406020: FUEL CONTROL,MAIN,TURBINE ENGINE.
FUEL CONTROL,MAIN,TURBINE ENGINE. Key specifications include fsc_application_data: ENGINE FUEL SYSTEM COMPONENTS,AIRCRAFT, end_item_identification: J79-GE-15/-15A ENGINE A, reference_number_differentiating_characteristics: AS DIFFERENIATED BY SOURCE CONTROL NO. 635E223P19.
This part is cataloged in the U.S. Government catalog under NSN 4730-00-702-6342, 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.
| fsc_application_data | ENGINE FUEL SYSTEM COMPONENTS,AIRCRAFT |
| end_item_identification | J79-GE-15/-15A ENGINE A |
| reference_number_differentiating_characteristics | AS DIFFERENIATED BY SOURCE CONTROL NO. 635E223P19 |
| NSN | 4730-00-702-6342 |
| FLOW ANGLE | 90.0 DEGREES |
| NOMINAL PIPE SIZE ACCOMMODATED | 2.000 INCHES ALL ENDS IN |
| CONNECTION STYLE | SOCKET (PIPE) ALL ENDS |
| CONNECTION TYPE | UNTHREADED INTERNAL PIPE ALL ENDS |
| MATERIAL DOCUMENT AND CLASSIFICATION | ASTM D2466 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OPERATING PRESSURE | 260.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM FIRST RESPONSE LBS |
| OPERATING PRESSURE | 260.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SECOND RESPONSE LBS |
| LEG LENGTH | 2.750 INCHES NOMINAL ALL ENDS IN |
| SPECIFICATION/STANDARD DATA | 81346-ASTMD2466 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| MAXIMUM OPERATING TEMP | 25.0 FAHRENHEIT FIRST RESPONSE DEGF |