Part Details | AVIATION TURBINE FUEL
9130-01-234-1737 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: ASTMD1655, ASTM-D-1655, ASTM D6615, JAB, 9130-01-234-1737, 01-234-1737, 9130012341737, 012341737
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | JUN 09, 1986 | 01-234-1737 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-234-1737
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ASTM-D-1655 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| ASTM D6615 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| JAB | 52838 | DEFENSE LOGISTICS AGENCYDBA DLA ENERGY |
Technical Data | NSN 9130-01-234-1737
| Characteristic | Specifications |
|---|---|
| FUEL GRADE CLASSIFICATION | KERO/B |
| SPECIFIC GRAVITY VALUE AT 15.56 DEG CELSIUS | 15.560 NOMINAL |
| DENSITY VALUE | 751.000 KILOGRAMS PER CUBIC METER MINIMUM AND 802.000 KILOGRAMS PER CUBIC METER MAXIMUM |
| DENSITY TEMP | 15.0 DEG CELSIUS |
| FREEZING POINT MAXIMUM TEMP | -50.0 DEG CELSIUS |
| REID VAPOR PRESSURE RATING | 14.0 KILOPASCALS MINIMUM AND 21.0 KILOPASCALS MAXIMUM |
| 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 | 90-145 DEG C AT 20PCT, 110-190 DEG C AT 50 PCT AND 245 DEG C MAXIMUM AT 90 PCT |
| MAXIMUM DISTILLATION RESIDUE VOLUME PERCENTAGE | 1.5 |
| MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE | 1.5 |
| SUPPLY CLASSIFICATION | BULK |
| TEST DATA DOCUMENT | 81348-STMD1655 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |