1、 AEROSPACE STANDARD (R) CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 5 THRU 15 AMP, TYPE I AS24510 Copyright 2007 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, mechanica
2、l, 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: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 1999-07REVISED 2007-04
3、 THIRD ANGLE PROJECTION CUSTODIAN: SAE AE-8/AE-8B1 REV. A FEDERAL SUPPLY CLASS5925 AS24510 SHEET 1 OF 4 REV. A PROCUREMENT SPECIFICATION: AS58091SAE TechnicalStandards Board Rules provide that: “This report is published by SAE toadvance thestate of technical andengineering sciences. Theuse of thisre
4、port is entirely voluntary, andits applicabilityandsuitability forany particularuse,including any patent infringement arising therefrom, is thesole responsibility oftheuser.” SAE reviews each technical report at least every five yearsat which time it may be reaffirmed, revised, orcancelled.SAE invit
5、es yourwritten commentsandsuggestions. RATIONALE 5 YEAR REVIEW AND CLEAN UP DRAWING TO ENSURE PRODUCT IS AS SUPPLIED. THE REQUIREMENTS FOR ACQUIRING THE PRODUCT(S) DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION SHEET AND THE ISSUE OF THE FOLLOWING SPECIFICATION LISTED IN THAT ISSUE OF THE DODI
6、SS SPECIFIED IN THE SOLICITATION: SAE AS58091. FIGURE 1 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD (R) CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 5 THRU 15 AMP, TYPE I
7、AS24510 REV. A AS24510 SHEET 2 OF 4 REV.A FIGURE 2 REQUIREMENTS: 1. THE PART NUMBERS FOR CIRCUIT BREAKERS IN ACCORDANCE WITH THIS SPECIFICATION SHALL CONFORM TO THE EXAMPLE BELOW. WHEN A DESIGNATOR IS NOT APPLICABLE IT SHALL BE OMITTED FROM THE PART NUMBER. 2. CIRCUIT BREAKERS ARE RECYCLING AS DEFIN
8、ED IN AS58091. 3. .425 MIN. TYP. CLEARANCE FROM CENTERLINE OF SCREW TO CASE. 4. MOUNTING NUT TORQUE: 65 INCH-POUNDS MAXIMUM. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD (R) CIR
9、CUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 5 THRU 15 AMP, TYPE I AS24510 REV. A AS24510 SHEET 3 OF 4 REV.A TABLE 1 TABLE 2 TABLE 3 TABLE 4 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPAC
10、E STANDARD (R) CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 5 THRU 15 AMP, TYPE I AS24510 REV. A AS24510 SHEET 4 OF 4 REV.A QUALIFICATION: QUALIFICATION IS REQUIRED FOR U.S. GOVERNMENT PROCUREMENT. THE QUALIFIED PRODUCT LIST (QPL) QUALIFICATION ACTIVITY FOR U.S. DEPARTMENT OF DEFENSE PROCUREMEN
11、T PURPOSES, NAVAL AIR SYSTEMS COMMAND (CODE 4.4.5.3) 22229 ELMER ROAD, BUILDING 2360, PATUXENT RIVER, MD 20670-1900. NOTES: 1. DIMENSIONS ARE IN INCHES UNLESS OTHERWISE SPECIFIED. TOLERANCE: DECIMALS .031; ANGLES 2. 2. PHANTOM LINES INDICATE THAT CONTOUR IS OPTIONAL PROVIDED MAXIMUM DIMENSIONS ARE N
12、OT EXCEEDED. 3. VOLTAGE RATING: 28 VDC NOMINAL OR 115 V 400 Hz NOMINAL. 4. THE 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. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
