Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-110-5977 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: K350P26, K350P18, 9661M50P18, 9601M75P02, 2840-00-110-5977, 00-110-5977, 2840001105977, 001105977
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 09, 1968 | 00-110-5977 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-110-5977
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| K350P26 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| K350P18 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9661M50P18 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9601M75P02 | 51992 | UNION MACHINE COMPANY OF LYNN, INC. |
Technical Data | NSN 2840-00-110-5977
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 6.289 INCHES MINIMUM AND 6.309 INCHES MAXIMUM |
| OVERALL WIDTH | 1.696 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF-39 |