NSN 2840-00-217-6691
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-00-217-6691 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: 6877092, 6877092, 2840-00-217-6691, 00-217-6691, 2840002176691, 002176691
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 06, 1973 | 00-217-6691 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-217-6691
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6877092 | 73342 | ALLISON TRANSMISSION, INC. |
| 6877092 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-00-217-6691
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | CRES EMS73648-2,FSCM 73342,48 BLADES,6.409 IN. MIN,6.411 IN. MAXOD,EXTERNAL SPLINE LOCATED ON HUB END,17 TEETH,0.557 IN. MIN,0.562 IN.MAX OD,0.5313 IN. NOM PITCH DIA,30 DEG PRESSURE ANGLE,0.8438-32 UNJSEXTERNAL THD LOCATED 1.112 IN.MIN,1.132 IN. MAX DISTANCE FROM HUB END,0.210 IN. NOM THD LG |
| END ITEM IDENTIFICATION | T-63 SERIES ENGINES |
