SAE AMS 1640C-2011 Corrosion Removing Compound for Aircraft Surfaces《飞机表面用腐蚀去除剂》.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 2011 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/AMS1640C AEROSPACE MATERIAL SPECIFICATION AMS1640 REV. C Issued 1979-01 Reaffirme
5、d 2000-06 Revised 2011-12 Superseding AMS1640B Corrosion Removing Compound for Aircraft Surfaces RATIONALE Normal specification review. 1. SCOPE 1.1 Form This specification covers a corrosion-removing compound in the form of a liquid concentrate. 1.2 Application This method is primarily concerned wi
6、th the removal of pitting corrosion and heavy surface oxidation from exterior aluminum surfaces of aircraft. 1.3 Precautions Compounds meeting the requirements of this specification may cause hydrogen embrittlement of high-strength steels and will remove cadmium plate. 1.4 Safety - Hazardous Materia
7、ls 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. SAE AMS1640
10、C 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 AMS2825 Material Safety Data Sheets AMS4049 Aluminum Alloy,
11、 Sheet and Plate, Alclad, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet -T651 Plate), Solution and Precipitation Heat Treated AMS-QQ-A-250/4 Aluminum Alloy 2024, Plate and Sheet 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken,
12、 PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM D 93 Flash Point by Pensky-Martens Closed Cup Tester ASTM D 1193 Reagent Water ASTM D 1568 Sampling and Chemical Analysis of Alkybenzene Sulfonates ASTM D 2196 Viscosity Measurements and Rheological Properties of Non-Newtonian Materials by Rotati
13、onal (Brookfield) Viscometer 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 502 Effects of Cleaning and Chemical Maintenance Materials on Plated Aircraft Surfaces ASTM F
14、 503 Preparing Aircraft Cleaning Compounds, Liquid Type, for Storage Stability Testing ASTM F 2111 Measuring Intergranular Attack or End Grain Pitting on Metals Caused by Aircraft Chemical Processes 2.3 U. S. Government Publications Available from the Document Automation and Production Service (DAPS
15、), Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6257, http:/assist.daps.dla.mil/quicksearch/. MIL-PRF-25690 Plastic, Sheets and Parts, Modified Acrylic Base, Monolithic, Crack Propagation Resistant MIL-STD-794 Parts and Equipment, Procedures for Packaging and Packing o
16、f SAE AMS1640C Page 3 of 6 3. TECHNICAL REQUIREMENTS 3.1 Material Compounds meeting the requirements of this specification shall be viscous, thixotropic, and concentrated. Compounds will readily mix with water to form a homogeneous solution. Compound, diluted with ASTM D 1193, Type IV, water, to use
17、 concentration in accordance with manufacturers recommendations, shall retain its thixotropic properties, shall be suitable for application by rinsing or spraying, and shall be readily removable by wiping or rinsing procedures. 3.1.1 There shall be no violent or dangerous reactions when the concentr
18、ate is diluted for use in accordance with manufacturers recommendations. 3.2 Properties Compound shall conform to the following requirements; tests shall be performed in accordance with specified test methods on the product supplied in concentrated form and at use dilution recommended by the manufac
19、turer as hereinafter specified. 3.2.1 Concentrated Compound 3.2.1.1 Flash Point Shall be not lower than 150 F (65 C), determined in accordance with ASTM D 93 Pensky Martins Closed Cup Tester. 3.2.1.2 Solubility Compound shall be completely soluble in water to make a uniform solution free from gelati
20、nous lumps, layering of ingredients, and sediment. 3.2.1.3 Stability Compound shall remain homogeneous and free from sedimentation and layering of ingredients, determined in accordance with ASTM F 503. Compound, stored in unopened shipping container or use package, shall meet all other technical req
21、uirements of this specification at any time up to one year from date of receipt by purchaser. 3.2.2 Concentrated Compound and at Use Dilution 3.2.2.1 Viscosity Shall be not lower than the following, determined in accordance with ASTM D 2196 at 68 F 4 (20 C 2) using a No. 1 spindle at 6 RPM: Concentr
22、ated Compound 550 cP (mPas) 50% Solution of Concentrate in ASTM D 1193, Type IV, Water 55 cP (mPas) 3.2.2.2 Immersion Corrosion Compound shall neither show evidence of pitting, or corrosion nor cause an average weight change on AMS4049 and AMS-QQ-A-250/4 aluminum alloys panels greater than 2.5 mg/in
23、2per 30 minutes (0.4 mg/cm2per 30 minutes), determined in accordance with ASTM F 483 under the test conditions given in 3.2.2.2.1. Staining is not acceptable for AMS4049 panels but is allowable for the AMS-QQ-A-250/4 panels. 3.2.2.2.1 The weighed panels shall be totally immersed in 100 mL of compoun
24、d, immediately removed, and suspended vertically for 30 minutes 1 at 77 F 4 (25 C 2). SAE AMS1640C Page 4 of 6 3.2.2.3 Intergranular and Pitting Attack on Aluminum. The compound shall not cause end grain pitting in excess of 0.001 inch (25.4 microns) or intergranular attack in excess of 0.0002 inch
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