330063-1: VALVE ASSEMBLY,TEMPERATURE DATUM.
VALVE ASSEMBLY,TEMPERATURE DATUM. Key specifications include material: ALUMINUM ALLOY, fsc_application_data: ENGINE FUEL TEMPERATURE SYSTEM,C-130 AIRCRAFT, end_item_identification: T56-A-7B AIRCRAFT ENGINE, reference_data_and_literature: T.O.6J15-3-87-4;PB-A3 TEMPERATUREDATUM VALVE ASSEMBLY, reference_number_differentiating_characteristics: AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO.. This part is cataloged in the U.S.
Government catalog under NSN 2915-00-628-3572, 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 | ALUMINUM ALLOY |
| fsc_application_data | ENGINE FUEL TEMPERATURE SYSTEM,C-130 AIRCRAFT |
| end_item_identification | T56-A-7B AIRCRAFT ENGINE |
| reference_data_and_literature | T.O.6J15-3-87-4;PB-A3 TEMPERATUREDATUM VALVE ASSEMBLY |
| reference_number_differentiating_characteristics | AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO. |
| NSN | 2915-00-628-3572 |
| FSC APPLICATION DATA | ENGINE FUEL TEMPERATURE SYSTEM,C-130 AIRCRAFT |
| REFERENCE DATA AND LITERATURE | T.O.6J15-3-87-4;PB-A3 TEMPERATUREDATUM VALVE ASSEMBLY |
| END ITEM IDENTIFICATION | T56-A-7B AIRCRAFT ENGINE |
| MATERIAL | ALUMINUM ALLOY |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO. |