1465M50G08: AUGMENTOR NOZZLE SECTION,INNER,A.
AUGMENTOR NOZZLE SECTION,INNER,A. Key specifications include material: STEEL, overall_length: 22.090 INCHES MINIMUM AND 22.170 INCHES MAXIMUM IN, special_features: 2J-F110-4, FIG 2-78/2-73, end_item_identification: F110GE129 AIRCRAFT ENGINE, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: FLAP, EXHAUST NOZZLE-DIVERGENT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-381-5393, 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 | STEEL |
| overall_length | 22.090 INCHES MINIMUM AND 22.170 INCHES MAXIMUM IN |
| special_features | 2J-F110-4, FIG 2-78/2-73 |
| end_item_identification | F110GE129 AIRCRAFT ENGINE |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | FLAP, EXHAUST NOZZLE-DIVERGENT |
| NSN | 2840-01-381-5393 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 22.090 INCHES MINIMUM AND 22.170 INCHES MAXIMUM IN |
| SPECIAL FEATURES | 2J-F110-4, FIG 2-78/2-73 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLAP, EXHAUST NOZZLE-DIVERGENT |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| MATERIAL | STEEL |
No substitute or cross-reference records for this part.