| EDGE RADIUS | 0.473 INCHES NOMINAL |
| END HOLE INSIDE DIAMETER | 0.418 INCHES NOMINAL |
| BODY THICKNESS AT PISTON CONNECTING END | 0.450 INCHES NOMINAL |
| BODY THICKNESS AT SHAFT CONNECTING END | 0.450 INCHES NOMINAL |
| BODY WIDTH AT PISTON CONNECTING END | 0.540 INCHES NOMINAL |
| BODY WIDTH AT SHAFT CONNECTING END | 0.625 INCHES NOMINAL |
| CENTER TO CENTER EFFECTIVE LENGTH | 3.875 INCHES NOMINAL |
| CROSS-SECTIONAL SHAPE STYLE | I-SECTION TYPE |
| END THICKNESS | 0.730 INCHES NOMINAL |
| FABRICATION METHOD | CAST AND MACHINED |
| MATERIAL | ALUMINUM ALLOY |
| PISTON CONNECTING END BEARING | NOT INCLUDED |
| PISTON CONNECTING END LUBRICATION DRILL FEATURE | NOT INCLUDED |
| PISTON CONNECTING END LUBRICATION METHOD | SPLASH |
| PISTON END CONNECTION STYLE | SMALL ENGINE AND AUTOMOTIVE STANDARD |
| SHAFT CONNECTING END HOLE INSIDE DIAMETER | 0.878 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 | 0.714 INCHES NOMINAL |
| SHAFT CONNECTING END WIDTH | 1.754 INCHES NOMINAL |
| SHAFT CONNECTING END EDGE RADIUS | 0.824 INCHES NOMINAL |
| SHAFT CONNECTING END BEARING | NOT INCLUDED |
| SPECIAL FEATURES | GRUMMAN AEROSPACE A-10 AIRCRAFT |