1、 AEROSPACE STANDARD (R) CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, STRAIGHT, CATEGORY 4C (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, S81703) AS85049/53Copyright 2016 SAE International All rights reserved. No part of this publication may be reproduced, stored in a re
2、trieval 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: +1 724-776-4970 (outside USA) Fax: 724-776-0790 Email: Cus
3、tomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED2001-07 REVISED2016-09THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8C1 REV.C FEDERAL SUPPLY CLASS 5935 AS85049/53 SHEET 1 OF 3 REV. C PROCUREMENT SPECIFICATION: AS85049 SAE Technical Standards BoardRules providethat:“This reportis publishedby
4、SAE toadvancethestateoftechnicalandengineering sciences. The use of this report isentirely voluntary, andits applicability andsuitability for any particularuse, includingany patentinfringement arising therefrom,is the soleresponsibility of theuser.”SAE reviews eachtechnical reportatleast every fivey
5、ears atwhichtimeitmay berevised,reaffirmed, stabilized,orcancelled. SAE invites yourwrittencomments andsuggestions.SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS85049/53C RATIONALE REVISION IS REQUIRED TO IMPROVE DRAWINGS, M
6、OVE NOTES TO DESIGN PARAGRAPH TO FOLLOW C1 AS STANDARD FORMAT, REMOVE IMAGES, ADD PLASTIC TIE WRAP RESTRICTION TO NOTICE ON 1ST PAGE AND CLARIFY RESTRICTIONS, ADD AS95234 IN TITLE AND IN TABLE 1 UNDER AS50151 CRIMP, REMOVE THE .19 MINIMUM KNURL CALLOUT AND POINT TO THE COUPLING NUT KNURL AND STATE:
7、KNURL (STYLE OPTIONAL)” AND ADD METRIC EQUIVALENTS TO FIGURE 1. NOTICE THE COMPLETE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS85049. SEE APPLICATION NOTE 1. FIGURE 1 ACCESSORY CONFIGURATION AND DIMENSIONS AEROSPACE STANDARD AS85
8、049/53 SHEET 2 OF 3 REV. C (R) CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, STRAIGHT, CATEGORY 4C (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, S81703) TABLE 1 - DIMENSIONS DASH NO. FOR CONNECTOR SHELL, SIZE (REF) A MAX. B MAX. C DIA. MAX. D MAX. WIRING ENTRY MAX. AS817
9、03 SERIES 3 MIL-DTL- 26482 SERIES 2 AS50151 CRIMP AS95234 MIL-DTL- 83723 SERIES III 03 3 - - - .954 (24.23) .540 (13.72) .669 (16.99) 1.310 (33.27) .260 (6.60) 08 - 8 8S 8 .954 (24.23) .540 (13.72) .617 (15.67) 1.310 (33.27) .260 (6.60) 10 - 10 10,10SL 10 .954 (24.23) .540 (13.72) .734 (18.64) 1.310
10、 (33.27) .365 (9.27) 12 7 12 12,12S 12 .954 (24.23) .540 (13.72) .858 (21.79) 1.560 (39.62) .501 (12.73) 14 12 14 14,14S 14 1.204 (30.58) .540 (13.72) .984 (24.99) 1.560 (39.62) .575 (14.61) 16 19 16 16,16S 16 1.204 (30.58) .540 (13.72) 1.112 (28.24) 1.560 (39.62) .700 (17.78) 18 27 18 18 18 1.204 (
11、30.58) .540 (13.72) 1.218 (30.94) 1.560 (39.62) .779 (19.79) 20 37 20 20 20 1.310 (33.27) .540 (13.72) 1.345 (34.16) 1.666 (42.32) .904 (22.96) 22 - 22 22 22 1.430 (36.32) .540 (13.72) 1.468 (37.29) 1.786 (45.36) 1.029 (26.14) 24 - 24 24 24 1.560 (39.62) .540 (13.72) 1.593 (40.46) 1.916 (48.67) 1.14
12、4 (29.06) 28 - - 28 - 1.560 (39.62) .702 (17.83) 1.969 (50.01) 2.098 (53.29) 1.379 (35.03) REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS85049. 1. DESIGN AND CONSTRUCTION: ACCESSORIES SHALL BE DESIGNED IN ACCORDANCE WITH FIGURE 1 AND TABLE 1. DIMENSIONS ARE
13、IN INCHES AND APPLY AFTER PLATING. UNLESS OTHERWISE SPECIFIED TOLERANCES SHALL BE: .XX = .03 AND .XXX = .015 ANGULAR TOLERANCES X = 2. METRIC EQUIVALENTS ARE IN PARENTHESES, ARE GIVEN FOR GENERAL INFORMATION ONLY AND ARE BASED UPON 1 INCH = 25.4 MM. INTERFACE DIMENSIONS SHALL BE IN ACCORDANCE WITH A
14、S85049, FIGURE 4 OR 4A. COMPLETE STRAIN RELIEF UNIT CONSISTS OF COUPLING NUT AND A FOLLOWER WITH STRAIN RELIEF ARM. THE COUPLING SHALL BE CAPTIVATED TO THE FOLLOWER AND SHALL BE FREE TO ROTATE. 2. STRAIN RELIEF UNIT IS USED WITH MS3367-1-X PLASTIC STRAP (SEE APPLICATION NOTE 1) QUALIFIED IN ACCORDAN
15、CE WITH AS23190, MIL-DTL-713 LACING TWINE, OR A-A-52080 THRU 52084 LACING TAPE, OR EQUIVALENT, NOT SUPPLIED WITH THE CONNECTOR ACCESSORY. 3. THIS CLAMP WILL NOT ACCOMMODATE CONNECTORS USING SIZE 8, 4, AND 0 CONTACTS. 4. MATERIAL AND FINISH: SEE TABLE 2. TABLE 2 - MATERIAL AND FINISH FIGURE MATERIAL
16、FINISH COUPLING NUT AND FOLLOWER ALUMINUM ALLOY IN ACCORDANCE WITH AS85049 A, 1/ N, 2/ W, X, Y 2/ Z TIE MOUNT POLYAMIDE (OPTIONAL) NONE FASTENER STAINLESS STEEL (OPTIONAL) NONE 1/ N FINISH NOT RECOMMENDED FOR USE IN APPLICATIONS THAT MAY BE SUSCEPTIBLE TO SALT WATER CORROSION. 2/ W AND Z FINISH NOT
17、RECOMMENDED FOR USE IN APPLICATIONS THAT MAY BE SUSCEPTIBLE TO OUT GASSING (ALSO SEE SPECIFICATION NOTES). 5. QUALIFICATION: SEE AS85049, CATEGORY 4C. AEROSPACE STANDARD AS85049/53 SHEET 3 OF 3 REV. C (R) CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, STRAIGHT, CATEGORY 4C (FOR
18、AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, S81703) 6. PART NUMBER: SEE EXAMPLE BELOW: EXAMPLE: M85049/ 53 10 W BASIC PART NUMBER SPECIFICATION SHEET DASH NUMBER (SEE TABLE 1) FINISH 7. SUPERSESSION DATA: MS3152 * M85049/53 - * * DASH NUMBER FINISH OLD NEW ELECTROLESS W NICKEL APPLICATION NOTES:
19、 1. PLASTIC CABLE STRAPS ARE NOT RECOMMENDED FOR USE ON PLATFORMS UNDER THE JURISDICTION OF AS50881. AS85049/118 IS RECOMMENDED FOR NEW DESIGN. SPECIFICATION NOTES: NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONC
20、ERNING CADMIUMS USE. 1. 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 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.
