ROCKER ARM ASSEMBLY,ENGINE POPPE. Key specifications include material: COPPER ALLOY SEDIMENT BOWL, mesh_size: 100.0, body_width: 2.750 INCHES NOMINAL IN, body_height: 3.875 INCHES MAXIMUM IN, body_length: 3.250 INCHES NOMINAL IN, mounting_type: INLET CONNECTION AND OUTLET CONNECTION HEAD SIDE. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2910-00-778-8646, 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 | COPPER ALLOY SEDIMENT BOWL |
| mesh_size | 100.0 |
| body_width | 2.750 INCHES NOMINAL IN |
| body_height | 3.875 INCHES MAXIMUM IN |
| body_length | 3.250 INCHES NOMINAL IN |
| mounting_type | INLET CONNECTION AND OUTLET CONNECTION HEAD SIDE |
| wire_diameter | 0.0045 INCHES NOMINAL IN |
| special_features | GRUMMAN AEROSPACE CORP A10 AIRCRAFT |
| style_designator | UNTHREADED SHELL W/SELECTIVE FLOW |
| features_provided | DRAIN PLUG AND MANUAL SHUT-OFF VALVE |
| filtering_media_design | MESH SINGLE FILTERING MEDIA RESPONSE |
| media_for_which_designed | FUEL/OIL, HYDROCARBON |
| NSN | 2910-00-778-8646 |