4079208-01: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 0.885 INCHES MINIMUM AND 0.895 INCHES MAXIMUM IN, end_item_identification: ACFT ENG F100PW229, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-366-2957, 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 | NICKEL ALLOY OVERALL |
| stage_number | 8 |
| overall_length | 0.885 INCHES MINIMUM AND 0.895 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG F100PW229 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-366-2957 |
| STAGE NUMBER | 8 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 0.885 INCHES MINIMUM AND 0.895 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | ACFT ENG F100PW229 |
| MATERIAL | NICKEL ALLOY OVERALL |