SAE AS 3124A-2009 Pin Expansion - CRES 416 or 416SE Short UNS S41600 UNS S41623《膨胀螺钉 UNS S41600 UNS S41623短型416或416SE CRES》.pdf

《SAE AS 3124A-2009 Pin Expansion - CRES 416 or 416SE Short UNS S41600 UNS S41623《膨胀螺钉 UNS S41600 UNS S41623短型416或416SE CRES》.pdf》由会员分享，可在线阅读，更多相关《SAE AS 3124A-2009 Pin Expansion - CRES 416 or 416SE Short UNS S41600 UNS S41623《膨胀螺钉 UNS S41600 UNS S41623短型416或416SE CRES》.pdf（2页珍藏版）》请在麦多课文档分享上搜索。

1、AEROSPACE STANDARD (R) PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, SHORT, UNS A92024 AS3124Copyright 2009 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, phot

2、ocopying, 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 1981-02REAFFIRMED 2006-05 REV

3、ISED 2009-02THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.AFEDERAL SUPPLY CLASS 5315 AS3124SHEET 1 OF 2REV. APROCUREMENT SPECIFICATION: NONESAE TechnicalStandards Board Rules provide that: “This report is published by SAE toadvance thestate of technical andengineering sciences. Theuse of thisreport is

4、entirely voluntary, andits applicabilityandsuitability forany particularuse, including any patent infringement arising therefrom, is thesole responsibility oftheuser.”SAE reviews each technical report at least every five yearsat which time it may be reaffirmed, revised, orcancelled. SAE invites your

5、written commentsandsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS3124ARATIONALE UPDATE SUPPLIER PART NUMBERS, CLARIFY PART MARKING, UPDATE MATERIAL USAGE, CORRECT DIMENSIONAL ERRORS, AND GENERAL SAE UPDATING FOR

6、OBSOLETE SPECIFICATIONS AND FORMATING REQUIREMENTS. FIGURE 1 TABLE 1 PART NUMBERS AND DIMENSIONS AEROSPACE STANDARD PART NUMBER /7/MANUFACTURERS PART NUMBER /7/ANOM B NOM C MAXD NOM ENOM F NOM APPROX MASSLB/100 AS3124-01 PLGA0934010A .062 .069 .020 .0417 30 .056 .002 AS3124-02 PLGA1254010A .086 .095

7、 .020 .0417 10 .085 .006 AS3124-03 PLGA1564010A .078 .118 .032 .0417 13 .107 .008 AS3124-04 PLGA1874010A .114 .154 .040 .0417 10 .139 .020 AS3124-05 PLGA2184010A .145 .179 .040 .0417 (a) (a) .034 AS3124-06 PLGA2504010A .160 .212 .040 .0417 10 .196 .055 AS3124-07 PLGA2814010A .193 .245 .040 .0313 10

8、.233 .087 AS3124-08 PLGA3434010A .216 .290 .060 .0156 10 .277 .137 AS3124-09 PLGA4064010A .255 .357 .060 .0208 10 .344 .246 AS3124-10 PLGA4684010A .285 .427 .060 .0208 (a) (a) .402 AS3124-11 PLGA5314010A .375 .486 .060 .0156 10 .471 .675 AS3124-12 PLGA6564010A .390 .598 .060 .0182 10 .581 1.081(a) .

9、01-.02 RADIUS INSTEAD OF A CHAMFER NOTES: 1. MATERIAL: AMS4120 SIMILAR TO UNS A92024 (AL ALLOY 2024-T4; SIZES 01 THRU 08 AND AL ALLOY 2024-T351; SIZES 09 THRU 12), OR AMS-QQ-A-225/6 UNS A92024 (AL ALLOY 2024-T4; SIZES 01 THRU 08 , AND AL ALLOY 2024-T351; SIZES 09 THRU 12) 2. FINISH: MIL-DTL-5541, TY

10、PE 1, CLASS 1A OR 3, DYED YELLOW. 3. PINS ARE PREWAXED TO AID DRIVING. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS3124SHEET 2 OF 2REV. A(R) PIN, EXPANSION - ALUMINUM, 2024-T

11、4 AND 2024-T351, SHORT, UNS A92024 4. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M, REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 250 MICROINCHES Ra. 5. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. 6. DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED, TOLERANCE: ANGULAR

12、DIMENSIONS 2 DEGREES. DIMENSIONS APPLY AFTER FINISH. /7/ MARK AS3124-( ) PART NUMBER AND MANUFACTURERS PART NUMBER ON PACKAGE IN ACCORDANCE WITH AS478, METHOD 37. 8. USE WITH AS3123 PLUGS. SEE AIR3277 FOR INSTALLATION PROCEDURES. SEE AS3588 FOR AS3123 PLUG AND AS3124 PIN SET OF PARTS. 9. DIMENSIONIN

13、G AND TOLERANCING PER ASME Y14.5M-1994. 10. DO NOT USE UNASSIGNED PART NUMBERS. 11. AS, AIR AND AMS ARE SAE INTERNATIONAL PUBLICATIONS. ASME IS AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION. MIL IS US GOVERNMENT PUBLICATION. 12. A CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONV

14、ENIENCE 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, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USE

15、D IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY. APPROVED SOURCE OF SUPPLY: THE LEE CO WESTBROOK, CT FEDERAL SUPPLY CODE FOR MANUFACTURERS NO 92555. ONLY THE ITEM DESCRIBED ON THIS DRAWING WHEN PROCURED FROM THE VENDOR LISTED HEREON IS APPROVED FOR USE IN THE APPLICA

16、TIONS SPECIFYING THIS AEROSPACE STANDARD IDENTIFICATION NUMBER. A SUBSTITUTE ITEM SHALL NOT BE USED WITHOUT PRIOR TESTING AND APPROVAL BY THE DESIGN ACTIVITY RESPONSIBLE FOR THE APPLICATION. IDENTIFICATION OF THE APPROVED SOURCE HEREON IS NOT TO BE CONSTRUED AS A GUARANTEE OF PRESENT OR CONTINUED AVAILABILITY AS A SOURCE OF SUPPLY FOR THE ITEM DESCRIBED ON THE DRAWING. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-