The INJECTOR ASSEMBLY,FUEL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2014 OVERALL, nut_style: TUBE COUPLING, nut_height: 0.719 INCHES NOMINAL IN, seat_angle: 45.0 DEGREES NOMINAL, thread_class: 3B, thread_series: UNF. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 4730-00-555-8203, 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 2014 OVERALL |
| nut_style | TUBE COUPLING |
| nut_height | 0.719 INCHES NOMINAL IN |
| seat_angle | 45.0 DEGREES NOMINAL |
| thread_class | 3B |
| thread_series | UNF |
| thread_direction | RIGHT-HAND |
| surface_treatment | ANODIZE OVERALL |
| length_to_shoulder | 0.547 INCHES NOMINAL IN |
| width_across_flats | 0.562 INCHES NOMINAL IN |
| nominal_thread_size | 0.437 INCHES IN |
| smallest_inside_diameter | 0.300 INCHES NOMINAL IN |
| NSN | 4730-00-555-8203 |
| THREAD CLASS | 3B |
| NOMINAL THREAD SIZE | 0.438 INCHES IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL | ALUMINUM ALLOY 2014 OR ALUMINUM ALLOY 2024 OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367,T6 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-225/6,T6,T62 OR T851 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| THREAD SERIES | UNIFIED NATIONAL JOINT FINE (UNJF) |
| SEAT ANGLE | 45.00 DEGREES NOMINAL |
| THREAD QUANTITY PER INCH | 20 |
| END ITEM IDENTIFICATION | AIRCRAFT APPLICATION,IROQUIS UH-1,CHINOOK CH-47 HELICOPTER,DELTA DART F-106,F-111. TOMCAT F-14A,STARLIFTER C-141 AIRCRAFT,E-3A AIRCRAFT WARNING AND CONTROL SYSTEM (AWACS) A |
| WIDTH ACROSS FLATS | 0.562 INCHES NOMINAL IN |