SAE AMS 1650C-2001 Polish Aircraft Metal《飞机金属抛光剂》.pdf
《SAE AMS 1650C-2001 Polish Aircraft Metal《飞机金属抛光剂》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 1650C-2001 Polish Aircraft Metal《飞机金属抛光剂》.pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACEMATERIALSPECIFICATIONAMS 1650CIssued JAN 1978Revised MAR 2001Superseding AMS 1650BPolish, Aircraft Metal1. SCOPE:1.1 Form: This specification covers a metal polish in the form of a liquid or paste.1.2 Application: This product has been used typically for polishing unpainted aluminum alloy s
2、urfaces of aircraft, but usage is not limited to such applications, but usage is not limited to such applications. This polish is not intended for use on plastic or painted surfaces.1.3 Classification: The metal polish covered by this specification is classified as follows Type 1 - LiquidType 2 - Pa
3、ste1.3.1 Unless a specific type is ordered, either Type 1 or Type 2 may be supplied.1.4 Safety - Hazardous Materials: While the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this specification does not addres
4、s 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 materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.SAE Technical Standards Boar
5、d 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 therefrom, is the sole responsibili
6、ty of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2008 SAE International All rights reserved. No part of this publication may be reproduced, stored in a
7、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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: Cust
8、omerServicesae.org SAE WEB ADDRESS: http:/www.sae.org Reaffirmed JAN 2008AMS 1650C SAE AMS 1650C- 2 -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 work to a
9、 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, 400 Commonwealth Drive, War
10、rendale, PA 15096-0001.AMS 4045 Aluminum Alloy Sheet and Plate, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, (7075; -T6 Sheet,-T651 Plate), Solution and Precipitation Heat TreatedAMS 4049 Aluminum Alloy Sheet and Plate, Alclad, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet, -T651 Plate), Solution and Pr
11、ecipitation Heat Treated2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.ASTM D 56 Flash Point by Tag Closed TesterASTM D 562 Consistency of Paints Using the Stormer ViscometerASTM F 483 Total Immersion Corrosion Test for Aircraft Maintenance Chemic
12、alsASTM F 484 Stress Crazing of Acrylic Plastics in Contact with Liquid or Semi-Liquid CompoundsASTM F 485 Effects of Cleaners on Unpainted Aircraft SurfacesASTM F 502 Effects of Cleaning and Chemical Maintenance Materials on Painted Aircraft SurfacesASTM F 1110 Sandwich Corrosion Test2.3 U.S. Gover
13、nment Publications: Available from DODSSP, Subscription Services Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.MIL-P-25690 Plastic, Sheets, and Parts, Modified Acrylic Base, Monolithic Crack Propagation Resistant3. TECHNICAL REQUIREMENTS: 3.1 Material: The formulation of the pol
14、ish shall be optional with the manufacturer except as restricted by 3.1.1 and 3.2.3.1.1 Toxicity: The polish shall not be hazardous as defined by OSHA regulations.AMS 1650C SAE AMS 1650C- 3 -3.2 Properties: The polish shall conform to the following requirements; tests shall be performed in accordanc
15、e with specified test methods on the product supplied:3.2.1 Flash Point: Shall be not lower than 60 C (140 F), determined in accordance with ASTM D 56.3.2.2 Viscosity (Type 1 Only): Shall be 50 to 70 Krebs units, determined in accordance with ASTM D 562 at 24 C 3 (75 F 5).3.2.3 Corrosion of Metal Su
16、rfaces: 3.2.3.1 Sandwich Corrosion: Polish shall produce a rating not worse than 1, determined in accordance with ASTM F 1110.3.2.3.2 Total Immersion Corrosion: Polish shall not cause a weight change greater than 0.3 mg/cm2per 24 hours for any panel of AMS 4045 and AMS 4049 aluminum alloy, determine
17、d in accordance with ASTM F 483. The product shall cause no evidence of etching, selective attack, or presence of corrosion products after any time period and only a slight dulling at the end of the test.3.2.4 Effect on Plastic: Polish shall not craze, stain, or discolor stretched MIL-P-25690 plasti
18、c, determined in accordance with ASTM F 484.3.2.5 Effect on Painted Surfaces: Polish shall neither decrease the hardness of the paint film by more than two pencil hardness levels nor shall it produce any staining or blistering of the paint film, determined in accordance with ASTM F 502.3.2.6 Effect
19、on Unpainted Surfaces: Polish, tested in accordance with ASTM F 485, shall neither produce streaking nor leave any stains on AMS 4045 and AMS 4049 aluminum alloys which require polishing to remove.3.2.7 Settling Number (Type 1 Only): Shall be not greater than 20, determined as in 3.2.7.1.3.2.7.1 Pla
20、ce 50 mL of well-mixed Type 1 polish in a 1 x 6 inch (25 x 152 mm) test tube. Cap the tube and allow the tube to remain undisturbed in an upright position for not less than 24 hours. After the settling period, invert the test tube repeatedly until the solid matter is dislodged and begins to disperse
21、 evenly. Record the number of inversions as the settling number.3.2.8 Low-Temperature Stability: The polish shall be restorable to its original appearance by vigorous shaking or by stirring after being temperature cycled as in 3.2.8.1.AMS 1650C SAE AMS 1650C- 4 -3.2.8.1 Place approximately 100 mL of
22、 Type 1 polish or 100 grams of Type 2 polish in each of two 125 mL wide-mouth Pyrex jars and stopper the jars. Set aside one of the jars at 20 to 25 C (68 to 77 F) for the duration of the test period as a control sample. Place the second jar containing the test sample in a cold box maintained at -10
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS1650C2001POLISHAIRCRAFTMETAL 飞机 金属 抛光 PDF

链接地址:http://www.mydoc123.com/p-1020522.html