Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-076-5887 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 6898782, 6898782, 6898782, 2840-01-076-5887, 01-076-5887, 2840010765887, 010765887
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 08, 1979 | 01-076-5887 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-076-5887
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6898782 | 73342 | ALLISON TRANSMISSION, INC. |
| 6898782 | D3309 | MTU AERO ENGINES AGDBA MTU DEUTSCHE AEROSPACE |
| 6898782 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-076-5887
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | CRES EMS73649-2,FSCM 73342,48 BLADES EQUALLY SPACED ON OUTER PERIPHERY,6.409 IN. MIN,6.411 IN. MAX OD,EXTERNAL SPLINE,17 TEETH,0.562 IN. MIN,0.567 IN. MAX OD,0.5313 IN. NOM PITCH DIA,30 DEG PRESSURE ANGLE,EXTERNAL THD,0.8438 IN.-32 UNJS CLASS 3A THD,0.8378 IN. MIN,0.8438 IN. MAX OD. FLIGHT SAFETY CRITICAL AIRCRAFT PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | T63-A-700 AND T63-A-720 ENGINES |