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1、 AEROSPACE STANDARD BOLT, MACHINE - HEXAGON HEAD, STEEL, CADMIUM PLATED, UNS G87400, 125 KSI MIN, .2500-28 UNJF-3A AS9519 Copyright 2007 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 means, ele
2、ctronic, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 1999
3、-04 REVISED 2007-07 THIRD ANGLE PROJECTION CUSTODIAN: SAE E-25 REV. B FEDERAL SUPPLY CLASS 5306 AS9519 SHEET 1 OF 3 REV. B SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely
4、 voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites y
5、our written comments and suggestions. RATIONALE CADMIUM WARNING NOTE UPDATED AND THREAD SPECIFICATION REVISED TO AS8879. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9519A. THIS SAE STANDARD RETAINS THE SAME PART NUMBERS ESTABLISHED BY THE ORIG
6、INAL MILITARY DOCUMENT. ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS 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. .003 Y THREAD RUNOUT PER A 3062S 250 250 32
7、K L CHAMFER 25 - 35 TO .428 - .448 OO .003/1 .006 Z - Y - .232 .222 SEE NOTE 1 .013 Y .013 Y R 32 CHAMFER .021- .041 X 45 APPROX O .2500-28 UNJF-3A PER AS8879 - Z - .025 .015 .166 .146 .398 MIN BEARING SURFACE .448 MAX VIEW A .439 .429 .480 MIN A .026 .006 MARK PART NUMBER AND MANUFACTURERS IDENTIFI
8、CATION PER CLASS AAS478 FIGURE 1 - BOLT SHAPE IN THIS AREA OPTIONAL 250 SECTION THRU THREAD PROFILE 32 Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 20:54:29 MSTNo reproduction or networking permitted without licen
9、se from IHS -,-,- AEROSPACE STANDARD BOLT, MACHINE - HEXAGON HEAD, STEEL, CADMIUM PLATED, UNS G87400, 125 KSI MIN, .2500-28 UNJF-3A AS9519 REV. B AS9519 SHEET 2 OF 3 REV. B TABLE 1 - PART NUMBERS AND DIMENSIONS PART NO. L K APPROX. MASS LB/100 PART NO. L K APPROX. MASS LB/100 MS9519-04 MS9519-05 MS9
10、519-06 MS9519-07 MS9519-08 MS9519-09 MS9519-10 MS9519-11 MS9519-12 MS9519-13 MS9519-14 MS9519-15 MS9519-16 MS9519-17 MS9519-18 MS9519-19 MS9519-20 MS9519-21 MS9519-22 MS9519-23 MS9519-24 MS9519-25 MS9519-26 MS9519-27 MS9519-28 MS9519-29 MS9519-30 MS9519-31 MS9519-32 MS9519-33 .365- .385 .428- .448 .
11、490- .510 .552- .572 .615- .635 .678- .698 .740- .760 .802- .822 .865- .885 .928- .948 .990-1.010 1.052-1.072 1.115-1.135 1.178-1.198 1.240-1.260 1.302-1.322 1.365-1.385 1.428-1.448 1.490-1.510 1.552-1.572 1.615-1.635 1.678-1.698 1.740-1.760 1.865-1.885 1.990-2.010 2.115-2.135 2.240-2.260 2.365-2.38
12、5 2.490-2.510 2.615-2.635 .079- .099 .079- .099 .079- .099 .079- .099 .079- .099 .079- .099 .079- .099 .079- .099 .079- .125 .128- .188 .190- .250 .252- .312 .315- .375 .378- .438 .440- .500 .502- .562 .565- .625 .628- .688 .690- .750 .752- .812 .815- .875 .878- .938 .940-1.000 1.065-1.125 1.190-1.2
13、50 1.315-1.375 1.440-1.500 1.565-1.625 1.690-1.750 1.815-1.875 1.16 1.23 1.30 1.37 1.44 1.51 1.58 1.66 1.73 1.80 1.87 1.94 2.01 2.09 2.16 2.23 2.30 2.37 2.44 2.52 2.59 2.66 2.73 2.87 3.02 3.16 3.30 3.45 3.59 3.73 MS9519-34 MS9519-35 MS9519-36 MS9519-37 MS9519-38 MS9519-39 MS9519-40 MS9519-41 MS9519-
14、42 MS9519-43 MS9519-44 MS9519-45 MS9519-46 MS9519-47 MS9519-48 MS9519-49 MS9519-50 MS9519-51 MS9519-52 MS9519-53 MS9519-54 MS9519-55 MS9519-56 MS9519-57 MS9519-58 MS9519-59 MS9519-60 2.740-2.760 2.865-2.885 2.990-3.010 3.115-3.135 3.240-3.260 3.365-3.385 3.490-3.510 3.615-3.635 3.740-3.760 3.865-3.8
15、85 3.990-4.010 4.115-4.135 4.240-4.260 4.365-4.385 4.490-4.510 4.615-4.635 4.740-4.760 4.865-4.885 4.990-5.010 5.115-5.135 5.240-5.260 5.365-5.385 5.490-5.510 5.615-5.635 5.740-5.760 5.865-5.885 5.990-6.010 1.940-2.000 2.065-2.125 2.190-2.250 2.315-2.375 2.440-2.500 2.565-2.625 2.690-2.750 2.815-2.8
16、75 2.940-3.000 3.065-3.125 3.190-3.250 3.315-3.375 3.440-3.500 3.565-3.625 3.690-3.750 3.815-3.875 3.940-4.000 4.065-4.125 4.190-4.250 4.315-4.375 4.440-4.500 4.565-4.625 4.690-4.750 4.815-4.875 4.940-5.000 5.065-5.125 5.190-5.250 3.88 4.02 4.16 4.31 4.45 4.60 4.74 4.88 5.03 5.17 5.31 5.46 5.60 5.74
17、 5.89 6.03 6.17 6.32 6.46 6.60 6.75 6.89 7.03 7.18 7.32 7.46 7.61 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. FOR PART NUMBERS MS9519-04 THRU MS9519-18 THE THREAD PD (DATUM -Z- )
18、 SHALL REPLACE DATUM -Y- . 2. MATERIAL: LOW ALLOY STEEL AMS 6322 (UNS G87400). 3. PROCUREMENT SPECIFICATION: AS7452. 4. HEAD TO SHANK FILLET RADIUS: FOR PART NUMBERS MS9519-15 AND LARGER, THE HEAD TO SHANK FILLET SHALL BE COLD ROLLED AFTER HEAT TREATMENT TO REMOVE ALL VISUAL EVIDENCE OF GRINDING OR
19、TOOL MARKS. Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 20:54:29 MSTNo reproduction or networking permitted without license from IHS -,-,- AEROSPACE STANDARD BOLT, MACHINE - HEXAGON HEAD, STEEL, CADMIUM PLATED, U
20、NS G87400, 125 KSI MIN, .2500-28 UNJF-3A AS9519 REV. B AS9519 SHEET 3 OF 3 REV. B NOTES (CONTINUED): 5. FINISH: CADMIUM PLATE PER AMS 2400. DIMENSIONS ARE AFTER PLATING. 6. MAGNETIC PARTICLE INSPECTION PER ASTM E 1444 BEFORE PLATING. 7. INCOMPLETE THREADS NOT TO ENTER FILLET. 8. SURFACE TEXTURE: SYM
21、BOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra. 9. BREAK SHARP EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 10. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M-1982 (ASME PUBLICATION). 11. DIMENSIONS IN INCHES. 12. DO NOT USE UNASSIG
22、NED PART NUMBERS. 13. THE 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 REV
23、ISION OF THE DOCUMENT. AS AND AMS ARE SAE INTERNATIONAL PUBLICATIONS. ASME IS AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION. ASTM IS AN ASTM INTERNATIONAL PUBLICATION. Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 20:54:29 MSTNo reproduction or networking permitted without license from IHS -,-,-