2840PL2128152: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 3.825 INCHES NOMINAL IN, overall_length: 0.532 INCHES MINIMUM AND 0.542 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-54; 35 HOLES EQ SP 0.520-0.540.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-322-2051, 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 | 20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| overall_width | 3.825 INCHES NOMINAL IN |
| overall_length | 0.532 INCHES MINIMUM AND 0.542 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-54; 35 HOLES EQ SP 0.520-0.540 |
| material_thickness | 0.050 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-322-2051 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.532 INCHES MINIMUM AND 0.542 INCHES MAXIMUM IN |
| OVERALL WIDTH | 3.825 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL THICKNESS | 0.050 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN |
| SPECIAL FEATURES | T.O. 2J-F100-54; 35 HOLES EQ SP 0.520-0.540 |
No substitute or cross-reference records for this part.