4079207-01: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 18.802 INCHES NOMINAL IN, material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, overall_length: 1.006 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-366-2958, 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 | 18.802 INCHES NOMINAL IN |
| material | NICKEL ALLOY OVERALL |
| design_type | COMPRESSOR |
| stage_number | 7 |
| overall_length | 1.006 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-366-2958 |
| STAGE NUMBER | 7 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 18.802 INCHES NOMINAL IN |
| OVERALL LENGTH | 1.006 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |