1. SCOPE
1.1 This standard applies to two grades of kerosene-type aviation turbine fuel (grades JET A and JET A-1), consistingentirely of petroleum-derived hydrocarbons, naturally occurring non-hydrocarbons and additives as specifiedherein. Kerosene-type aviation turbine fuels are distillates having a minimum flash point of 38°C.
1.1.1 The two grades differ only in freezing point. Grade JET A has a maximum freezing point of -40°C and GradeJET A-1 has a maximum freezing point of -47°C.
1.2 The fuels are normally used in civil aviation operations.
1.3 Limitations for Use — Aircraft operators should consult their aircraft manuals for the type of fuel, fuel additivesand any temperature-related or other limitations.
1.3.1 Temperature Limitations — When temperatures are close to the fuel freezing-point, fuel operability problemscan be experienced. JET A, with a specification freezing point of -40°C, is not intended for use during extremelycold weather conditions or when the ambient temperature is close to, or below, -40°C. It also requires morerestrictive use than JET A-1. For more information concerning temperature limitations, see Transport Canada’sAirworthiness Notice No. B021 (par. 2.1.2) and par. 8.4.
1.4 The testing and evaluation of a product against this standard may require the use of materials and/or equipmentthat could 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 appropriatehealth and safety practices in conjunction with any applicable regulatory requirements prior to its use.
- Published:
- 01/01/2009
- Number of Pages:
- 15
- File Size:
- 2 files , 580 KB
- Note:
- This product is unavailable in Russia, Belarus
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