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 Federal Logistics Information System (FLIS) 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 |
| MEDIA FOR WHICH DESIGNED | STEAM FIRST RESPONSE |
| MEDIA FOR WHICH DESIGNED | WATER-OIL-GAS SECOND RESPONSE |
| PIPE WALL THICKNESS DESIGNATION FOR WHICH DESIGNED | SCHEDULE 40 ALL ENDS |
| MATERIAL DOCUMENT AND CLASSIFICATION | ASTM D2466 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OPERATING PRESSURE | 260.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SECOND RESPONSE LBS |
| FLOW ANGLE | 90.0 DEGREES |
| SPECIFICATION/STANDARD DATA | 81346-ASTMD2466 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| MATERIAL | PLASTIC POLYVINYL CHLORIDE (PVC) OVERALL |
| NOMINAL PIPE SIZE ACCOMMODATED | 2.000 INCHES ALL ENDS IN |
| OPERATING PRESSURE | 260.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM FIRST RESPONSE LBS |