Part Details | AVIATION TURBINE FUEL
9130-01-305-4096 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: ASTM D1655, IA1, 9130-01-305-4096, 01-305-4096, 9130013054096, 013054096
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | AUG 05, 1989 | 01-305-4096 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-305-4096
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ASTM D1655 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| IA1 | 52838 | DEFENSE LOGISTICS AGENCYDBA DLA ENERGY |
Technical Data | NSN 9130-01-305-4096
| Characteristic | Specifications |
|---|---|
| FUEL GRADE CLASSIFICATION | JET A-1 |
| VISCOSITY AT RATED TEMP | 8.00 MAXIMUM -20 DEG CELSIUS |
| MINIMUM FLASH POINT AND TEST METHOD | 38.0 DEG CELSIUS TAG CLOSED CUP |
| DENSITY VALUE | 775.000 KILOGRAMS PER CUBIC METER MINIMUM AND 840.000 KILOGRAMS PER CUBIC METER MAXIMUM |
| DENSITY TEMP | 15.0 DEG CELSIUS |
| FREEZING POINT MAXIMUM TEMP | -47.0 DEG CELSIUS |
| MINIMUM HEAT OF COMBUSTION VALUE | 42.8 MEGAJOULES PER KILOGRAM |
| 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 | 205.0 DEG C AT 10.0 PCT AND 300.0 DEG C AT FINAL BOILING PT. |
| MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE | 1.5 |
| SUPPLY CLASSIFICATION | BULK |
| SPECIAL FEATURES | THIS PRODUCT IS APPLICABLE ONLY TO INTO-PLANE PROCUREMENTS/CONTRACTS- IN ACCORDANCE WITH MIL-STD-1548 REQUIREMENTS. |