SAE AS 39029 122-2015 CONTACTS ELECTRICAL CONNECTOR PIN CRIMP REMOVABLE EXPANDED PERFORMANCE SIZES 10 12 16 20 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS).pdf

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1、 AEROSPACE STANDARD CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, EXPANDED PERFORMANCE, SIZES 10, 12, 16,20, 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS)AS39029/122Copyright 2015 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieva

2、l 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: CustomerS

3、ervicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 2015-02THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8C1 FEDERAL SUPPLY CLASS 5970AS39029/122 SHEET 1 OF 8 PROCUREMENT SPECIFICATION: AS39029SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of tech

4、nicalandengineeringsciences.The useofthis reportisentirelyvoluntary, andits applicability and suitability forany particular use,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay berev

5、ised,reaffirmed, stabilized, orcancelled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS39029/122 RATIONALE THIS DETAIL SPECIFICATION SHEET IS REQUIRED TO ALIGN/HARMONIZE THE CO

6、NTACT PERFORMANCE REQUIREMENTS WITH THE APPLICABLE CONNECTOR PERFORMANCE REQUIREMENTS AND INCLUDE ADDITIONAL VERIFICATION TESTING FOR THE VIBRATION AND SHOCK REQUIREMENTS INCLUDING PERIODIC TESTING, TO ADD SIZE 23 CONTACT DETAILS/PART NUMBERS, TO ADD METAL TOOLING, TO CHANGE THE APPLICABLE CONNECTOR

7、S TO 38999 SERIES III ONLY, TO CHANGE SIZE 23-28 TO 23-26, TO DELETE SIZES 22 AND 22M, TO ADD WIRE RANGE ACCOMMODATION FOR SIZE 26 WIRE BARREL, TO DELETE THE .445-.425 DIMENSION FROM FIGURE 2, TO CLARIFY VISUAL/VIBRATION TESTING DETAILS AND TO ADD THE BLENDED RADIUS OPTION TO THE H DIMENSION. NOTICE

8、 THE COMPLETE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS39029. FIGURE 1 - CONNECTOR CONTACT (ALL SIZES EXCEPT 23) AEROSPACE STANDARD AS39029/122SHEET 2 OF 8CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, EXPANDED PERFORMANC

9、E, SIZES 10, 12, 16, 20, 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS)DETAIL T (SIZE 22D ONLY) FIGURE 1 - CONNECTOR CONTACT (ALL SIZES EXCEPT 23) (CONTINUED) FIGURE 1 - CONNECTOR CONTACT (CONTINUED) AEROSPACE STANDARD AS39029/122SHEET 3 OF 8CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE,

10、 EXPANDED PERFORMANCE, SIZES 10, 12, 16, 20, 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS)SIZE 23-22 AND 23-26 WIRE BARRELS DETAIL X FIGURE 2 - CONNECTOR CONTACT (SIZE 23 ONLY) AEROSPACE STANDARD AS39029/122SHEET 4 OF 8CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, EXPANDED PERFORMANCE,

11、 SIZES 10, 12, 16, 20, 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS)TABLE 1 - FIGURE 1 AND 2 DIMENSIONS BINCODE MATINGENDSIZEWIREBARREL SIZEARADIUS B C D E F G H669 23 26 SHER.RAD. APPROX. .0275 (0.699).0260 (0.660).0555 (1.41).0540 (1.37).022 (0.60) .018 (0.46) .0235 (0.60) .0215 (0.55) N/A.0

12、480 (1.219).0465 (1.181).006 (0.152).002 (0.051)670 23 22 SHER.RAD. APPROX. .0275 (0.699).0260 (0.660).0555 (1.41).0540 (1.37).022 (0.60) .018 (0.46) .0355 (0.90) .0335 (0.85) N/A.0480 (1.219).0465 (1.181).006 (0.152).002 (0.051)671 22 22D .020 (0.508) .010 (0.254) .0305 (0.774).0295 (0.749) .062 (1

13、.57) .060 (1.52) .022 (0.56) .018 (0.46) .0355 (0.90) .0335 (0.85) .011 (0.28) MAX.048 (1.22) .046 (1.17) .005 (0.13) .003 (0.08)672 20 20 .025 (0.635) .015 (0.381) .041 (1.04) .039 (0.991) .094 (2.39) .091 (2.31) .032 (0.81) .026 (0.66) .048 (1.22) .046 (1.17) .015 (0.38) MAX.070 (1.78) .068 (1.73)

14、 .010 (0.25) .005 (0.13)673 16 16 .025 (0.635) .020 (0.508) .0635 (1.613).0615 (1.562) .130 (3.30) .127 (3.23) .042 (1.07) .036 (0.914).068 (1.73) .066 (1.68) .030 (0.76) .011 (0.28) .103 (2.62) .101 (2.57) 674 12 12 .095 (2.41) .093 (2.36) .182 (4.62) .179 (4.55) .102 (2.59) .098 (2.49) .062 (1.57)

15、 .043 (1.09) .151 (3.84) .148 (3.76) .016 (0.41) .005 (0.13)675 10 10 .126 (3.20) .124 (3.15) .242 (6.15) .238 (6.05) .052 (1.32) .040 (1.02) .140 (3.56) .134 (3.40) .094 (2.39) .074 (1.88) .213 (5.41) .207 (5.26) TABLE 1 - FIGURE 1 AND 2 DIMENSIONS (CONTINUED) BIN CODE MATINGEND SIZE WIREBARREL SIZ

16、EKMINIMUM M S T(REF) 669 23 26 .145 MIN. (3.68) N/A.218 (5.54) .208 (5.28) .636 (16.15) 670 23 22 N/A .218 (5.54) .208 (5.28) .636 (16.15) 671 22 22D .141 (3.58) - .237 (6.02) .231 (5.87) .531 (13.49) 672 20 20 .209 (5.31) .078 (1.98) .072 (1.83) 673 16 16 .088 (2.24) .082 (2.08) 674 12 12 675 10 10

17、 .355 (9.02) .115 (2.92) .108 (2.74) .405 (10.29) .395 (10.03) .647 (16.43) AEROSPACE STANDARD AS39029/122SHEET 5 OF 8CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, EXPANDED PERFORMANCE, SIZES 10, 12, 16, 20, 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS)TABLE 2 - DESIGN CHARACTERISTICS

18、BIN CODE COLOR BANDS MATINGEND SIZEWIREBARRELSIZE TYPE CLASS 1ST2ND3RD669 BLUE BLUE WHITE 23 26 A B 670 BLUE VOILET BLACK 23 22 671 BLUE VOILET BROWN 22 22D 672 BLUE VOILET RED 20 20 673 BLUE VOILET ORANGE 16 16 674 BLUE VOILET YELLOW 12 12 675 BLUE VOILET GREEN 10 10 TABLE 3 - TOOLS BINCODE BASIC C

19、RIMPING TOOL POSITIONER INSTALLING TOOL 1/ REMOVAL TOOL WIREDCONTACT UNWIREDCONTACT 669 M22520/2-01 M22520/2-16 M81969/1-05 (METAL FOR BIN CODES 672, 673, 674, AND 675, DIAMETERS E AND G TO BE CONCENTRIC WITH .001 TOTAL INDICATOR READING (TIR) OF MAXIMUM MATERIAL CONDITION (MMC). THE .036-.041 DIAME

20、TER IN DETAIL “T” SHALL BE CONCENTRIC TO G DIAMETER WITHIN .003 (TIR) (RFS). FOR DIMENSION H, THE FOLLOWING BLEND RADIUS DIMENSIONS ARE OPTIONAL: SIZE 23 - BLEND RADIUS .010 INCH .005 INCH. SIZE 22 - BLEND RADIUS .010 INCH .005 INCH. SIZE 20 - BLEND RADIUS .015 INCH .005 INCH. SIZE 16 - BLEND RADIUS

21、 .020 INCH .005 INCH. SIZE 12 - BLEND RADIUS .020 INCH .010 INCH. SIZE 10 - BLEND RADIUS .020 INCH .010 INCH. FIGURE 2 ADDITIONAL DETAILS: UNLESS OTHERWISE SPECIFIED, SPHERICAL END DIMENSIONS SHALL CONFORM TO AS39029. A .001 INCH MAXIMUM BURR IS PERMITTED ON THE PERIPHERY OF SHOULDER (SEE VIEW X). 2

22、. TOOLS: TOOLS REQUIRED FOR CRIMPING CONTACTS TO 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 4. SUPERSEDED PART NUMBERS ARE AS SPECIFIED. 4. MATERIALS: MATERIALS SHALL BE IN

23、ACCORDANCE WITH AS39029. 5. MECHANICAL: MECHANICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. 6. ELECTRICAL: ELECTRICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. 7. ENVIRONMENTAL: ENVIRONMENTAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029 AND AS LISTED BELOW: VIBRATION: THE FOLLOWING VI

24、BRATION TESTS SHALL BE PERFORMED ON SEPARATE SAMPLES FOR EACH TEST. EACH TEST SAMPLE MUST COMPLY WITH THE AS39029 BASIC SPECIFICATION SAMPLE REQUIREMENTS. SAMPLE PREPARATION:a. THE SAMPLE SIZE OF CONTACTS FOR GROUP 2 SHALL BE TRIPLED TO ALLOW FOR 3 GROUPS OF CONTACTS TO BE SUBJECTED TO THE VIBRATION

25、 TEST. b. THE CONTACTS SHALL BE DIVIDED INTO 3 SUB-GROUPS AND MOUNTED IN MIL-DTL-38999 CONNECTORS (MATING FREE PLUG AND RECEPTACLE) RATED AT 200 qC. c. HIGH STRENGTH WIRE MAY BE USED FOR VIBRATION TESTING. AEROSPACE STANDARD AS39029/122SHEET 7 OF 8CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE

26、, EXPANDED PERFORMANCE, SIZES 10, 12, 16, 20, 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS)VIBRATION TESTS: a. THE FIRST SUB-GROUP SHALL BE TESTED TO THE VIBRATION REQUIREMENTS OF MIL-DTL-38999 SINE VIBRATION PARAGRAPH. THE HIGH TEMPERATURE PART OF THE TEST SHALL BE PERFORMED AT A TEMPERATURE

27、OF 200 qC. b. THE SECOND SUB-GROUP SHALL BE TESTED TO THE VIBRATION REQUIREMENTS OF MIL-DTL-38999 RANDOM VIBRATION PARAGRAPH APPLICABLE TO SERIES 1, III AND IV ONLY AT A TEMPERATURE OF 200 qC. c. THE THIRD SUB-GROUP SHALL BE TESTED TO THE VIBRATION REQUIREMENTS OF MIL-DTL-38999 RANDOM VIBRATION PARA

28、GRAPH APPLICABLE TO SERIES 1, III AND IV ONLY, TEST CONDITION 5 USING THE VIBRATION ENVELOPE SHOWN IN THE APPLICABLE FIGURE, AT AMBIENT TEMPERATURE d. DURING EACH OF THE ABOVE VIBRATION TESTS THE CONTACTS SHALL BE MONITORED FOR ELECTRICAL DISCONTINUITY TO THE REQUIREMENTS OF EIA364-46. THERE SHALL B

29、E NO DISCONTINUITIES IN EXCESS OF 1 MICROSECOND. e. FOLLOWING THE VIBRATION TESTS ABOVE, THE CONTACTS SHALL BE INDIVIDUALLY MEASURED FOR CONTACT RESISTANCE IN ACCORDANCE WITH EIA364-06. THE CONTACTS SHALL BE MEASURED AT AMBIENT TEMPERATURE AND UNDISTURBED WHILE STILL WITHIN THE CONNECTOR. THE MEASUR

30、ING POINTS SHALL BE AT A TOTAL DISTANCE OF 6 INCHES APART. THE CONTACT RESISTANCE SHALL MEET THE REQUIREMENTS OF AS39029 TABLES 5 OR 6 (WHERE APPROPRIATE) AT THE CURRENTS SHOWN IN THE TABLES. SHOCK: CONNECTORS/CONTACTS SHALL BE TESTED IN ACCORDANCE WITH EIA-364-27, TEST CONDITION D. THE FOLLOWING DE

31、TAILS SHALL APPLY: a. THE PULSE SHALL BE AN APPROXIMATE HALF SINE WAVE OF 300 G 15% MAGNITUDE WITH A DURATION OF 3 MILLISECONDS 1 MILLISECOND. b. THE WIRE BUNDLE SHALL BE CLAMPED TO FIXED POINTS AT LEAST 8 INCHES FROM THE REAR OF THE CONNECTOR. HIGH-IMPACT SHOCK: WIRED AND MATED CONNECTORS SHALL BE

32、SUBJECTED TO THE TEST SPECIFIED IN MIL-S-901, GRADE A WITH THE FOLLOWING MODIFICATIONS AND ADDITIONS. CONNECTORS SHALL BE COUPLED TOGETHER BY NORMAL COUPLING MEANS. DURING THE HIGH IMPACT SHOCK TESTING, THE CONTACTS SHALL BE MONITORED FOR ELECTRICAL DISCONTINUITY AS REQUIRED B Y EIA364-46. THERE SHA

33、LL BE NO DISCONTINUITIES IN EXCESS OF 1 MICROSECOND. MOUNTING FIXTURES SHALL BE IN ACCORDANCE WITH MIL-S-901, LIGHTWEIGHT. THE CABLE OR WIRE BUNDLE SHALL BE SUPPORTED ON A STATIONARY FRAME IN SUCH A MANNER TO PROVIDE A FREE FLEXING CABLE LENGTH BETWEEN THE FRAME AND FIXTURE OF NOT LESS THAN 36 INCHE

34、S (914.4 MILLIMETERS). THE PLUG SHALL BE TERMINATED WITH AT LEAST 80% OF WIRED CONTACTS. THE WIRE BUNDLE SHALL BE PROVIDED WITH STRAIGHT, OPEN FRAME, STRAIN RELIEF ACCESSORY HARDWARE. FOLLOWING THE SHOCK TEST THE CONTACTS SHALL BE INDIVIDUALLY MEASURED FOR CONTACT RESISTANCE IN ACCORDANCE WITH EIA36

35、4-06. THE CONTACTS SHALL BE MEASURED UNDISTURBED WHILE STILL WITHIN THE CONNECTOR. THE MEASURING POINTS SHALL BE AT A TOTAL DISTANCE OF 6 INCHES APART. THE LOW LEVEL CONTACT RESISTANCE SHALL MEET THE REQUIREMENTS OF AS39029 TABLES 5 OR 6 (WHERE APPROPRIATE) AT THE CURRENTS SHOWN IN THE TABLES. VISUA

36、L EXAMINATION: FOLLOWING THE COMPLETION OF THE VIBRATION AND SHOCK TESTS THE INDIVIDUAL CONTACTS SHALL BE REMOVED FROM THE CONNECTORS AND VISUALLY EXAMINED FOR EVIDENCE OF CORROSION FRETTING USING A MINIMUM OF X10 MAGNIFICATION. THERE SHALL BE NO EXPOSURE OF BASE MATERIAL AT X10. BASE MATERIAL EXPOS

37、URE DETECTED AT MAGNIFICATION LEVELS HIGHER THAT X10 SHALL NOT BE CONSIDERED FAILURES.8. QUALIFICATION: QUALIFICATION SHALL BE IN ACCORDANCE WITH AS39029. PERIODIC/RETENTION TESTING: IN ADDITION TO THE PERIODIC TESTS REQUIRED BY AS39029, THE ABOVE LISTED VIBRATION AND SHOCK TESTS SHALL BE REPEATED A

38、T AN INTERVAL OF 72 MONTHS FROM THE DATE OF INITIAL APPROVAL, AND AT 72 MONTH INTERVALS THEREAFTER. THE MANUFACTURERS RELIABILITY ASSURANCE PROGRAM SHALL COMPLY WITH THE AS9100 AEROSPACE STANDARD FOR QUALITY MANAGEMENT SYSTEM REQUIREMENTS. OTHER ESTABLISHED AND INDUSTRY RECOGNIZED QUALITY ASSURANCE

39、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, MEASURE, AND VALIDATE COM

40、PLIANCE AT THEIR DISCRETION. AEROSPACE STANDARD AS39029/122SHEET 8 OF 8CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, EXPANDED PERFORMANCE, SIZES 10, 12, 16, 20, 22 AND 23 (FOR MIL-DTL-38999 SERIES III CONNECTORS)APPLICATION NOTES: 1. CONTACT MATES DIRECTLY WITH AN AS39029/121 SOCKET CONTACT

41、AS SHOWN IN TABLE 5. TABLE 5 - CONTACT MATING PART NUMBERS AS39029/122 BIN CODE MATING AS39029 SLASH SHEET/BIN CODE -669 M39029/121-662-670 M39029/121-663-671 M39029/121-664 -672 M39029/121-665-673 M39029/121-666-674 M39029/121-667-675 M39029/121-6682. INTERFERENCE MAY BE EXPERIENCED DURING INSTALLA

42、TION AND REMOVAL OF CONTACTS IN SOME LANYARD RELEASE CONNECTORS. IF SO, USE THE INSTALLING/REMOVAL TOOLS RECOMMENDED BY THE CONNECTOR MANUFACTURER. 3. THIS CONTACT IS FUNCTIONALLY INTERCHANGEABLE WITH THE AS39029/58 CONTACT, HOWEVER IT INCLUDES ADDITIONAL PERFORMANCE REQUIREMENTS. ADDITIONAL PERFORM

43、ANCE REQUIREMENTS INCLUDE THE VIBRATION/SHOCK REQUIREMENTS OF THE APPLICABLE MIL-DTL-38999 CONNECTOR SPECIFICATION. THIS CONTACT ALSO INCLUDES THE ADDITIONAL VIBRATION/SHOCK VERIFICATION TESTING AND REQUIRED PERIODIC TESTING INTERVALS FOR THE VIBATION AND SHOCK TESTING. THIS SPECIFICATION ALSO INCLU

44、DES REQUIREMENTS FOR SIZE 23 CONTACTS. SPECIFICATION NOTES: 1. A 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, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY.