NSN 9130-01-305-5595
Part Details | AVIATION TURBINE FUEL
9130-01-305-5595 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: ASTMD1655, ASTMD6615, ASTM-D-6615, IAB, IAB, 9130-01-305-5595, 01-305-5595, 9130013055595, 013055595
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | AUG 08, 1989 | 01-305-5595 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-305-5595
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ASTMD1655 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| ASTM-D-6615 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| IAB | 52838 | DEFENSE LOGISTICS AGENCYDBA DLA ENERGY |
| IAB | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9130-01-305-5595
| Characteristic | Specifications |
|---|---|
| FUEL GRADE CLASSIFICATION | KERO/B |
| DENSITY VALUE | HRB751.000 KILOGRAMS PER CUBIC METER AND HRC802.000 KILOGRAMS PER CUBIC METER |
| DENSITY TEMP | 15.0 DEG CELSIUS |
| FREEZING POINT MAXIMUM TEMP | -50.0 DEG CELSIUS |
| REID VAPOR PRESSURE RATING | LGB14.0 KILOPASCALS AND LGC21.0 KILOPASCALS |
| 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 | 25.0 |
| DISTILLATION POINT PERCENTAGE AT MAXIMUM TEMP | 145.0 DEG C AT 20.0 PCT,190.0 DEG C AT 50.0 PCT AND 245.0 DEG C AT 90.0 PCT. |
| 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. |