AS4139: INJECTOR ASSEMBLY,FUEL.
The INJECTOR ASSEMBLY,FUEL is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY OVERALL, leg_length: 1.204 INCHES NOMINAL SECOND END IN, seat_angle: 24.0 DEGREES SECOND END, thread_class: 3A THIRD END A, nominal_width: 0.577 INCHES ALL ENDS IN, connection_type: THREADED EXTERNAL TUBE THIRD END. This part is cataloged in the U.S.
Government catalog under NSN 4730-01-583-1044, 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 | TITANIUM ALLOY OVERALL |
| leg_length | 1.204 INCHES NOMINAL SECOND END IN |
| seat_angle | 24.0 DEGREES SECOND END |
| thread_class | 3A THIRD END A |
| nominal_width | 0.577 INCHES ALL ENDS IN |
| connection_type | THREADED EXTERNAL TUBE THIRD END |
| connection_style | SWIVEL NUT FLARELESS (SWIVEL NUT ATTACHMENT METHOD OPTIONAL)(TUBE) FIRST END |
| special_features | ITEM IS FAA CERTIFIED |
| style_designator | TEE |
| surface_treatment | PHOSPHATE FLUORIDE OVERALL |
| operating_pressure | 3000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| nominal_thread_size | 0.750 INCHES ALL ENDS IN |
| NSN | 4730-01-583-1044 |
| END ITEM IDENTIFICATION | UH-1 4 BLADED ROTOR HEAD UPGRADE |