1、 AEROSPACE STANDARD (R) CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMPREMOVABLE (THERMOCOUPLE FOR MIL-DTL-38999 SERIESII, MIL-DTL-83733, AND MIL-DTL-24308 CONNECTORS) AS39029/89Copyright 2009 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval s
2、ystem 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: CustomerServ
3、icesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 2000-07REAFFIRMED 2006-10REVISED 2009-09THIRD ANGLE PROJECTION CUSTODIAN: AE-8C1 REV.A FEDERAL SUPPLY CLASS 5999 AS39029/89SHEET 1 OF 6 REV. A PROCUREMENT SPECIFICATION: SAE Technical Standards Board Rules provide that: “This report ispublished by
4、 SAE toadvance thestate of technicalandengineering sciences. Theuse ofthisreport is entirelyvoluntary, andits applicability and suitability forany particularuse,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every fiv
5、e years at which time itmay bereaffirmed, revised,orcancelled.SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS39029/89A RATIONALE REVISE TO INCLUDE COMMENTS RECEIVED BY THE GOVERN
6、MENT AND INDUSTRY, REMOVE GOVERNMENT JARGON, UPDATE REFERENCES, ALIGN SPECIFICATION WITH SAE GUIDELINES, AND REVIEW SPECIFICATION FOR KNOWN TECHNICAL PROBLEMS. NOTICE THE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION SHEET AND THE LATEST ISSUE OF SAE AS3
7、9029. FIGURE 1 - SOCKET CONTACTS (SEE DESIGN PARAGRAPH FOR ADDITIONAL DIMENSIONAL DETAILS). Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/89SHEET 2 OF 6 REV. A (R) CONTAC
8、TS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (THERMOCOUPLE FOR MIL-DTL-38999 SERIES II, MIL-DTL-83733, AND MIL-DTL-24308 CONNECTORS) TABLE 1 - CONTACT DIMENSIONS BIN CODE A REF B DIA C DIA D DIA E DIA F DIA MAX G DIA H J K MIN M N P DIA MIN 494 THROUGH 497 .518 (13.16) .031 (.79) MIN .062 (1.57
9、) .060 (1.52) .022 (.56) .018 (.46) .0355 (.90) .0335 (.85) .062 (1.57) .048 (1.22) .046 (1.17) .005 (.13) .003 (.08) .289 (7.34) .279 (7.09) .141 (3.58) N/A 50 44 .047 (1.19) 498 THROUGH 501 .0415 (1.05) MIN .094 (2.39) .091 (2.31) .032 (.81) .026 (.66) .048 (1.22) .046 (1.17) .078 (1.98) .070 (1.7
10、8) .068 (1.73) .010 (.25) .005 (.13) .209 (5.31) .078 (1.98) .072 (1.83) 47 28 .053 (1.35) 502 THROUGH 505 .064 (1.63) MIN .130 (3.30) .127 (3.23) .042 (1.07) .036 (.914) .068 (1.73) .066 (1.68) .113 (2.87) .103 (2.62) .101 (2.57) .088 (2.24) .082 (2.08) .084 (2.13) TABLE 2 - MARKING AND DESIGN CHAR
11、ACTERISTICS BIN CODE COLOR BANDS MATING END SIZEWIRE BARRELL SIZE TYPE CLASS 1ST2ND3RD494 YELLOW WHITE YELLOW 22 22D C (SEE TABLE 4) B 495 YELLOW WHITE GREEN 22 22D 496 YELLOW WHITE BLUE 22 22D 497 YELLOW WHITE VIOLET 22 22D 498 YELLOW WHITE GRAY 20 20 499 YELLOW WHITE WHITE 20 20 500 GREEN BLACK BL
12、ACK 20 20 501 GREEN BLACK BROWN 20 20 502 GREEN BLACK RED 16 16 503 GREEN BLACK ORANGE 16 16 504 GREEN BLACK YELLOW 16 16 505 GREEN BLACK GREEN 16 16 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A
13、EROSPACE STANDARD AS39029/89SHEET 3 OF 6 REV. A (R) CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (THERMOCOUPLE FOR MIL-DTL-38999 SERIES II, MIL-DTL-83733, AND MIL-DTL-24308 CONNECTORS) TABLE 3 - TOOLS BIN CODE BASIC CRIMPING TOOL POSITIONER INSTALLING TOOL REMOVAL TOOL 494, 495, 496, 497
14、M22520/2-01 OR M22520/7-01 M22520/2-06 OR M22520/7-06 M81969/8-01 OR M81969/14-01 M81969/8-02 OR M81969/14-01 498, 499, 500, 501 M22520/1-01 OR M22520/2-01 OR M22520/7-01 M22520/1-04 OR M22520/2-10 OR M22520/7-08 M81969/8-05 OR M81969/14-02 M81969/8-06 OR M81969/14-02 502, 503, 504, 505 M22520/1-01
15、OR M22520/7-01 M22520/1-04 OR M22520/7-04 M81969/8-07 OR M81969/14-03 M81969/8-08 OR M81969/14-03 TABLE 4 - MATERIALS, PLATING, AND TENSILE STRENGTH BIN CODE MATERIALS PLATING TENSILE STRENGTH 1/ WIRE SIZE AXIAL LOAD WIRE SIZE AXIAL LOAD 494 JN NONE 28 MIN 1.5 22 MAX 6 495 KN NONE 496 KP NONE 497 JP
16、 CADMIUM PLATE 2/498 JN NONE 24 MIN 4.5 20 MAX 14 499 KN NONE 500 KP NONE 501 JP CADMIUM PLATE 2/502 JN NONE 20 MIN 14 16 MAX 33 503 KN NONE 504 KP NONE 505 JP CADMIUM PLATE 2/1/ APPLIES TO TYPE 1 WIRE PER MIL-W-5846 2/ CHROMATE CLEAR COAT Copyright SAE International Provided by IHS under license wi
17、th SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/89SHEET 4 OF 6 REV. A (R) CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (THERMOCOUPLE FOR MIL-DTL-38999 SERIES II, MIL-DTL-83733, AND MIL-DTL-24308 CONNECTORS) TABLE 5 - PART
18、 NUMBER AND BIN CODE PART NUMBER BIN CODE SUPERSEDED M39029/89-494 494 M39029/892222C1 M39029/89-495 495 M39029/892222C2 M39029/89-496 496 M39029/892222C3 M39029/89-497 497 M39029/892222C4 M39029/89-498 498 1/ M39029/892020C1 M39029/89-499 499 1/ M39029/892020C2 M39029/89-500 500 1/ M39029/892020C3
19、M39029/89-501 501 1/ M39029/892020C4 M39029/89-502 502 1/ M39029/891616C1 M39029/89-503 503 1/ M39029/891616C2 M39029/89-504 504 1/ M39029/891616C3 M39029/89-505 505 1/ M39029/891616C4 1/ NOT FOR USE WITH MIL-DTL-83733 OR MIL-DTL-24308 CONNECTORS (FOR MIL-DTL-83733 CONTACT SIZES 20 AND 16, SEE AS390
20、29/10). REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE OF AS39029. 1. DESIGN; CONTACTS SHALL BE DESIGNED IN ACCORDANCE WITH FIGURE 1, TABLES 1 AND 2. DIMENSIONS ARE IN INCHES, METRIC EQUIVALENTS ARE GIVEN FOR GENERAL INFORMATION ONLY. DIMENSIONS SHOWN APPLY A
21、FTER PLATING. FOR SIZE 22D ONLY, DIAMETERS E AND G ARE TO BE CONCENTRIC WITHIN .003 (TIR) REGARDLESS OF FEATURE SIZE (RFS); FOR ALL OTHER CONTACT SIZES, DIAMETERS E AND G TO BE CONCENTRIC WITHIN .001 (TIR) AT MAXIMUM MATERIAL CONDITION (MMC). THE .248 MIN DIMENSION IS THE POINT AT WHICH A SQUARE END
22、ED PIN OF THE SAME BASIC DIAMETER AS THE MATING CONTACT FIRST ENGAGES THE SOCKET CONTACT SPRING. THE .029-.033 DIMENSION IS NOT APPLICABLE FOR SIZE 22D.HOODS SHALL NOT EXCEED CONTACT BODY DIAMETER REGARDLESS OF FEATURE SIZE (RFS) IN ATTACHMENT AREA. 2. TOOLS: TOOLS REQUIRED FOR CRIMPING CONTACTS TO
23、THE WIRE/CABLE AND THE INSTALLING/REMOVAL FROM THE CONNECTOR SHALL BE IN ACCORDANCE WITH TABLE 3. 3. PART NUMBERS: CONTACT PART NUMBERS SHALL BE IN ACCORDANCE WITH TABLE 5. SUPERSEDING PART NUMBERS ARE AS SPECIFIED. 4. MATERIALS AND PLATING: SEE TABLE 4 5. TENSILE STRENGTH: SEE TABLE 4. 6. RANDOM VI
24、BRATION: CONNECTORS/CONTACTS SHALL BE TESTED IN ACCORDANCE WITH EIA-364-28 THE FOLLOWING DETAILS SHALL APPLY: a. TEST CONDITION VI, LETTER I, EXCEPT CLASS Y SHALL BE LETTER G. b. VIBRATION TO BE CONDUCTED AT STANDARD TEST CONDITIONS. c. DURATION SHALL BE 8 HOURS IN THE LONGITUDINAL DIRECTION AND 8 H
25、OURS IN A PERPENDICULAR DIRECTION FOR A TOTAL OF 16 HOURS. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/89SHEET 5 OF 6 REV. A (R) CONTACTS, ELECTRICAL CONNECTOR, SOCKET,
26、 CRIMP REMOVABLE (THERMOCOUPLE FOR MIL-DTL-38999 SERIES II, MIL-DTL-83733, AND MIL-DTL-24308 CONNECTORS) 7. SHOCK: CONNECTORS/CONTACTS SHALL BE TESTED IN ACCORDANCE WITH EIA-364-27. THE FOLLOWING DETAILS SHALL APPLY: a. THE PULSE SHALL BE AN APPROXIMATE HALF SINE WAVE OF 300 G 15 PERCENT MAGNITUDE W
27、ITH A DURATION OF 3 MILLISECONDS 1. b. THE WIRE BUNDLE SHALL BE CLAMPED TO FIXED POINTS AT LEAST 8 INCHES (203.2MM) FROM THE REAR OF THE CONNECTOR. 8. RESISTANCE TO TEST PROBE DAMAGE: SEE TABLE 6. TABLE 6 - PROBE DAMAGE INSERTION DEPTHS CONTACT SIZE INSERTION DEPTH (+.020 - .000 INCHES) 22D, 20 .083
28、 (2.11) - .125 (3.18) 1/ 16 .135 (3.43) 12 1.66 (42.16)1/ INDICATED DIMENSIONS REPRESENT AND DEPTHS. 9. QUALIFICATION: THE MANUFACTURERS RELIABILITY ASSURANCE PROGRAM SHALL COMPLY WITH THE AS9100 AEROSPACE STANDARD FOR QUALITY MANAGEMENT SYSTEM REQUIREMENTS. OTHER ESTABLISHED AND INDUSTRY RECOGNIZED
29、 QUALITY ASSURANCE STANDARDS THAT ASSURE ALL PRODUCTS PRODUCED CONFORM TO THE CONTRACT REQUIREMENTS ARE ACCEPTABLE. HOWEVER, IF USED, IT IS THE RESPONSIBILITY OF THE MANUFACTURER TO PROVIDE EVIDENCE OF COMPLIANCE TO AS9100. THE QUALIFYING ACTIVITY (QA) AUTHORITY RESERVES THE RIGHT TO MONITOR, MEASUR
30、E, AND VALIDATE COMPLIANCE AT THEIR DISCRETION. APPLICATION NOTES: 1. CONTACT MATES DIRECTLY TO AN AS39029/87 PIN AS SHOWN IN TABLE 7. TABLE 7 - CONTACT MATING PART NUMBERS AS39029/89 BIN CODE MATING AS39029/87 SLASH SHEET/BIN CODE -494 -470-495 -471 -496 -472-497 -473-498 -474-499 -475-500 -476-501
31、 -477 -502 -478-503 -479-504 -480-505 -4812. THE COMPOSITION DESIGNATIONS HAVE BEEN CHANGED AS LISTED BELOW: JN = TYPE J NEGATIVE (FORMERLY CONSTANTAN) KN = TYPE K NEGATIVE (FORMERLY ALUMEL) KP = TYPE K POSITIVE (FORMERLY CHROMEL) JP = TYPE J POSITIVE (FORMERLY IRON) Copyright SAE International Prov
32、ided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/89SHEET 6 OF 6 REV. A (R) CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (THERMOCOUPLE FOR MIL-DTL-38999 SERIES II, MIL-DTL-83733, AND MIL-DTL-2430
33、8 CONNECTORS) 1. SPECIFICATION NOTES: NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. A CHANGE BAR (|) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TEC
34、HNICAL 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. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
