540423-6: RESTRICTOR,FLUID FLOW.
The RESTRICTOR,FLUID FLOW is a the manufacturer industrial component. Key specifications include length: 2.500 INCHES NOMINAL IN, material: ALUMINUM, design_type: TUBULAR, thread_class: 2B LOCATION NOT OTHERWISE SPECIFIED, thread_length: 0.280 INCHES NOMINAL LOCATION NOT OTHERWISE SPECIFIED IN, thread_series: UNIFIED NATIONAL COARSE (UNC) LOCATION NOT OTHERWISE SPECIFIED. This part is cataloged in the U.S.
Government catalog under NSN 4730-00-618-8335, 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.
| length | 2.500 INCHES NOMINAL IN |
| material | ALUMINUM |
| design_type | TUBULAR |
| thread_class | 2B LOCATION NOT OTHERWISE SPECIFIED |
| thread_length | 0.280 INCHES NOMINAL LOCATION NOT OTHERWISE SPECIFIED IN |
| thread_series | UNIFIED NATIONAL COARSE (UNC) LOCATION NOT OTHERWISE SPECIFIED |
| orifice_diameter | 0.075 INCHES NOMINAL IN |
| outside_diameter | 0.275 INCHES NOMINAL IN |
| thread_direction | RIGHT-HAND LOCATION NOT OTHERWISE SPECIFIED |
| thread_provision | THREADED LOCATION NOT OTHERWISE SPECIFIED |
| fsc_application_data | FUEL SYSTEM,ENGINE,AIRCRAFT |
| thread_size_designator | NO. 6-32 LOCATION NOT OTHERWISE SPECIFIED |
| NSN | 4730-00-618-8335 |
| FSC APPLICATION DATA | FUEL SYSTEM,ENGINE,AIRCRAFT |
| LENGTH | 2.500 INCHES NOMINAL IN |
| THREAD PROVISION | THREADED LOCATION NOT OTHERWISE SPECIFIED |
| DESIGN TYPE | TUBULAR |
| THREAD SERIES | UNIFIED NATIONAL COARSE (UNC) LOCATION NOT OTHERWISE SPECIFIED |
| THREAD LENGTH | 0.280 INCHES NOMINAL LOCATION NOT OTHERWISE SPECIFIED IN |
| OUTSIDE DIAMETER | 0.275 INCHES NOMINAL IN |
| THREAD DIRECTION | RIGHT-HAND LOCATION NOT OTHERWISE SPECIFIED |
| THREAD SIZE DESIGNATOR | NO. 6-32 LOCATION NOT OTHERWISE SPECIFIED |
| THREAD CLASS | 2B LOCATION NOT OTHERWISE SPECIFIED |
No substitute or cross-reference records for this part.