SAE AMS 1536B-2001 Cleaner for Aircraft Components Cold Tank Type Solvent-Base《冷箱类溶剂型飞机零部件清洁剂》.pdf
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1、AEROSPACE MATERIAL SPECIFICATIONAMS 1536BIssued JAN 1981Revised APR 2001Superseding AMS 1536ACleaner for Aircraft ComponentsCold Tank Type, Solvent-Base1. SCOPE:1.1 Form: This specification covers a tank-type cleaner in the form of a liquid.1.2 Application: This cleaner has been used typically for r
2、emoving greasy soils, carbon, or rubber from painted and unpainted aircraft components, such as wheels and landing gear, by immersion in cleaner as supplied or as solvent diluted, but usage is not limited to such applications. This cleaner is not recommended for use on plastic or aircraft windows du
3、e to possible crazing.1.3 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 address the hazards which may be involved in such use. It is the sol
4、e 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.2. APPLICABLE DOCUMENTS: The issue of the following documents in effect on the date of the
5、 purchase order forms a part of this specification 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 canceled and no superseding document has been specified, the last publi
6、shed issue of that document shall apply.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
7、 any patent infringement arising therefrom, 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 2008 SAE International All rights r
8、eserved. No part of this publication 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 C
9、anada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org Reaffirmed JAN 2008AMS 1536B SAE AMS 1536B- 2 -2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.AMS 2470 Anodic Treatment of Aluminum A
10、lloys, Chromic Acid ProcessAMS 2475 Protective Treatments, Magnesium AlloysAMS 4037 Aluminum Alloy Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn (2024: -T3 Flat Sheet, -T351 Plate), Solution Heat TreatedAMS 4041 Aluminum Alloy Alclad, Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad
11、2024-T3 Flat Sheet, 1-1/2% Alclad 2024-T351 Plate)AMS 4049 Aluminum Alloy Sheet and Plate, Alclad, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet, -T651 Plate), Solution and Precipitation Heat TreatedAMS 4376 Magnesium Alloy Plate, 3.0Al - 1.0Zn (AZ31B-H26), Cold Rolled and Partially Anneale
12、dAMS 4911 Titanium Alloy Sheet, Strip, and Plate, 6Al - 4V, AnnealedAMS 5045 Steel Sheet and Strip, 0.25 max Carbon, Hard Temper2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.ASTM D 13 Spirits of TurpentineASTM D 93 Flash Point by Pensky-Martens C
13、losed TesterASTM D 4057 Manual Sampling of Petroleum and Petroleum ProductsASTM F 482 Total Immersion Corrosion Test for Tank-Type Aircraft Maintenance ChemicalsASTM F 485 Effects of Cleaners on Unpainted Aircraft SurfacesASTM F 502 Effects of Cleaning and Chemical Maintenance Materials on Painted A
14、ircraft SurfacesASTM F 519 Mechanical Hydrogen Embrittlement Evaluation of Plating Processes and Service EnvironmentsASTM F 1105 Preparing Aircraft Cleaning Compounds, Liquid Type, Solvent Base, for Storage Stability TestingASTM F 1110 Sandwich Corrosion TestASTM F 1111 Corrosion of Low Embrittling
15、Cadmium Plate by Aircraft Maintenance Chemicals2.3 U.S. Government Publications: Available from DODSSP, Subscription Services Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.MIL-C-306 Carbon, Black, Powdered, DryMIL-A-356 Asphaltum (Gilsonite)MIL-L-6082 Lubricating Oil, Aircraft R
16、eciprocating Engine (Piston)P-D-680 Dry Cleaning SolventAMS 1536B SAE AMS 1536B- 3 -3. TECHNICAL REQUIREMENTS: 3.1 Material: The composition of the cleaner shall be optional with the manufacturer but should contain water, biodegradable surfactants and/or soaps, emulsifiers, and solvents as required
17、to produce a homogeneous product meeting the requirements of 3.2.3.2 Properties: The cleaner shall conform to the following requirements; tests shall be performed in accordance with specified test methods on the cleaner supplied in concentrated form and at use dilution recommended by the manufacture
18、r.3.2.1 Corrosion of Metal Surfaces: 3.2.1.1 Sandwich Corrosion: Cleaner shall produce a rating not worse than 1, determined in accordance with ASTM F 1110.3.2.1.2 Total Immersion Corrosion: The cleaner shall neither cause evidence of corrosion nor a weight change of any test panel greater than show
19、n in Table 1, determined in accordance with ASTM F 482:3.2.1.3 Low-Embrittling Cadmium Plate: Test panels, coated with low-embrittling cadmium plate, shall not show a weight change greater than 0.3 mg/cm2 per 24 hours, determined in accordance with ASTM F 1111.3.2.2 Hydrogen Embrittlement: The clean
20、er shall be non-embrittling, determined in accordance with ASTM F 519, Type 1A, 1C, or 2a.3.2.3 Flash Point: Shall be not lower than 60 C (140 F), determined in accordance with ASTM D 93.TABLE 1 - Allowable Weight ChangeWeight ChangeTest Panel mg/cm2 per 24 hoursAMS 4037 Aluminum Alloy, anodized as
21、in AMS 2470 0.3AMS 4041 Aluminum Alloy 0.3AMS 4049 Aluminum Alloy 0.3AMS 4376 Magnesium Alloy, dichromate treated as in AMS 2475 0.2AMS 4911 Titanium Alloy 0.1AMS 5045 Carbon Steel 0.8AMS 1536B SAE AMS 1536B- 4 -3.2.4 Effect on Painted Surfaces: The cleaner shall neither decrease the hardness of the
22、 paint film 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 502.3.2.5 Effect on Unpainted Surfaces: The cleaner, tested in accordance with ASTM F 485, shall neither produce streaking nor
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