MS21916W6-4: INJECTOR ASSEMBLY,FUEL.
The INJECTOR ASSEMBLY,FUEL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY OVERALL, reducer_type: CONCENTRIC, thread_class: 3A ALL ENDS A, connection_type: THREADED EXTERNAL BOSS ALL ENDS, connection_style: EXTERNAL SEAT FOR GASKET SEAL (BOSS) ALL ENDS, surface_treatment: ANODIZE OUTSIDE. This part is cataloged in the U.S.
Government catalog under NSN 4730-00-166-4191, 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 | ALUMINUM ALLOY OVERALL |
| reducer_type | CONCENTRIC |
| thread_class | 3A ALL ENDS A |
| connection_type | THREADED EXTERNAL BOSS ALL ENDS |
| connection_style | EXTERNAL SEAT FOR GASKET SEAL (BOSS) ALL ENDS |
| surface_treatment | ANODIZE OUTSIDE |
| operating_pressure | 3000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| nominal_thread_size | 0.438 INCHES SECOND END IN |
| nominal_overall_length | 1.219 INCHES IN |
| media_for_which_designed | AERONAUTICAL FLUID SINGLE RESPONSE |
| thread_series_designator | UNIFIED NATIONAL JOINT FINE (UNJF) ALL ENDS |
| material_document_and_classification | QQ-A-250/12,ALLOY 7075 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 4730-00-166-4191 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE OUTSIDE |
| CONNECTION STYLE | EXTERNAL SEAT FOR GASKET SEAL (BOSS) ALL ENDS |
| NOMINAL OVERALL LENGTH | 1.219 INCHES IN |
| CONNECTION TYPE | THREADED EXTERNAL BOSS ALL ENDS |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12,ALLOY 7075 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| OPERATING PRESSURE | 3000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| NOMINAL THREAD SIZE | 0.438 INCHES SECOND END IN |
| NOMINAL THREAD SIZE | 0.562 INCHES FIRST END IN |
| SURFACE TREATMENT | ANODIZE OUTSIDE |
| MEDIA FOR WHICH DESIGNED | AERONAUTICAL FLUID SINGLE RESPONSE |