NSN 9130-01-221-1880
Part Details | AVIATION TURBINE FUEL
9130-01-221-1880 A liquid petroleum distillate refined especially for use in aviation turbine engines.
Alternate Parts: ASTMD1655, ASTM-D-1655, J50, 9130-01-221-1880, 01-221-1880, 9130012211880, 012211880
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | NOV 25, 1985 | 01-221-1880 | 26646 ( TURBINE FUEL, AVIATION ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-221-1880
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ASTM-D-1655 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| J50 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9130-01-221-1880
| Characteristic | Specifications |
|---|---|
| FUEL GRADE CLASSIFICATION | JET A-1 |
| VISCOSITY AT RATED TEMP | 8.00 MAXIMUM -20 DEG CELSIUS |
| MINIMUM FLASH POINT AND TEST METHOD | 37.8 DEG CELSIUS TAG CLOSED CUP |
| SPECIFIC GRAVITY VALUE AT 15.56 DEG CELSIUS | 0.8024 NOMINAL |
| FREEZING POINT MAXIMUM TEMP | -50.0 DEG CELSIUS |
| MINIMUM HEAT OF COMBUSTION VALUE | 18400.0 BRITISH THERMAL UNITS PER POUND |
| 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 | 20.0 |
| DISTILLATION POINT PERCENTAGE AT MAXIMUM TEMP | 204.4DEGCELSIUSAT10.0PERCENT |
| MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE | 1.5 |
| SUPPLY CLASSIFICATION | PACKAGED |
| QUANTITY WITHIN EACH UNIT PACKAGE | 55.0 GALLONS |
| TEST DATA DOCUMENT | 81346-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.). |
