SAE AMS 1374A-1992 Remover Polyurethane Epoxy Paint Alkaline Hot-Tank Type《热箱式碱式聚氨基甲酯 环氧涂料清洗剂》.pdf
《SAE AMS 1374A-1992 Remover Polyurethane Epoxy Paint Alkaline Hot-Tank Type《热箱式碱式聚氨基甲酯 环氧涂料清洗剂》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 1374A-1992 Remover Polyurethane Epoxy Paint Alkaline Hot-Tank Type《热箱式碱式聚氨基甲酯 环氧涂料清洗剂》.pdf(7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 entirelyvoluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefro
2、m, is the sole responsibility 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 2004 SAE InternationalAll rights reserved. No part of this publication may be
3、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: 724-776-4970 (outside USA)Fax: 724-
4、776-0790Email: custsvcsae.orgSAE WEB ADDRESS: http:/www.sae.orgRemover, Polyurethane/Epoxy PaintAlkaline, Hot-Tank Type1. SCOPE:1.1 Form: This specification covers two types of paint remover in the form of a liquid.1.2 Application: This product has been used typically as a stripper for polyurethane/
5、epoxy painted aircraft wheels and landing gear, but usage is not limited to such applications.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
6、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 materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.1.3 Classification
7、: Paint remover covered by this specification is classified as follows:Type 1, Class 1 - Phenolic, SealedType 1, Class 2 - Phenolic, UnsealedType 2, Class 1 - Non-Phenolic, SealedType 2, Class 2 - Non-Phenolic, Unsealed1.3.1 If a specific type and class is not specified, either type and class may be
8、 supplied.AEROSPACE MATERIAL SPECIFICATIONAMS 1374AIssued JUL 1986Revised OCT 1992Reaffirmed FEB 2004Superseding AMS 1374AMS 1374A SAE AMS 1374A- 2 -2. APPLICABLE DOCUMENTS:The following publications form a part of this specification to the extent specified herein. The latest issue of SAE publicatio
9、ns shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order.2.1 SAE Publications:Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.AMS 2471 Anodic Treatment of Aluminum Alloys, Sulfuric Acid Process, Undyed CoatingAMS
10、2475 Protective Treatments, Magnesium AlloysAMS 2825 Material Safety Data SheetsAMS 4037 Aluminum Alloy Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate), Solution Heat TreatedAMS 4041 Aluminum Alloy Sheet and Plate, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Al
11、clad 2024-T3 Flat Sheet; 1-1/2% Alclad 2024-T351 Plate)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 Shee
12、t, -T651 Plate), Solution and Precipitation Heat TreatedAMS 4377 Magnesium Alloy Sheet and Plate, 3.0Al - 1.0Zn (AZ31B-H24), Cold Rolled, Partially AnnealedAMS 4911 Titanium Alloy Sheet, Strip, and Plate, 6Al - 4V, AnnealedMAM 4911 Titanium Alloy Sheet, Strip, and Plate, 6Al - 4V, AnnealedAMS 5045 S
13、teel Sheet and Strip, 0.25 Carbon, Maximum, Hard Temper2.2 ASTM Publications:Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.ASTM D 93 Flash Point by Pensky-Martens Closed TesterASTM D 1568 Sampling and Chemical Analysis of Alkylbenzene SulfonatesASTM F 483 Total Immersi
14、on Corrosion Test for Aircraft Maintenance ChemicalsASTM F 519 Mechanical Hydrogen Embrittlement Testing of Plating Processes and Aircraft Maintenance ChemicalsASTM F 1110 Sandwich Corrosion TestASTM F 1111 Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance ChemicalsAMS 1374A SAE AMS
15、 1374A- 3 -2.3 U.S. Government Publications:Available from DODSSP, Subscription Services Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.MIL-P-23377 Primer Coating, Epoxy Polyamide, Chemical and Solvent ResistantMIL-C-83286 Coating, Polyurethane, for Aircraft ApplicationsMIL-STD-2
16、073-1 DOD Materiel, Procedures for Development and Application of Packaging Requirements 3. TECHNICAL REQUIREMENTS: 3.1 Material: Shall be an alkaline liquid meeting the requirements of 3.2. Type 1 shall contain phenols, cresols, or both. Type 2 shall contain no phenols or cresols. Class 1 remover s
17、hall contain a water or oil seal of not more than 15% by volume; Class 2 remover shall not contain a seal.3.2 Properties: The product shall conform to the following requirements; tests shall be performed in accordance with specified test methods on the product supplied in concentrated form:3.2.1 Cor
18、rosion of Metal Surfaces: 3.2.1.1 Total Immersion Corrosion: The product shall neither produce evidence of corrosion of the panels nor cause a weight change of any panel greater than that shown in Table 1, determined in accordance with ASTM F 483:TABLE 1 - Maximum Immersion Corrosion Weight ChangeTe
19、st PanelWeight Changemg/cm2per 24 hoursAMS 4037 Aluminum Alloy 0.3AMS 4041 Aluminum Alloy 0.3AMS 4045 Aluminum Alloy 0.3AMS 4049 Aluminum Alloy 0.3AMS 4377 Magnesium Alloy, dichromate treated as in AMS 2475 0.2AMS 4911 or MAM 4911 Titanium Alloy 0.1AMS 5045 Carbon Steel 0.8AMS 1374A SAE AMS 1374A- 4
20、 -3.2.1.2 Sandwich Corrosion: Specimens shall pass the sandwich corrosion test, determined in accordance with ASTM F 1110.3.2.1.3 Low-Embrittling Cadmium Plate: Panels plated with low-embrittling cadmium plate shall not show a weight change greater than 0.3 mg/cm2per 24 hours, determined in accordan
21、ce with ASTM F 1111.3.2.2 Hydrogen Embrittlement: The product shall be non-embrittling, determined in accordance with ASTM F 519, Types 1a, 1c, or 2a, at recommended operating temperature.3.2.3 Flash Point: Shall be not lower than 60 C (140 F), determined in accordance with ASTM D 93, and should exc
22、eed the maximum operating temperature by at least 5 C (9 F).3.2.4 Performance: The product, used in accordance with manufacturers recommendations, shall remove epoxy polyamine/aliphatic isocyanate urethane, epoxy polyamine/epoxy polyamide, or both topcoat paint systems from substrates, determined in
23、 accordance with 4.5.1. Product shall remove not less than 90% of the paint within one hour without brushing.3.2.5 Storage Stability: Concentrated product, stored for six months in a 1 gallon (4 L) glass bottle, shall show no visible evidence of deterioration and shall conform to the other requireme
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