SAE AS 9583C-2017 BOLT MACHINE C HEXAGON HEAD DRILLED 6 HOLES FULL SHANK UNS S66286 130 KSI MIN 1900-32 UNJF-3A.pdf

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1、 AEROSPACE STANDARD BOLT, MACHINE HEXAGON HEAD, DRILLED, 6 HOLES, FULL SHANK, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3A AS9583Copyright 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、ED2000-08REAFFIRMED 2007-06REVISED2017-04THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.C FEDERAL SUPPLY CLASS 5306 AS9583 SHEET 1 OF 3 REV. C PROCUREMENT SPECIFICATION: AS7477 SAE Technical Standards Board Rules provide that: “This report is published by SAEtoadvance thestate of technicaland engineerin

4、gsciences. The useof this report is entirely voluntary, and its applicability andsuitability for any particularuse, includingany patent infringement arisingtherefrom,is thesole responsibility of theuser.” SAE reviews eachtechnical reportatleast every fiveyears at whichtime it may be revised, reaffir

5、med, stabilized, or cancelled. SAE invites your written comments and suggestions.SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AS9583C RATIONALE LIGHTENING HOLE DIAMETER CORRECTED FROM .099-.199 TO .099-.119. NOTICE THE INITIAL SAE PUBLICAT

6、ION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9583A, AMENDMENT 1, NOTICE 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

7、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 .0 1 1 Y.4 1 0 M IN.3 7 6.3 6 7M A R K P A R T N U M B E R A N DM A N U F A C T U R E R S ID E N T IF IC A T IO NP E R A S 4 7 8 C L A S S A.0 2 6.0 0 6R

8、 .0 2 5.0 1 532KL32.0 0 3T H R E A D R U N O U TP E R A S 3 0 6 22 5 0.1 9 0 0 -3 2 U N J F -3 AP E R A S 8 8 7 9 .0 0 3 /1.0 0 6. 3 8 5 M A XV IE W A E N L A R GE D32S E C T IO N T H R UT H R E A D P R O F IL E.1 8 9.1 8 6/3 /AUC H A M F E R.0 2 1 - .0 4 1X 4 5 A P P R O XZZYC H A M F E R 2 5 - 3 5

9、 T O .3 6 5 - .3 8 5.1 9 8.1 7 82 5 0.1 2 5.0 6 8.0 4 8W.0 9 9.1 1 9.0 1 1B E A R IN G S U R F A C E .3 3 5 M INYS H A P E IN T H ISA R E A OP T ION A LY6 X 6 0 A R R A N G E M E N T O P T IO N A L6 X .0 3 7 - .0 5 7 T H R U .0 5 0 - .0 7 0 X 8 5 - 9 0 WYUM M .0 1 52 5 0AEROSPACE STANDARD AS9583 SHE

10、ET 2 OF 3 REV. C BOLT, MACHINE HEXAGON HEAD, DRILLED, 6 HOLES, FULL SHANK, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3A TABLE 1 - PART NUMBERS AND DIMENSIONS PART NUMBER L K APPROX MASS LB/100 PART NUMBER L K APPROX MASS LB/100 MS9583-04 .365- .385 .072- .092 .86 MS9583-26 1.740-1.760 1.080-1.120 1.95

11、MS9583-05 .428- .448 .072- .092 .91 MS9583-44 1.802-1.822 1.122-1.182 2.00 MS9583-06 .490- .510 .072- .092 .96 MS9583-27 1.865-1.885 1.185-1.245 2.05 MS9583-07 .552- .572 .072- .092 1.01 MS9583-45 1.928-1.948 1.248-1.308 2.10 MS9583-08 .615- .635 .072- .092 1.06 MS9583-28 1.990-2.010 1.310-1.370 2.1

12、5 MS9583-09 .678- .698 .072- .092 1.11 MS9583-29 2.115-2.135 1.435-1.495 2.25 MS9583-10 .740- .760 .072- .120 1.16 MS9583-30 2.240-2.260 1.560-1.620 2.34 MS9583-11 .802- .822 .122- .182 1.21 MS9583-31 2.365-2.385 1.685-1.745 2.44 MS9583-12 .865- .885 .185- .245 1.26 MS9583-32 2.490-2.510 1.810-1.870

13、 2.54 MS9583-13 .928- .948 .248- .308 1.31 MS9583-33 2.615-2.635 1.935-1.995 2.64 MS9583-14 .990-1.010 .310- .370 1.36 MS9583-34 2.740-2.760 2.060-2.120 2.74 MS9583-15 1.052-1.072 .372- .432 1.41 MS9583-35 2.865-2.885 2.185-2.245 2.84 MS9583-16 1.115-1.135 .435- .495 1.46 MS9583-36 2.990-3.010 2.310

14、-2.370 2.94 MS9583-17 1.178-1.198 .498- .558 1.51 MS9583-37 3.115-3.135 2.435-2.495 3.03 MS9583-18 1.240-1.260 .560- .620 1.55 MS9583-38 3.240-3.260 2.560-2.620 3.13 MS9583-19 1.302-1.322 .622- .682 1.60 MS9583-39 3.365-3.385 2.685-2.745 3.23 MS9583-20 1.365-1.385 .685- .745 1.65 MS9583-40 3.490-3.5

15、10 2.810-2.870 3.33 MS9583-21 1.428-1.448 .748- .808 1.70 MS9583-41 3.615-3.635 2.935-2.995 3.43 MS9583-22 1.490-1.510 .810- .870 1.75 MS9583-42 3.740-3.760 3.060-3.120 3.53 MS9583-23 1.552-1.572 .872- .932 1.80 MS9583-43 3.865-3.885 3.185-3.245 3.63 MS9583-24 1.615-1.635 .935- .995 1.85 MS9583-25 1

16、.678-1.698 .998-1.058 1.90 NOTES 1. MATERIAL: CORROSION AND HEAT RESISTANT STEEL PER AMS5731 (UNS S66286). 2. PROCUREMENT SPECIFICATION: AS7477. 3. FOR PART NUMBERS MS9583-04 THROUGH MS9583-14, THE THREAD PD DATUM Z SHALL REPLACE DATUM Y. 4. FLUORESCENT PENETRANT INSPECTION PER ASTM E1417/E1417M, TY

17、PE 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 SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra. 7. BREAK SHARP EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 8. DIMENSIONING AND TOLERANCI

18、NG 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 MANUFACTURED TO PREVIOUS REVISIONS OF THE APPLICABLE DRAWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED. AEROSPACE ST

19、ANDARD AS9583 SHEET 3 OF 3 REV. C BOLT, MACHINE HEXAGON HEAD, DRILLED, 6 HOLES, FULL SHANK, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3A 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,

20、 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.