1、SAE-AMS-C-19853ADOPTION NOTICESAE-AMS-C-19853, “CARBON REMOVING COUMPOUND (FOR USE INAGITIATED TANK)“, was adopted on 21-SEP-98 for use by theDepartment of Defense (DoD). Proposed changes by DoDactivities must be submitted to the DoD Adopting Activity:Commander, Naval Air Warfare Center, Aircraft Di
2、vision, Code414100B120-3, Highway 547, Lakehurst, NJ 08733-5100. Copies ofthis document may be purchased from the Society of AutomotiveEngineers 400 Commonwealth Drive Warrendale, Pennsylvania, UnitedStates, 15096-0001. http:/www.sae.org/_Custodians: Adopting Activity:Navy - ASNavy - ASAir Force - 1
3、1Reviewer Activities:Navy - MSDLA - GSFSC 6850DISTRIBUTION STATEMENT A: Approved for public release; distributionis unlimited.SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and enginee ring sciences. The use of this report is enti
4、relyvoluntary, 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 five years at which time it may be reaffirmed, revised, or cancelled. SAE invit e
5、s your written comments and suggestions.Copyright 1998 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.A.QUESTIONS REGARDING THIS DOCUMENT: (724) 772-7161 FAX: (724) 776-0243TO PLACE A DOCUMENT ORDER: (724) 776-4970 FAX: (724) 776-0790SAE WEB ADDRESS: http:/www.sae.org400 Co
6、mmonwealth Drive, Warrendale, PA 15096-0001AEROS PACE MATERIAL SPECIFIC ATIONSubmitted for recognition as an American National StandardAMS-C-19853Issued JUL 1998Carbon Removing Compound (For Use in Agitated T ank)NOTICEThis document has been taken directly from U.S. Military Specification MIL-C-1985
7、3D and contains only minor editorial and format changes required to bring it into conformance with the publishing requirements of SAE technical standards. The initial release of this document is intended to replace MIL-C-19853D. Any part numbers established by the original specification remain uncha
8、nged.The original Military Specification was adopted as an SAE standard under the provisions of the SAE Technical Standards Board (TSB) Rules and Regulations (TSB 001) pertaining to accelerated adoption of government specifications and standards. TSB rules provide for (a) the publication of portions
9、 of unrevised government specifications and standards without consensus voting at the SAE Committee level, and (b) the use of the existing government specification or standard format.Under Department of Defense policies and procedures, any qualifications requirements and associated qualified product
10、s lists are mandatory to DOD contracts. Any requirement relating to qualified products lists (QPLs) has not been adopted by SAE and is not part of this technical report.1. SCOPE:1.1 Scope: This specification covers requirements for the acquisition of two types and two classes of material that will r
11、emove or loosen carbon from components of internal combustion engines and compressor sections of jet engines.AMS-C-19853 SAE AMS-C-19853- 2 -1.2 Classification: The carbon removing compound is to be furnished in the following types and classes as specified (see 6.2c):Type I - PhenolicType II - Non-p
12、henolicClass 1 - Unsealed (Single layer)Class 2 - Sealed (Two layers)2. APPLICABLE DOCUMENTS: The following publications, of the issue in effect on date of invitation for bids or request for proposal, form a part of this specification to the extent specified herein.2.1 U.S. Government Publications:
13、Available from DODSSP, Subscription Services Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.MIL-M-3171 Magnesium Alloy, Processes for Pretreatment and Prevention of Corrosion onMIL-L-6082 Lubricating Oil, Aircraft Piston Engine (Non Dispersant Mineral Oil)MIL-S-7952 Steel, Sheet
14、and Strip, Uncoated, Carbon (1020 however, information pertaining to qualification of products and authorization for submittal of sample may be obtained from the Director, Aircraft and Crew Systems Technology Directorate, Code 60622, Naval Air Warfare Center aircraft Division Warminster, Warminster,
15、 PA 18974-0591.6.3.1 Withdrawal from qualified products list: Material furnished under contract shall be identical to carbon removing compound samples which have been submitted by the manufacturer and have been inspected and approved for inclusion in the Qualified Products List. In the event that ma
16、terial furnished under contract is found to deviate from the composition of the approved product or that the product fails to perform satisfactorily in service, approval of such material will be subject to immediate withdrawal from the Qualified Products List.6.4 Consideration of data requirements:
17、The following data requirements should be considered when this specification is applied on a contract. The applicable Data Item Descriptions (DIDs) should be reviewed in conjunction with the specific acquisition to ensure that only essential data are requested/provided and that the DIDs are tailored
18、 to reflect the requirements of the specific acquisition. To ensure correct contractual application of the data requirements, a Contract Data Requirements List (DD Form 1423) must be prepared to obtain the data, except where DOD FAR Supplement 27.475-1 exempts the requirement for a DD Form 1423.The
19、above DIDs were those cleared as of the date of this specification. The current issue of DOD 5010.12-L, Acquisition Management Systems and Data requirements Control List (AMSDL), must be researched to ensure that only current, cleared DIDs are cited on the DD Form 1423.6.5 Safety data sheet: A copy
20、of the material safety data sheet should be forwarded to the Navy Environmental Health Center, Naval Station, Norfolk, VA 23511.Reference Paragraph DID Number DID Title Suggested Tailoring4.4 DI-NDTI-80809A Test/InspectionReport-AMS-C-19853 SAE AMS-C-19853- 16 -6.6 Safety: Contact the local industri
21、al hygienist for safe handling advice.6.7 Part number: A specification part numbering system for cataloging purposes may be derived as follows:6.8 Cross reference of classification: The classification under this amendment is as follows:6.9 Subject term (key word) listing: Engines, aircraftNon-phenol
22、icPhenolicQualificationSealedUltrasonic cleaningUnsealedMIL-C-19853D MIL-C-19853C MIL-C-19853BType I, Class 1 Type I Type IType I, Class 2 - -Type II, Class 1 Type II -Type II, Class 2 - Type IIAMS-C-19853 SAE AMS-C-19853- 17 -TABLE I. Qualification inspection.InspectionParagraphRequirement Test met
23、hodpH of seal 3.4 4.5.1Specific gravity 3.5 4.5.2Flammability 3.6 4.5.3Volatility 3.7 4.5.4Separation of layers(Class 1 only)3.8 4.5.5Phenol Content (type II only) 3.9 4.5.6Storage stability 3.10 4.5.7Oil removal 3.11 4.5.9Carbon removal 3.12 4.5.10Corrosiveness 3.13 4.5.11Rinsing properties 3.14 4.
24、5.12Compatibility (type I only) 3.15 4.5.13Emulsification 3.16 4.5.14Cold stability 3.17 4.5.15Temperature cycle (stability) 3.18 4.5.16Seal content (Class 2 only) 3.19 4.5.17Workmanship 3.20 -TABLE II. Net content.Lot size (containers) Sample size (containers)Up to 50 551 - 500 7501 - 35,000 835,00
25、1 and over 11AMS-C-19853 SAE AMS-C-19853- 18 -1 / Eighty five (85) parts by volume of the control formula product shall be mixed with fifteen (15) parts by volume of distilled water.PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “J”TABLE III. Control formula product. 1 /Ingredients Percent composi
26、tion by weightCresol (USP) 33.62Phenol (USP) 1.00Oleic acid (USP) 6.80Potassium hydroxide (45 percent) 3.52Methylene chloride 54.90Ethylenediaminetetraacetic (EDTA) acid 0.16TABLE IV. Metal test panels.No. Metal Specification Surface Specification1 Aluminum cladAluminum alloyQQ-A-250/13 - -2 Aluminum alloy QQ-A-250/4 Anodized MIL-A-86253 Steel MIL-S-7952 Polished -4 Steel MIL-S-7952 Cadmium QQ-P-4165 Magnesium alloy AMS 4375 ChromepickledMIL-M-3171,type I
