SAE AS 92001C-2017 NUT HEXAGON DRILLED BOSS CONNECTION ALUMINUM C UNS A92014.pdf

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1、 AEROSPACE STANDARD NUT, HEXAGON, DRILLED, BOSS CONNECTION, ALUMINUM UNS A92014 AS92001Copyright 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, electronic, mechanical, photocopying,

2、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 ISSUED2000-09REAFFIRMED 2006-06REVISED2017-

3、08THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.C FEDERAL SUPPLY CLASS 5310 AS92001 SHEET 1 OF 3 REV. C PROCUREMENT SPECIFICATION: NONE SAE Technical Standards Board Rules provide that: “This report is published by SAEtoadvance thestate of technicaland engineering sciences. The useof this report is ent

4、irely 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, reaffirmed, stabilized, or cancelled. SAE invi

5、tes your written comments and suggestions.SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AS92001C RATIONALE FIGURE REDRAWN, USEAGE OF PART NOTE ADDED, FOLLOWING FIVE YEAR REVIEW. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN

6、DIRECTLY FROM U.S. MILITARY STANDARD MS9200C, 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 CONTRACTS. REQUIREMENTS RELATING TO QPLS HAV

7、E NOT BEEN ADOPTED BY THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT. E L LTTAF 250. 0 1 0 YE3. 0 9 0. 1 5 0KUB O T H S I D E S. 0 0 5 Y/ 6 /1 0 - 2 0 B O T H S I D E S A B1 0 5 - 1 1 5 T O A BB O T H S I D E S63P63T H R E A D DP E R A S 8 8 7 9Y2 X J . 0 1 0 U YMB R E A K E D G E S

8、 O F H O L E S . 0 0 5 - . 0 1 5FIGURE 1 - NUT AEROSPACE STANDARD AS92001 SHEET 2 OF 3 REV. C NUT, HEXAGON, DRILLED, BOSS CONNECTION, ALUMINUM UNS A92014 TABLE 1 PART NUMBERS AND DIMENSIONS PART NUMBER NOM TUBE OD D - NOMINAL THREAD AF E MIN AB MS9200-02 .125 .3125-24-UNJF-3B .553- .564 .623 .312- .

9、332 MS9200-03 .188 .3750-24UNJF-3B .616- .627 .694 .375- .395 MS9200-04 .250 .4375-20UNJF-3B .679- .690 .766 .438- .458 MS9200-05 .312 .5000-20UNJF-3B .741- .752 .836 .500- .520 MS9200-06 .375 .5625-18UNJF-3B .803- .814 .907 .562- .582 MS9200-07 .438 .6250-18UNJF-3B .865- .877 .978 .625- .645 MS9200

10、-08 .500 .7500-16UNJF-3B .990-1.002 1.121 .750- .770 MS9200-09 .562 .8125-16UNJ-3B 1.052-1.064 1.191 .812- .832 MS9200-10 .625 .8750-14UNJF-3B 1.114-1.127 1.262 .875- .895 MS9200-11 .688 1.0000-12UNJF-3B 1.301-1.314 1.475 1.000-1.020 MS9200-12 .750 1.0625-12UNJ-3B 1.364-1.377 1.547 1.062-1.082 MS920

11、0-14 .875 1.1875-12UNJ-3B 1.489-1.502 1.690 1.188-1.208 MS9200-16 1.000 1.3125-12UNJ-3B 1.614-1.627 1.833 1.312-1.332 MS9200-18 1.125 1.5000-12UNJ-3B 1.800-1.814 2.045 1.500-1.520 MS9200-20 1.250 1.6250-12UNJ-3B 1.926-1.940 2.189 1.625- 1.645 MS9200-24 1.500 1.8750-12UNJ-3B 2.176-2.190 2.474 1.875-

12、1.895 MS9200-28 1.750 2.2500-12UNJ-3B 2.549-2.564 2.899 2.250-2.270 MS9200-32 2.000 2.5000-12UNJ-3B 2.799-2.814 3.185 2.500- 2.520 TABLE 1 PART NUMBERS AND DIMENSIONS (CONTINUED) PART NUMBER NOM TUBE OD K L MIN P T J APPROX MASS LB/100 MS9200-02 .125 .209-.229 .552 .110 .240 .042-.052 .43 MS9200-03

13、.188 .209-.229 .615 .110 .240 .042-.052 .49 MS9200-04 .250 .240-.260 .678 .125 .305 .042-.052 .66 MS9200-05 .312 .240 -.260 .740 .125 .340 .050-.060 .75 MS9200-06 .375 .256 -.276 .802 .133 .370 .050-.060 .88 MS9200-07 .438 .256 -.276 .865 .133 .405 .050-.060 .99 MS9200-08 .500 .302-.322 .990 .157 .4

14、70 .057- .067 1.39 MS9200-09 .562 .302-.322 1.052 .157 .500 .057- .067 1.47 MS9200-10 .625 .349-.369 1.115 .180 .540 .057- .067 1.89 MS9200-11 .688 .396-.416 1.302 .204 .625 .065-.075 3.06 MS9200-12 .750 .396-.416 1.365 .204 .660 .065-.075 3.26 MS9200-14 .875 .396-.416 1.490 .204 .725 .065-.075 3.64

15、 MS9200-16 1.000 .396-.416 1.615 .204 .790 .065-.075 4.07 MS9200-18 1.125 .396-.416 1.802 .204 .890 .065-.075 4.70 MS9200-20 1.250 .396-.416 1.928 .204 .960 .065-.075 5.15 MS9200-24 1.500 .396-.416 2.178 .204 1.095 .065-.075 6.06 MS9200-28 1.750 .396-.416 2.552 .204 1.295 .065-.075 7.47 MS9200-32 2.

16、000 .396-.416 2.802 .204 1.425 .065-.075 8.47 AEROSPACE STANDARD AS92001 SHEET 3 OF 3 REV. C NUT, HEXAGON, DRILLED, BOSS CONNECTION, ALUMINUM UNS A92014 NOTES 1. MATERIAL ALUMINUM ALLOY AMS4121 (SIMILAR TO UNS A92014). 2. SURFACE FINISH: ANODIC TREATMENT PER AMS2470. DIMENSIONS APPLY AFTER COATING.

17、3. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra. 4. BREAK EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 5. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M-1982 (ASME PUBLICATION). 6. MARKING: MARK MATERIAL CODE “

18、E3” AS SHOWN IN ACCORDANCE WITH AS478, CLASS C. MULTIPLE MARKING OF BAR STOCK PERMISSIBLE PROVIDED POSITIVE IDENTIFICATION IS SHOWN. DASH NUMBERS MAY APPEAR ON ADJACENT FLATS. PARTS SHALL BE MARKED BEFORE THREADING. 7. DIMENSIONS ARE IN INCHES. 8. DO NOT USE UNASSIGNED PART NUMBERS. 9. UNLESS OTHERW

19、ISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OF THE APPLICABLE DRAWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED. 10. REVISION INDICATOR: A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVIS

20、IONS, 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.