400872: CONNECTOR,RECEPTACLE,ELECTRICAL.
CONNECTOR,RECEPTACLE,ELECTRICAL. Key specifications include body_style: RECTANGULAR SHAPE, overall_width: 0.340 INCHES NOMINAL IN, overall_height: 0.458 INCHES NOMINAL IN, overall_length: 3.195 INCHES NOMINAL IN, insert_material: PLASTIC POLYESTER GLASS FILLED SINGLE MATING END, special_features: ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-784-5962, 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.
| body_style | RECTANGULAR SHAPE |
| overall_width | 0.340 INCHES NOMINAL IN |
| overall_height | 0.458 INCHES NOMINAL IN |
| overall_length | 3.195 INCHES NOMINAL IN |
| insert_material | PLASTIC POLYESTER GLASS FILLED SINGLE MATING END |
| special_features | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| precious_material | GOLD |
| terminal_location | BACK SINGLE MATING END SINGLE CONTACT GROUPING |
| mating_end_quantity | 1 |
| included_contact_type | BIFURCATED SPRING SINGLE MATING END SINGLE CONTACT GROUPING |
| supplementary_features | MOUNTING METHOD - UNTHREADED HOLE |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| NSN | 2840-00-784-5962 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.