1、 AEROSPACE STANDARD TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDTHRU TYPE, LIGHT WEIGHT, SERIES IAS81714/14Copyright 2012 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
2、, 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.org ISSUED 2000-03R
3、EAFFIRMED 2012-01THIRD ANGLE PROJECTION CUSTODIAN: AE-8C2 FEDERAL SUPPLY CLASS 5940 AS81714/14SHEET 1 OF 7 SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthis report is entirely voluntary, andits appli
4、cability 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 berevised, reaffirmed, stabilized, orcancelled. SAE invites yourwrittencomments andsug
5、gestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS81714/14 RATIONALE AS81714/14 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. NOTICETHIS DOCUMENT HAS BEEN TAKEN DIRECTLY FROM U.S. MILITARY SPECIFIC
6、ATION MIL-T-81714/14C AND CONTAINS ONLY MINOR EDITORIAL AND FORMAT CHANGES REQUIRED TO BRING IT INTO CONFORMANCE WITH THE PUBLISHING REQUIREMENTS OF SAE TECHNICAL STANDARDS. THE INITIAL RELEASE OF THIS DOCUMENT IS INTENDED TO REPLACE MIL-T-81714/14C. ANY PART NUMBERS ESTABLISHED BY THE ORIGINAL SPEC
7、IFICATION REMAIN UNCHANGED.THE ORIGINAL MILITARY SPECIFICATION WAS ADOPTED AS AN SAE STANDARD UNDER THE PROVISIONS OF THE SAE TECHNICAL STANDARDS BOARD (TSB) RULES AND REGULATIONS (TSB 001) PERTAINING TO ACCELERATED ADOPTION OF GOVERNMENT SPECIFICATIONS AND STANDARDS. TSB RULES PROVIDE FOR (A) THE P
8、UBLICATION OF PORTIONS OF UNREVISED GOVERNMENT SPECIFICATIONS AND STANDARDS WITHOUT CONSENSUS VOTING AT THE SAE COMMITTEE LEVEL, AND (B) THE USE OF THE EXISTING GOVERNMENT SPECIFICATION OR STANDARD FORMAT.UNDER DEPARTMENT OF DEFENSE POLICIES AND PROCEDURES, ANY QUALIFICATION REQUIREMENTS AND ASSOCIA
9、TED QUALIFIED PRODUCTS LISTS ARE MANDATORY FOR DOD CONTRACTS. ANY REQUIREMENT RELATING TO QUALIFIED PRODUCTS LISTS (QPLS) HAS NOT BEEN ADOPTED BY SAE AND IS NOT PART OF THIS SAE TECHNICAL DOCUMENT.AEROSPACE STANDARD AS81714/14SHEET 2 OF 7 TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDTHRU TYPE
10、, LIGHT WEIGHT, SERIES I THE COMPLETE REQUIREMENTS FOR ACQUIRING THE RACK DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF SPECIFICATION MIL-T-81714.AEROSPACE STANDARD AS81714/14SHEET 3 OF 7 TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDTHRU TYPE, LIGHT WEIGHT, SERIES I
11、AEROSPACE STANDARD AS81714/14SHEET 4 OF 7 TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDTHRU TYPE, LIGHT WEIGHT, SERIES I AEROSPACE STANDARD AS81714/14SHEET 5 OF 7 TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDTHRU TYPE, LIGHT WEIGHT, SERIES I TABLE IAEROSPACE STANDARD AS81714/14SHEET 6
12、OF 7 TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDTHRU TYPE, LIGHT WEIGHT, SERIES I REQUIREMENTS:1. MATERIALS:RACK, END BRACKET AND LOCKING CLAMP; ALUMINUM ALLOY 6063, TEMPER T5 IN ACCORDANCE WITH QQ-A-200/9 OR STAINLESS STEEL IN ACCORDANCE WITH QQ-S-766.2. FINISH:ALUMINUM PARTS SHALL BE ANOD
13、IC COATED IN ACCORDANCE WITH MIL-A-8625, TYPE II, CLASS 2, BLACK. STAINLESS STEEL PARTS SHALL BE PASSIVATED IN ACCORDANCE WITH QQ-P-35.3. THE INDEXING INDICATOR SHALL BE MARKED ON THE SPECIFIED TOP RAIL ONLY.4. THE RACK SHALL BE DESIGNED FOR INSTALLATION OF MIL-T-81714/6, MIL-T-81714/7, MIL-T-81714/
14、8 AND MIL-T-81714/9 BLOCKS.5. THE RACK SHALL BE DESIGNED SO THAT THE ZONE NUMBERS ON THE BOTTOM RAIL ARE A REVERSE IMAGEOF THOSE SHOWN ON THE SPECIFIED TOP RAIL.6. LOCKING CLAMP SHALL BE DESIGNED TO BE PERMANENTLY RETAINED IN RACK. THE LOCKING CLAMPSCREW SHALL BE CROSS RECESSED IN ACCORDANCE WITH MS
15、9006, 8-32UNC-2A x .500, CORROSION-RESISTANT STEEL, PASSIVATED, SELF-LOCKING OR EQUIVALENT.7. THESE DIMENSIONS ARE TYPICAL OF EACH SIDE OF THE RAIL ASSEMBLY.8. RACKS ARE TO BE FREE OF ALL BURRS AND SHARP EDGES .015 MAX.9. ZONE NUMBERS AND ZONE LINES SHALL BE WHITE.AEROSPACE STANDARD AS81714/14SHEET
16、7 OF 7 TERMINAL JUNCTION SYSTEM, RACK ASSEMBLY, TRACK, FEEDTHRU TYPE, LIGHT WEIGHT, SERIES I NOTES:1. UNLESS OTHERWISE SPECIFIED, DIMENSIONS IN INCHES, TOLERANCES: DECIMALS .005.2. PART NUMBER: THE PART NUMBER CONSISTS OF THE LETTER M, SPECIFICATION SHEET NUMBER, ANDDASH NUMBER FROM TABLE I. WHEN PA
17、RTS ARE MADE OF ALUMINUM, ADD NO LETTER AFTER THE DASHNUMBER. WHEN PARTS ARE MADE FROM STAINLESS STEEL, ADD AN S AFTER THE DASH NUMBER.PART NUMBER EXAMPLE:M81714/14-1ALUMINUM FEEDTHRU TYPE RACK ASSEMBLY DASH NUMBER 1.3. METRIC EQUIVALENTS (TO THE NEAREST .01 MM) ARE GIVEN FOR GENERAL INFORMATION ONLY AND AREBASED UPON 1 INCH = 25.4 MM.4. INTERNATIONAL INTEREST, SEE SPECIFICATION MIL-T-81714.
