Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-00-940-8452 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: 6847449, 6847449, 2840-00-940-8452, 00-940-8452, 2840009408452, 009408452
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 11, 1965 | 00-940-8452 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-940-8452
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6847449 | 73342 | ALLISON TRANSMISSION, INC. |
| 6847449 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-00-940-8452
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | CRES,EMS73634 FSCM 73342,44 BLADES,7.170 IN. MIN,7.172 IN. MAX O/A OD,1.319 IN. MIN,1.321 IN. MAX O/A LG,1ST END HUB,EXT SPLINES,20 TEETH,30 DEG PRESSURE ANGLE,1.938 IN.-24 EXT THD LOCATED 0.090 IN. NOM DISTANCE FROM 1ST END,0.250 IN. NOM THD LG,10 HOLES 0.200 IN. NOM DIA EQUALLY SPACED ON OD HUB,0.520IN. NOM C TO C DISTANCE FROM 1ST END TO HOLES,2ND END HUB,EXT SPLINES,20 TEETH,30 DEG PRESSURE ANGLE,STEPPED ID,1.1585 IN. MIN,1.1590 IN. MAX SMALLEST ID.FLIGHT SAFETY CRITICAL AIRCRAFT PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | T63-A-700 AND T63-A-720 ENGINES |