1、 AEROSPACE STANDARD SCREW, MACHINE - HEXAGON HEAD, SLOTTED, FULL SHANK, ALLOY STEEL, UNS K14675, 135 KSI MIN, .1900-32 UNS-3A AS9316Copyright 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
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3、g ISSUED2000-08REVISED2012-08REAFFIRMED 2017-04THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.B FEDERAL SUPPLY CLASS 5305 AS9316 SHEET 1 OF 3 REV. B PROCUREMENT SPECIFICATION: AS7454 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSXEOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJLneering sciences. T
4、he useof this report is entirely voluntary, and its applicability andsuitability for any particularuse, includingany patent infringement arisingtherefrom,is thesole responVLELOLWRIWKHXVHUSAE reviews eachtechnical reportatleast every fiveyears at whichtime it may be revised, reaffirmed, stabilized, o
5、r cancelled. SAE invites your written comments and suggestions.SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AS9316B RATIONALE AS9316B HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. NOTICE THE INITIAL SAE PUBLICATION OF
6、 THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9316. THIS SAE STANDARD MAY RETAIN THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT. ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LISTS (QPL) MAY CONTINUE TO BE MANDATORY FOR DOD CONTRACTS. REQUIREMENTS RELATIN
7、G TO QPLS HAVE NOT BEEN ADOPTED BY THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT. FIGURE 1 - SCREW AEROSPACE STANDARD AS9316 SHEET 2 OF 3 REV. B SCREW, MACHINE - HEXAGON HEAD, SLOTTED, FULL SHANK, ALLOY STEEL, UNS K14675, 135 KSI MIN, .1900-32 UNS-3A TABLE 1 - PART NUMBERS AND DIME
8、NSIONS NOTES: NOTICED THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. 1. FOR PARTS NUMBERS MS9316-02 THRU MS9316-10 THE THREAD PD (DATUM -Z- ) SHALL REPLACE DATUM -Y- . 2. MATERIAL: LOW ALLOY STEEL P
9、ER AMS6304 (UNS K14675). 3. PROCUREMENT SPECIFICATION: AS7454. 4. FINISH: DIFFUSED NICKEL-CADMIUM PLATE PER AMS2416. DIMENSIONS ARE AFTER PLATING. CONTACT POINTS PERMISSIBLE. PD MAY BE REDUCED .0012 MAXIMUM BEFORE PLATING. 5. MAGNETIC PARTICLE INSPECTION PER ASTM E 1444 BEFORE PLATING. 6. SURFACE TE
10、XTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 250 MICROINCHES Ra. 7. MARK PART NUMBER AND MANUFACTURERS IDENTIFICATION PER AS478 CLASS A. FOR PARTS MANUFACTURED PRIOR TO ISSUE OF AS9316 REV. A, PARTS MARKED ONLY WITH THE MATERIAL CODE “E37”
11、ARE ACCEPTABLE. 8. BREAK SHARP EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 9. DIMENSIONS ARE IN INCHES. 10. DIMENSIONING AND TOLERANCING PER ANSI Y14.5-1982 (ASME PUBLICATION). 11. DO NOT USE UNASSIGNED PART NUMBERS. AEROSPACE STANDARD AS9316 SHEET 3 OF 3 REV. B SCREW, MACHINE - HEXAGON HEAD, SL
12、OTTED, FULL SHANK, ALLOY STEEL, UNS K14675, 135 KSI MIN, .1900-32 UNS-3A 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 ISSUE OF THIS DOCUMENT. AN (R) SYMBOL TO THE
13、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.
