SAE AMS 1378A-1991 Compound Carbon Soil and Paint Remover Aircraft Turbine Engine Components Room Temperature Application《室温下飞机涡轮发动机组件用碳质污垢和涂料清洗剂的化合物》.pdf
《SAE AMS 1378A-1991 Compound Carbon Soil and Paint Remover Aircraft Turbine Engine Components Room Temperature Application《室温下飞机涡轮发动机组件用碳质污垢和涂料清洗剂的化合物》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 1378A-1991 Compound Carbon Soil and Paint Remover Aircraft Turbine Engine Components Room Temperature Application《室温下飞机涡轮发动机组件用碳质污垢和涂料清洗剂的化合物》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、The Engineering SocietyFor Advancing Mobility AEROSPACE AMS 1378ALand Sea Air and SpaceINTERNATIONAL400 Commonwealth Drive, Warrendale, PA 15096-0001SPECIFICATIONSubmitted for recognition as an American National StandardIssued 1 APR 1985Superseding AMS 1378Revised 1 JUL 1991COMPOUND, CARBON SOIL AND
2、 PAINT REMOVERAircraft Turbine Engine ComponentsRoom Temperature Application1. SCOPE:1.1 Form: This specification covers a carbon soil and paint remover compound inthe form of a liquid.1.2 Application: Primarily for removal of carbonaceous soils and paint fromaircraft turbine engine parts by immersi
3、ng the parts in liquid at roomtemperature.1.3 Safety - Hazardous Materials: While the materials, methods, applications,and processes described or referenced in this specification may involve theuse of hazardous materials, this specification does not address the hazardswhich may be involved in such u
4、se. It is the sole responsibility of theuser to ensure familiarity with the safe and proper use of any hazardousmaterials and to take necessary precautionary measures to ensure the healthand safety of all personnel involved.2. APPLICABLE DOCUMENTS: The following publications form a part of thisspeci
5、fication to the extent specified herein. The latest issue of SAEpublications shall apply. The applicable issue of other publications shallbe the issue in effect on the date of the purchase order.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale,PA 15096-0001.2.1.1 Aerospac
6、e Material Specifications:AMS 2825 - Material Safety Data Sheets2.1.2 Aerospace Recommended Practices:ARP1755 - Effect of Cleaning Agents on Aircraft Engine Materials, StockLoss Test MethodSAE Technical Board Rules provide that: “This report is published by SAE to advance the state of technical and
7、engineering sciences.The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringementarising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it ma
8、y be reaffirmed, revised, or cancelled. SAE invites yourwritten comments and suggestions.Copyright 1991 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.A.MATERIALAMS 1378A SAE AMS 1378A2.2 ASTM Publications: Available from ASTM, 1916 Race Street, Philadelphia, PA19103-1187.A
9、STM D 1568 - Sampling and Chemical Analysis of Alkylbenzene SulfonatesASTM D 2667 - Biodegradability of Alkylbenzene SulfonatesASTM F 519 - Mechanical Hydrogen Embrittlement Testing of Plating Processesand Aircraft Maintenance ChemicalsASTM F 945 - Stress-Corrosion of Titanium Alloys by Aircraft Eng
10、ineCleaning Materials2.3 U.S. Government Publications: Available from Standardization DocumentsOrder Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-50942.3.1 Military Standards:MIL-STD-2073-1 - DOD Materiel, Procedures for Developmenof Packaging Requirements3. TECHNICAL REQUIREMENTS:3
11、.1 Composition: Shall be optional with the manufacturer but, when prepared inaccordance with manufacturers instructions, shall form a liquid product,with no solid sediment at room temperature, meeting the requirements of 3.2.and Application3.1.1 Compound containing volatile solvents shall be provide
12、d with an upperliquid seal serving to retard evaporation of solvents from the lowerworking layer. Solution make up, depth of seal if required, and solutioncontrol for the lower and seal phases shall be in accordance withmanufacturers instructions and purchasers requirements.3.2 Properties: Compound
13、shall conform to the following requirements; tests0 shall be performed in accordance with specified test methods on the productsupplied at the maximum concentration recommended by manufacturer; if a sealis specified, tests shall be performed on the lower liquid layer through theseal:3.2.1 Stock Loss
14、: Test panels of alloys or electrodeposits shall not incurstock loss exceeding 0.000025 inch (0.635 m) per surface and plasmadeposited coatings shall not incur stock loss exceeding 0.0001 inch(2.5 m) when tested in accordance with ARP1755, Category 1. Whererequired in ARP1755, stock loss figures sha
15、ll be reported. Manufacturermay indicate where remover is not recommended for particular alloys orsurface coatings.3.2.2 Corrosion: Test panels and bars used for the stock loss test of 3.2.1shall exhibit no surface attack when examined at 50X magnification undergood oblique surface lighting conditio
16、ns.3.2.3 Biodegadability: Vendor shall supply evidence that surfactants used inthe compound shall be at least 90% biodegradable, determined either inaccordance with ASTM D 2667 where relevant to surfactant type or byalternative methods appropriate to surfactant type acceptable to purchaser.-2-AMS 13
17、78A SAE AMS 1378A3.2.3.1 Evidence of surfactant biodegradability does not guarantee that thecompound may be discharged in either concentrated or diluted form intopublic waterways or sewerage systems; manufacturers shall give advice onthe means for disposal.3.2.4 Storage Stability: Compound, stored a
18、t 25C 5 (77F 9) for one year,shall show no visual evidence of deterioration and shall meet all othertechnical requirements of this specification.3.2.5 Stress-Corrosion of Titanium Alloys: The compound, when used according to0 manufacturers instructions, shall not cause stress-corrosion cracking ofti
19、tanium alloys, determined in accordance with ASTM F 945, Method A or B.3.2.6 Hydrogen Absorption: Compound shall be non-embrittling, determined inaccordance with ASTM F 519, Type la, lc, or 2a, but usingnon-electroplated test specimens.3.2.7Performance:The compound, prepared and used in accordance w
20、ithmanufacturers instructions, shall remove carbonaceous soils and paintfrom parts. Compounds which meet all other technical requirments shall betested for cleaning performance in an approved engine overhaul facilityfor not less than six months, during which time at least ten turbofan orturbojet eng
21、ines, or equivalent, shall be processed with satisfactoryresults before approval for service use is granted by the applicableengine manufacturer.3.3 Quality: The compound, as received by purchaser, shall be clear,homogeneous, and free from solid particles and separation and from foreignmaterials det
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