R11525: MANIFOLD,FLUID,AIRCRAFT.
The MANIFOLD,FLUID,AIRCRAFT is a the manufacturer industrial component. Key specifications include functional_description: USED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE, end_item_identification: T-38A AIRCRAFT ENGINE A, part_name_assigned_by_controlling_agency: MANIFOLD,ENGINE FUEL,RH ENG. This part is cataloged in the U.S.
Government catalog under NSN 2995-00-884-3285, 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.
| special_features | NO FLAMMABLE MATERIALS SHALL BE USED. DISSIMILAR METALS SHALL NOT BE USED. METALLIC SURFACES SHALL BE TREATED I/A/W MIL-F-7179 |
| functional_description | USED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE |
| supplementary_features | FUEL PRESSURE WILL BE 50 PSIG,FLUID TEMPERATURE WILL RANGE FROM -65F TO 110F,AMBIENT TEMPERATURE WILL RANGE FROM -65F TO 200F |
| end_item_identification | T-38A AIRCRAFT ENGINE A |
| part_name_assigned_by_controlling_agency | MANIFOLD,ENGINE FUEL,RH ENG |
| NSN | 2995-00-884-3285 |
| SUPPLEMENTARY FEATURES | FUEL PRESSURE WILL BE 50 PSIG,FLUID TEMPERATURE WILL RANGE FROM -65F TO 110F,AMBIENT TEMPERATURE WILL RANGE FROM -65F TO 200F |
| SPECIAL FEATURES | NO FLAMMABLE MATERIALS SHALL BE USED. DISSIMILAR METALS SHALL NOT BE USED. METALLIC SURFACES SHALL BE TREATED I/A/W MIL-F-7179 |
| FUNCTIONAL DESCRIPTION | USED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MANIFOLD,ENGINE FUEL,RH ENG |
| END ITEM IDENTIFICATION | T-38A AIRCRAFT ENGINE A |