NSN 9130-01-373-0208

Part Details | AVIATION TURBINE FUEL


9130-01-373-0208 A liquid petroleum distillate refined especially for use in aviation turbine engines.

Alternate Parts: AN8, MILT83133, MIL-T-83133, MILDTL83133, MIL-DTL-83133, 9130-01-373-0208, 01-373-0208, 9130013730208, 013730208

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
91MAR 25, 199301-373-020826646 ( TURBINE FUEL, AVIATION )
REFERENCE DRAWINGS & PICTURES

Cross Reference | NSN 9130-01-373-0208
Part Number Cage Code Manufacturer
AN852838DEFENSE LOGISTICS AGENCYDBA DLA ENERGY
MIL-T-8313381349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-DTL-8313381349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY

Technical Data | NSN 9130-01-373-0208
Characteristic Specifications
FUEL GRADE CLASSIFICATION JP-8
VISCOSITY AT RATED TEMP8.00 MAXIMUM -20 DEG CELSIUS
MINIMUM FLASH POINT AND TEST METHOD38.0 DEG CELSIUS PENSKY-MARTENS CLOSED CUP
DENSITY VALUE0.775 KILOGRAMS PER LITER MINIMUM AND 0.840 KILOGRAMS PER LITER MAXIMUM
DENSITY TEMP15.0 DEG CELSIUS
FREEZING POINT MAXIMUM TEMP-72.0 DEG FAHRENHEIT
MINIMUM HEAT OF COMBUSTION VALUE42.8 MEGAJOULES PER KILOGRAM
COPPER CORROSION CLASSIFICATION NUMBER1
MAXIMUM AMOUNT OF EXISTENT GUM7.0
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT0.0015
MAXIMUM AROMATICS PERCENTAGE BY VOLUME25.0
MAXIMUM OLEFINS CONTENT PERCENTAGE BY VOLUME5.0
DISTILLATION POINT PERCENTAGE AT MAXIMUM TEMP205.0 DEG C AT 10.0 PCT AND 300.0DEG C AT THE END POINT
MAXIMUM DISTILLATION RESIDUE VOLUME PERCENTAGE1.5
MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE1.5
SUPPLY CLASSIFICATION BULK
SPECIAL FEATURESPRODUCT IS FOR NATIONAL SCIENCE FOUNDATION-SPONSORED ANTARCTIC FUELS OPERATIONS ONLY
DEPARTURE FROM CITED DOCUMENTDEPRESSED FREEZE POINT