SAE AS 123301 THRU AS123450D-2017 RIVET SOLID UNIVERSAL HEAD NICKEL ALLOY UNS N06600.pdf

1、 AEROSPACE STANDARD RIVET, SOLID, UNIVERSAL HEAD, NICKEL ALLOY, UNS N06600 AS123301-AS123450Copyright 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, mechanical, photocopy

2、ing, 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 ISSUED1999-12REAFFIRMED 2012-11REVISED

3、2017-07THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.D FEDERAL SUPPLY CLASS 5320 AS123301 - AS123450 SHEET 1 OF 3 REV. D PROCUREMENT SPECIFICATION: AS7232 SAE Technical Standards Board Rules provide that: “This report is published by SAEtoadvance thestate of technicaland engineering sciences. The useof

4、 this report is entirely voluntary, and its applicability andsuitability for any particularuse, includingany patent infringement arisingtherefrom,is thesole responsibility of theuser.” SAE reviews eachtechnical reportatleast every fiveyears at whichtime it may be revised, reaffirmed, stabilized, or

5、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/AS123301D RATIONALE THIS IS A LIMITED SCOPE REVISION. CORRECT DRAWING NOTE REFERENCE CALLOUT IN TABLE1 FOR D. NOTICE THE INITIAL SAE

6、PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD AN123301 THROUGH AN123450, REVISION 4. THIS SAE STANDARD MAY RETAIN THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT. ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LISTS (QPLS) MAY CONTINUE TO BE MAN

7、DATORY 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. AT o l X Z BR.0 2 0.0 0 5E R A D( C )L.0 1 5 M A X F L A T P E R M IS S IB L EO N T H IS E D G EA P P ROX M A T E RIA L F O R F UL L H E A D D/8 /ZFIGURE

8、1 TABLE 1 - DIMENSIONS D /8/ MIN MAX A MIN MAX B MIN MAX (C) E .010 X .061 .063 .119 .131 .027 .037 .112 .054 .010 .093 .095 .179 .197 .040 .050 .169 .082 .010 .123 .126 .238 .262 .054 .064 .225 .108 .010 .154 .157 .296 .328 .067 .077 .281 .135 .015 .186 .189 .356 .394 .080 .090 .338 .164 .015 .248

9、.252 .475 .525 .107 .117 .450 .217 .020 .310 .314 .594 .656 .133 .143 .561 .272 .020 .373 .377 .713 .787 .161 .171 .675 .328 .020 AEROSPACE STANDARD AS123301 - AS123450 SHEET 2 OF 3 REV. D RIVET, SOLID, UNIVERSAL HEAD, NICKEL ALLOY, UNS N06600 TABLE 2 - DIMENSIONS AND PART NUMBERS L .010 DIAMETER AN

10、D PART NUMBERS .062 .094 .125 .156 .188 .250 .312 .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 AN1

11、23301 AN123308 AN123302 AN123309 AN123303 AN123310 AN123304 AN123311 AN123305 AN123312 AN123306 AN123313 AN123307 AN123318 AN123314 AN123319 AN123315 AN123320 AN123316 AN123321 AN123317 AN123322 AN123329 AN123323 AN123330 AN123324 AN123331 AN123325 AN123332 AN123333 AN123349 AN123326 AN123350 AN1233

12、65 AN123366 AN123327 AN123381 AN123382 AN123383 AN123328 AN123334 AN123397 AN123335 AN123398 AN123336 AN123399 AN123337 AN123400 AN123338 AN123401 AN123339 AN123402 AN123340 AN123403 AN123341 AN123404 AN123413 AN123414 AN123342 AN123415 AN123416 AN123417 AN123343 AN123418 AN123419 AN123420 AN123344

13、AN123421 AN123429 AN123430 AN123345 AN123431 AN123432 AN123433 AN123346 AN123434 AN123435 AN123436 AN123347 AN123437 AN123438 AN123439 AN123348 AN123351 AN123440 AN123352 AN123441 AN123353 AN123442 AN123354 AN123443 AN123355 AN123444 AN123356 AN123445 AN123357 AN123446 AN123447 AN123448 AN123358 AN1

14、23449 AN123450 AN123359 AN123360 AN123361 AN123362 AN123363 AN123364 AN123367 AN123368 AN123369 AN123370 AN123371 AN123372 AN123373 AN123374 AN123375 AN123376 AN123377 AN133378 AN123379 AN123380 AN123384 AN123385 AN123386 AN123387 AN123388 AN123389 AN123390 AN123391 AN123392 AN123393 AN123394 AN1233

15、95 AN123396 AN123405 AN123406 AN123407 AN123408 AN123409 AN123410 AN123411 AN123412 AN123422 AN123423 AN123424 AN123425 AN123426 AN123427 AN123428 AEROSPACE STANDARD AS123301 - AS123450 SHEET 3 OF 3 REV. D RIVET, SOLID, UNIVERSAL HEAD, NICKEL ALLOY, UNS N06600 NOTES 1. MATERIAL: NICKEL ALLOY (UNS N0

16、6600) IN ACCORDANCE WITH AS7232. 2. PROCUREMENT SPECIFICATION: AS7232. 3. REMOVE BURRS AND BREAK SHARP EDGES .000 TO .015. 4. DIMENSIONS ARE IN INCHES. UNLESS OTHERWISE SPECIFIED, DIMENSIONING AND TOLERANCING IN ACCORDANCE WITH ASME Y14.5M-1982 (ASME PUBLICATION). 5. DO NOT USE UNASSIGNED PART NUMBE

17、RS. 6. IDENTIFICATION: PER AS7232. 7. PART NUMBER: THE PART NUMBER SHALL CONSIST OF THE BASIC AN NUMBER TAKEN FROM TABLE 2. EXAMPLE: AN123301 - RIVET, SOLID, UNIVERSAL HEAD, .062 DIAMETER, .125 LENGTH AN123391 - RIVET, SOLID, UNIVERSAL HEAD, .250 DIAMETER, .875 LENGTH /8/ DIAMETER D TO BE GAGED FROM

18、 END OF SHANK TO WITHIN .100 OF BASE OF HEAD. 9. REVISION INDICATOR: A CHANGE BAR (I) 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

19、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.