| EDGE RADIUS | 0.594 INCHES NOMINAL |
| END HOLE INSIDE DIAMETER | 0.750 INCHES NOMINAL |
| BEARING REPLACEABILITY | NONREPLACEABLE |
| BODY THICKNESS AT PISTON CONNECTING END | 0.906 INCHES NOMINAL |
| BODY THICKNESS AT SHAFT CONNECTING END | 0.969 INCHES NOMINAL |
| BODY WIDTH AT PISTON CONNECTING END | 1.031 INCHES NOMINAL |
| BODY WIDTH AT SHAFT CONNECTING END | 1.031 INCHES NOMINAL |
| CENTER TO CENTER EFFECTIVE LENGTH | 5.062 INCHES NOMINAL |
| CROSS-SECTIONAL SHAPE STYLE | I-SECTION TYPE |
| END THICKNESS | 1.125 INCHES NOMINAL |
| FABRICATION METHOD | CAST |
| MATERIAL | ALUMINUM |
| 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 HOLE INSIDE DIAMETER | 1.625 INCHES NOMINAL |
| SHAFT CONNECTING END LUBRICATION DRILL FEATURE | NOT INCLUDED |
| SHAFT CONNECTING END LUBRICATION METHOD | SPLASH |
| SHAFT CONNECTING END STYLE | 2 BOLT 45 DEGREES |
| SHAFT CONNECTING END THICKNESS | 1.125 INCHES NOMINAL |
| SHAFT CONNECTING END WIDTH | 2.875 INCHES NOMINAL |
| SHAFT CONNECTING END BEARING REPLACEABILITY | NONREPLACEABLE |
| SHAFT CONNECTING END BEARING | INCLUDED |
| SHAFT CONNECTING END EDGE RADIUS | 1.125 INCHES NOMINAL |
| SPECIAL FEATURES | GRUMMAN AEROSPACE A-10 AIRCRAFT |