| END HOLE INSIDE DIAMETER | 0.859 INCHES NOMINAL |
| BEARING REPLACEABILITY | REPLACEABLE |
| CROSS-SECTIONAL SHAPE STYLE | FLAT TYPE |
| END THICKNESS | 1.181 INCHES MINIMUM AND 1.189 INCHES MAXIMUM |
| FABRICATION METHOD | ANY ACCEPTABLE |
| PISTON CONNECTING END LUBRICATION METHOD | OIL VAPOR |
| PISTON CONNECTING END BEARING | INCLUDED |
| PISTON CONNECTING END LUBRICATION DRILL FEATURE | INCLUDED |
| PISTON END CONNECTION STYLE | SMALL ENGINE AND AUTOMOTIVE STANDARD |
| PROPRIETARY CHARACTERISTICS | PACS |
| SHAFT CONNECTING END BEARING REPLACEABILITY | REPLACEABLE |
| SHAFT CONNECTING END BEARING | INCLUDED |
| SHAFT CONNECTING END HOLE INSIDE DIAMETER | 1.811 INCHES NOMINAL |
| SHAFT CONNECTING END LUBRICATION DRILL FEATURE | NOT INCLUDED |
| SHAFT CONNECTING END LUBRICATION METHOD | SPLASH |
| SHAFT CONNECTING END STYLE | AUTOMOTIVE STANDARD SPLIT BEARING 2 BOLT |
| SHAFT CONNECTING END THICKNESS | 1.181 INCHES MINIMUM AND 1.183 INCHES MAXIMUM |
| SPECIAL FEATURES | GRUMMAN AEROSPACE A-10 AIRCRAFT |