FREEZING POINT OF AVIATION FUELSASTM D2386 - IP 16 - NFM 07048 - ISO 3013 - DIN 51421This standard describes a method of determination of the temperature below which solid hydrocarbon crystals may form in turbine and reciprocating engine fuels under cooling conditions which may occur during flight or on airfield.
CHARACTERISTICS
SPECIFICATION Complete Tester including Dewar flask, sample tube, holed cork, manual stirrer, tight joint, ASTM 114C thermometer, holder with upright, boss and clamp, REF.941556 Complete freezing point apparatus, comprising : jacketed sample tube, brass packing gland for stirrer, brass wire stirrer, vacuum flask unsilvered with support and thermometer REFERENCE FLUID (on request) SPARE PARTS (2 years basis) 9415561 Jacketed sample tube (double w alls) 9415562 Gland, brass packing for stirrer 9415563 Stirrer 9415564 Vacuum f lask unsilvered 9911566 ASTM thermometer 114C 9913463 Cork for sample tube see also: Automatic determination of the freezing point Model NPC 452 Automatic determination of the freezing point |