578041: BLADE SET,COMPRESSOR,AIRCRAFT GA.
BLADE SET,COMPRESSOR,AIRCRAFT GA. Key specifications include component_quantity: 16, end_item_identification: TF33-PW-102C AIRCRAFT GAS TURBINE ENGINE, reference_data_and_literature: T.O. 2J-TF33-34, FIG 3, IND 3.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-458-3129, 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.
| component_quantity | 16 |
| unit_package_quantity | 2 |
| end_item_identification | TF33-PW-102C AIRCRAFT GAS TURBINE ENGINE |
| reference_data_and_literature | T.O. 2J-TF33-34, FIG 3, IND 3 |
| NSN | 2840-01-458-3129 |
| COMPONENT QUANTITY | 16 |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 3, IND 3 |
| UNIT PACKAGE QUANTITY | 2 |
| SPECIAL FEATURES | MATL TITANIUM ALLOY, AMS 4928; DESIGN TYPE, AXIAL COMPRESSOR; ENGINE LOCATION, COMPRESSOR; STAGE 1; BLADE ATTACHMENT, DOVETAIL; WIDTH 0.839; HEIGHT 3.870-8.880; THIS ITEM COMES OFF A JT3D-7 COMMERICAL ENGINE; THE ORIGINAL P/N 572901 REPLC P/N 430401; IT TAKES 2 OF P/N 572901 TO MAKE SET; THE FORM, FIT, FUNCTION IS EXACTLY THE SAME, THE ANGLE OF THE BLADE IS DIFFERENT; BLADE WILL PROVIDE 1200 LBS MORE THRUST WHEN IN USE; ONCE REPLD WILL MODIFY THE TF33-PW-102B TO THE 102C; JOINT STAR AIRCRAFT PROJECT LBS |
| END ITEM IDENTIFICATION | TF33-PW-102C AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.