Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-027-2398 An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 4051072, 4039092, 4051092, 2840-01-027-2398, 01-027-2398, 2840010272398, 010272398
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 12, 1976 | 01-027-2398 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-027-2398
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4051072 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4039092 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4051092 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-027-2398
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 2 |
| BLADE ATTACHMENT METHOD | LOCK |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 140, IND 49; NEEDS 60 UNITS PER ASSY; NEED 2 OF P/N 4039092 OR 4051072 TO MAKE P/N 4041272 |
| END ITEM IDENTIFICATION | ACFT ENGINE F100 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |