1、 AEROSPACE STANDARD STUD, STEPPED, 2 DIA ENGAGEMENT, CADMIUM PLATED, STEEL UNS G87400, .3125-18 UNS X .2500-28 UNF-3A AS155001 THRUAS155300Copyright 2016 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or
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3、sae.org ISSUED1999-12REAFFIRMED 2005-05REVISED2016-04THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.B FEDERAL SUPPLY CLASS 5307 AS155001 THRU AS155300 SHEET 1 OF 3 REV. B PROCUREMENT SPECIFICATION: AS7456 SAE Technical Standards Board Rules provide that: “This report is published by SAEtoadvance thesta
4、te of technicaland engineering sciences. 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 whicht
5、ime it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS155001B RATIONALE FIGURE REDRAWN TO CORRECT GEOMETRIC TOLERANCE FRA
6、MES, CORRECT CADMIUM PLATE NOTICE ADDED, SPECIFICATIONS UPDATED, AND PART USAGE NOTE ADDED. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD AN155001 THROUGH AN155300 REVISION 3, NOTICE 1. THIS SAE STANDARD MAY RETAIN THE SAME PART NUMBERS ESTABLISHE
7、D 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 HAVE NOT BEEN ADOPTED BY THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT. E 1 1R.0 6 2.0 3 163C H A M FE
8、 R .0 2 1 - . 0 4 1 X 4 5 A P P R O XB M IN F U L L T H R E A DM IN F U L L O R I N C O M P L E T ET H R E A D = B + 2 T H DC H A M FE R.0 5 2 - . 0 7 2 X 4 5 A P P R O XM IN F U L L T H R E A D.6 1 5L C.1 2 0.0 6 0U N D E R S IZE A N D O V E R S IZ EID E N T IF IC A T I O N S E E T A B L E 1P E R A
9、 S 4 7 8 C L A S S 1.3 1 2 5 - 1 8 U N S / 7 /F O R P D S E E T A B L E 1Z45A P P R O X.2 3 1.2 2 1.0 1 0 M A X D E P T HS E E / 8 /.0 9 0.0 4 0.2 5 0 0 - 2 8 U N F - 3 A / 7 /. 0 0 6 ZY32S E C T IO N T H R UT H R E A D P R O F IL E B O T H E N D S+- .0 1 0.6 3 5FIGURE 1 - STUD AEROSPACE STANDARD AS
10、155001 THRU AS155300 SHEET 2 OF 3 REV. B STUD, STEPPED, 2 DIA ENGAGEMENT, CADMIUM PLATED, STEEL UNS G87400, .3125-18 UNS X .2500-28 UNF-3A TABLE 1 - PART NUMBERS AND DIMENSIONS AEROSPACE STANDARD AS155001 THRU AS155300 SHEET 3 OF 3 REV. B STUD, STEPPED, 2 DIA ENGAGEMENT, CADMIUM PLATED, STEEL UNS G8
11、7400, .3125-18 UNS X .2500-28 UNF-3A NOTES: NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. 1. MATERIAL: STEEL AMS6322 (UNS G87400). 2. PROCUREMENT SPECIFICATION: AS7456. 3. HARDNESS: 26-32 HR
12、C. 4. FINISH: CADMIUM PLATE PER AMS2400. DIMENSIONS ARE AFTER PLATING, EXCEPT WHERE SHOWN. 5. MAGNETIC PARTICLE INSPECTION PER ASTM E1444/ E1444M. AFTER PLATING. 6. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra.
13、7. SCREW THREAD PER ASME B1.1 AND ACCEPTABILITY REQUIREMENTS PER ASME B1.3, SYSTEM 22. 8. MARK MATERIAL CODE “E11“ AS SHOWN PER AS478 CLASS A, EXCEPT METHODS 2D AND 2E (VIBRO PEEN) NOT PERMITTED. MAXIMUM DEPTH .010. 9. BREAK SHARP EDGES .003 TO .15 UNLESS OTHERWISE SPECIFIED. 10. DIMENSIONING AND TO
14、LERANCING PER ANSI Y14.5M-1982 (ASME PUBLICATION). 11. DIMENSIONS ARE IN INCHES. 12. DO NOT USE UNASSIGNED PART NUMBERS. 13. UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OF THE APPLICABLE DRAWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED. 14.
15、REVISION INDICATOR: 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 ISSUE OF THIS DOCUMENT. AN (R) SYMBOL TO THE LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION
16、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. MIL-S-7742 IS A U.S. GOVERNMENT PUBLICATION.
