Part Details | AVIATION TURBINE FUEL
9130-01-527-7832 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: DPK, MILDTL83133, MIL-DTL-83133, 9130-01-527-7832, 01-527-7832, 9130015277832, 015277832
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | FEB 17, 2005 | 01-527-7832 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-527-7832
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| DPK | 52838 | DEFENSE LOGISTICS AGENCYDBA DLA ENERGY |
| MIL-DTL-83133 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9130-01-527-7832
| Characteristic | Specifications |
|---|---|
| FUEL GRADE CLASSIFICATION | JP-8 |
| 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 MEGAJOULES PER KILOGRAM |
| COPPER CORROSION CLASSIFICATION NUMBER | 1 |
| MAXIMUM AMOUNT OF EXISTENT GUM | 7.0 |
| MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT | 0.20 |
| MAXIMUM AROMATICS PERCENTAGE BY VOLUME | 25.0 |
| DISTILLATION POINT PERCENTAGE AT MAXIMUM TEMP | 205.0 DEG C AT 10.0 PCT & 300.0 DEG C AT THE END POINT |
| MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE | 1.5 |
| SUPPLY CLASSIFICATION | BULK |
| SPECIAL FEATURES | THIS NSN IS APPLICABLE TO PIPELINE MOVEMENTS OF AVIATION FUEL AND IS USED ONLY FOR TRACKING PURPOSES WITHIN DLA; FOR REQUISITIONING PURPOSES USE NSN 9130-01-031-5816 |