SAE-AS-123601-THRU-AS-123750B-2007.pdf

AEROSPACE STANDARD RIVET, SOLID, 100° FLUSH HEAD, NICKEL ALLOY UNS N06600 AS123601 THRU AS123750 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, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 1999-12 REVISED 2007-07 THIRD ANGLE PROJECTION CUSTODIAN: SAE E-25 REV. B FEDERAL SUPPLY CLASS 5320 AS123601 THRU AS123750 SHEET 1 OF 3 REV. B PROCUREMENT SPECIFICATION: AS7232 EXCEPT AS NOTED oard 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 y and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. 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 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 your written comments and suggestions. RATIONALE REVISE TABLE 1 TO REMOVE COLUMN E THAT WAS INADVERTENTLY ADDED IN REVISION A AND REVISE COLUMN ØA VALUES A TYPO DURING REVISION A. NOTICE THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD AN123601 THRU AN123750 REVISION 4. THIS SAE STANDARD RETAINS 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 RELATING TO QPL'S HAVE NOT BEEN ADOPTED BY THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT. FIGURE 1 TABLE 1 - DIMENSIONS ØD /7/ MIN MAX ØA MIN MAX B MIN MAX (C) TOL X .061 .063 .099 .107 .019 .023 .112 .010 .093 .095 .164 .172 .033 .037 .169 .010 .123 .126 .210 .218 .039 .043 .225 .010 .154 .157 .272 .280 .052 .056 .281 .015 .186 .189 .337 .347 .067 .071 .338 .015 .248 .252 .460 .470 .092 .096 .450 .020 .310 .314 .548 .558 .103 .107 .561 .020 .373 .377 .678 .692 .131 .135 .675 .020 Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 19:43:17 MSTNo reproduction or networking permitted without license from IHS -,-,- AEROSPACE STANDARD RIVET, SOLID, 100° FLUSH HEAD, NICKEL ALLOY UNS N06600 AS123601 THRU AS123750 REV. B AS123601 THRU AS123750 SHEET 2 OF 3 REV. B TABLE 2 - DIMENSIONS AND PART NUMBERS DIAMETER AND PART NUMBERS L ±.010 Ø.062 Ø.094 Ø.125 Ø.156 Ø.188 Ø.250 Ø.312 Ø.375 .125 .156 .188 .219 .250 .281 .312 .344 .375 .406 .438 .469 .500 .531 .562 .594 .625 .656 .688 .719 .750 .781 .812 .844 .875 .906 .938 .969 1.000 1.031 1.062 1.094 1.125 1.156 1.188 1.219 1.250 1.281 1.312 1.344 1.375 1.406 1.438 1.469 1.500 AN123601 AN123610 AN123602 AN123611 AN123603 AN123612 AN123604 AN123613 AN123605 AN123614 AN123606 AN123615 AN123607 AN123616 AN123608 AN123617 AN123609 AN123618 AN123629 AN123619 AN123630 AN123620 AN123631 AN123621 AN123632 AN123622 AN123633 AN123623 AN123634 AN123624 AN123635 AN123625 AN123649 AN123650 AN123651 AN123626 AN123665 AN123666 AN123667 AN123627 AN123668 AN123681 AN123682 AN123628 AN123636 AN123683 AN123637 AN123684 AN123638 AN123685 AN123639 AN123686 AN123640 AN123697 AN123641 AN123698 AN123699 AN123700 AN123642 AN123701 AN123702 AN123703 AN123643 AN123704 AN123713 AN123714 AN123644 AN123715 AN123716 AN123717 AN123645 AN123718 AN123719 AN123720 AN123646 AN123721 AN123729 AN123730 AN123647 AN123731 AN123732 AN123733 AN123648 AN123652 AN123734 AN123653 AN123735 AN123654 AN123736 AN123655 AN123737 AN123656 AN123738 AN123657 AN123739 AN123740 AN123741 AN123658 AN123742 AN123743 AN123744 AN123659 AN123745 AN123746 AN123747 AN123660 AN123748 AN123749 AN123750 AN123661 AN123662 AN123663 AN123664 AN123669 AN123670 AN123671 AN123672 AN123673 AN123674 AN123675 AN123676 AN123677 AN123678 AN123679 AN123680 AN123687 AN123688 AN123689 AN123690 AN123691 AN123692 AN123693 AN123694 AN123695 AN123696 AN123705 AN123706 AN123707 AN123708 AN123709 AN123710 AN123711 AN123712 AN123722 AN123723 AN123724 AN123725 AN123726 AN123727 AN123728 Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 19:43:17 MSTNo reproduction or networking permitted without license from IHS -,-,- AEROSPACE STANDARD RIVET, SOLID, 100° FLUSH HEAD, NICKEL ALLOY UNS N06600 AS123601 THRU AS123750 REV. B AS123601 THRU AS123750 SHEET 3 OF 3 REV. B NOTES: 1. MATERIAL: NICKEL ALLOY (UNS N06600) IN ACCORDANCE WITH AS7232. 2. REMOVE BURRS AND BREAK SHARP EDGES .000 TO .015. 3. DIMENSIONS ARE IN INCHES. UNLESS OTHERWISE SPECIFIED, DIMENSIONING AND TOLERANCING IN ACCORDANCE WITH ANSI Y14.5M-1982 (ASME PUBLICATION). 4. DO NOT USE UNASSIGNED PART NUMBERS. 5. IDENTIFICATION: PER AS7232. 6. PART NUMBER: THE PART NUMBER SHALL CONSIST OF THE BASIC AN NUMBER TAKEN FROM TABLE 2. EXAMPLE: AN123601 - RIVET, SOLID, 100° FLUSH HEAD, .062 DIA., .125 LENGTH AN123691 - RIVET, SOLID, 100° FLUSH HEAD, .250 DIA., .875 LENGTH /7/ DIAMETER D TO BE GAGED FROM END OF SHANK TO WITHIN .100 OF BASE OF HEAD. 8. 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 REVISION OF THE DOCUMENT. AS AND AMS ARE SAE INTERNATIONAL PUBLICATIONS. ASME IS AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATIONS. Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 19:43:17 MSTNo reproduction or networking permitted without license from IHS -,-,-