625 4.76 MS9585-48 4.740-4.760 3.815
14、-3.875 11.80 MS9585-21 1.552-1.572 .628- .688 4.89 MS9585-49 4.865-4.885 3.940-4.000 12.07 MS9585-22 1.615-1.635 .690- .750 5.03 MS9585-50 4.990-5.010 4.065-4.125 12.34 MS9585-23 1.678-1.698 .752- .812 5.17 MS9585-51 5.115-5.135 4.190-4.250 12.61 MS9585-24 1.740-1.760 .815- .875 5.30 MS9585-52 5.240
15、-5.260 4.315-4.375 12.88 MS9585-59 1.802-1.822 .878- .938 5.44 MS9585-53 5.365-5.385 4.440-4.500 13.15 MS9585-25 1.865-1.885 .940-1.000 5.57 MS9585-54 5.490-5.010 4.565-4.625 13.42 MS9585-60 1.928-1.948 1.002-1.062 5.71 MS9585-55 5.615-5.635 4.690-4.750 13.69 MS9585-26 1.990-2.010 1.065-1.125 5.84 M
16、S9585-56 5.740-5.760 4.815-4.875 13.96 MS9585-27 2.115-2.135 1.190-1.250 6.11 MS9585-57 5.865-5.885 4.940-5.000 14.22 MS9585-28 2.240-2.260 1.315-1.375 6.38 MS9585-58 5.990-6.010 5.065-5.125 14.50 MS9585-29 2.365-2.385 1.440-1.500 6.65 MS9585-30 2.490-2.510 1.585-1.625 6.92 MS9585-31 2.615-2.635 1.6
17、90-1.750 7.19 AEROSPACE STANDARD AS9585 SHEET 3 OF 3 REV. C BOLT, MACHINE HEXAGON HEAD, DRILLED, 6 HOLES, FULL SHANK, UNS S66286, 130 KSI MIN, .3125-24 UNJF-3A NOTES 1. MATERIAL: CORROSION AND HEAT RESISTANT STEEL PER AMS5731 (UNS S66286). 2. PROCUREMENT SPECIFICATION: AS7477. 3. FOR PART NUMBERS MS
18、9585-04 THROUGH MS9585-18, THE THREAD PD DATUM Z SHALL REPLACE DATUM Y. 4. FLUORESCENT PENETRANT INSPECTION PER ASTM E1417/E1417M, TYPE 1, SENSITIVITY LEVEL 2. 5. INCOMPLETE THREADS NOT TO ENTER FILLET. 6. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECI
19、FIED, SURFACES TO BE 125 MICROINCHES Ra. 7. BREAK SHARP EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 8. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M-1982 (ASME PUBLICATION). 9. DIMENSIONS ARE IN INCHES. 10. DO NOT USE UNASSIGNED PART NUMBERS. 11. UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFAC
20、TURED TO PREVIOUS REVISIONS OF THE APPLICABLE DRAWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED. SPECIFICATION NOTES 1. REVISION INDICATOR: A CHANGE BAR (I) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS, NOT EDITORIA
21、L 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.
