1、 AEROSPACE STANDARD REMOVAL TOOL, CONNECTOR, ELECTRICAL CONTACT, TYPE II, CLASS 1, COMPOSITION A AS81969/9Copyright 2015 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, mechani
2、cal, 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.org ISSUED 2015-06THIRD ANGL
3、E PROJECTION CUSTODIAN: AE-8/AE-8C2 FEDERAL SUPPLY CLASS 5120AS81969/9 SHEET 1 OF 3 PROCUREMENT SPECIFICATION: AS81969SAE Technical Standards Board Rules provide that: “This report ispublished by SAE toadvance thestate of technicalandengineering sciences. Theuse ofthisreport is entirelyvoluntary, an
4、dits applicability and suitability forany particularuse,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay berevised,reaffirmed, stabilized, orcancelled. SAE invites yourwrittencomment
5、s andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS81969/9 RATIONALE THIS DETAIL SPECIFICATION SHEET IS REQUIRED TO ALLOW THE CANCELLATION AND SUPERSESSION OF MIL-I-81969/9 WITH THIS DOCUMENT, TO IMPROVE DRAWING
6、LEGIBILITY, TO UPDATE QUALIFICATION INFORMATION, TO REMOVE GOVERNMENT JARGON AND TO UPDATE REFERENCES. NOTICE THE COMPLETE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS81969. FIGURE 1 - TOOL CONFIGURATION AND DIMENSIONS TABLE 1 - ME
7、TRIC EQUIVALENTS INCHES MILLIMETERS INCHES MILLIMETERS INCHES MILLIMETERS .001 0.025 .05 1.27 .395 10.03 .010 0.254 .115 2.92 1.00 25.40.02 0.508 .17 4.32 1.40 35.56 .044 1.12 .365 9.27 1.60 40.64AEROSPACE STANDARD AS81969/9 SHEET 2 OF 3 REMOVAL TOOL, CONNECTOR, ELECTRICAL CONTACT, TYPE II, CLASS 1,
8、 COMPOSITION A FIGURE 2 - INSTALLING CONTACT FIGURE 3 - REMOVING CONTACT REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS81969. 1. DESIGN: THE TOOL SHALL BE DESIGNED IN ACCORDANCE WITH FIGURE 1. DIMENSIONS ARE IN INCHES. METRIC EQUIVALENTS IN TABLE 1 ARE GIVEN
9、 FOR GENERAL INFORMATION ONLY AND ARE BASED ON 1 INCH = 25.4 MILLIMETERS. UNLESS OTHERWISE SPECIFIED, TOLERANCE IS .005 INCH (0.13 MILLIMETERS). 2. MATERIAL: STEEL PER AMS-QQ-S-700. 3. PLATING: NICKEL PER AMS-QQ-N-290, .000030 INCH THICK MINIMUM. 4. CONTACT INSTALLATION AND REMOVAL: INSTALLING CONTA
10、CT - SEE FIGURE 2. BE CERTAIN THE CONTACT LANCE IS SPRUNG ABOUT 15. ALIGN THE SOLDER TAB WITH THOSE ALREADY IN THE RECEPTACLE. REMOVING CONTACT - SEE FIGURE 3. PUSH TOOL TIP THROUGH THE NARROW OPENING OF THE REAR CAVITY, BETWEEN THE SOLDER TAB AND THE HOUSING. THIS WILL DEPRESS THE LANCE. PUSH CONTA
11、CT THROUGH THE CAVITY BY DEPRESSING ON THE SOLDER TAB. 5. PART NUMBER: M81969/9-01 EACH TOOL SHALL BE LEGIBLY AND PERMANENTLY MARKED WITH THE MANUFACTURERS IDENTIFICATION AND PART NUMBER IN ACCORDANCE WITH MIL-STD-130. MANUFACTURER SYMBOL, IF USED, SHALL BE IN ACCORDANCE WITH AIR1351. 6. QUALIFICATI
12、ON: QUALIFICATION SHALL BE IN ACCORDANCE WITH AS81969 WITH THE FOLLOWING EXCEPTIONS: ROTATION - NOT APPLICABLE THRUST - NOT APPLICABLE IMPACT STRENGTH - NOT APPLICABLE PLUNGER FORCE - NOT APPLICABLE ALTERNATIVE QUALIFICATION REQUIREMENTS SUCH AS CERTIFICATION, FIRST ARTICLE OR QC TESTING MAY BE IMPO
13、SED BY THE QUALIFYING ACTIVITY (QA). THE QA SHALL SUBMIT A WRITTEN REQUEST TO THE AE-8C2 COMMITTEE FOR REVIEW AND APPROVAL OF THE ALTERNATIVE QUALIFICATION TESTING PROGRAM PRIOR TO IMPLEMENTATION OF THE REQUIREMENT. AEROSPACE STANDARD AS81969/9 SHEET 3 OF 3 REMOVAL TOOL, CONNECTOR, ELECTRICAL CONTAC
14、T, TYPE II, CLASS 1, COMPOSITION A APPLICATION NOTES: 1. THIS TOOL SHALL BE USED TO REMOVE CONTACTS CONFORMING TO MIL-DTL-55302/32 AS SPECIFIED IN MIL-DTL-55302/24, /25, AND /27. 2. THIS DOCUMENT SUPERSEDES MIL-I-81969/9B DATED 2 OCTOBER 1980 AND MIL-C-55302/28A DATED 20 MAY 1972. SPECIFICATION NOTE
15、S: 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.
