Part Details | AVIATION TURBINE FUEL
9130-01-287-2704 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: MILT5624, MILDTL5624T, MIL-DTL-5624T, JP5, 9130-01-287-2704, 01-287-2704, 9130012872704, 012872704
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | OCT 19, 1988 | 01-287-2704 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-287-2704
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MILT5624 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-DTL-5624T | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| JP5 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9130-01-287-2704
| Characteristic | Specifications |
|---|---|
| FUEL GRADE CLASSIFICATION | JP-5 |
| NATO CODE NUMBER | F44 |
| VISCOSITY AT RATED TEMP | 8.50 MAXIMUM -20 DEG CELSIUS |
| MINIMUM FLASH POINT AND TEST METHOD | 60.0 DEG CELSIUS PENSKY-MARTENS CLOSED CUP |
| DENSITY VALUE | 0.788 KILOGRAMS PER LITER MINIMUM AND 0.845 KILOGRAMS PER LITER MAXIMUM |
| DENSITY TEMP | 15.0 DEG CELSIUS |
| FREEZING POINT MAXIMUM TEMP | -46.0 DEG CELSIUS |
| MINIMUM HEAT OF COMBUSTION VALUE | 42.6 MEGAJOULES PER KILOGRAM |
| COPPER CORROSION CLASSIFICATION NUMBER | 1B |
| MAXIMUM AMOUNT OF EXISTENT GUM | 7.0 |
| MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT | 0.4 |
| MAXIMUM AROMATICS PERCENTAGE BY VOLUME | 25.0 |
| MAXIMUM OLEFINS CONTENT PERCENTAGE BY VOLUME | 5.0 |
| DISTILLATION POINT PERCENTAGE AT MAXIMUM TEMP | 300.0 DEG CELSIUS AT THE FBP |
| MAXIMUM DISTILLATION RESIDUE VOLUME PERCENTAGE | 1.5 |
| MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE | 1.5 |
| MANDATORY ADDITIVE | FSII AND CORROSION INHIBITOR |
| SUPPLY CLASSIFICATION | PACKAGED |
| QUANTITY WITHIN EACH UNIT PACKAGE | 5.0 GALLONS |
| SPECIFICATION/STANDARD DATA | 81349-MIL-T-5624 GOVERNMENT SPECIFICATION |