1、 AEROSPACE STANDARD BOLT, TEE HEAD - AMS5662, CHAMFERED, .3125-24 UNJF-3A (STRESS RUPTURE RESISTANT) AS3411Copyright 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 means, electronic, mechan
2、ical, 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.org ISSUED1988-06REAFFIRMED
3、 2006-05REVISED2017-04THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.C FEDERAL SUPPLY CLASS 5306 AS3411 SHEET 1 OF 3 REV. C PROCUREMENT SPECIFICATION: AS7467, SEE NOTE 3 SAE Technical Standards Board Rules provide that: “This report is published by SAEtoadvance thestate of technicaland engineering scien
4、ces. The useof this report is entirely voluntary, and its applicability andsuitability for any particularuse, includingany patent infringement arisingtherefrom,is the sole responsibility of theuser.” SAE reviews eachtechnical reportatleast every fiveyears at whichtime it may be revised, reaffirmed,
5、stabilized, or 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/AS3411C RATIONALE MASS ADDED FOR AS3411-04, NOTE ADDED FOR USE OF EXISTING STOCK , NOTES 4 AND 5 UPDATED. LEAD IN CHAM
6、FER ALTERED TO AGREE WITH AS1132 REV J. 4 7 4 3 M A R K P A R T N U M B E R A N D M A N U F A C T U R E R S I D E N T I F I C A T I O NP E R A S 4 7 8 C L A S S A A. 0 0 5M. 5 5 0. 5 7 0. 0 0 5 MBB. 4 3 0. 4 4 0LKG. 1 7 8. 1 9 8. 0 0 3 BT H R E A DR U N O U T / 3 / 2 5 0. 3 1 2 5 - 2 4 U N J F -3 AP
7、 E R A S 8 8 7 9A. 2 9 0. 2 8 0 . 0 0 3 / 1 . 0 0 6 BA. 3 6 0. 3 5 0. 0 0 5 MR. 0 9 0. 1 0 0. 0 2 5. 0 3 0R. 0 1 0. 0 1 5V I E W A E N L A R G E DS E C T I O N T H R UT H R E A D P R O F I L E32/ 1 /B2 5 04 X R . 0 1 5 - . 0 3 5 324 5 A P P R O X/ 1 /. 2 3 9. 2 5 9/ 3 /FIGURE 1 AEROSPACE STANDARD AS
8、3411 SHEET 2 OF 3 REV. C BOLT, TEE HEAD - AMS5662, CHAMFERED, .3125-24 UNJF-3A (STRESS RUPTURE RESISTANT) TABLE 1 PART NUMBER L G MIN K MAX APPROX. MASS LB/100 PART NUMBER L G MIN K MAX APPROX. MASS LB/100 AS3411-04 .490- .510 .063 .150 2.27 AS3411-34 2.740-2.760 1.732 1.875 6.41 AS3411-05 .552- .57
9、2 .063 .150 2.38 AS3411-35 2.865-2.885 1.857 2.000 6.64 AS3411-06 .615- 635 .063 .150 2.49 AS3411-36 2.990-3.010 1.982 2.125 6.87 AS3411-07 .678- .698 .063 .150 2.60 AS3411-37 3.115-3.135 2.107 2.250 7.11 AS3411-08 .740- .760 .063 .150 2.71 AS3411-38 3.240-3.260 2.232 2.375 7.34 AS3411-09 .802- .822
10、 .063 .150 2.82 AS3411-39 3.365-3.385 2.357 2.500 7.57 AS3411-10 .865- 885 .063 .150 2.94 AS3411-40 3.490-3.510 2.482 2.625 7.81 AS3411-11 .928- .948 .063 .150 3.05 AS3411-41 3.615-3.635 2.607 2.750 8.03 AS3411-12 .990-1.100 .063 .150 3.16 AS3411-42 3.740-3.760 2.732 2.875 8.28 AS3411-13 1.052-1.072
11、 .063 .188 3.28 AS3411-43 3.865-3.885 2.857 3.000 8.50 AS3411-14 1.115-1.135 .107 .250 3.39 AS3411-44 3.990-4.010 2.982 3.125 8.73 AS3411-15 1.178-1.198 .170 .312 3.50 AS3411-45 4.115-4.135 3.107 3.250 8.97 AS3411-16 1.240-1.260 .232 .375 3.62 AS3411-46 4.240-4.260 3.232 3.375 9.20 AS3411-17 1.302-1
12、322 .294 .438 3.74 AS3411-47 4.365-4.385 3.357 3.500 9.43 AS3411-18 1.365-1.385 .357 .500 3.85 AS3411-48 4.490-4.510 3.482 3.625 9.66 AS3411-19 1.428-1.448 .420 .562 3.97 AS3411-49 4.615-4.635 3.607 3.750 9.90 AS3411-20 1.490-1.510 .482 .625 4.09 AS3411-50 4.740-4.760 3.732 3.875 10.12 AS3411-21 1.
13、552-1.572 .544 .688 4.20 AS3411-51 4.865-4.885 3.857 4.000 13.36 AS3411-22 1.615-1.635 .607 .750 4.32 AS3411-52 4.990-5.010 3.982 4.125 10.65 AS3411-23 1.678-1.698 .670 .812 4.43 AS3411-53 5.115-5.135 4.107 4.250 10.83 AS3411-24 1.740-1.760 .732 .875 4.55 AS3411-54 5.240-5.260 4.232 4.375 11.06 AS34
14、11-25 1.802-1.822 .794 .938 4.67 AS3411-55 5.365-5.385 4.357 4.500 11.29 AS3411-26 1.865-1.885 .857 1.000 4.78 AS3411-56 5.615-5.635 4.482 4.625 11.53 AS3411-27 1.928-1.948 .920 1.062 4.90 AS3411-57 5.615-5.635 4.607 4.750 11.75 AS3411-28 1.990-2.010 .982 1.125 5.02 AS3411-58 5.740-5.760 4.732 4.875
15、 11.99 AS3411-29 2.115-2.135 1.107 1.250 5.24 AS3411-59 5.865-5.885 4.857 5.000 12.22 AS3411-30 2.240-2.260 1.232 1.375 5.48 AS3411-60 5.990-6.010 4.982 5.125 12.45 AS3411-31 2.365-2.385 1.357 1.500 5.72 AS3411-32 2.490-2.510 1.482 1.625 5.94 AS3411-33 2.615-2.635 1.607 1.750 6.19 AEROSPACE STANDARD
16、 AS3411 SHEET 3 OF 3 REV. C BOLT, TEE HEAD - AMS5662, CHAMFERED, .3125-24 UNJF-3A (STRESS RUPTURE RESISTANT) NOTES /1/ FOR PART NUMBERS AS3411-04 THROUGH AS3411-19, B IN TOL. NOTES SHALL BE CHANGED TO A. 2. MATERIAL: CORROSION AND HEAT RESISTANT NICKEL ALLOY AMS5662. /3/ MANUFACTURING SPECIFICATION:
17、 AS7467 EXCEPT ROLL THREAD AND COLD WORK .010 TO .015 FILLET RADIUS AFTER PRECIPITATION HARDENING. INCOMPLETE THREAD NOT TO ENTER THE FILLET AREA. 4. FLUORESCENT PENETRANT INSPECTION PER ASTM E1417/E1417M, TYPE 1, SENSITIVITY LEVEL 2 MIN. 5. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PE
18、R ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra, EXCEPT UPSET HEAD TO BE 250 MICROINCHES Ra. 6. BREAK SHARP EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 7. DIMENSIONS ARE IN INCHES. 8. DIMENSIONS AND TOLERANCING: ANSI Y14.5M-1982 (ASME PUBLICATION). 9. DO NOT USE UNASS
19、IGNED PART NUMBERS. 10. UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OF THE APPLICABLE DRAWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED 11. REVISION INDICATOR: A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN
20、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 AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION. ASTM IS AN ASTM INTERNATIONAL PUBLICATION.
