| ELONGATION PERCENTAGE | 125 MAXIMUM |
| CENTER HOLE DIAMETER | 2.158 INCHES MINIMUM AND 2.192 INCHES MAXIMUM |
| CROSS-SECTIONAL HEIGHT | 0.100 INCHES MINIMUM AND 0.106 INCHES MAXIMUM |
| HARDNESS RATING | 70.0 SHORE DUROMETER A MINIMUM AND 80.0 SHORE DUROMETER A MAXIMUM |
| MATERIAL | RUBBER |
| PERIPHERAL DIAMETER | 2.381 INCHES NOMINAL |
| SPECIAL FEATURES | MATERIAL RUBBER FLUOROCARBON CLASS FKM AMS7276;CROSS-SECTIONAL SHAPE STYLE: O-RING;CROSS SECTION OUTSIDE DIAMETER: 0.100 IN. MIN, AND 0.106 IN. MAX.;FUNCTIONAL DESCRIPTION: AIRCRAFT ENGINE AND PROPELLER |
| SPECIFICATION/STANDARD DATA | 81343-AS3209 GOVERNMENT STANDARD |
| TEMP RATING | -29.0 CELSIUS AND 204.0 CELSIUS |