SAE AMS 1534C-2013 Cleaner Aircraft Glass Window《航空器玻璃窗清洁剂》.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 2013 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:/www.sae.org/technical/standards/AMS1534C AEROSPACE MATERIAL SPECIFICATION AMS1534 REV. C Issued 1983-01 Reaffirme
5、d 2004-02 Revised 2013-11 Superseding AMS1534B Cleaner, Aircraft Glass Window RATIONALE Changes in this revision include format/editorial changes as well update to specification revisions. 1. SCOPE 1.1 Form This specification covers two types of aircraft glass window cleaners in the form of a ready-
6、to-use liquid. 1.2 Application Primarily for removing soils, contaminants, and residues from aircraft glass windows by manual application. 1.3 Classification The cleaners covered by this specification shall be of the following types as ordered: Type I - Regular Type II - Antifogging 1.4 Safety - Haz
7、ardous 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 address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure
8、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. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purchase order forms a part of this sp
9、ecification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall appl
10、y. SAE INTERNATIONAL AMS1534C Page 2 of 6 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2350 Standards and Test Methods AMS4041 Aluminum Alloy, Alclad
11、Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn, Alclad 2024 and 1-1/2% Alclad 2024, -T3 Flat Sheet; 1-1/2% Alclad 2024-T351 Plate AMS4049 Aluminum Alloy Sheet and Plate, Alclad, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet, -T651 Plate), Solution and Precipitation Heat Treated AMS4376 Magnesium A
12、lloy Plate, 3.0A1 - 1.0Zn (AZ31B-H26), Cold Rolled and Partially Annealed ARP1511 Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832
13、-9585, www.astm.org. ASTM D 56 Flash Point by Tag Closed Tester ASTM D 1015 Freezing Points of High-Purity Hydrocarbons ASTM D 1193 Reagent Water ASTM D 1568 Sampling and Chemical Analysis of Alkylbenzene Sulfonates ASTM F 483 Total Immersion Corrosion Test for Aircraft Maintenance Chemicals ASTM F
14、484 Stress Crazing of Acrylic Plastics in Contact with Liquid or Semi-Liquid Compounds ASTM F 485 Effects of Cleaners on Unpainted Aircraft Surfaces ASTM F 502 Effects of Cleaning and Chemical Maintenance Materials on Painted Aircraft Surfaces ASTM F 503 Preparing Aircraft Cleaning Compounds, Liquid
15、 Type, for Storage Stability Testing ASTM F 519 Mechanical Hydrogen Embrittlement Testing of Plating Processes and Aircraft Maintenance Chemicals ASTM F 1111 Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals 2.3 U.S. Government Publications Availab
16、le from DLA Document Services, Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: (215) 697-6257, http:/quicksearch.dla.mil/. MIL-STD-2073-1 Standard Practice for Military Packaging MIL-STD-870 Cadmium Plating, Low Embrittlement, Electro-Deposition FED-STD-313 Material Safety Data S
17、heets, Preparation of SAE INTERNATIONAL AMS1534C Page 3 of 6 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall be optional with the manufacturer, shall be a homogenous liquid suitable for the intended usage, and shall meet the requirements of 3.2. 3.2 Properties Cleaner shall conform to the following
18、requirements; tests shall be performed in accordance with specified test methods on the product supplied: 3.2.1 Corrosion of Metal Surfaces 3.2.1.1 Total Immersion Corrosion The cleaner shall neither show evidence of corrosion nor cause a weight change of any test panel greater than the following, d
19、etermined in accordance with ASTM F 483: TABLE 1 Test Panel Weight Change mg/cm2per 24 hours AMS4041 Aluminum Alloy 0.3 AMS4049 Aluminum Alloy 0.4 AMS4376 Magnesium Alloy 0.8 3.2.1.2 Low-Embrittling Cadmium Plate Test panels, coated with low-embrittling cadmium plate, shall not show a weight change
20、greater than 1.0 mg/cm2per 24 hours, determined in accordance with ASTM F 1111. 3.2.2 Effect on Plastics The cleaner shall not craze, stain, or discolor transparent plastics, determined in accordance with ASTM F 484. 3.2.3 Effect on Painted Surfaces The cleaner shall neither decrease the hardness of
21、 polyurethane or other paint films specified by purchaser by more than two pencil hardness levels nor shall it produce any streaking, discoloration, or blistering of the paint film, determined in accordance with ASTM F 502. 3.2.4 Effect on Unpainted Surfaces The cleaner, tested in accordance with AS
22、TM F 485, shall neither produce streaking nor leave any stains requiring polishing to remove. 3.2.5 Hydrogen Embrittlement The product shall be non-embrittling, determined in accordance with ASTM F 519, utilizing Type 1a, 1c, or 2a specimens, cadmium plated in accordance with MIL-STD-870, Class 1, T
23、ype I. Type 1a and Type 1c specimens shall be loaded to 45% of the predetermined notch fracture strength, and Type 2a specimens loaded to 80% of the yield strength. The entire 2a stressed specimen, or just the notched area of the 1a and 1c stressed specimen, shall be immersed continuously in the sol
24、ution under test for 150 hours at a temperature between 20 and 30 C (68 to 86 F). 3.2.6 Flash Point Shall be not lower than 158 F (70 C), determined in accordance with ASTM D 56. SAE INTERNATIONAL AMS1534C Page 4 of 6 3.2.7 Freeze Point Shall be determined in accordance with ASTM D 1015 and the resu
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