SAE AS 85075-2000 Tie down Assembly Helicopter Blade General Specification for《直升机桨叶的栓固装置 FSC 1730通用规范 用于代替2000年5月26日作废的MIL-T-85075A(AS)》.pdf
《SAE AS 85075-2000 Tie down Assembly Helicopter Blade General Specification for《直升机桨叶的栓固装置 FSC 1730通用规范 用于代替2000年5月26日作废的MIL-T-85075A(AS)》.pdf》由会员分享,可在线阅读,更多相关《SAE AS 85075-2000 Tie down Assembly Helicopter Blade General Specification for《直升机桨叶的栓固装置 FSC 1730通用规范 用于代替2000年5月26日作废的MIL-T-85075A(AS)》.pdf(12页珍藏版)》请在麦多课文档分享上搜索。
1、_ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2017 SAE International All rights reserved. No part of this p
3、ublication 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: +1 724-776-4970
4、 (outside USA)Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AS85075 AEROSPACESTANDARDAS85075 Issued 2000-03 Reaffirmed 2017-11 Tie Down Assembly, Helicopter
5、Blade, General Specification For FSC 1730 RATIONALE AS85075 has been reaffirmed to comply with the SAE Five-Year Review policy. NOTICEThis document has been taken directly from U.S. Military Specification MIL-T-85075A(AS) and contains only minor editorial and format changes required to bring it into
6、 conformance with the publishing requirements of SAE technical standards. The initial release of this document is intended to replace MIL-T-85075A(AS). Any part numbers established by the original specification remain unchanged.The original Military Specification was adopted as an SAE standard under
7、 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 publication of portions of unrevised government specifications and standards without consensus votin
8、g 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 associated qualified products lists are mandatory for DOD contracts. Any requirement relating to qualified
9、 products lists (QPLs) has not been adopted by SAE and is not part of this SAE technical document.1. SCOPE:1.1 Scope:This specification covers the tie down assemblies for use on helicopter blades.2. APPLICABLE DOCUMENTS:2.1 Government documents:2.1.1 Specifications, standards, and handbooks: The fol
10、lowing specifications, standards, and handbooks form a part of this specification to the extend specified herein. Unless otherwise specified, the issues of these documents shall be those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and supplement th
11、ereto, cited in the solicitation.SPECIFICATIONSFEDERALQQ-C-320 Chromium Plating (Electrodeposited)QQ-N-290 Nickel Plating (Electrodeposited)QQ-P-416 Plating, Cadmium (Electrodeposited)QQ-S-365 Silver Plating, Electrodeposited, General Requirements forMILITARYMIL-C-5541 Chemical Conversion Coatings o
12、n Aluminum AlloysMIL-H-6875 Heat Treatment of Steel, Process forMIL-A-8625 Anodic Coatings, for Aluminum and Aluminum AlloysMIL-T-10727 Tin Plating, Electrodeposited or Hot-dipped, for Ferrous and Nonferrous MetalsMIL-C-26074 Coatings, Electroless Nickel, Requirements forMIL-T-85075/1 Tie Down Assem
13、bly, Helicopter Blade, CH-46 HelicopterMIL-T-85075/2 Tie Down Assembly, Helicopter Blade, CH-53 HelicopterSTANDARDSMILITARYMIL-STD-105 Sampling Procedures and Tables for Inspection by AttributesMIL-STD-129 Marking for Shipment and StorageMIL-STD-130 Identification Marking of U.S. Military PropertyMI
14、L-STD-143 Standards and Specifications, Order of Precedence for the Selection ofMIL-STD-704 Aircraft Electric Power CharacteristicsSAE INTERNATIONAL AS85075 Page 2 of 12_ 2.1.1 (Continued):MIL-STD-794 Part and Equipment, Procedures for Packaging and Packing ofMIL-STD-810 Environmental Test MethodsMI
15、L-STD-831 Test Reports, Preparation ofMIL-STD-889 Dissimilar MetalsMILITARY HANDBOOKSMIL-HDBK-5 Aerospace Vehicle Structures, Metallic Materials and Elements for(Copies of specifications, standards, handbooks, drawings and publications required by manufacturers in connection with specific acquisitio
16、n functions should be obtained from the contracting activity or as directed by the contracting officer.)2.2 Other publications:The following document(s) form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of the documents which are DoD adopted sha
17、ll be those listed in the issue of the DoDISS specified in the solicitation. Unless otherwise specified, the issues of the documents not listed in the DoDISS shall be the issue of the nongovernment documents which is current on the date of the solicitation.AMERICAN SOCIETY FOR TESTING AND MATERIALS
18、(ASTM)B633-78 Electrodeposited Coatings of Zinc on Iron and Steel, Specification forAMS 5643 Steel Bars, Forgings, Tubing and Rings, Corrosion Resistant(Application for copies should be addressed to the American Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103.)2.3 Order o
19、f precedence:In the event of a conflict between the text of this specification and the references cited herein (except for associated detail specifications, specification sheets or MS standards), the text of this specification shall take precedence. Nothing in this specification, however, shall supe
20、rsede applicable laws and regulations unless a specific exemption has been obtained.3. REQUIREMENTS:3.1 Specification sheets:The individual item requirements shall be as specified herein and in accordance with the applicable specification sheets. In the event of any conflict between requirements of
21、this specification and the specification sheet, the latter shall govern.SAE INTERNATIONAL AS85075 Page 3 of 12_ 3.2 First article:When specified in the contract or purchase order (see 4.3 and 6.2.1), the contractor shall furnish sample tie down assemblies for first article inspection(s) and approval
22、. A new contractor, supplier, or manufacturer shall be required to complete a first article inspection (4.3).3.3 Materials:Materials used in the manufacture of tie down assemblies shall be of aircraft quality, suitable for the purpose, and shall conform to applicable Government specifications. Mater
23、ials conforming to contractors specifications may be used, provided they are equivalent to Government specifications with respect to operating characteristics and that a savings in weight or cost can be accomplished. Contractors specifications must be satisfactory to the Government and contain provi
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