| ANTIROTATION/LUBRICATION TYPE AND QUANTITY | 3 HOLE |
| BODY INSIDE DIAMETER | 3.1330 INCHES MINIMUM AND 3.1370 INCHES MAXIMUM |
| BODY OUTSIDE DIAMETER | 3.3550 INCHES MINIMUM AND 3.3560 INCHES MAXIMUM |
| CORNER SHAPE | CHAMFERED INSIDE RIGHT CORNER |
| CORNER SHAPE | CHAMFERED OUTSIDE LEFT CORNER |
| CORNER SHAPE | ROUND INSIDE LEFT CORNER |
| CORNER SHAPE | SQUARE OUTSIDE RIGHT CORNER |
| FEATURES PROVIDED | CASEHARDENED |
| HARDNESS RATING | 30.0 ROCKWELL C MINIMUM AND 40.0 ROCKWELL C MAXIMUM OVERALL |
| HOLE DIAMETER | 0.1225 INCHES MINIMUM AND 0.1245 INCHES MAXIMUM FIRST |
| LEFT INTERNAL FLANGE HOLE DIAMETER | 2.8900 INCHES MINIMUM AND 2.9100 INCHES MAXIMUM |
| LEFT INTERNAL FLANGE WIDTH | 0.0830 INCHES MINIMUM AND 0.0870 INCHES MAXIMUM |
| LUBRICANT ACCOMMODATION STYLE | GROOVED CIRCULAR |
| OVERALL LENGTH | 0.8600 INCHES MINIMUM AND 0.8800 INCHES MAXIMUM |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6260 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| MATERIAL | STEEL COMP E9310 OVERALL |
| SPECIAL FEATURES | FAILURE COULD CAUSE CATASTROPHIC OR CRITICAL FAILURE RESULTING IN THE LOSS OF OR SERIOUS DAMAGE TO THE AIRCRAFT OR WEAPON SYSTEM OR AN UNCOMMANDED ENGINE SHUTDOWN THAT JEOPARDIZES SAFETY |
| STYLE DESIGNATOR | SOLID, PLAIN, NO OUTSIDE FLANGES, INTERNAL FLANGE ONE END |
| SURFACE FINISH | 63.0 MICROINCHES INTERMEDIATE LAYER |
| SURFACE GROOVE LOCATION AND QUANTITY | 1 INTERNAL |