NSN 9130-01-233-8852
Part Details | AVIATION TURBINE FUEL
9130-01-233-8852 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: ASTMD1655, ASTM-D-1655, JAB, 9130-01-233-8852, 01-233-8852, 9130012338852, 012338852
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
91 | JUN 04, 1986 | 01-233-8852 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-233-8852
Part Number | Cage Code | Manufacturer |
---|---|---|
ASTM-D-1655 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
JAB | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9130-01-233-8852
Characteristic | Specifications |
---|---|
FUEL GRADE CLASSIFICATION | KERO/B |
SPECIFIC GRAVITY VALUE AT 15.56 DEG CELSIUS | 0.776 NOMINAL |
FREEZING POINT MAXIMUM TEMP | -50.0 DEG CELSIUS |
REID VAPOR PRESSURE RATING | 3.0 POUNDS PER SQUARE INCH MAXIMUM |
MINIMUM HEAT OF COMBUSTION VALUE | 18400.0 BRITISH THERMAL UNITS PER POUND |
COPPER CORROSION CLASSIFICATION NUMBER | 1 |
MAXIMUM AMOUNT OF EXISTENT GUM | 7.0 |
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT | 0.3 |
MAXIMUM AROMATICS PERCENTAGE BY VOLUME | 20.0 |
DISTILLATION POINT PERCENTAGE AT MAXIMUM TEMP | 243.3DEGCELSIUSAT90.0PERCENT |
MAXIMUM DISTILLATION RESIDUE VOLUME PERCENTAGE | 1.5 |
MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE | 1.5 |
EVAPORATION PERCENTAGE AT MAXIMUM TEMP | 143.3 20 PERCENT DEG CELSIUS |
SUPPLY CLASSIFICATION | BULK |
QUANTITY WITHIN EACH UNIT PACKAGE | 54.000 GALLONS |
TEST DATA DOCUMENT | 81348-STMD1655 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |