1264M12P04: MANIFOLD,FLUID,AIRCRAFT.
The MANIFOLD,FLUID,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL, metering_valves: NOT PROVIDED, connection_diameter: 0.375 INCHES NOMINAL IN, fsc_application_data: MISCELLANEOUS ENGINE ACCESSORIES,AIRCRAFT, functional_description: USED FOR STATOR ACTR,ROD END, supplementary_features: CONNECTION WALL THK 0.028 IN. IN.
This part is cataloged in the U.S. Government catalog under NSN 2995-01-198-9265, 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 | STEEL |
| metering_valves | NOT PROVIDED |
| connection_diameter | 0.375 INCHES NOMINAL IN |
| connection_quantity | 3 |
| fsc_application_data | MISCELLANEOUS ENGINE ACCESSORIES,AIRCRAFT |
| functional_description | USED FOR STATOR ACTR,ROD END |
| supplementary_features | CONNECTION WALL THK 0.028 IN. IN |
| relationship_to_similar_equipment | SIMILAR TO PN 9504M49 |
| NSN | 2995-01-198-9265 |
| FSC APPLICATION DATA | MISCELLANEOUS ENGINE ACCESSORIES,AIRCRAFT |
| RELATIONSHIP TO SIMILAR EQUIPMENT | SIMILAR TO PN 9504M49 |
| SUPPLEMENTARY FEATURES | CONNECTION WALL THK 0.028 IN. IN |
| SPECIAL FEATURES | HYDRAULIC PRESSURE TEST PER AMS 2615 CL-A PRIOR TO FINAL FLUOR PENETRANT INSPECTION AT 3000 PSIG FOR 1 MINUTE MINIMUM; AFTER WELDING AND PRIOR TO FLUOR PENETRANT INSPECTION, STRESS RELIEVE AT 1100 DEGREES FAHRENHEIT, + OR - 25F FOR 1 TO 2 HOURS IN A VACCUM PER P10TF1 CL-A (VACUUM HEAT TREATING AND BRAZING) OR IN AN INERT ATMOSPHERE PER AMS 2801 (HEAT TREATMENT OF TITANIUM PARTS) |
| FUNCTIONAL DESCRIPTION | USED FOR STATOR ACTR,ROD END |
| MATERIAL | STEEL |
| CONNECTION QUANTITY | 3 |
| CONNECTION DIAMETER | 0.375 INCHES NOMINAL IN |
| METERING VALVES | NOT PROVIDED |