The 94851 is a the manufacturer industrial component. Key specifications include material: RUBBER SYNTHETIC AND TITANIUM ALLOY OVERALL, overall_length: 3.200 INCHES MAXIMUM IN, style_designator: STRIP, attachment_method: ROUND HOLE, end_item_identification: F/A-18E/F AIRCRAFT, attachment_feature_width: 0.500 INCHES NOMINAL IN. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2240-00-367-4105, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | RUBBER SYNTHETIC AND TITANIUM ALLOY OVERALL |
| overall_length | 3.200 INCHES MAXIMUM IN |
| style_designator | STRIP |
| attachment_method | ROUND HOLE |
| end_item_identification | F/A-18E/F AIRCRAFT |
| attachment_feature_width | 0.500 INCHES NOMINAL IN |
| attachment_hole_diameter | 0.228 INCHES NOMINAL IN |
| attachment_feature_length | 2.740 INCHES NOMINAL IN |
| attachment_feature_quantity | 3 |
| material_document_and_classification | MIL-T-9046 COND ANL MIL SPEC 2ND MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | SEAL,CLOSEOUT-ENGINE BAY DOOR,AFT FUS |
| attachment_feature_center_to_center_distance_along_length | 0.720 INCHES NOMINAL IN |
| NSN | 2240-00-367-4105 |
| END ITEM IDENTIFICATION | 22301749135,22302972041,22202896465 |