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SAE AS85049-38B-2009

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SAE AS85049-38B-2009 AEROSPACE STANDARD CONNECTOR ACCESSORIES, ELECTRICAL,STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS) A S8 50 49 /3 8 Copyright 2009 SAE International All rights ...
SAE AS85049-38B-2009
AEROSPACE STANDARD CONNECTOR ACCESSORIES, ELECTRICAL,STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS) A S8 50 49 /3 8 Copyright 2009 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, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerService@sae.org SAE WEB ADDRESS: http://www.sae.org IS SU ED 2 00 0- 05 R EV IS ED 2 00 9- 08 THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8C1 R EV . B FEDERAL SUPPLY CLASS 5935 AS85049/38 SHEET 1 OF 5 REV. B PROCUREMENT SPECIFICATION: AS85049 SA E Te ch ni ca l S ta n da rd s Bo ar d R ul es p ro vid e th at : “ Th is re po rt is pu bl ish ed by S AE to a dv an ce th e st at e o f t ec hn ic al a n d e n gi ne er in g sc ie nc es . Th e u se o f t hi s re po rt is e n tir el y vo lu nt ar y, a nd its a pp lic ab ilit y a n d su ita bi lity fo r a ny p ar tic u la r u se , in cl ud in g a n y pa te n t i nf rin ge m e n t a ris in g th er ef ro m , is th e so le re sp o n si bi lity of th e u se r. ” SA E re vi ew s ea ch te ch ni ca l r e po rt a t l ea st e ve ry fi ve y ea rs a t w hi ch ti m e it m ay b e re af fir m ed , re vi se d, o r ca nc e lle d. SA E in vit es y ou r w rit te n co m m e n ts a nd su gg es tio ns . SAE values your input. To provide feedback on this Technical Report, please visit http://www.sae.org/technical/standards/AS85049/38B RATIONALE REVISED TO INCLUDE COMMENTS RECEIVED BY THE GOVERNMENT AND INDUSTRY, REMOVE GOVERNMENT JARGON, INCORPORATE AMENDMENTS, AND UP-DATE SPECIFICATION REFERENCES. THE REQUIREMENTS FOR ACQUIRING THE ACCESSORIES DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE OF SAE AS85049. FIGURE 1 - DIMENSION AND CONFIGURATION (SELF-LOCKING ONLY) Copyright SAE International Provided by IHS under license with SAE Not for ResaleNo reproduction or networking permitted without license from IHS - - ` , , ` ` ` , , , , ` ` ` ` - ` - ` , , ` , , ` , ` , , ` - - - AEROSPACE STANDARD AS85049/38 SHEET 2 OF 5 REV. B CONNECTOR ACCESSORIES, ELECTRICAL,STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS) TABLE 1A - SHELL SIZES AND DIMENSIONS (SELF LOCKING ONLY) CONNECTOR SHELL SIZE SHELL SIZE CODE (REF) C MAX OVERALL LENGTH D MAX E WIRE BUNDLE ACCOMMODATE RANGE SEE NOTE 5 F MAX DIA G SCREW LENGTH SCREW THREADS A MAX (SEE NOTE 6) MIN MAX 9 A 1.21 (30.7) .85 (21.6) .098 (2.49) .234 (5.94) .858 (21.79) .500 (12.70) 6-32 .91 (23.1) 11 B 1.21 (30.7) .90 (22.9) .153 (3.89) .234 (5.94) .984 (24.99) .500 (12.70) 6-32 .91 (23.1) 13 C 1.31 (33.3) 1.10 (27.9) .190 (4.83) .328 (8.33) 1.157 (29.39) .625 (15.88) 6-32 1.01 (25.70) 15 D 1.35 (34.3) 1.15 (29.2) .260 (6.60) .457 (11.61) 1.279 (32.49) .750 (19.05) 6-32 1.06 (26.9) 17 E 1.45 (36.8) 1.30 (33.0) .283 (7.19) .614 (15.60) 1.406 (35.71) .750 (19.05) 6-32 1.16 (29.5) 19 F 1.71 (43.4) 1.50 (38.1) .325 (8.26) .634 (16.10) 1.516 (38.51) .750 (19.05) 8-32 1.41 (35.8) 21 G 1.81 (46.0) 1.60 (40.6) .343 (8.71) .698 (17.73) 1.642 (41.71) .875 (22.23) 8-32 1.51 (38.4) 23 H 1.95 (49.5) 1.70 (43.2) .381 (9.68) .823 (20.90) 1.768 (44.91) 1.000 (25.40) 8-32 1.66 (42.2) 25 J 2.05 (52.1) 1.80 (45.7) .418 (10.62) .853 (21.67) 1.889 (47.98) 1.125 (28.58) 8-32 1.76 (44.7) NOTES: 1. DIMENSIONS ARE IN INCHES. 2. DIMENSIONS APPLY AFTER PLATING. 3. METRIC EQUIVALENTS ARE GIVEN FOR GENERAL INFORMATION ONLY. 4. MILLIMETERS ARE IN PARENTHESES. 5. WIRE BUNDLE ACCOMMODATION RANGE DIMENSION IS DEFINED AS THE ENVELOPE AREA OF THE WIRE BUNDLE. THIS DIMENSION IS NOT MEANT TO DEFINE THE CLAMP HARDWARE LIMITS. 6. THE “A” DIMENSION IS MEASURED FROM THE BOTTOM OF THE ACCESSORY TEETH TO THE END OF THE CLAMP. Copyright SAE International Provided by IHS under license with SAE Not for ResaleNo reproduction or networking permitted without license from IHS - - ` , , ` ` ` , , , , ` ` ` ` - ` - ` , , ` , , ` , ` , , ` - - - AEROSPACE STANDARD AS85049/38 SHEET 3 OF 5 REV. B CONNECTOR ACCESSORIES, ELECTRICAL,STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS) FIGURE 2 - DIMENSIONS AND CONFIGURATIONS (NON-SELF-LOCKING ONLY) Copyright SAE International Provided by IHS under license with SAE Not for ResaleNo reproduction or networking permitted without license from IHS - - ` , , ` ` ` , , , , ` ` ` ` - ` - ` , , ` , , ` , ` , , ` - - - AEROSPACE STANDARD AS85049/38 SHEET 4 OF 5 REV. B CONNECTOR ACCESSORIES, ELECTRICAL,STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS) TABLE 1B - SHELL SIZES AND DIMENSIONS (NON-SELF-LOCKING ONLY) CONNECTOR SHELL SIZE SHELL SIZE CODE (REF A MAX F WIRE BUNDLE ACCOMMODATION RANGE (SEE NOTE 5) G MAX DIA L MAX W +.000 -.062 SCREW LENGTH SCREW SIZE MIN MAX 9 A .75 (19.1) .098 (2.49) .234 (5.94) .85 (21.6) 1.10 (27.9) .500 (12.70) 6-32 11 B .85 (21.6) .153 (3.89) .234 (5.94) .90 (22.9) 1.10 (27.9) .500 (12.70) 6-32 13 C 1.00 (25.4) .190 (4.83) .328 (8.33) 1.10 (27.9) 1.20 (30.5) .625 (15.88) 6-32 15 D 1.10 (27.9) .260 (6.60) .457 (11.61) 1.15 (29.2) 1.25 (31.8) .750 (19.05) 6-32 17 E 1.25 (31.8) .283 (7.19) .614 (15.60) 1.30 (33.0) 1.35 (34.3) .750 (19.05) 6-32 19 F 1.40 (35.6) .325 (8.26) .634 (16.10) 1.50 (38.1) 1.60 (40.6) .750 (19.05) 8-32 21 G 1.50 (38.1) .343 (8.71) .698 (17.73) 1.60 (40.6) 1.70 (43,2) .875 (22.23) 8-32 23 H 1.65 (41.9) .381 (9.68) .823 (20.90) 1.70 (43.2) 1.85 (47.0) 1.000 (25.40) 8-32 25 J 1.75 (44.5) .418 (10.62) .853 (21.67) 1.80 (45.7) 1.95 (49.5) 1.125 (28.58) 8-32 NOTES: 1. DIMENSIONS ARE IN INCHES. 2. DIMENSIONS APPLY AFTER PLATING. 3. METRIC EQUIVALENTS ARE GIVEN FOR GENERAL INFORMATION ONLY. 4. MILLIMETERS ARE IN PARENTHESES. 5. WIRE BUNDLE ACCOMMODATION RANGE DIMENSION IS DEFINED AS THE ENVELOPE AREA OF THE WIRE BUNDLE. THIS DIMENSION IS NOT MEANT TO DEFINE THE CLAMP HARDWARE LIMITS. REQUIREMENTS 1. DESIGN AND CONSTRUCTION: DIMENSIONS AND CONFIGURATION: SEE FIGURES 1 AND 2. 2. INTERFACE DIMENSIONS: IN ACCORDANCE WITH SAE AS85049, FIGURE 3. 3. ACCESSORY: CONSISTS OF A COUPLING NUT AND FOLLOWER. THE COUPLING NUT SHALL BE CAPTIVATED TO AND SHALL BE ROTATEABLE. FIGURE 2 DIMENSION F MAX IS APPLICABLE WHEN END OF SCREW IS FLUSH WITH BB OR A MAXIMUM OF TWO SCREW THREADS PROTRUDE. 4. DETENTED SELF-LOCKING PROVIDES A POSITIVE AUDIBLE DETENTED COUPLING. 5. CLAMPS SHALL HAVE NO PROTRUSIONS OR SHARP EDGES WHICH MAY PINCH CABLE. 6. MATERIAL AND FINISH: SEE TABLE 2. ACCESSORIES SHALL BE AS SHOWN IN TABLE 2. Copyright SAE International Provided by IHS under license with SAE Not for ResaleNo reproduction or networking permitted without license from IHS - - ` , , ` ` ` , , , , ` ` ` ` - ` - ` , , ` , , ` , ` , , ` - - - AEROSPACE STANDARD AS85049/38 SHEET 5 OF 5 REV. B CONNECTOR ACCESSORIES, ELECTRICAL,STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS) TABLE 2 - MATERIAL AND FINISH FIGURE MATERIAL FINISH 1 & 2 ALUMINUM ALLOY IN ACCORDANCE WITH SAE AS85049 A N 1/ W 2/ 1 & 2 CORROSION RESISTANT STEEL 300 SERIES IN ACCORDANCE WITH SAE AMS763 S 1/ NOT FOR NAVY USE. AIR FORCE USE IS FOR SPACE APPLICATIONS ONLY. W IS THE PREFERRED FINISH. 2/ W IS NOT FOR USE IN SPACE APPLICATION. ALSO SEE SPECIFICATION NOTE 7. CLAMP SCREW AND LOCKWASHERS: 300 SERIES CORROSION-RESISTANT STEEL, PASSIVATE. 8. SELF-LOCKING DEVICES DESIGN AND CONSTRUCTION: COUPLINGS WITH SELF-LOCKING DEVICES SHALL MEET ALL THE REQUIREMENTS SPECIFIED HEREIN FOR ITS SPECIFIC CATEGORY AND THE FOLLOWING ADDITIONAL TESTS a. LIFE CYCLE: SEE SAE AS85049, PARAGRAPH 4.6.15. b. VIBRATION: SEE SAE AS85049, PARAGRAPH 3.5.4.1. 9. QUALIFICATION: SEE SAE AS85049, CATEGORY 4C. 10. ACCESSORIES ARE NOT RECOMMENDED FOR CONNECTORS USING CO-AX, DATA BUS, NO. 8, 6, 4 OR 0 CONDUCTORS. WHEN USED WITH MAXIMUM DENSITY ARRANGEMENTS, CLAMP MAY OPEN OUTER WIRE SEALS. 11. PART NUMBER: SEE EXAMPLE BELOW: M85049/ 38 S 11 W EXAMPLE: BASIC PART NUMBER SPECIFICATION SHEET CONFIGURATIONS; “S” FOR DETENTED SELF-LOCKING (SEE REQM’T 4) “N” FOR NON-DETENTED SELF-LOCKING “-“ (DASH) FOR NON-SELF-LOCKING DASH NUMBER FINISH (SEE TABLE 2) SPECIFICATION NOTES NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUM'S USE. A CHANGE BAR (|) 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. Copyright SAE International Provided by IHS under license with SAE Not for ResaleNo reproduction or networking permitted without license from IHS --`,,```,,,,````-`-`,,`,,`,`,,`---
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