Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-447-2506 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: KDS 28404003, KDS 2840-4003, 1881M11P01, 2840-01-447-2506, 01-447-2506, 2840014472506, 014472506
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 30, 1997 | 01-447-2506 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-2506
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| KDS 2840-4003 | 3999F | DEFENSE ACQUISITION PROGRAMADMINISTRATION, R.O.K |
| 1881M11P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-447-2506
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 4.784 INCHES MINIMUM AND 4.794 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F110-14 FIG 90 IND 1 |
| END ITEM IDENTIFICATION | ACFT ENG F110GE129 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,LOW PRESSURE TURBINE ROTOR-STAGE 1, MACH |