SAE AMS 1523B-2008 Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type Water-Base《飞行器外表面用水基凝胶清洁剂》.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 theref
2、rom, 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 reserved. No part of this publication ma
3、y 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: 724-776-4970 (outside USA)
4、Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org AMS1523B AEROSPACE MATERIAL SPECIFICATION Issued 1992-01 Revised 2008-03 Superseding AMS1523A Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type, Water-Base RATIONALE This specification was revised to meet c
5、urrent verbiage required by SAE standards with no technical changes. 1. SCOPE 1.1 Form This specification covers a thickened, water-base, type cleaner in the form of a gel. 1.2 Application This cleaner has been used typically for removing soils from exterior surfaces of aircraft, such as landing gea
6、rs, wheel wells, and flap cavities, but usage is not limited to such applications. 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
7、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. 2. APPLICABLE DOCUMENTS The i
8、ssue 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 subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled a
9、nd no superseding document has been specified, the last published issue of that document shall apply. 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. AMS247
10、0 Anodic Treatment of Aluminum Alloys, Chromic Acid Process AMS2475 Protective Treatments, Magnesium Alloys AMS4037 Aluminum Alloy, Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate), Solution Heat Treated SAE AMS1523B - 2 - AMS4041 Aluminum Alloy, Alclad Sheet and Plate, 4.
11、4Cu - 1.5Mg - 0.60Mn, Alclad 2024 and 1-1/2% Alclad 2024, -T3 Flat Sheet; 1-1/2% Alclad 2024-T351 Plate AMS4045 Aluminum Alloy Sheet and Plate, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, 7075: (-T6 Sheet, -T651 Plate), Solution and Precipitation Heat Treated AMS4049 Aluminum Alloy, Sheet and Plate, Alclad, 5.6
12、Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet; -T651 Plate), Solution and Precipitation Heat Treated AMS4376 Plate, Magnesium Alloy, 3.0Al - 1.0Zn - 0.20Mn (AZ31B-H26), Cold Rolled and Partially Annealed AMS4911 Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V, Annealed AMS5044 Steel, Sheet a
13、nd Strip, 0.15 Carbon, Maximum, Half Hard Temper AMS5046 Carbon Steel, Sheet, Strip, and Plate, (SAE 1020 and 1025), Annealed AMS-P-83310 Plastic Sheet, Polycarbonate, Transparent 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 194
14、28-2959, Tel: 610-832-9585, www.astm.org. ASTM D 93 Flash Point by Pensky-Martens Closed Cup Tester ASTM D 471 Rubber Property - Effect of Liquids ASTM D 1193 Reagent Water ASTM D 1568 Sampling and Chemical Analysis of Alkylbenzene Sulfonates ASTM F 483 Total Immersion Corrosion Test for Aircraft Ma
15、intenance Chemicals ASTM F 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 519 Mechanical Hydroge
16、n Embrittlement Testing of Plating Processes and Aircraft Maintenance Chemicals ASTM F 1080 Determining the Consistency of Viscous Liquids Using a Consistometer ASTM F 1104 Preparing Aircraft Cleaning Compounds, Liquid Type, Water Base, for Storage Stability Testing ASTM F 1110 Sandwich Corrosion Te
17、st ASTM F 1111 Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals 2.3 U.S. Government Publications Available from the Document Automation and Production Service (DAPS), Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6257, http:/assist.daps.dla.m
18、il/quicksearch/. MIL-PRF-25690 Plastic, Sheets and Parts, Modified Acrylic Base, Monolithic, Crack Probagation Resistant MIL-STD-870 Cadmium Plating, Low Embrittlement, Electrodeposition 3. TECHNICAL REQUIREMENTS 3.1 Material The composition of the cleaner shall be optional with the manufacturer, bu
19、t should contain water, biodegradable surfactants, emulsifiers, inhibitors and thickeners to produce a thickened or gel-type product meeting the requirements of 3.2. Cleaner shall not contain aliphatic or aromatic solvents, such as kerosene solvents. 3.2 Properties Cleaner shall conform to the follo
20、wing requirements; tests shall be performed in accordance with specified test methods on the product supplied in concentrated form: 3.2.1 Consistency Cleaner shall flow to a point between 13 and 23 centimeters in 10 seconds, determined in accordance with ASTM F 1080. SAE AMS1523B - 3 - 3.3 Corrosion
21、 of Metal Surfaces 3.3.1.1 Sandwich Corrosion Specimens of AMS4045 and AMS4049, after testing in accordance with ASTM F 1110, shall not show a corrosion rating worse than one or worse than that on control panels tested using ASTM D 1193, Type IV, water. 3.3.1.2 Total Immersion Corrosion Cleaner shal
22、l neither cause evidence of corrosion nor a weight change of any test panel greater than shown in Table 1, determined in accordance with ASTM F 483: TABLE 1 - MAXIMUM WEIGHT CHANGE Panel Weight Change mg/cm2per 24 hours AMS4037 Aluminum Alloy, anodized as in AMS2470 0.3 AMS4041 Aluminum Alloy 0.3 AM
23、S4049 Aluminum Alloy 0.3 AMS4376 Magnesium Alloy, dichromate treated as in AMS2475 0.2 AMS4911 Titanium Alloy 0.1 AMS5044 Steel 0.8 3.3.1.3 Low-Embrittling Cadmium Plate Panels coated with low-embrittling cadmium plate shall not show a weight change greater than 0.3 mg/cm2per 24 hours, determined in
24、 accordance with ASTM F 1111. 3.3.2 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, Type I. Type 1a and 1c specimens shall be loaded to 45% of the pr
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