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Significance and Use
5.1 This test method provides a gravimetric measurement of the particulate matter present in a sample of aviation turbine fuel delivered to a laboratory for evaluation. The objective is to minimize these contaminants to avoid filter plugging and other operational problems. Although tolerable levels of particulate contaminants have not yet been established for all points in fuel distribution systems, the total contaminant measurement is normally of most interest.
1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements, see 4.2, 7.3, 7.5, 11.2, and X1.7.2. Before using this standard, refer to supplier's safety labels, material safety data sheets, and technical literature.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
D56 Test Method for Flash Point by Tag Closed Cup Tester
D93 Test Methods for Flash Point by Pensky-Martens Closed Cup Tester
D1193 Specification for Reagent Water
D1535 Practice for Specifying Color by the Munsell System
D2244 Practice for Calculation of Color Tolerances and Color Differences from Instrumentally Measured Color Coordinates
D2276 Test Method for Particulate Contaminant in Aviation Fuel by Line Sampling
D3828 Test Methods for Flash Point by Small Scale Closed Cup Tester
D4306 Practice for Aviation Fuel Sample Containers for Tests Affected by Trace Contamination
D4865 Guide for Generation and Dissipation of Static Electricity in Petroleum Fuel Systems
D6615 Specification for Jet B Wide-Cut Aviation Turbine Fuel
ICS Number Code 75.160.20 (Liquid fuels)
UNSPSC Code 15101504(Aviation fuel)