SAE AMS 1531D-2008 Cleaner for Aircraft Exterior Surfaces Wipe-On Wipe-Off Containing Suspended Abrasive Solids《涂和擦洗飞行器外表面用含悬浮擦洗固体颗粒的清洁剂》.pdf
《SAE AMS 1531D-2008 Cleaner for Aircraft Exterior Surfaces Wipe-On Wipe-Off Containing Suspended Abrasive Solids《涂和擦洗飞行器外表面用含悬浮擦洗固体颗粒的清洁剂》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 1531D-2008 Cleaner for Aircraft Exterior Surfaces Wipe-On Wipe-Off Containing Suspended Abrasive Solids《涂和擦洗飞行器外表面用含悬浮擦洗固体颗粒的清洁剂》.pdf(6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 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 AMS1531D AEROSPACE MATERIAL SPECIFICATION Issued 1978-01 Revised 2008-03 Superseding AMS1531C Cleaner for Aircraft Exterior Surfaces Wipe-On, Wipe-Off, Containing Suspended Abrasive Solids RATIONALE This specification
5、 was revised to meet current verbiage required by SAE standards with no technical changes. 1. SCOPE 1.1 Form This specification covers a water-soluble cleaner containing suspended abrasive solids in the form of a ready-to-use liquid. 1.2 Application This cleaner has been used typically for removing
6、resistant soils from exhaust areas of exterior metal and painted surfaces of aircraft by a wipe-on, wipe-off procedure not requiring a water rinsing operation, but usage is not limited to such applications. NOT recommended for use on stretched or cast acrylic plastic. 1.3 Safety - Hazardous Material
7、s 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 familiarity wi
8、th 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 specification to
9、 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 apply. 2.1 SAE Pub
10、lications 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. AMS2475 Protective Treatments, Magnesium Alloys AMS4049 Aluminum Alloy, Sheet and Plate, Alclad, 5.6Zn - 2.5Mg - 1.6Cu
11、- 0.23Cr (Alclad 7075; -T6 Sheet, -T651 Plate), Solution and Precipitation Heat Treated SAE AMS1531D - 2 - 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 AMS5045 Steel, Sheet a
12、nd Strip, 0.25 Carbon, Maximum, Hard Temper 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM D 56 Flash Point by Tag Closed Tester ASTM D 1404 Estimation of Deleterious Particles in
13、Lubricating Grease ASTM F 483 Total Immersion Corrosion Test for Aircraft Maintenance 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 Main
14、tenance Materials on Painted Aircraft Surfaces ASTM F 519 Mechanical Hydrogen Embrittlement Testing of Plating Processes and Aircraft Maintenance Chemicals ASTM F 1104 Preparing Aircraft Cleaning Compounds, Liquid Type, Water Base, for Storage Stability Testing ASTM F 1110 Sandwich Corrosion Test AS
15、TM 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.mil/q
16、uicksearch/. MIL-PRF-23377 Primer Coating, Epoxy Polyamide, Chemical and Solvent Resistant MIL-PRF-25690 Plastic, Sheets and Parts, Modified Acrylic Base, Monolithic, Crack Propagation Resistant MIL-PRF-85285 Coating, Polyurethane, Aircraft and Supply Equipment MIL-STD-870 Cadmium Plating, Low Embri
17、ttlement, Electrodeposition 3. TECHNICAL REQUIREMENTS 3.1 Material Shall consist of a mixture of selected solvents, mild abrasives, detergents, soaps, and water, either with or without thickening agents, to produce a product meeting the requirements of 3.2. 3.2 Properties The cleaner shall conform t
18、o the following requirements; tests shall be performed in accordance with specified test methods on the product as-received in concentrated form: 3.2.1 Corrosion of Metal Surfaces 3.2.1.1 Sandwich Corrosion Specimens, after test, cleaner shall produce a rating not worse than 1, determined in accorda
19、nce with ASTM F 1110. 3.2.1.2 Total Immersion Corrosion The product shall neither show evidence of corrosion nor cause a weight change of any test panel greater than that shown in Table 1, determined in accordance with ASTM F 483: SAE AMS1531D - 3 - TABLE 1 - MAXIMUM IMMERSION WEIGHT CHANGE Test Pan
20、el Material Weight Change mg/cm2per 24 hours AMS4049 Aluminum Alloy 0.3 AMS4376 Magnesium Alloy, Dichromate Treated as in AMS2475 0.2 AMS4911 Titanium Alloy 0.1 AMS5045 Carbon Steel 0.8 3.2.1.3 Low-Embrittling Cadmium Plate Panels coated with low-embrittling cadmium plate shall not show a weight cha
21、nge greater than 0.3 mg/cm2per 24 hours, determined in accordance with ASTM F 1111. 3.2.2 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. Typ
22、e 1a and 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 solution under tes
23、t for 150 hours at a temperature between 68 to 86 F (20 to 30 C). 3.2.3 Flash Point Shall be not lower than 140 F (60 C), determined in accordance with ASTM D 56. 3.2.4 Effect on Plastics The product shall not craze, stain, or discolor MIL-PRF-25690 stretched acrylic plastic, determined in accordanc
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