SAE AMS 2420E-2017 Plating of Aluminum for Solderability Zinc Immersion Pre-Treatment Process.pdf
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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: +1 724-776-497
4、0 (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/AMS2420E AEROSPACE MATERIAL SPECIFICATION AMS2420 REV. E Issued 1957-07 Reaffirmed 2012-08 Revi
5、sed 2017-11 Superseding AMS2420D Plating of Aluminum for Solderability Zinc Immersion Pre-Treatment Process RATIONALE AMS2420E results from a Five-Year Review and update, with changes made to Ordering Information and paragraphs 4.2.1, 4.2.2, 4.2.3, 4.3.1.1, 4.3.2, and 4.3.4.1. ORDERING INFORMATION:
6、The following information shall be provided to the plating processor by the purchaser. 1) Purchase order shall specify not less than the following: AMS2420E Quantity of pieces to be plated Permissible electrical contact locations, if not specified (see 3.2.2.1) Class of plating desired (see 1.3) Pla
7、ting thickness desired if other than that specified in 3.3.1 Basis metal to be plated Reflow, when necessary (see 3.2.4) 2) Parts manufacturing operations such as heat treating, forming, joining and media finishing can affect the condition of the substrate for plating, or if performed after plating,
8、 could adversely affect the plated part. The sequencing of these types of operations should be specified by the cognizant engineering organization and is not controlled by this specification. SAE INTERNATIONAL AMS2420E Page 2 of 7 1. SCOPE 1.1 Purpose This specification covers the requirements for p
9、reparation of aluminum and aluminum alloys for soldering by zinc immersion pre-treatment followed by copper plating and tin or tin-zinc alloy plating. 1.2 Application This process has been used typically to facilitate soldering of aluminum and aluminum alloy mechanical and electronic instrument encl
10、osures, but usage is not limited to such applications. 1.3 Classification The final plating shall be one of the following. When a Class is not specified, Class 1 shall apply. Class 1 - Tin Plating Class 2 - Tin-Zinc Plating 1.4 Safety-Hazardous Materials While the materials, methods, applications, a
11、nd processes described or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous mate
12、rials and to take necessary precautionary measures to ensure the health and safety of all personnel involved. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may w
13、ork to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been canceled and no superseding document has been specified, the last published issue of that document shall apply. 2.1 SAE Publications Available from SAE International, 400 C
14、ommonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2408 Plating, Tin AMS2418 Plating, Copper AMS2434 Plating, Tin-Zinc Alloy AMS4751 Tin - Lead Eutectic, 63Sn - 37Pb ARP1917 Clarification of Terms Used in Aerospac
15、e Metals Specifications ARP4992 Periodic Test for Processing Solutions AS2390 Chemical Process Test Specimen Material SAE INTERNATIONAL AMS2420E Page 3 of 7 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9
16、585, www.astm.org. ASTM B253 Preparation of Aluminum Alloys for Electroplating ASTM B487 Measurement of Metal and Oxide Coating Thickness by Microscopical Examination of Cross Section ASTM B567 Measurement of Coating Thickness by the Beta Backscatter Method ASTM B568 Measurement of Coating Thickness
17、 by X-Ray Spectrometry ASTM B571 Qualitative Adhesion Testing of Metallic Coatings 3. TECHNICAL REQUIREMENTS 3.1 Preparation 3.1.1 Cleaning and Deoxidizing Parts shall have clean, water break-free surfaces and shall be deoxidized to prepare for zinc immersion coating as a pretreatment for plating. 3
18、.2 Procedure 3.2.1 Zinc Immersion Coating Parts shall be processed in accordance with ASTM B253 or other method acceptable to purchaser. 3.2.2 Plating Parts shall be pre-plated with a brass or copper strike from an alkaline solution, followed by electrodeposition of copper in accordance with AMS2418
19、. When Class 1 is specified, parts shall receive a final deposit of tin in accordance with AMS2408. When Class 2 is specified, parts shall receive a final deposit of a tin-zinc alloy in accordance with AMS2434 with a maximum of 25% zinc. 3.2.2.1 Except for barrel plating, electrical contact points s
20、hall be as follows. For parts which are to be plated all over, locations shall be acceptable to purchaser; for parts which are not to be plated all over, locations shall be in areas on which plating is not required. 3.2.3 Spotting-in is not permitted. 3.2.4 When reflow is specified for tin plate the
21、 deposit shall be reflowed to a bright, shiny appearance by immersion in hot oil at 490 to 525 F (254 to 274 C). 3.3 Properties The deposit shall conform to the following requirements: 3.3.1 Thickness Shall be as follows, determined in accordance with ASTM B487, ASTM B567, ASTM B568, or other method
22、 acceptable to purchaser. 3.3.1.1 Copper Plate Shall be 0.0003 to 0.0007 inch (8 to 18 m). SAE INTERNATIONAL AMS2420E Page 4 of 7 3.3.1.2 Tin or Tin-Zinc Alloy Plate Shall be 0.0003 to 0.0005 inch (8 to 13 m). 3.3.1.3 The plate shall be substantially uniform in thickness on significant surfaces, exc
23、ept that build-up at exterior corners or edges will be permitted provided finished drawing dimensions are met. 3.3.1.4 No requirements are established for minimum plate thickness on surfaces of holes, recesses, internal threads, contact areas of parts plated all over, and other areas where a control
24、led deposit cannot be obtained under normal plating conditions, but such surfaces shall not be masked to prevent plating. The resultant thickness shall be considered only when such surfaces can be touched by a sphere 0.75 inch (19.0 mm) in diameter. 3.3.2 Heat Resistance Parts shall show no visual e
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