1、AEROSPACE STANDARDCONTACTS, ELECTRICAL, CONNECTOR, SOCKET,CRIMP REMOVABLE (FOR AS81714TERMINAL JUNCTION SYSTEM SERIES II)AS39029/22Copyright 2016 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any me
2、ans, 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: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgISS
3、UED2001-03REAFFIRMED 2008-04REVISED2016-08THIRD ANGLE PROJECTIONCUSTODIAN: AE-8/AE-8C1REV. CFEDERAL SUPPLY CLASS5935AS39029/22SHEET 1 OF 5REV.CPROCUREMENT SPECIFICATION: AS39029SAE Technical Standards BoardRules providethat:“This reportis publishedby SAE to advance thestateoftechnical andengineering
4、 sciences. The useofthis reportis entirely voluntary, and its applicability and suitability forany particularuse, includingany patent infringement arising therefrom,is thesole responsibility of theuser.”SAE reviews eachtechnical reportatleastevery fiveyears at whichtime itmay berevised, reaffirmed,
5、stabilized, or cancelled. SAEinvites your written comments and suggestions.SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS39029/22CRATIONALEREVISION IS REQUIRED TO ADD THE M22520/1-18 PART NUMBER TO TABLE 4, TO IMPROVE DRAWING
6、 LEGIBILITY, TO UPDATE REFERENCES AND DOCUMENT FORMAT TO LATEST SAE GUIDELINES AND TO ADD METRICEQUIVALENTS.NOTICETHE COMPLETE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS39029.FIGURE 1 - CONTACT CONFIGURATIONS, SOCKET SIZE 22, 20,
7、 16AEROSPACE STANDARD AS39029/22SHEET 2 OF 5REV.CCONTACTS, ELECTRICAL, CONNECTOR, SOCKET,CRIMP REMOVABLE (FOR AS81714TERMINAL JUNCTION SYSTEM SERIES II)FIGURE 2 CONTACT CONFIGURATIONS, SOCKET SIZE 12TABLE 1 - FIGURES 1 AND 2 METRIC EQUIVALENTSINCHES MILLIMETERS INCHES MILLIMETERS INCHES MILLIMETERS
8、INCHES MILLIMETERS.002 0.05 .006 0.15 .012 0.30 .054 1.37.003 0.08 .009 0.23 .029 0.74 .121 3.07.005 0.13 .010 0.25 .033 0.84TABLE 2 FIGURES 1 AND 2 DIMENSIONSBIN CODEADIA.BDIA.MAX.CDIA.DDIA.EDIA.FDIA. H JKREF.LCHAM.MMIN. N P R190 .033(0.84).031(0.79).060(1.52).0615(1.56).0600(1.52).0200(0.51).0180(
9、0.46).0480(1.22).0465(1.18).017(0.43).013(0.33).175(4.45).160(4.06).170(4.32).160(4.06).327(8.31).006(0.15).003(0.08).130(3.30).166(4.22).158(4.01).137(3.48).120(3.05).035(0.89).033(0.84)191.0355(0.90).0335(0.85).022(0.56).018(0.46)192.044(1.12).042(1.07).076(1.93).094(2.39).091(2.31).048(1.22).046(
10、1.17).070(1.78).068(1.73).027(0.69).023(0.58).349(8.86).010(0.25).005(0.13).150(3.81).188(4.78).180(4.57).055(1.40).053(1.35)193.066(1.68).064(1.63).108(2.74).130(3.30).127(3.23).068(1.73).066(1.68).103(2.62).101(2.57)605.100(2.54).097(2.46).168(4.27).171(4.34).168(4.27).102(2.59).096(2.44).152(3.86
11、).148(3.76).030(0.76).019(0.48).220(5.59).205(5.21).215(5.46).205(5.21).446(11.33).016(0.41).005(0.13).176(4.47).240(6.10).230(5.84).187(4.75).170(4.32)AEROSPACE STANDARD AS39029/22SHEET 3 OF 5REV.CCONTACTS, ELECTRICAL, CONNECTOR, SOCKET,CRIMP REMOVABLE (FOR AS81714TERMINAL JUNCTION SYSTEM SERIES II
12、)TABLE 3 - DESIGN CHARACTERISTICSBIN CODECOLOR BANDS MATING END SIZEWIRE BARREL SIZE TYPE CLASS1ST 2ND 3RD1/ 190 BROWN WHITE BLACK 22 28A B191 BROWN WHITE BROWN 22 22192 BROWN WHITE RED 20 20193 BROWN WHITE ORANGE 16 16605 BLUE BLACK GREEN 12 121/ SEE APPLICATION NOTE.TABLE 4 - TOOLSBINCODEBASICCRIM
13、PING TOOL POSITIONERINSTALLING/REMOVALTOOLS190M22520/7-01M22520/7-11 M81969/14-01191192 M22520/7-12 M81969/14-10193 M22520/7-13 M81969/14-03605 M22520/1-01M22520/1-18TH343 1/650065 1/M81969/8-09/M81969/8-10M81969/16-031/ TH343 IS A DANIELS MANUFACTURING CORP. PART NUMBER AND 650065 IS AN ASTRO TOOL
14、CORP. PART NUMBER. THESE COMMERCIAL PART NUMBERSWILL NO LONGER BE VALID AFTER A QPL SOURCE HAS BEEN ESTABLISHED FOR THE M22520/1-18.TABLE 5 - CONTACT RESISTANCEENGAGING END SIZEWIRE SIZE RANGETEST CURRENT (AMPERES)MAXIMUM VOLTAGE DROP (MILIVOLTS)25 C 3 C25 C 3 CAFTERCONDITIONING200 C+3 C, - 0C22 283
15、2 1.51.0 6095 70105 10013522 2226 5.02.0 7060 8070 12010020 2024 7.53.0 5545 6555 958016 1620 13.07.5 5045 6055 858012 12 1/14 23.017.0 6055 7065 100951/ SILVER PLATED WIRE.TABLE 6 - CONTACT ENGAGEMENT AND SEPERATION FORCESOCKET ENGAGING END SIZETEST PIN DIAMETERMIN +.0001, -.0000 MAX +.0000, -.0001
16、22 .0295 .030520 .0395 .040516 .0615 .062512 .0935 .0945AEROSPACE STANDARD AS39029/22SHEET 4 OF 5REV.CCONTACTS, ELECTRICAL, CONNECTOR, SOCKET,CRIMP REMOVABLE (FOR AS81714TERMINAL JUNCTION SYSTEM SERIES II)TABLE 7 - PROBE DAMAGESOCKET ENGAGINGEND SIZE TEST PROBE DIAMETERBENDING MOMENTDEPTH OF INSERTI
17、ONMOMENT(MAX IN-LB)22 .0305.0295 .105.095 .1020 .0405.0395 .135.125.2516 .0625.0615 .3712 .0935.0945 .185.175 .55TABLE 8 - TENSILE STRENGTHWIRE BARRELL SIZEWIRE SIZE (AWG)AXIAL LOAD (POUNDS) 1/ MAXIMUM RECOMMENDED CRIMP BARREL GROWTH PER DIASILVER OR TIN PLATED COPPER WIRENICKEL PLATED COPPER WIRE28
18、 2832 2.71.0 1.71.0.001522 2226 12.05.0 8.03.020 2024 20.08.0 10.06.0 .003016 1620 50.020.0 29.010.0 .005012 1214 100.060.0 65.034.0 .00701/ UNTIL A TEST METHOD IS DEFINED FOR VERIFICATION, THE MAXIMUM GROWTH DIAMETER WILL REMAIN A RECOMMENDATION RATHER THAN A REQUIREMENT.TABLE 9 - PART NUMBERAS3902
19、9 PART NUMBERBINCODESUPERSEDEDPART NUMBER(S)M39029/22-190 190 M39029/22-22-28M39029/15-22-28M39029/22-191 191 M39029/22-22-22M39029/15-22-22M39029/22-192 192 M39029/22-20-20M39029/22-193 193 M39029/22-16-16M39029/22-605 605 AIR FORCE LOGISTIC COMMANDB2070520-2-1REQUIREMENTS: ALL REQUIREMENTS SHALL C
20、ONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS39029.1. DESIGN:CONTACTS SHALL BE DESIGNED IN ACCORDANCE WITH FIGURES 1 AND 2 AND TABLES 2 AND 3. DIMENSIONS ARE IN INCHES. DIMENSIONS SHOWN APPLY AFTER PLATING. DIMENSION “M“ IS THE DISTANCE BETWEEN REAR OF CONTACT SHOULDER AND POINT AT WHICH A GAGE
21、 PIN, OF SAME BASIC DIAMETER AS MATING PIN CONTACT AND A SQUARE FACE, FIRST ENGAGES SOCKET CONTACT SPRING MEMBER. THE MAXIMUM ALLOWABLE GAP BETWEEN THE HOOD AND BODY OF THE CONTACT IS .010 INCH. AXIAL CONCENTRICITY: ALL DIAMETERS TO BE CONCENTRIC WITHIN .004 FIM EXCEPT AS NOTED.2. TOOLS: TOOLS REQUI
22、RED FOR CRIMPING CONTACTS TO WIRE/CABLE AND THE INSTALLING/REMOVAL FROM THE CONNECTOR SHALLBE IN ACCORDANCE WITH TABLE 4.3. PART NUMBERS: CONTACT PART NUMBERS SHALL BE IN ACCORDANCE WITH TABLE 9. SUPERSEDED PART NUMBERS ARE AS SPECIFIED.AEROSPACE STANDARD AS39029/22SHEET 5 OF 5REV.CCONTACTS, ELECTRI
23、CAL, CONNECTOR, SOCKET,CRIMP REMOVABLE (FOR AS81714TERMINAL JUNCTION SYSTEM SERIES II)4. MATERIALS: MATERIALS AND PLATING SHALL BE IN ACCORDANCE WITH AS39029. 5. MECHANICAL: MECHANICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029.TENSILE STRENGTH: SEE TABLE 8.PROBE DAMAGE: TEST PROBE DIAMETERS, DE
24、PTHS OF INSERTION, AND BENDING MOMENTS SHALL BE AS SPECIFIED IN TABLE 7.CONTACT ENGAGEMENT AND SEPARATION FORCE: SEE TABLE 6.6. ELECTRICAL: ELECTRICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029.CONTACT RESISTANCE: WHEN MATED TO .100 DEPTH WITH AS39029/18 CONTACT PIN WIRED WITH SILVER PLATED COND
25、UCTOR IN ACCORDANCE WITH AS39029 “PREPARATION OF SAMPLES,“ THE CONTACT RESISTANCE REQUIREMENTS SHALL BE AS SPECIFIED IN TABLE 5.7. ENVIRONMENTAL:ENVIRONMENTAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029.VIBRATION: IN ACCORDANCE WITH AS39029.SINE VIBRATION SHALL BE IN ACCORDANCE WITH MIL-STD-202 T
26、EST METHOD 204, TEST CONDITION G. DURATION SHALL BE 4 HOURS AT -50 C, 4 HOURS AT +200 C, AND 4 HOURS AT AMBIENT TEMPERATURE.SHOCK (SPECIFIED PULSE): IN ACCORDANCE WITH EIA-364-27, TEST CONDITION A.APPLICATION NOTES1. THESE CONTACTS ARE FOR USE IN COMPONENTS DESIGNED TO AS81714. THESE CONTACTS REPLAC
27、E AS39029/15 SIZE 22THROUGH 28 AND SIZE 22 THROUGH 22 FOR USE WITH AS81511 SERIES 3 AND 4 CLASS L CONNECTORS. THE AS81511APPLICABLE CONNECTOR DETAIL DOCUMENTS WERE CANCELLED IN 1979 AND CLASS L WAS REMOVED FROM MIL-C-81511IN 1992.2. BIN CODE 190 IS FOR INTERNAL BLACK BOX WIRING AND SHALL NOT BE USED
28、 IN AIRFRAME WIRING. IT IS ALSO NO LONGER SPECIFIED IN THE AS81714 BASE DOCUMENT.SPECIFICATION NOTES1. 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.
