SAE AMS 1379A-1992 Compound Alkaline Rust Remover Aircraft Turbine Engine Components《飞机涡轮发动机组件用碱性除锈剂化合物》.pdf
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1、AEROSPACEAMS 1379AMATERIALSPECIFICATION Superseding AMS 1379COMPOUND, ALKALINE RUST REMOVERAircraft Turbine Engine Components1. SCOPE:1.1 Form:This specification covers an alkaline rust remover compound in the form of aliquid concentrate or a water-soluble powder for dilution with water.1.2 Applicat
2、ion:This product has been used typically for removing rust, soils, or otheroxidation products from aircraft turbine engine parts by immersion in asolution of the compound at elevated temperature, but usage is not limited tosuch applications. These compounds are unsuitable for cleaning aluminumparts.
3、 Restrictions for cleaning titanium parts may be imposed by the enginemanufacturer.1.3 Classification:Compounds conforming to this specification are classified as follows:Type 1 - Liquid concentrateWater-soluble powder1.3.1 Type 1 shall be supplied unless Type 2 is ordered.1.4 Precautions:Remover co
4、mpound may contain chemicals which, if improperly used, could behazardous to the health and safety of operators. Protective clothingincluding eye shields, suitable gloves, and apron should be worn whenpreparing and using compound. Tanks shall be prepared and operated underconditions of adequate fume
5、 extraction and with due regard to the safetyrecommendations of the manufacturer of the compound together with localworkshop safety regulations.IssuedRevised 1 APR 19921 APR 1985Type 2 -Reaffirmed FEB 2007SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance t
6、he 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 therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least every f
7、ive years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2007 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, elect
8、ronic, 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) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org RATIONALE Thi
9、s document has been reaffirmed to comply with the SAE 5-year Review policy. AMS 1379A SAEAMS 1379A1.5 Safety - Hazardous Materials:While the materials, methods, applications, and processes described orreferenced in this specification may involve the use of hazardous materials,this specification does
10、 not address the hazards which may be involved in suchuse. It is the sole responsibility of the user to ensure familiarity withthe safe and proper use of any hazardous materials and to take necessaryprecautionary measures to ensure the health and safety of all personnelinvolved.2. APPLICABLE DOCUMEN
11、TS:The following publications form a part of this specification to the extentspecified herein. The latest issue of SAE publications shall apply. Theapplicable issue of other publications shall be the issue in effect on thedate of the purchase order.2.1 SAE Publications:Available from SAE, 400 Common
12、wealth Drive, Warrendale, PA 15096-0001.AMS 2825 Material Safety Data SheetsARP1755 Effect of Cleaning Agents on Aircraft Engine Materials, StockLoss Test Method2.2 ASTM Publications:Available from ASTM, 1916 Race Street, Philadelphia, PA 19103-1187.ASTM D 1568 Sampling and Chemical Analysis of Alky
13、lbenzene SulfonatesASTM D 2667 Biodegradability of Alkylbenzene SulfonatesASTM F 945 Stress Corrosion of Titanium Alloys by Aircraft Engine CleaningMaterials2.3 U.S. Government Publications:Available from Standardization Documents Order Desk, Building 4D, 700 RobbinsAvenue, Philadelphia, PA 19111-50
14、94.MIL-STD-2073-1 DOD Materiel, Procedures for Development and Application ofPackaging Requirements3. TECHNICAL REQUIREMENTS:3.1 Composition:The composition of the compound shall be optional with the manufacturerexcept that, when prepared for use, the solution shall be alkaline. Whenprepared in acco
15、rdance with manufacturers instructions, the compound shallform a liquid product, with no solid sediment at room temperature and shallmeet the requirements of 3.2.- 2 -AMS 1379A SAE AMS 1379A3.2 Properties:The compound shall conform to the following requirements; tests shall beperformed in accordance
16、 with specified test methods on the product suppliedat the maximum concentration and temperature recommended by the manufacturer.3.2.1 Stock Loss: Test panels of alloys or electrodeposits shall not incur stockloss exceeding 0.000025 inch (0.635 m) per surface and plasma depositedcoatings shall not i
17、ncur stock loss exceeding 0.0001 inch (2.5 m), whentested in accordance with ARP1755, Category 2. Stock loss figures shall bereported for all materials specified in ARP1755, Category 2. Vendor shallindicate where compound is not recommended for particular alloys orcoatings.3.2.2 Surface Attack: Test
18、 panels and bars used for the stock loss test of 3.2.1shall neither exhibit pitting corrosion nor show visual evidence ofdegradation, when examined at 50X magnification under good oblique surfacelighting conditions.3.2.3 Biodegradability: Vendor shall supply evidence that surfactants used inthe comp
19、ound are 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.3.2.3.1 Evidence of surfactant biodegradability does not guarantee that thecompound may be discharged
20、 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 at 25 C 5 (77 F 9) for one year from date of receipt by purchaser, shall show no visual evidence ofdeterioration and sh
21、all meet all other technical requirements of thisspecification.3.2.5 Stress-Corrosion of Titanium Alloys: The compound, when used at therequired concentrations, shall not cause stress-corrosion cracking oftitanium alloys, determined in accordance with ASTM F 945, Method A orMethod B.3.2.6 Performanc
22、e: The compound, prepared and used in accordance withmanufacturers instructions, shall be capable of removing soils, rust, andother oxidation products from all required parts. Compounds which meet allother technical requirements of this specification shall be service testedin an approved engine over
23、haul facility for not less than six months,during which time at least ten turbofan or turbojet engines, or equivalent,shall be processed with satisfactory results before approval for serviceuse is granted by the applicable engine manufacturer.- 3 -(R)(R)AMS 1379A SAE AMS 1379A3.3 Quality:The liquid
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