Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE SET
2840-01-458-3129 A blade set designed to be mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE
Alternate Parts: 578041, 2840-01-458-3129, 01-458-3129, 2840014583129, 014583129
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 20, 1998 | 01-458-3129 | 50515 ( BLADE SET, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-458-3129
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 578041 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-458-3129
| Characteristic | Specifications |
|---|---|
| COMPONENT QUANTITY | 16 |
| END ITEM IDENTIFICATION | TF33-PW-102C AIRCRAFT GAS TURBINE ENGINE |
| 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 |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 3, IND 3 |
| UNIT PACKAGE QUANTITY | 2 |