4077289-01: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 17.954 INCHES MINIMUM AND 17.964 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.855 INCHES MINIMUM AND 0.865 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 2840-01-322-4752, 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 | 17.954 INCHES MINIMUM AND 17.964 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 9 |
| overall_length | 0.855 INCHES MINIMUM AND 0.865 INCHES MAXIMUM IN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5536 ASSN STD 1ST MATERIAL RESPONSE AND AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-322-4752 |
| STAGE NUMBER | 9 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD 1ST MATERIAL RESPONSE AND AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
| DIAMETER | 17.954 INCHES MINIMUM AND 17.964 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.855 INCHES MINIMUM AND 0.865 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.