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本文(SAE AS 150801 THRU AS151100D-2016 STUD STEPPED 1 5 DIA ENGAGEMENT CADMIUM PLATED STEEL UNS G87400 3125-18 UNS X 2500-28 UNF-3A.pdf)为本站会员(brainfellow396)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

SAE AS 150801 THRU AS151100D-2016 STUD STEPPED 1 5 DIA ENGAGEMENT CADMIUM PLATED STEEL UNS G87400 3125-18 UNS X 2500-28 UNF-3A.pdf

1、AEROSPACE STANDARDSTUD, STEPPED. 1.5 DIA ENGAGEMENT,CADMIUM PLATED, STEEL UNS G87400,.3125-18 UNS X .2500-28 UNF-3AAS150801-AS151100Copyright 2016 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any m

2、eans, 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.orgIS

3、SUED1999-12STABILIZED2014-08REVISED2016-09THIRD ANGLE PROJECTIONCUSTODIAN: E-25REV. DFEDERAL SUPPLY CLASS5307AS150801 -AS151100SHEET 1 OF 3REV.DPROCUREMENT SPECIFICATION: AS7456SAE Technical Standards BoardRules providethat:“This reportis publishedby SAE to advance thestateoftechnical andengineering

4、 sciences. The useofthis reportis entirely voluntary, and its applicability and suitability forany particularuse, includingany patent infringement arising therefrom, is thesole responsibility of theuser.”SAE reviews eachtechnical reportatleastevery fiveyears at whichtime it may berevised, reaffirmed

5、, stabilized, or cancelled. SAEinvites your written comments and suggestions.SAE values your input. To provide feedbackon this Technical Report, please visit http:/standards.sae.org/AS150801DRATIONALECORRECT TYPOGRAPHICAL ERROR FOR L DIM (E.G., AN150855) AND CORRECT REFERENCES TO PARTS INACTIVE FOR

6、NEW DESIGN.NOTICETHE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD AN150801 THROUGH AN151100 REVISION 2, NOTICE 1. THIS SAE STANDARD MAY RETAIN THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL DOCUMENT.ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LIS

7、TS (QPLS) MAY CONTINUE TO BEMANDATORY 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 - STUDAEROSPACE STANDARD AS150801 -AS151100SHEET 2 OF 3REV.DSTUD, STEPPED. 1.5 DIA ENGAGEMENT, CADMIUM PLATED, STEE

8、L UNS G87400,.3125-18 UNS X .2500-28 UNF-3ATABLE 1 PART NUMBERS AND DIMENSIONSUNDERSIZE ANDOVERSIZEIDENTIFICATION-.003 STANDARD +.003 +.006 +.009 +.012(2) (2) (2) (2)C .307- .312 .307- .312 .307- .312 .307- .312 .316- .321 .316- .321PD BEFORE PLATING .2775-.2785 .2805-.2815 .2835-.2845 .2865-.2875 .

9、2895-.2905 .2925-.2935PD AFTER PLATING .2780-.2795 .2810-.2825 .2840-.2855 .2870-.2885 .2900-.2915 .2930-.2945PD LEAD THREAD .2714-.2734 .2744-.2764 .2774-.2794 .2804-.2824 .2834-.2854 .2864-.2884L BPART NUMBERPART NUMBERPART NUMBERPART NUMBERPART NUMBERPART NUMBER1.031 .438 AN150819 AN150820 AN1508

10、21 AN150822 AN150823 AN1508241.094 .500 AN150825 AN150826 AN150827 AN150828 AN150829 AN1508301.158 .562 AN150831 AN150832 AN150833 AN150834 AN150835 AN1508361.219 .562 AN150837 AN150838 AN150839 AN150840 AN150841 AN1508421.281 .562 AN150843 AN150844 AN150845 AN150846 AN150847 AN1508481.344 .562 AN15

11、0849 AN150850 AN150851 AN150852 AN150853 AN1508541.406 .562 AN150855 AN150856 AN150857 AN150858 AN150859 AN1508601.469 .562 AN150861 AN150862 AN150863 AN150864 AN150865 AN1508661.531 .562 AN150867 AN150868 AN150869 AN150870 AN150871 AN1508721.594 .562 AN150873 AN150874 AN150875 AN150876 AN150877 AN1

12、508781.656 .562 AN150879 AN150880 AN150881 AN150882 AN150883 AN1508841.719 .562 AN150885 AN150886 AN150887 AN150888 AN150889 AN1508901.781 .562 AN150891 AN150892 AN150893 AN150894 AN150895 AN1508961.844 .562 AN150897 AN150898 AN150899 AN150900 AN150901 AN1509021.906 .562 AN150903 AN150904 AN150905 A

13、N150906 AN150907 AN1509081.969 .562 AN150909 AN150910 AN150911 AN150912 AN150913 AN1509142.031 .562 AN150915 AN150916 AN150917 AN150918 AN150919 AN1509202.094 .562 AN150921 AN150922 AN150923 AN150924 AN150925 AN1509262.156 .562 AN150927 AN150928 AN150929 AN150930 AN150931 AN1509322.219 .562 AN150933

14、 AN150934 AN150935 AN150936 AN150937 AN1509382.344 .562 AN150939 AN150940 AN150941 AN150942 AN150943 AN1509442.469 .562 AN150945 AN150946 AN150947 AN150948 AN150949 AN1509502.594 .562 AN150951 AN150952 AN150953 AN150954 AN150955 AN1509562.719 .562 AN150957 AN150958 AN150959 AN150960 AN150961 AN15096

15、22.844 .562 AN150963 AN150964 AN150965 AN150966 AN150967 AN1509682.969 .562 AN150969 AN150970 AN150971 AN150972 AN150973 AN1509743.094 .562 AN150975 AN150976 AN150977 AN150978 AN150979 AN1509803.219 .562 AN150981 AN150982 AN150983 AN150984 AN150985 AN1509863.844 .562 AN150987 AN150988 AN150989 AN150

16、990 AN150991 AN1509923.969 .562 AN150993 AN150994 AN150995 AN150996 AN150997 AN1509981.281 .656 AN150999 AN151000 AN151001 AN151002 AN151003 AN1510041.406 .688 AN151005 AN151006 AN151007 AN151008 AN151009 AN1510101. INACTIVE FOR NEW DESIGN AFTER MARCH 25, 1955.2. MARKING IDENTIFICATION FOR OVERSIZE

17、PARTS MAY INCLUDE A PLUS SIGN (“+”) BEFORE THE IDENTIFICATION NUMBER. FOR EXAMPLE, PARTS FOR +.006 OVERSIZE MAY BE MARKED “6” OR “+6”.12963-3(1)(1)AEROSPACE STANDARD AS150801 -AS151100SHEET 3 OF 3REV.DSTUD, STEPPED. 1.5 DIA ENGAGEMENT, CADMIUM PLATED, STEEL UNS G87400,.3125-18 UNS X .2500-28 UNF-3AN

18、OTESNOTICETHIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE1. MATERIAL: STEEL AMS6322 (UNS G87400) AMS6320 MATERIAL MAY ALSO BE USED FOR PARTS UNTIL JANUARY 1, 1957.2. PROCUREMENT SPECIFICATION: AS7456.

19、3. HARDNESS: 26 TO 32 HRC.4. FINISH: CADMIUM PLATE PER AMS2400. DIMENSIONS ARE AFTER PLATING, EXCEPT WHERE SHOWN.5. MAGNETIC PARTICLE INSPECTION TO ASTM E1444.6. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED,SURFACES TO BE 125 MICROINCHES Ra.7. SC

20、REW THREADS PER MIL-S-7742.8. TOLERANCES: LINEAR DIMENSIONS .010.9. BREAK SHARP EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED.10. DIMENSIONS AND TOLERANCING PER ANSI Y14.5M-1982 (ASME PUBLICATION).11. DIMENSIONS ARE IN INCHES.12. DO NOT USE UNASSIGNED PART NUMBERS.13. REVISION INDICATOR: A CHANGE BA

21、R (I) 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 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 AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION.ASTM IS AN ASTM INTERNATIONAL PUBLICATION.

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