Part Details | AVIATION TURBINE FUEL
9130-01-180-5540 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: ASTMD1655TYA1MOD, 9130-01-180-5540, 01-180-5540, 9130011805540, 011805540
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
91 | MAY 30, 1984 | 01-180-5540 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-180-5540
Part Number | Cage Code | Manufacturer |
---|---|---|
ASTMD1655TYA1MOD | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
Technical Data | NSN 9130-01-180-5540
Characteristic | Specifications |
---|---|
FUEL GRADE CLASSIFICATION | JET A-1 |
VISCOSITY AT RATED TEMP | 12.22 MAXIMUM -20 DEG CELSIUS |
MINIMUM FLASH POINT AND TEST METHOD | 140.0 DEG FAHRENHEIT TAG CLOSED CUP |
SPECIFIC GRAVITY VALUE AT 15.56 DEG CELSIUS | 0.7753 MINIMUM AND 0.8398 MAXIMUM |
FREEZING POINT MAXIMUM TEMP | -47.0 DEG CELSIUS |
MINIMUM HEAT OF COMBUSTION VALUE | 18400.0 BRITISH THERMAL UNITS PER POUND |
MAXIMUM AMOUNT OF EXISTENT GUM | 7.0 |
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT | 0.3 |
MAXIMUM AROMATICS PERCENTAGE BY VOLUME | 20.0 |
MAXIMUM DISTILLATION RESIDUE VOLUME PERCENTAGE | 1.5 |
SUPPLY CLASSIFICATION | BULK |
SPECIAL FEATURES | MINIMUNFLASHPOINT60.0DEGCELSIUS |