1、AEROSPACE STANDARD SCREW, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUMPLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD,UNS K14675, 195 KSI MIN, .1640-36 UNJF-3AAS9207Copyright 2012 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitte
2、d, 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 SAE WEB
3、ADDRESS: http:/www.sae.org ISSUED 1998-01REVISED 2011-09 STABILIZED 2012-01THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.CFEDERAL SUPPLY CLASS 5305 AS9207SHEET 1 OF 2REV. CPROCUREMENT SPECIFICATION: AS7459SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestat
4、e 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 which ti
5、me 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/AS9207CRATIONALE THIS DOCUMENT HAS BEEN DETERMINED TO CONTAIN BASIC AND STABLE
6、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 REQUIREMEN
7、TS. NEWER TECHNOLOGY MAY EXIST. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9207(ASG). THIS SAE STANDARD RETAINS THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT. ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LISTS (QP
8、L) 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 networking pe
9、rmitted without license from IHS-,-,-AEROSPACE STANDARD AS9207SHEET 2 OF 2REV. CSCREW, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, UNS K14675, 195 KSI MIN, .1640-36 UNJF-3ATABLE 1 - PART NUMBERS AND DIMENSIONS PART NO. L K APPROX.MASSLB/100 PART NO. L K APPR
10、OX.MASSLB/100. MS9207-03 .302-.322 .062-.082 .451 MS9207-16 1.115-1.135 .487-.547 .847 MS9207-04 .365-.385 .062-.082 .482 MS9207-17 1.178-1.198 .550-.610 .878 MS9207-05 .428-.448 .062-.082 .513 MS9207-18 1.240-1.260 .612-.672 .908 MS9207-06 .490-.510 .062-.082 .543 MS9207-19 1.302-1.322 .674-.734 .9
11、38 MS9207-07 .552-.572 .062-.082 .573 MS9207-20 1.365-1.385 .737-.797 .969 MS9207-08 .615-.635 .062-.082 .604 MS9207-21 1.428-1.448 .800-.860 .999 MS9207-09 .678-.698 .062-.082 .634 MS9207-22 1.490-1.510 .862-.922 1.029 MS9207-10 .740-.760 .112-.172 .664 MS9207-23 1.552-1.572 .924-.984 1.060 MS9207-
12、11 .802-.822 .174-.234 .695 MS9207-24 1.615-1.635 .987-1.047 1.090 MS9207-12 .865-.885 .237-.297 .725 MS9207-25 1.678-1.698 1.050-1.110 1.121 MS9207-13 .928-.948 .300-.360 .756 MS9207-26 1.740-1.760 1.112-1.172 1.151 MS9207-14 .990-1.010 .362-.422 .786 MS9207-27 1.865-1.885 1.237-1.297 1.212 MS9207-
13、15 1.052-1.072 .424-.484 .816 MS9207-28 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 MS9207-03 THRU MS9207-12 THE THREAD PD (DATUM )
14、 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 PLATING. 6. MAGNE
15、TIC PARTICLE INSPECTION PER ASTM E 1444 BEFORE PLATING. 7. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra EXCEPT UPSET HEAD. 8. BREAK SHARP EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 9. DIMENSIONING AND TOLER
16、ANCING PER ANSI Y14.5M-1982 (ASME PUBLICATION). 10. DIMENSIONS IN INCHES. 11. DO NOT USE UNASSIGNED PART NUMBERS. 12. A CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO THE PREVIOUS IS
17、SUE 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. -Z- -Y-Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
