1、CAN/CGSB-3.22-2012Supersedes CAN/CGSB-3.22-2002Wide-Cut Type Aviation Turbine Fuel (Grade JET B)ICS 75.160.20National Standard of CanadaCopyright Canadian General Standards Board Provided by IHS under license with CGSBNot for ResaleNo reproduction or networking permitted without license from IHS-,-,
2、-The CANADIAN GENERAL STANDARDS BOARD (CGSB), under whose auspices this National Standard of Canada has been developed is a government agency within Public Works and Government Services Canada. CGSB is engaged in the production of voluntary standards in a wide range of subject areas through the medi
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9、is standard is stated in its Scope, it is important to note that it remains the responsibility of the users of the standard to judge its suitability for their particular purpose. The testing and evaluation of a product against this standard may require the use of materials and/or equipment that coul
10、d be hazardous. This document does not purport to address all the safety aspects associated with its use. Anyone using this standard has the responsibility to consult the appropriate authorities and to establish appropriate health and safety practices in conjunction with any applicable regulatory re
11、quirements prior to its use. CGSB neither assumes nor accepts any responsibility for any injury or damage that may occur during or as the result of tests, wherever performed. Attention is drawn to the possibility that some of the elements of this Canadian standard may be the subject of patent rights
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13、ed from: The Manager Standards Division Canadian General Standards Board Gatineau, Canada K1A 1G6 The STANDARDS COUNCIL OF CANADA is the coordinating body of the National Standards System, a coalition of independent, autonomous organizations working towards the further development and improvement of
14、 voluntary standardization in the national interest. The principal objects of the SCC are to foster and promote voluntary standardization as a means of advancing the national economy, benefiting the health, safety and welfare of the public, assisting and protecting the consumer, facilitating domesti
15、c and international trade, and furthering international cooperation in the field of standards. A National Standard of Canada (NSC) is a standard prepared or reviewed by an accredited Standards Development Organization (SDO) and approved by the SCC according to the requirements of CAN-P-2. Approval d
16、oes not refer to the technical content of the standard; this remains the continuing responsibility of the SDO. A NSC reflects a consensus of a number of capable individuals whose collective interests provide, to the greatest practicable extent, a balance of representation of general interests, produ
17、cers, regulators, users (including consumers), and others with relevant interests, as may be appropriate to the subject in hand. It normally is a standard, which is capable of making a significant and timely contribution to the national interest. Those who have a need to apply standards are encourag
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20、www.tpsgc-pwgsc.gc.ca/ongc-cgsb Copyright Canadian General Standards Board Provided by IHS under license with CGSBNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NATIONAL STANDARD OF CANADA CAN/CGSB-3.22-2012Supersedes CAN/CGSB-3.22-2002WIDE-CUT TYPE AVIATION TURBI
21、NE FUEL (GRADE JET B)CETTE NORME NATIONALE DU CANADA EST DISPONIBLE EN VERSIONSFRANAISE ET ANGLAISE.NATIONAL STANDARD OF CANADA CAN/CGSB-3.14-2006Prepared by the Approved by the Canadian General Standards Board Standards Council of CanadaPublished September 2012 by the Canadian General Standards Boa
22、rd Gatineau, Canada K1A 1G6 HER MAJESTY THE QUEEN IN RIGHT OF CANADA, as represented by the Minister of Public Works and Government Services, the Minister responsible for the Canadian General Standards Board (2012). No part of this publication may be reproduced in any form without the prior permissi
23、on of the publisher.Copyright Canadian General Standards Board Provided by IHS under license with CGSBNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CAN/CGSB-3.22-2012CANADIAN GENERAL STANDARDS BOARDCOMMITTEE ON AVIATION FUELS(Voting membership at date of approval
24、)ChairPoitras, P. National Defence (User)General Interest CategoryHanganu, A. OTI Canada GroupPickard, A.L. ConsultantTharby, R.D. Tharby Technology, ConsultantsVidian-Jones, C. Certispec Services Inc.Wispinski, D. Alberta Innovates-Technology FuturesProducer CategoryBurgazli, J. Innospec Inc.Conn,
25、A. Ethyl Corp.Jobin, J.L. Ultramar Ltd.Kenney, B. Suncor Energy Inc.Lund, C. Imperial Oil Ltd.Millard, P. GE Water and Process TechnologiesMitchell, K. Shell Canada Ltd.Robichaud S. Irving Oil Ltd.Regulator CategoryDhaliwal, R. Transport CanadaUser CategoryBrar, C. Air CanadaEveleigh, S. Government
26、of Northwest TerritoriesMacLeod, B. Public Works and Government Services CanadaMolinari, J. Air Transport Association of CanadaTauvette, G. WestJet Airlines Ltd.Waddleton, D. Pratt however, when results are obtained by both methods, D2276 shall be considered the referee method.7 The minimum micro-se
27、parometer (MSEP) rating applies up to the point immediately before the fuel enters dedicated transportation to airport storage. When the fuel enters dedicated transportation to airport storage, or when the fuel is already in airport storage, the MSEP rating requirement shall not apply. When a fuel s
28、ystem icing inhibitor (par. 5.5) or a corrosion inhibitor/lubricity improver (par. 5.6) is added, the MSEP limits apply before its addition.Copyright Canadian General Standards Board Provided by IHS under license with CGSBNot for ResaleNo reproduction or networking permitted without license from IHS
29、-,-,-4 CAN/CGSB-3.22-2012JET B Test MethodProperty Min. Max. ASTM4.12.1 Static dissipator additive (par. 5.2), mg/La. Original addition 3b. Cumulative 54.12.2 Antioxidant (par. 5.3), mg/LOptional 244.12.3 Metal deactivator (par. 5.4), mg/L Optionala. Original addition 2.0b. Cumulative 5.74.12.4 Fuel
30、 system icing inhibitor (par. 5.5), % by volume Optional D5006 0.10 0.154.12.5 Corrosion inhibitor/ lubricity improver (par. 5.6) Optional4.12.6 Leak detection additive (par. 5.7), mg/kg Optional 14.13 Density4.13.1 Density at 15C, kg/m3751 802 D12981orD40524.14 Sulphur The precision and bias of sul
31、phur determinations using ASTM D7039 on diluted samples have not been determined. The accuracy of this method for jet fuel beyond 2000 mg/kg sulphur has not been validated by an interlaboratory study. Users are cautioned to conduct their own validation when using this test method for fuel containing
32、 more than 2000 mg/kg sulphur.5. ADDITIVE REQUIREMENTS5.1 Only the additives listed in par. 5.2 to 5.7 may be added to the fuel. Refer to par. 4.12 for specified limiting values and test method for each property. When additives are added to the fuel, the supplier shall record the amount and names of
33、 the additive.5.1.1 The amount of each additive used in the fuel shall be determined by the test method (par. 4.12) or by volume reconciliation. Procedures for volume reconciliation should include recording the volume of additive introduced to the fuel and the volume of fuel additized, in appropriat
34、e units.5.2 Static Dissipator Additive (SDA) Static dissipator additive Stadis 4508shall be added to the fuel to meet the electrical conductivity requirements specified in par. 4.11.1. The original concentration of the SDA shall not exceed 3 mg/L.5.2.1 When additive depletion is evident by a conduct
35、ivity loss, further addition of the SDA is permitted as follows: If the original concentration of the SDA is not known, an original addition of 3 mg/L is assumed and further addition of SDA shall not exceed 2 mg/L. The cumulative concentration of the SDA shall not exceed 5 mg/L.8Stadis 450, a regist
36、ered trademark of Innospec Fuel Specialties LLC, is distributed globally by Innospec Fuel Specialties LLC.Copyright Canadian General Standards Board Provided by IHS under license with CGSBNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CAN/CGSB-3.22-2012 55.2.2 Ele
37、ctrical conductivity varies with temperature. A typical relationship follows:( )ktttakt1loglog1+=where:kt= electrical conductivity at temperature t, C= electrical conductivity at temperature t1, Ca = a factor that depends on fuel composition but normally within the range 0.013 to 0.018 for wide-cut
38、type aviation turbine fuels5.2.2.1 The temperature-conductivity factor, a, increases at or below an approximate temperature of -10C. For conductivity at very low temperatures, it is recommended that a separate factor be determined based on actual measurements at the lowest temperatures likely to be
39、encountered. For more information on how low temperature affects conductivity, see ASTM D2624.5.3 Antioxidants Only the following antioxidants may be added separately or in combination to the fuel. The total concentration (not including mass of solvent) shall not exceed 24 mg/L.a. 2,6-di-tert-butylp
40、henolb. 2,6-di-tert-butyl-4-methylphenolc. 2-tert-butyl-4,6-dimethylphenol (2,4-dimethyl-6-tertiary butylphenol)d. 75% minimum, 2,6-di-tert-butylphenol 25% maximum mixture of tert- and tri-tert-butylphenolse. 55% minimum, 2-tert-butyl-4,6-dimethylphenol (2,4-dimethyl-6-tertiary butylphenol) 15% mini
41、mum, 2,6-di-tert-butyl-4-methylphenol Remainder as methyl and dimethyl tert-butylphenolsf. 72% minimum, 2-tert-butyl-4,6-dimethylphenol (2,4-dimethyl-6-tertiary butylphenol) 28% maximum, methyl and dimethyl tert-butylphenols.Note: The names of the antioxidants conform to the International Union of P
42、ure and Applied Chemistry (IUPAC) naming convention. In some cases, the common name of the antioxidant has been included in brackets after the IUPAC name.5.4 Metal Deactivator Only N,N-disalicylidene-1,2-propane-diamine may be added as a metal deactivator at a concentration not exceeding 2.0 mg/L (n
43、ot including mass of solvent) on the initial fuel manufactured at the refinery. Higher concentrations are permitted in circumstances where copper contamination is suspected to have occurred during distribution. Cumulative concentration of metal deactivator when re-treating the fuel shall not exceed
44、5.7 mg/L (par. 7.3).5.5 Fuel System Icing Inhibitor When specified by the purchaser (par. 7.1) and agreed by the supplier and the purchaser, a fuel system icing inhibitor conforming to ASTM D4171 (Type III DIEGME) shall be added to the fuel (par. 4.12.4). 5.6 Corrosion Inhibitors/Lubricity Improvers
45、 When specified by the purchaser (par. 7.1) and agreed by the supplier and the purchaser, a corrosion inhibitor/lubricity improver shall be added to the fuel (par. 7.2).5.6.1 Only a corrosion inhibitor/lubricity improver qualified to U.S. Military Specification MIL-PRF-25017 and listed in the associ
46、ated Qualified Product List (QPL) 25017 shall be added to the fuel. The concentration of the additive in the fuel shall be as specified in the QPL, and its introduction into the fuel shall be separate from the addition of other additives.t1kt1Copyright Canadian General Standards Board Provided by IH
47、S under license with CGSBNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-6 CAN/CGSB-3.22-20125.7 Leak Detection Additive9 Only Tracer A (LDTA-A)10may be added as a leak detection additive. The maximum concentration is 1 mg/kg.6. INSPECTION6.1 Sampling Samples for t
48、esting shall be obtained in accordance with ASTM D4057. For automatic sampling ASTM D4177 shall be used. Sampling for volatility measurement shall be done in accordance with ASTM D5842.7. NOTES7.1 Options The following options may be specified in the application of this standard:a. Fuel system icing
49、 inhibitor (par. 5.5)b. Corrosion inhibitor/lubricity (par. 5.6).7.2 Lubricity Information Statement 7.2.1 Lubricity, which is the ability of jet fuel to act as a lubricant for certain aircraft fuel-wetted components, can vary considerably. It depends on the design, materials used and the intrinsic lubricity of the fuel. There have been a few isolated cases of e
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