Part Details | SYNTHETIC AIRCRAFT TURBINE ENGINE LUBRICATING OIL
9150-00-180-6266
Alternate Parts: MILPRF23699, MIL-PRF-23699, MILL23699 CI, MIL-L-23699 C/I, MILL23699, MILPRF23699 CI, MIL-PRF-23699 C/I, 9150-00-180-6266, 00-180-6266, 9150001806266, 001806266
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
91 | DEC 12, 1969 | 00-180-6266 | 26717 ( LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9150-00-180-6266
Part Number | Cage Code | Manufacturer |
---|---|---|
MIL-PRF-23699 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MIL-L-23699 C/I | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MILL23699 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MIL-PRF-23699 C/I | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9150-00-180-6266
Characteristic | Specifications |
---|---|
FATTY MATERIAL TYPE | ANY ACCEPTABLE |
BASIC INGREDIENT | SYNTHETIC BASE |
VISCOSITY AT RATED TEMP | 25.00 MINIMUM 100 DEG FAHRENHEIT AND 5.00 MINIMUM 210 DEG FAHRENHEIT AND 5.50 MAXIMUM 210 DEG FAHRENHEIT |
MAXIMUM POUR POINT | -65.0 DEG FAHRENHEIT |
MINIMUM FLASH POINT AND TEST METHOD | 475.0 DEG FAHRENHEIT CLEVELAND OPEN CUP |
SERVICE CHARACTERISTICS | ANTIFOAM AND ANTIWEAR AND D ANY ACCEPTABLE AND H ANY ACCEPTABLE AND J ANY ACCEPTABLE AND L ANY ACCEPTABLE |
QUANTITY WITHIN EACH UNIT PACKAGE | 7.500 OUNCES, FLUID |
SPECIAL FEATURES | NATO CODE 0-156 |