1、AEROSPACE STANDARD SCREW, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUMPLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD,DRILLED, UNS K14675, 195 KSI MIN, .1640-36 UNJF-3AAS9216Copyright 2012 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or t
2、ransmitted, in any form or by any 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
3、 SAE WEB ADDRESS: http:/www.sae.org ISSUED 1998-08REVISED 2011-08 STABILIZED 2012-01THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.CFEDERAL SUPPLY CLASS 5970 AS9216SHEET 1 OF 2REV. CPROCUREMENT SPECIFICATION: AS7459SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvanc
4、e thestate of technicalandengineering sciences. Theuse ofthis report is entirely voluntary, andits applicability and suitability forany particular use,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at
5、 which time itmay bereaffirmed, revised, stabilized or cancelled.SAEinvites yourwrittencommentsandsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS9216CRATIONALE THIS DOCUMENT HAS BEEN DETERMINED TO CONTAIN BASIC AN
6、D STABLE TECHNOLOGY WHICH IS NOT DYNAMIC IN NATURE. STABILIZED NOTICE THIS DOCUMENT HAS BEEN DECLARED “STABILIZED” BY THE E-25 TECHNICAL COMMITTEE AND WILL NO LONGER BE SUBJECTED TO PERIODIC REVIEWS FOR CURRENCY. USERS ARE RESPONSIBLE FOR VERIFYING REFERENCES AND CONTINUED SUITABILITY OF TECHNICAL R
7、EQUIREMENTS. NEWER TECHNOLOGY MAY EXIST. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9216(ASG). THIS SAE STANDARD RETAINS THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT. ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS
8、LISTS (QPL) MAY CONTINUE TO BE MANDATORY FOR DOD 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 - SCREW Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or netw
9、orking permitted without license from IHS-,-,-AEROSPACE STANDARD AS9216SHEET 2 OF 2REV. CSCREW, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, UNS K14675, 195 KSI MIN, .1640-36 UNJF-3ATABLE 1 - PART NUMBERS AND DIMENSIONS PART NO. L K APPROX.MASSLB/100
10、 PART NO. L K APPROX.MASSLB/100. MS9216-03 .302-.322 .062-.082 .451 MS9216-16 1.115-1.135 .487-.547 .847 MS9216-04 .365-.385 .062-.082 .482 MS9216-17 1.178-1.198 .550-.610 .878 MS9216-05 .428-.448 .062-.082 .513 MS9216-18 1.240-1.260 .612-.672 .908 MS9216-06 .490-.510 .062-.082 .543 MS9216-19 1.302-
11、1.322 .674-.734 .938 MS9216-07 .552-.572 .062-.082 .573 MS9216-20 1.365-1.385 .737-.797 .969 MS9216-08 .615-.635 .062-.082 .604 MS9216-21 1.428-1.448 .800-.860 .999 MS9216-09 .678-.698 .062-.082 .634 MS9216-22 1.490-1.510 .862-.922 1.029 MS9216-10 .740-.760 .112-.172 .664 MS9216-23 1.552-1.572 .924-
12、984 1.060 MS9216-11 .802-.822 .174-.234 .695 MS9216-24 1.615-1.635 .987-1.047 1.090 MS9216-12 .865-.885 .237-.297 .725 MS9216-25 1.678-1.698 1.050-1.110 1.121 MS9216-13 .928-.948 .300-.360 .756 MS9216-26 1.740-1.760 1.112-1.172 1.151 MS9216-14 .990-1.010 .362-.422 .786 MS9216-27 1.865-1.885 1.237-1
13、297 1.212 MS9216-15 1.052-1.072 .424-.484 .816 MS9216-28 1.990-2.010 1.362-1.422 1.273 NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. NOTES: 1. FOR PART NUMBERS MS9216-03 THRU MS9216-12 THE
14、THREAD PD (DATUM ) SHALL REPLACE DATUM . 2. MATERIAL: LOW ALLOY STEEL AMS6304 (UNS K14675). 3. PROCUREMENT SPECIFICATION: AS7459. 4. HARDNESS: 42-46 HRC. 5. FINISH: DIFFUSED NICKEL-CADMIUM PLATE AMS2416. DIMENSIONS ARE AFTER PLATING. CONTACT POINTS PERMISSIBLE. PD MAY BE REDUCED .0012 MAXIMUM BEFORE
15、 PLATING. 6. MAGNETIC PARTICLE INSPECTION PER ASTM E 1444 BEFORE PLATING. 7. INCOMPLETE THREADS NOT TO ENTER FILLET. 8. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra EXCEPT UPSET HEAD. 9. BREAK SHARP EDGES .003 T
16、O .015, UNLESS OTHERWISE SPECIFIED. 10. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M-1982 (ASME PUBLICATION). 11. DIMENSIONS IN INCHES. 12. DO NOT USE UNASSIGNED PART NUMBERS. 13. A CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVIS
17、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 E
18、DITORIAL CHANGES ONLY. AS AND AMS ARE SAE INTERNATIONAL PUBLICATIONS. ASME IS AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION. ASTM IS AN ASTM INTERNATIONAL PUBLICATION. -Z- -Y-Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
