| EDGE RADIUS | 0.750 INCHES NOMINAL |
| END HOLE INSIDE DIAMETER | 0.750 INCHES NOMINAL |
| BEARING REPLACEABILITY | REPLACEABLE |
| BODY THICKNESS AT PISTON CONNECTING END | 0.500 INCHES NOMINAL |
| BODY THICKNESS AT SHAFT CONNECTING END | 0.500 INCHES NOMINAL |
| BODY WIDTH AT PISTON CONNECTING END | 0.688 INCHES NOMINAL |
| BODY WIDTH AT SHAFT CONNECTING END | 0.812 INCHES NOMINAL |
| CENTER TO CENTER EFFECTIVE LENGTH | 8.000 INCHES NOMINAL |
| CROSS-SECTIONAL SHAPE STYLE | I-SECTION TYPE |
| END THICKNESS | 1.250 INCHES NOMINAL |
| FABRICATION METHOD | CAST |
| MATERIAL | STEEL |
| PISTON CONNECTING END BEARING | INCLUDED |
| PISTON CONNECTING END LUBRICATION DRILL FEATURE | INCLUDED |
| PISTON CONNECTING END LUBRICATION METHOD | SPLASH |
| PISTON END CONNECTION STYLE | SMALL ENGINE AND AUTOMOTIVE STANDARD |
| SHAFT CONNECTING END BEARING | NOT INCLUDED |
| SHAFT CONNECTING END EDGE RADIUS | 1.500 INCHES NOMINAL |
| SHAFT CONNECTING END HOLE INSIDE DIAMETER | 1.250 INCHES NOMINAL |
| SHAFT CONNECTING END LUBRICATION DRILL FEATURE | INCLUDED |
| SHAFT CONNECTING END LUBRICATION METHOD | SPLASH |
| SHAFT CONNECTING END STYLE | AUTOMOTIVE STANDARD SPLIT BEARING 2 BOLT |
| SHAFT CONNECTING END THICKNESS | 1.250 INCHES NOMINAL |
| SHAFT CONNECTING END WIDTH | 2.250 INCHES NOMINAL |
| SPECIAL FEATURES | GRUMMAN AEROSPACE A-10 AIRCRAFT |