Part Details | AVIATION TURBINE FUEL
9130-01-305-5597 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: IP8, MILT83133, MIL-T-83133, MILDTL83133, MIL-DTL-83133, 9130-01-305-5597, 01-305-5597, 9130013055597, 013055597
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | AUG 08, 1989 | 01-305-5597 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-305-5597
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| IP8 | 52838 | DEFENSE LOGISTICS AGENCYDBA DLA ENERGY |
| MIL-T-83133 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-DTL-83133 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9130-01-305-5597
| Characteristic | Specifications |
|---|---|
| FUEL GRADE CLASSIFICATION | JP-8 |
| NATO CODE NUMBER | F-34 |
| VISCOSITY AT RATED TEMP | 8.00 MAXIMUM -20 DEG CELSIUS |
| MINIMUM FLASH POINT AND TEST METHOD | 38.0 DEG CELSIUS PENSKY-MARTENS CLOSED CUP |
| DENSITY VALUE | 0.775 KILOGRAMS PER LITER MINIMUM AND 0.840 KILOGRAMS PER LITER MAXIMUM |
| DENSITY TEMP | 15.0 DEG CELSIUS |
| FREEZING POINT MAXIMUM TEMP | -47.0 DEG CELSIUS |
| MINIMUM HEAT OF COMBUSTION VALUE | -42.8$JCY18400.0 |
| 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 | 25.0 |
| MAXIMUM OLEFINS CONTENT PERCENTAGE BY VOLUME | 5.0 |
| DISTILLATION POINT PERCENTAGE AT MAXIMUM TEMP | 205.0 DEG C AT 10.0 PCT AND 300.0DEG C AT THE END POINT. |
| 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. |