4077434-01: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 19.207 INCHES MINIMUM AND 19.213 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.846 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54, material_thickness: 0.486 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-321-4453, 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.
| diameter | 19.207 INCHES MINIMUM AND 19.213 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 4 |
| overall_length | 0.846 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-54 |
| material_thickness | 0.486 INCHES NOMINAL IN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-321-4453 |
| STAGE NUMBER | 4 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 19.207 INCHES MINIMUM AND 19.213 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.846 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL THICKNESS | 0.486 INCHES NOMINAL IN |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |