The INJECTOR ASSEMBLY,FUEL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2014 OR ALUMINUM ALLOY 2024 OVERALL, nut_style: TUBE COUPLING, nut_height: 0.710 INCHES MINIMUM AND 0.730 INCHES MAXIMUM IN, seat_angle: 45.00 DEGREES NOMINAL, thread_class: 3B, thread_series: UNIFIED NATIONAL JOINT FINE (UNJF). 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 OR ALUMINUM ALLOY 2024 OVERALL |
| nut_style | TUBE COUPLING |
| nut_height | 0.710 INCHES MINIMUM AND 0.730 INCHES MAXIMUM IN |
| seat_angle | 45.00 DEGREES NOMINAL |
| thread_class | 3B |
| thread_series | UNIFIED NATIONAL JOINT FINE (UNJF) |
| special_features | GRUMMAN AEROSPACE CORP A10 AIRCRAFT; WEAPON SYSTEM ESSENTIAL |
| thread_direction | RIGHT-HAND |
| surface_treatment | ANODIZE OVERALL |
| length_to_shoulder | 0.537 INCHES MINIMUM AND 0.557 INCHES MAXIMUM IN |
| width_across_flats | 0.562 INCHES NOMINAL IN |
| nominal_thread_size | 0.438 INCHES 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 |