5054M61G08: MANIFOLD,FLUID,AIRCRAFT.
The MANIFOLD,FLUID,AIRCRAFT is a the manufacturer industrial component. Key specifications include overall_width: 3.000 INCHES NOMINAL IN, overall_length: 6.000 INCHES NOMINAL IN, metering_valves: NOT PROVIDED, overall_thickness: 1.500 INCHES NOMINAL IN, connection_diameter: 0.750 INCHES NOMINAL AND 0.250 INCHES NOMINAL IN, fsc_application_data: FUEL SYSTEM, AIRCRAFT PROPULSION. This part is cataloged in the U.S.
Government catalog under NSN 2995-01-310-2142, 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.
| overall_width | 3.000 INCHES NOMINAL IN |
| overall_length | 6.000 INCHES NOMINAL IN |
| metering_valves | NOT PROVIDED |
| overall_thickness | 1.500 INCHES NOMINAL IN |
| connection_diameter | 0.750 INCHES NOMINAL AND 0.250 INCHES NOMINAL IN |
| connection_quantity | 4 |
| fsc_application_data | FUEL SYSTEM, AIRCRAFT PROPULSION |
| end_item_identification | F110-GE-129;TURBO FAN AUGMENTED ENGINE;T.O.2J-F110-14;DISTRIBUTOR,FAN/CORE,AUGMENTER,FUEL |
| NSN | 2995-01-310-2142 |
| FSC APPLICATION DATA | FUEL SYSTEM, AIRCRAFT PROPULSION |
| OVERALL THICKNESS | 1.500 INCHES NOMINAL IN |
| OVERALL LENGTH | 6.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.000 INCHES NOMINAL IN |
| END ITEM IDENTIFICATION | F110-GE-129;TURBO FAN AUGMENTED ENGINE;T.O.2J-F110-14;DISTRIBUTOR,FAN/CORE,AUGMENTER,FUEL |
| CONNECTION QUANTITY | 4 |
| CONNECTION DIAMETER | 0.750 INCHES NOMINAL AND 0.250 INCHES NOMINAL IN |
| METERING VALVES | NOT PROVIDED |
No substitute or cross-reference records for this part.