4085003: DISK,COMPRESSOR,AIRCRAFT GAS TUR.
DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include design_type: AXIAL COMPRESSOR, special_features: ECP95NA047; INCREASED DISK LUG THICKNESS, REVISED SLOT RADII AND BLADE SHROUDS; REPLACES P/N 4059503; 3000 TAC, end_item_identification: F100-PW-100 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR, reference_data_and_literature: T.O. 2J-F100-14, FIG 139, IND 51, criticality_code_justification: CZBJ AND AGAV AND FEAT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-451-0692, 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.
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| special_features | ECP95NA047; INCREASED DISK LUG THICKNESS, REVISED SLOT RADII AND BLADE SHROUDS; REPLACES P/N 4059503; 3000 TAC |
| end_item_identification | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-F100-14, FIG 139, IND 51 |
| criticality_code_justification | CZBJ AND AGAV AND FEAT |
| NSN | 2840-01-451-0692 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND AGAV AND FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-14, FIG 139, IND 51 |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ECP95NA047; INCREASED DISK LUG THICKNESS, REVISED SLOT RADII AND BLADE SHROUDS; REPLACES P/N 4059503; 3000 TAC |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.