Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-008-5982 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: 114055007, 1-140-550-07, 114055007, 1-140-550-07, 2840-01-008-5982, 01-008-5982, 2840010085982, 010085982
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 26, 1975 | 01-008-5982 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-008-5982
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-140-550-07 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1-140-550-07 | 81996 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 2840-01-008-5982
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 62 BLADES,13.397 IN. MIN,13.399 IN. MAX OD. FLIGHT SAFETY CRITICAL AIRCRAFT PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | T-53 SERIES ENGINES |